Patent Application
20210247159
The present invention relates to firearms, and more particularly to an energizable electromagnetic trigger mechanism for the firing system of a firearm which provides a dynamically adjustable force and displacement profile for a trigger customizable by a user.
Traditional triggers for firearms provide a decisive intent-to-fire signal through mechanical motion that utilizes a displacement and force profile developed by using mechanical linkages, springs and the release of energy stored in a spring-biased hammer, striker, or sear. The trigger force and displacement curve or profile is normally fixed by these mechanical linkages and springs. A number of designs exist that provide adjustable characteristics for the force and displacement of the trigger using set screws, additional springs, or part changes to customize the force-displacement profile of firearm triggers mechanically.
An improved variable force trigger is desired which allows the trigger force-displacement profile to be more quickly and easily altered in a dynamically changeable manner without resort to strictly adjusting the position of mechanical components or physically exchanging such mechanical components and/or other hardware of the trigger mechanism.
An electromagnetically variable firing system for a firearm according to the present disclosure includes a trigger assembly or mechanism having an electromagnetically-operated control device which allows the user to preselect and adjust the trigger pull force-displacement profile electronically in an expeditious non-mechanical manner in one embodiment. The preselected trigger force may be implemented automatically and dynamically during the course of a trigger pull event based on sensing an applied force to the trigger by the user to initiate the firing sequence.
The electromagnetic control device is an integral part of the trigger mechanism, which in turn operably interfaces with other components of the firing system for discharging the firearm. The electromagnetically variable firing system may include a movable energy storage device such as a spring-biased cockable striking member such as a pivotable hammer or linearly-movable striker for striking a chambered ammunition cartridge or round, a movable sear operable to hold and release the hammer or striker from the cocked position, and other associated firing mechanism components which collectively operate together to discharge the firearm when actuated via a manual trigger pull. In some embodiments, the sear may be formed as an integral unitary structural part of the trigger mechanism instead of being a separate component.
In certain implementations, the trigger pull force and displacement profile is electrically/electronically adjustable via the trigger control device by changing or altering a magnetic field acting on a portion of the trigger mechanism, thereby increasing or decreasing resistance of the trigger to movement. The trigger pull force required may vary with displacement distance or travel of the trigger when actuated by the operator or user such that the initial trigger pull force may have an initial value or magnitude during the first stage or phase of the trigger pull (e.g. hard or easy) which is then followed by either a constant or varying different second values or magnitudes of trigger pull force during the subsequent and final phases of the trigger pull until the firearm is discharged.
To power, monitor, and control operation of the trigger control device and trigger mechanism including adjustment of the trigger pull force and displacement profile, the firearm may include a control system including a suitable power source (e.g. battery) mounted to a frame of the firearm or module attached thereto, and a programmable electronic processor such as a microprocessor or microcontroller including circuitry, memory, data storage devices, sensors, sensor and drive circuits, communication devices and interfaces (e.g. wired or wireless protocols), and other electronic devices, components, and circuits necessary for a fully functional microprocessor based control system. The microcontroller may preferably be disposed onboard the firearm. The microcontroller is operably coupled to the power source to control via an actuation control circuit to energize or de-energize the trigger control device.
In one embodiment, the electromagnetically-operated trigger control device may comprise a magnetorheological fluid device or operator which is selectably alterable electrically/electronically via the microcontroller to vary the trigger pull force and displacement profile characteristics.
In another embodiment, the electromagnetically-operated trigger control device may comprise a magnetic device or operator such as an electromagnetic snap actuator of a non-bistable design which is selectably alterable electrically/electronically via the microcontroller to vary the trigger pull force and displacement profile characteristics by altering the magnet field force of the trigger mechanism. The electromagnetic actuator forms an integral part of the trigger mechanism, and in some embodiments may constitute substantially the entirety of the trigger mechanism with minimal appurtenances for operational simplicity and reliability. The electromagnetic actuator may generally include a stationary yoke attached to the firearm frame, a rotatable member pivotably movable relative to the yoke, and an electromagnet coil electrically connected to the on-firearm electric power source. In some implementations, the trigger mechanism may be configured to establish a closed single or double flux loop that limits susceptibility to external magnetic fields which might inadvertently change the trigger pull force or displacement of the trigger mechanism. This completely contained flux loop around the permanent magnet optimizes the magnetic coupling force between the yoke and rotating member making this design inherently resistant to external magnetic fields.
Certain implementations of the control device may also employ mechanical components to assist with adjusting the trigger pull force and displacement profile. The trigger control device may be used as an on/off safety in some embodiments, and/or to vary trigger pull force which may be adjusted by the user to meet personal preferences.
Embodiments of the present electromagnetic trigger mechanisms may be employed with any type of trigger-operated small arms including without limitation as some examples pistols, revolvers, long guns (e.g. rifles, carbines, shotguns), grenade launchers, etc. Accordingly, the present invention is expressly not limited in its applicability and breadth of use.
Accordingly, embodiments of the present invention provide a trigger mechanism or assembly for use in a firearm that provides a changeable and variable force of resistance (i.e. trigger pull force) as the trigger moves and is displaced in distance.
The foregoing or other embodiments of the present invention may control the change in resistance force dynamically during the actual displacement of the trigger linkage by the operator or user at the time of operation.
The foregoing or other embodiments of the present invention provide that the trigger force can be controlled by varying the viscosity of a magnetorheological fluid incorporated into the trigger mechanism.
The foregoing or other embodiments of the present invention provide that the trigger force can be controlled by varying the magnetic field of an electromagnetic snap actuator incorporated into and configured as a trigger mechanism or assembly for discharging the firearm.
The foregoing or other embodiments of the present invention provide that the trigger force can be programmed remotely from an external smartphone, tablet, personal wearable device, or other remote device using a wireless communications standard such as Bluetooth, BLE (Bluetooth Low Energy), NFC (Near-Field Communication), LoRa (Long Range wireless), WiFi, or a proprietary wireless protocol or other protocol.
The foregoing or other embodiments of the present invention may be configured to capture cycle count and direct sensing of the trigger mechanism for the implementation of data collection on the performance and operation of the device. Shot counting, shot timing, pre-fire trigger analysis, and post firing performance analysis can be tied to internal sensing of the trigger event and electrically interfaced to the user through external electronic devices, such as without limitation cellphones, tablets, pads, wearables, or web applications.
In one aspect, an electromagnetically variable trigger force firing system comprises: a frame; a striking member supported by the frame for movement between a rearward cocked position and forward firing position for discharging the firearm; an electromagnetic actuator trigger unit affixed to the frame and comprising: a stationary yoke comprising an electromagnet coil; a rotating member movable about a pivot axis relative to the stationary yoke and operable for releasing the striking member from the cocked position to the firing position; a trigger operably engaged with the rotating member, the trigger manually movable by a user from a first position to a second position which rotates the rotating member for discharging the firearm; and a permanent magnet generating a static magnetic field in the stationary yoke and rotating member, the static magnetic field creating a primary resistance force opposing movement of the trigger when pulled by the user; an electric power source operably coupled to the coil; the electromagnet coil when energized generating a user-adjustable secondary magnetic field interacting with the static magnetic field, the secondary magnetic field operating to change the primary resistance force dynamically during a trigger pull event initiated by the user.
In another aspect, an electromagnetic firing system for a firearm comprises: a frame; a striking member supported by the frame and movable between a rearward cocked position and forward firing position for discharging the firearm; an electromagnetically adjustable trigger mechanism operably coupled to the striking member for discharging the firearm, the trigger mechanism comprising an electromagnetic actuator including: a stationary yoke comprising an electromagnet coil operably coupled to an electric power source, the coil having an energized state and a de-energized state; a rotating member pivotably coupled to the stationary yoke for movement between an unactuated and actuated positions, the rotating member operably coupled to the striking member for moving the striking member from the cocked position to the firing position; a trigger movably coupled to the stationary yoke and interacting with the rotating member, the trigger manually movable by a user from a first actuation position to a second actuation position which rotates the rotating member for discharging the firearm; and a permanent magnet generating a static magnetic flux in the yoke and rotating member, the static magnetic flux creating a primary resistance force opposing movement of the trigger when pulled by the user; a programmable microcontroller operably coupled to the electromagnetic actuator of the trigger mechanism and pre-programmed with a trigger force setpoint, the microcontroller configured to: receive an actual trigger force applied to the trigger by a user and measured by a trigger sensor communicably coupled to the microcontroller; compare the actual trigger force to the preprogrammed trigger force setpoint; and selectively energize the electromagnetic actuator based on the comparison of the actual trigger force to the trigger force setpoint; wherein the electromagnet coil when energized generates a user-adjustable secondary magnetic flux interacting with the static magnetic field, the secondary magnetic field operating to increase or decrease the primary resistance force when the trigger is pulled by the user.
In another aspect, an electromagnetic firing system for a firearm comprises: a frame; a striking member supported by the frame and movable between a rearward cocked position and forward firing position for discharging the firearm; a pivotable sear configured to selectively hold the striking member in the cocked position; an electromagnetic actuator trigger mechanism supported by the frame, the trigger mechanism configured to create a dual loop magnetic flux circuit and comprising: a stationary yoke comprising an electromagnet coil operably coupled to an electric power source, the coil having an energized state and a de-energized state; a rotating member pivotably coupled to the stationary yoke about a pivot axis, the rotating member movable between an unactuated position engaging with the sear and an actuated position disengaging the sear; a trigger operably engaged with the rotating member and manually movable by a user for applying an actual trigger force on the rotating member; and a permanent magnet generating a static magnetic flux holding the rotating member in the unactuated position, the permanent magnet generating a static magnetic flux creating a primary resistance force opposing movement of the trigger when pulled by the user; a programmable microcontroller operably coupled to the power source and communicably coupled to a trigger sensor configured to sense the applied trigger force, the microcontroller when detecting the applied trigger force being configured to transmit an electric pulse to the electromagnet coil of the trigger mechanism; the electromagnet coil when energized generating a secondary magnetic flux interacting with the static magnetic field, the secondary magnetic field being configurable by the user via the microcontroller to increase or decrease the primary resistance force when the trigger is pulled by the user.
In another aspect, an electromagnetically variable trigger system comprises: a frame; an electromagnetic actuator trigger unit affixed to the frame and comprising: a stationary yoke comprising an electromagnet coil; a rotating member movable about a pivot axis relative to the stationary yoke; a trigger operably engaged with the rotating member, the trigger manually movable by a user from a first position to a second position which rotates the rotating member; and a permanent magnet generating a static magnetic field in the stationary yoke and rotating member, the static magnetic field creating a primary resistance force opposing movement of the trigger when pulled by the user; an electric power source operably coupled to the coil; the electromagnet coil when energized generating a user-adjustable secondary magnetic field interacting with the static magnetic field, the secondary magnetic field operating to change the primary resistance force dynamically during a trigger pull event initiated by the user. The trigger system may further comprise an electronic actuation control circuit operably coupled between to the power source and coil, the actuation control circuit configurable by the user to selectively energize the coil upon detection of a trigger pull and de-energize the coil in an absence of the trigger pull, and a trigger sensor communicably coupled to the actuation control circuit and operable to detect movement of the trigger initiated by the user.
The present application further discloses non-electric magnetic only trigger mechanisms of the closed and open magnetic loop designs.
According to one aspect, a closed loop magnetically variable trigger force trigger mechanism for a firearm comprises: a stationary yoke configured for mounting to the firearm; a rotatable trigger member pivotably coupled to the stationary yoke about a pivot axis, the trigger member and stationary yoke collectively configured to form a closed magnetic loop; an openable and closeable first air gap formed between the trigger member and the stationary yoke; a permanent magnet arranged to generate a static magnetic field in the closed magnetic loop, the static magnetic field creating a primary resistance force opposing movement of the trigger member when pulled by the user; a control insert selectively movable relative to a second control air gap formed in the yoke which attenuates the static magnetic field, the control insert constructed and operable to change the static magnetic field; wherein the static magnetic field is changeable via varying position of the control insert relative to the control air gap to adjust a trigger pull force of the trigger mechanism.
In another aspect, a closed loop magnetically variable trigger force trigger mechanism for a firearm comprises: a stationary yoke configured for mounting to the firearm; a rotatable trigger member pivotably movable about a pivot axis relative to the stationary yoke, the trigger member and stationary yoke collectively configured to form a closed magnetic loop; an openable and closeable first air gap formed between the trigger member and the stationary yoke; a control insert selectively movable into and out of a second control air gap formed in the yoke which attenuates the static magnetic field, the control insert operable to change the static magnetic field; the control insert comprising a non-magnetic carrier and a permanent magnet operable to generate a static magnetic field in the closed magnetic loop, the static magnetic field creating a primary resistance force opposing movement of the trigger member when pulled by the user; wherein the static magnetic field is changeable via varying position of the permanent magnet in the control insert relative to the second control air gap to adjust a trigger pull force of the trigger mechanism.
In another aspect, a closed loop magnetically variable trigger force trigger mechanism for a firearm comprises: a stationary yoke configured for mounting to the firearm; a rotatable trigger member pivotably movable about a pivot axis relative to the stationary yoke, the trigger member and stationary yoke collectively configured to form a closed magnetic loop; an openable and closeable first air gap formed between the trigger member and the stationary yoke; a control insert comprising a permanent magnet rotatably disposed in a second control air gap formed in the yoke which attenuates the static magnetic field, the permanent magnet operable to generate a static magnetic field in the closed magnetic loop, the static magnetic field creating a primary resistance force opposing movement of the trigger member when pulled by the user; wherein the static magnetic field is changeable via rotating the permanent magnet of the control insert relative to the second control air gap to adjust a trigger pull force of the trigger mechanism.
In another aspect, a method for adjusting the trigger pull force of a closed loop magnetically variable trigger force trigger mechanism for a firearm comprises: providing a stationary yoke configured for mounting in the firearm, a rotating trigger member pivotably movable about a pivot axis relative to the stationary yoke, the trigger member and stationary yoke collectively configured to form a closed magnetic loop, and an openable and closeable first air gap being formed between the trigger member and the stationary yoke; providing a control insert comprising a non-magnetic carrier and a permanent magnet operable to generate a static magnetic field in the closed magnetic loop, the static magnetic field creating a primary resistance force opposing movement of the trigger member when pulled by the user; rotating an actuator operably coupled to the control insert in a first direction to advance the permanent magnet into a second control air gap formed in the stationary yoke, the magnet creating a first static magnetic field strength in the closed magnetic loop which resists movement of the trigger member relative to the stationary yoke at the first air gap; rotating the actuator in an opposite second direction to withdraw the magnet from the second control air gap, the magnet creating a second static magnetic field strength in the closed magnetic loop less than the first magnetic field strength; wherein the strength of the static magnetic field is changeable via varying position of the permanent magnet in the control insert relative to the second control air gap in order to adjust a trigger pull force of trigger mechanism.
The present disclosure further discloses a microcontroller-operated firing event (shot) tracking system.
In one aspect, an electromagnetic firing system for a firearm with firing event tracking comprises: an electromagnetic actuator trigger unit comprising: a stationary yoke configured for mounting to the firearm; a rotating member movable about a pivot axis relative to the stationary yoke and operably coupled to a firing mechanism of the firearm; a trigger operably coupled to the rotating member, the trigger manually movable by a user from a first position to a second position which rotates the rotating member for discharging the firearm; and a permanent magnet generating a static magnetic field in the stationary yoke and rotating member, the static magnetic field creating a primary resistance force opposing movement of the trigger when pulled by the user; a magnetic coil operably coupled to an electric power source and the yoke or rotating member; the magnetic coil when energized generating a user-adjustable secondary magnetic field interacting with the primary resistance force which changes a trigger pull force required to be exerted by a user to overcome the primary resistance force and discharge the firearm in response to a trigger pull event; a programmable microcontroller configured to detect the trigger pull event and selectively energize the coil via the power source in accordance with a user-selected trigger force or displacement setpoint preprogrammed into the microcontroller thereby defining a firing event; the microcontroller further configured to record and store each firing event and an associated time/date stamp.
In another aspect, an electromagnetic firing system for a firearm with firing event tracking comprises: a trigger unit mounted in the firearm, the trigger unit comprising: an electromagnetic actuator including a stationary yoke, a rotating member movable about a pivot axis relative to the stationary yoke and operably coupled to a firing mechanism of the firearm, a trigger operable when pulled by a user to move the rotating member between an unactuated position and an actuated position for discharging the firearm, and a magnetic coil when energized generating a user-adjustable magnetic field which changes a trigger pull force required to be exerted by a user on the trigger to discharge the firearm; a programmable microcontroller operably coupled to the electromagnetic actuator and configured to selectively energize the coil for discharging the firearm in response to detecting a trigger pull event; the microcontroller further configured to count each energization of the coil as indicative of a firing event and record the firing event.
In another aspect, a method for tracking firing events in a firearm with an electromagnetic firing system comprises: mounting a trigger unit in the firearm, the trigger unit comprising a trigger and an electromagnetic actuator operably coupled to the trigger and a firing mechanism of the firearm, the actuator including a magnetic coil which when energized moves the actuator from an unactuated position to an actuated position which discharges the firearm; providing a programmable microcontroller operably coupled to the actuator, the microcontroller configured to detect a trigger pull event and selectively energize the coil for discharging the firearm in response thereto; the microcontroller: detecting the trigger pull event; energizing the coil of the actuator via a power source; counting energizing the coil as indicative of a firing event; and recording the firing event in memory.
The present disclosure further discloses an interruptible electronic trigger system with microcontroller-operated electromagnetic actuator trigger unit operably interfaced with an external advanced fire control targeting system. The microcontroller-operated targeting system is configured to interact with the trigger unit and perform ballistics computations to assist the firearm user in accurately aiming the firearm and acquiring the target. The targeting system may be embodied in an adaptive optics unit mountable to the firearm for use in sighting the target by the user.
In one aspect, an interruptible electronic trigger system for a firearm comprises: an electromagnetic actuator trigger unit configured for mounting to the firearm, the trigger unit comprising: a stationary yoke; a rotating member movable about a pivot axis relative to the stationary yoke and operably coupled to a firing mechanism component operable to discharge the firearm; a trigger operably coupled to the rotating member, the trigger manually movable by a user from a first position to a second position for discharging the firearm; a permanent magnet generating a static magnetic field in the stationary yoke and rotating member, the static magnetic field creating a primary resistance force opposing movement of the trigger when pulled by the user; a coil operably coupled to an electric power source and the yoke or rotating member, the coil when energized operable to rotate the rotating member and discharge the firearm; a programmable trigger unit microcontroller operably coupled to the trigger unit, the trigger unit microcontroller configured to: detect a trigger pull event; send a shot initiation signal to a fire control targeting system operably coupled to the trigger unit microcontroller; and receive a shot authorization signal returned from the fire control targeting system in response to receiving the shot initiation signal. The electronic trigger system is operable to revert to manual firing mode thereby allowing the user to fire the firearm mechanically when the system senses that an applied trigger force or displacement of the trigger exceeds a preprogrammed maximum allowable trigger pull force or displacement limit.
According to another aspect, a firearm with interruptible electromagnetic trigger system comprises: an electronic trigger unit mounted to the firearm and operable to discharge the firearm, the trigger unit including an electromagnetic actuator comprising: a rotating member operably coupled with a firing mechanism component movable to discharge the firearm, the rotating member rotatable about a pivot axis to actuate the firing mechanism component for discharging the firearm; a trigger operably coupled to the rotating member, the trigger manually movable by a user between first and second positions; a permanent magnet generating a static magnetic field in the rotating member, the static magnetic field creating a primary resistance force opposing movement of the rotating member and trigger when pulled by the user; the coil when energized generating a secondary magnetic field in the rotating member which overcomes the primary resistance force and rotates the rotating member to discharge the firearm; a programmable trigger unit microcontroller operably coupled to the electromagnetic actuator of the trigger unit, the trigger unit microcontroller further operably coupled to an external fire control targeting system and configured to: detect user activity on the trigger sensed by a trigger sensor communicably coupled to the trigger unit microcontroller, the user trigger activity comprising an applied trigger force or trigger displacement; compare the user activity on the trigger to a preprogrammed first trigger setpoint; and transmit a shot initiation signal to the fire control targeting system when the user activity on the trigger exceeds the first trigger setpoint. The electronic trigger system is operable to revert to manual firing mode thereby allowing the user to fire the firearm mechanically when the system senses that an applied trigger force or displacement of the trigger exceeds a preprogrammed maximum allowable trigger pull force or displacement limit.
According to another aspect, a method for discharging a firearm with an interruptible firing system comprises: providing an electronic trigger unit operably coupled to a power source and mounted to the firearm, the trigger unit comprising a programmable trigger unit microcontroller, a trigger, and an electromagnetic actuator operably coupled to the trigger and a firing mechanism of the firearm, the actuator including a magnetic coil which when energized moves the actuator from a ready-to-fire unactuated position to an actuated firing position which discharges the firearm; providing a fire control targeting system comprising an electronic adaptive optics unit mounted to the firearm for sighting a target, the adaptive optics unit including a programmable targeting microcontroller operably coupled to the trigger unit microcontroller; the trigger unit microcontroller detecting trigger activity initiated by a user, the trigger activity comprising a trigger pull force or displacement; the trigger unit microcontroller sending a shot initiation signal to the targeting microcontroller when the trigger activity exceeds a preprogrammed first trigger setpoint; the targeting microcontroller sending a shot authorization control signal to the trigger unit microcontroller in response to receiving the shot initiation signal; the trigger unit microcontroller energizing the actuator in response to receiving the shot authorization signal which changes the actuator from the unactuated position to the firing position which discharges the firearm.
These and other features and advantages of the present invention will become more apparent in the light of the following detailed description and as illustrated in the accompanying drawings.
The features of the exemplary embodiments will be described with reference to the following drawings where like elements are labeled similarly, and in which:
All drawings are schematic and not necessarily to scale. Any reference herein to a whole figure number (e.g.
The features and benefits of the invention are illustrated and described herein by reference to example (“exemplary”) embodiments. This description of exemplary embodiments is intended to be read in connection with the accompanying drawings, which are to be considered part of the entire written description. In the description of embodiments disclosed herein, any reference to direction or orientation is merely intended for convenience of description and is not intended in any way to limit the scope of the present invention. Relative terms such as “lower,” “upper,” “horizontal,” “vertical,”, “above,” “below,” “up,” “down,” “top” and “bottom” as well as derivative thereof (e.g., “horizontally,” “downwardly,” “upwardly,” etc.) should be construed to refer to the orientation as then described or as shown in the drawing under discussion. These relative terms are for convenience of description only and do not require that the apparatus be constructed or operated in a particular orientation. Terms such as “attached,” “affixed,” “connected,” and “interconnected,” refer to a relationship wherein structures are secured or attached to one another either directly or indirectly through intervening structures, as well as both movable or rigid attachments or relationships, unless expressly described otherwise. Accordingly, the disclosure expressly should not be limited to such exemplary embodiments illustrating some possible non-limiting combination of features that may exist alone or in other combinations of features.
As used throughout, any ranges disclosed herein are used as shorthand for describing each and every value that is within the range. Any value within the range can be selected as the terminus of the range.
The dynamics of the trigger feel are one of the most important aspects of the shooter's experience, impacting accuracy, repeatability, and safety of the firearm. A conventional trigger pull consists of three stages: take-up or pre-travel, the break-over point of release of stored energy in the hammer, striker, or sear, and finally over-travel. In a conventional trigger mechanism, these stages are fixed by the springs, linkages, and mechanical components that make up the trigger system. An adjustable trigger allows adjustments to the travel distance, force, and feel of the trigger pull during one or more of these stages or phases.
The desired trigger pull force and displacement characteristic is dependent upon the type of firearm, application, safety, reliability, and individual preferences. For example, a shooter may wish for a medium to heavy trigger pull weight for hunting and a significantly lighter and different feel for competition shooting.
The current state of the art for making changes in the trigger pull force requirement and shape of the force profile (e.g. between a heavy and light trigger pull) is to physically adjust spring or linkage tensions within the trigger mechanism or directly replace existing and install alternate parts to attain the desired trigger force and displacement characteristics. These approaches both limit the shape of the possible trigger force verses displacement curve and the timing of how it can be adjusted. Additionally, the adjustment is usually only possible over a narrow range of trigger pull forces unfortunately due to physical limitations of the physical trigger mechanism components.
The present invention includes a novel trigger mechanism which allows the trigger pull force and displacement to be controlled by a magnetic field. By actively adjusting the magnetic field, dynamic real-time variability of the trigger pull force over a wide range of displacement can advantageously be achieved. In addition, the “feel” of the trigger may be improved by tailoring this force-displacement curve to provide a large range of variation that is not possible with conventional mechanical springs, linkages, and levers.
One method disclosed herein to control the force-displacement profile may be to use a rheological fluid. An electric or magnetic field can influence the viscosity of certain fluids. This characteristic can be exploited to design a variable force trigger for firearms, turn on or off a manual safety feature, or provide active damping of recoil.
Magnetorheological (MR) fluids have the unique property of changing from a free-flowing liquid to a semi-solid state in the presence of a magnetic field. This dynamically changeable viscosity property has significant potential for control applications in firearms. Currently, magnetorheological fluids, such as the commercially available MRF-132DG by LORD Corporation, provide a range of fast response time, dynamic yield strength, temperature resistance to meet the needs of an adjustable force trigger system in firearms. Other materials such as ferro-fluids, electrorheological fluids, and devices based on the Giant Electrorheological effect may also provide a reliable alternative to the use of magneto-rheological fluids in this application.
Embodiments of Dynamic Variable-Force Trigger Using MR Fluids
Magneto-rheological (MR) fluids can respond almost instantly to varying levels of a magnetic field precisely and proportionally for controlled force loading. By dynamically adjusting the viscosity of the MR fluid, it is possible to construct a dynamically variable trigger force apparatus. If the movement of a trigger transfer linkage is constrained by using an MR fluid-filled spring loaded piston as disclosed herein, the viscosity of the MR fluid using a magnetic field, we can then be dynamically changed. The resulting viscosity change results in a significant change in force loading necessary to move the trigger transfer linkage to the fire position, which translates into a user-variable trigger pull force resistance opposing movement of the trigger linkage.
In a basic implementation of a simple non-electromagnetic MR fluid actuator shown in
By replacing the permanent magnet 615 with an electromagnet coil 614 as already described herein, one can dynamically change the MR fluid viscosity and hence resulting trigger pull force-displacement profile examples of which are shown in
Using multiple magnetic force concentration points, or a piston plunger port configuration that extends through an adjustable magnetic field during the full travel of the trigger, it is possible to dynamically change the viscosity (trigger force) during a single trigger pull. Such a configuration allows dynamically changing force verses displacement curves of an unlimited nature that could allow custom trigger feel optimized for certain users and use profiles.
Another embodiment related to the variable force-displacement effect is the use of MR fluids as an ON/OFF Trigger Safety. Movement of a trigger transfer mechanism would move freely through a MR fluid reservoir when no magnetic field is applied. When a magnetic field is applied to the MR fluid, its yield stress increases inhibiting movement of the trigger transfer mechanism. Ideally the use of a permanent magnet could be used as a fail-safe always on trigger safety.
In its most basic form, this could be implemented by a permanent magnet mounted on a mechanical linkage that could be manually moved in and out of the critical proximity to the MR fluid like a manual safety lever. While functional this provides no advantage over a conventional mechanical safety.
To take full advantage of the magnetic on/off nature of the MR fluid, an electro-magnet may be included to control the on/off function. This would allow an electrical signal to control the on/off function of the trigger. The reversible and almost instantaneous changes from a free-flowing liquid to a semi-solid with high yield strength would allow the safety to be electrically controlled based on control logic.
Only when an electromagnet is actuated would the effects of the permanent magnet be nulled and allow the MR fluid become more liquid and allow free movement of the trigger mechanism (reference
To minimize power consumption, an enhancement to the concept would place a fixed permanent magnet in place so that the trigger linkage is in the blocked state when at rest. To reverse the MR fluid back to a flowing liquid state, a secondary electro-magnet could be energized to balance out the permanent magnets field. In this configuration, the electromagnet could enable the trigger operation at almost the point that the operator fires while using no power at any other time. The default static unpowered state of the system would be in the no-fire or ready-to-fire condition.
While the use of a MR fluid could be used as a standalone ON/OFF trigger safety feature, the preferred embodiment would combine this active safety feature with a dynamic variable force trigger configuration that acts as both an adjustable trigger force and trigger on/off safety. By applying a fixed permanent magnet field in proximity to the MR fluid filled piston, sufficient to block movement when the firearm is not require to operate, we would have the features of a firearm safety. The magnet field could then be nulled out by the addition of a reverse magnetic field using an electro-magnet and thus enabling the dynamic variable force trigger features.
Embodiments of Dynamic Variable-Force Trigger Using Electromagnetic Actuators
Another embodiment for dynamically controlling the displacement force profile of a firearm trigger utilizes magnetic fields to directly constrain the movement of the trigger linkage until a preselected release force is reached. In one embodiment, a combination of a continuous primary static magnetic field and an intermittently acting dynamic electromagnetic field may be used.
The electromagnetic trigger mechanism 100 generally comprises an electromagnetic snap actuator 123 configured as a trigger assembly for discharging the firearm. The trigger mechanism 100 forms an integral part of the firing system or mechanism of the firearm itself, and does not merely act on the firing mechanism. Actuator 123 is configured as a release type actuator which directly or indirectly releases the energy in the energy storage device such as a spring-biased striking member (e.g. rotatable hammer or linearly movable striker) operable to strike a chambered cartridge positioned in the barrel of the firearm. If a sear which releases the striking member is built directly into the release actuator 123 as shown in
Referring now again to
The stationary yoke 102 of the electromagnetic trigger mechanism 100 may be substantially C-shaped in one embodiment including a horizontal upper portion 110, horizontal lower portion 112 spaced apart and parallel to the upper portion, and a vertical intermediate portion 114 extending between the upper and lower portions. The intermediate portion 114 is integrated with captive ends of the upper and lower portions 110, 112 being a unitary structural part of the entire yoke 102 in one embodiment. The portions 110, 112, and 114 may have any suitable transverse cross-sectional shape including polygonal such as rectilinear as shown, non-polygonal (e.g. circular), or combinations thereof which lend themselves to winding the coil 106 thereto. Although the stationary yoke 102 is illustrated herein as have a C-shaped configuration, it will be appreciated that other configurations of the yoke are possible and may be used.
The rotating trigger member 104 may have a vertically elongated and substantially linear shaped body in one embodiment as shown. The rotating trigger member 104 may lie in the same vertical reference plane as the yoke 102 and is pivotably movable within that plane. The vertical reference plane may intersect the longitudinal axis of the firearm in one embodiment.
Rotating trigger member 104 is pivotably disposed in the frame of the firearm. In one embodiment, rotating trigger member 104 may be pivotably coupled to stationary yoke 102 via pivot 101 formed by cross pin 126a which defines a pivot axis PA of rotation oriented transversely to the longitudinal axis LA of the firearm (see, e.g.
It will be appreciated that in alternative embodiments, for example, the rotating trigger member 104 may alternatively be pivotably mounted to the frame 22 of the firearm 20 instead of via the pivot 101 to achieve the same manner of movement relative to the yoke 102. Either arrangement may be used in various embodiments to best fit the design of the firearm in which the trigger mechanism 100 will be used.
With continuing reference to
In one embodiment, as shown in
The terminal end portion of upper portion 110 of yoke 102 and terminal end portion of the upper portion 120 of rotating trigger member 104 are movable together and apart via the pivoting action of the rotating trigger member 104 relative to the stationary yoke 102. Accordingly, an openable and closeable air space or gap A is formed at the interface between the yoke 102 and rotating trigger member 104. The rotating trigger member 104 is pivotably and manually movable between two actuation states or positions by a user. Rotating trigger member 104 is movable between a first unactuated or rest position physically engaged with the yoke 102 when the trigger is not pulled, and a second actuated or fire position disengaged from the yoke 102 when the trigger is pulled to discharge the firearm. In the actuated position, air gap A is opened whereas the gap is closed in the unactuated position. Also in the actuated position, the axis of tilt TA of the rotating trigger member 104 is obliquely oriented and angled to the stationary axis SA defined by yoke 102, whereas the axis of tilt TA is parallel to axis SA when the rotating trigger member is in the upright unactuated position.
With continuing reference to
The stationary yoke 102 and rotating trigger member 104 may be formed of any suitable soft magnetic metal capable of being magnetized, such as without limitation iron, low-carbon steel, nickel-iron, cobalt-iron, etc.
The trigger mechanism 100 in one embodiment includes a preferably strong permanent magnet 108 which creates a relatively high threshold static magnetic attractive or holding force between the yoke 102 and rotating trigger member 104 which acts to draw these two components into mutual engagement. This static and primary resistance force created by the magnetic field between yoke and trigger member acts to inhibit movement of the rotating trigger member 104 about its pivot axis PA between its two actuation positions when trigger 121 is pulled by a user. The magnetically-induced static resistance corresponds to a trigger pull force required to be exerted and surpassed by the user in order to rotate the trigger member sufficiently to discharge the firearm. The magnet 108 may have a flat rectilinear plate-like shape in one embodiment; however, other shapes may be used. Magnet 108 biases the rotating trigger member 104 into the first unactuated position engaged with the upper portion 110 of yoke 102 at magnet 108.
Permanent magnet 108 may be disposed anywhere within the magnetic loop formed by the yoke 102 and the movable upper portion 120 of rotating trigger member 104. In one embodiment, the magnet 108 may be mounted on the front terminal end of the upper portion 110 of the yoke. Alternatively, the magnet 108 may be disposed on the rear surface of the rotating trigger member 104 and positioned to engage upper portion 110 of the yoke 102. The magnet 108 may therefore be interposed directly between the movable upper portion 120 of the rotating trigger member 104 and stationary yoke 102 to maximize the magnetic attraction of the rotating trigger member to the magnet 108. Other less preferred but still satisfactory locations for mounting the magnet 108 on yoke 102 may alternatively be used. Magnet 108 preferably may be dimensioned and has a cross-sectional area approximately commensurate with and similar to the dimensions and cross-sectional area of the yoke 102 or rotating trigger member in or on which the magnet is arranged.
The present invention further provides a user-selectable and dynamically variable secondary electromagnetic field generated when the electromagnetic actuator 123 is energized. This secondary electromagnetic field interacts with the primary static magnetic field produced by the permanent magnet 108. By electrically and preferentially biasing the magnet flux in the closed loop of the actuator 123 to add or detract from the static magnetic field using the actuator's electromagnet, a dynamically variable trigger pull force or resistance and profile is created which can be selected by the user to meet personal preferences. When coil 106 of the trigger mechanism snap actuator 123 is not energized, a trigger pull force sufficient to only overcome the primary fixed or static magnetic field force of the permanent magnet 108 on the rotating trigger member 104 would be needed to initiate and displace the trigger through a trigger pull event. This allows the trigger member to be actuated in the event power is lost to the actuator 123 (e.g. depleted battery charge).
Electrical energy supplied to the actuator coil 103 and its concomitant dynamically changeable electromagnetic field created when the coil is energized can be made additive or subtractive to the static magnetic field flux generated by the permanent magnet 108 such as by changing the polarity of the electric power. For example, if the user wishes to increase the pull force required over a portion of the travel or displacement of the trigger, the microcontroller 200 may be programmed to change polarity of power source 122 to make the electromagnetic field of the snap actuator additive. In such a setup, the electromagnetic lines of flux of the actuator when energized circulate and act in the same direction in the single closed flux loop as the static magnetic flux generated in the trigger mechanism 100 by the permanent magnet 108. The flux density increases at the air gap A. This increases the magnetic attraction between the yoke 102 and rotating trigger member 104, thereby concomitantly increasing the resistance to rotation of the trigger member by the user making it harder to further pull the trigger (i.e. heavier trigger pull).
Conversely, if the user wishes to decrease the pull force over the travel of the trigger, the microcontroller may be programmed to change polarity of power source 122 to make the electromagnetic field of the snap actuator subtractive. In such a setup, the electromagnetic lines of flux of the actuator when energized circulate and act in the opposite direction in the closed flux loop as the static magnetic flux generated in the trigger mechanism 100 by the permanent magnet 108. The flux density decreases at the air gap A. This decreases the magnetic attraction between the yoke 102 and rotating trigger member 104, thereby concomitantly decreasing the resistance to rotation of the trigger member by the user making it easier to further pull the trigger (i.e. light trigger pull).
The magnitude of the peak trigger pull force required to fully actuate the electromagnetic trigger mechanism 100 may also be altered by the user. This may be achieved in one embodiment by configuring the actuation control circuit 202 associated with microcontroller 200 to increase or decrease the output voltage to the electromagnet coil 106 of snap actuator 123 from power source 122 which passes through and is controlled by the actuation control circuit 202 (reference
It bears noting that inclusion of the permanent magnet 108 also advantageously conserves energy by reducing power consumption. The static magnetic field of the permanent magnet 108 automatically maintains the rotating trigger member 104 of electromagnetic trigger mechanism in the unactuated state or position at rest. Accordingly, the magnetic field generated when the coil 106 of the trigger mechanism snap actuator 123 is energized is not required at all times such as when the trigger 121 is not pulled to simply hold the rotating trigger member 104 in the vertical unactuated state or position. To minimize power consumption, the trigger mechanism actuator therefore only needs to be energized once the trigger (i.e. rotating trigger member 104) is pulled, which is sensed by trigger sensor 159 and the control system. After the trigger pull is completed and the firearm is discharged, the actuator coil may be de-energized until the next trigger pull cycle. This arrangement and mode of operation advantageously extends battery life of the power source 122. Accordingly, the permanent magnet 108 provides energy conservation benefits in addition to creating the initial trigger pull force and primary resistance to movement of the electromagnetic trigger mechanism 100.
As shown in
Microcontroller 200 includes a programmable processor 210, a volatile memory 212, and non-volatile memory 214. The non-volatile memory 214 may be any type of non-removable or removable semi-conductor non-transient computer readable memory or media. Both the volatile memory 212 and the non-volatile memory 214 may be used for saving sensor data received by the microcontroller 200, for storing program instructions (e.g. control logic or software), and storing operating parameters (e.g. baseline parameters or setpoints) associated with operation of the actuator control system. The programmable microcontroller 200 may be communicably and operably coupled to a user display 205, a geolocation module 216 (GPS), grip force sensor 206, motion sensor 207, battery status sensor 208, audio module 218 to generate sound, and a communication module 209 configured for wired and/or wireless communications with other off-firearm external electronic devices configured to interface with the microcontroller. The geolocation module 161 generates a geolocation signal, which identifies the geolocation of the firearm (to which the programmable controller is attached), and communicates the geolocation signal to the programmable microcontroller 200, which in turn may communicate its location to a remote access device. The audio module 218 may be configured to generate suitable audible alert sounds or signals to the user such as confirming activation of the actuator system, successful or failed system access attempts, component failure attention alerts, or other useful status information.
The communication module 209 comprises a communication port providing an input/output interface which is configured to enable two-way communications with the microcontroller and system. The communication module 163 further enables the programmable microcontroller 200 to communicate wirelessly or wired with other external electronic devices directly and/or over a wide area network (e.g. local area network, internet, etc.). Such remote devices may include for example cellular phones, wearable devices (e.g. watches wrist bands, etc.), key fobs, tablets, notebooks, computers, servers, or the like.
The display 205 may be a static or touch sensitive display in some embodiments of any suitable type for facilitating interaction with an operator. In other embodiments, the display may simply comprise status/action LEDs, lights, and/or indicators. In certain embodiments, the display 205 may be omitted and the programmable microcontroller 200 may communicate with a remote programmable user device via a wired or wireless connection using the wireless communication module 209 and use a display included with that remote unit for displaying information about the actuator system and firearm status.
Besides a battery sensor 208 and trigger sensor(s) 159, the additional sensors noted above which are operably and communicably connected to microcontroller 200 may be used to enhance operation in some embodiments. In one example, a grip force sensor 206 may be used to wake up the microcontroller 200 (e.g. usable in Step 502 of control logic process 500 in
An intentional trigger pull to discharge the firearm may be sensed or detected in one embodiment via one or more trigger sensors 159. At least one trigger sensor is provided. Sensor 159 is positioned proximate to rotating trigger member 104 and operable to detect movement of the trigger such as by direct engagement or proximity detection. In some embodiments, the trigger sensor 159 may be a displacement type sensor configured to sensing movement and displacement position of the trigger during its travel. Sensor 159 may alternatively be a force sensing type sensor operable to sense and measure the trigger pull force F exerted on the trigger by the user. A force sensing resistor may used in some embodiments. Trigger sensor 159 is operably and communicably connected to the microcontroller 200 via wired and/or wireless communication links 201 (represented by the directional arrowed lines shown in
Another example of potentially desirable sensors is an accelerometer or other motion sensing device such as motion sensor 207 if the firearm is moved the user indicating potential onset of an intentional firing event. By monitoring the acceleration or motion of the firearm, the sensor 207 may be used may be used in addition to or instead of grip force sensor 206 to wake up the microcontroller 200 (e.g. usable in Step 502 of control logic process 500 in
One possible enhancement to the firearm control would be to sense the movement of the trigger using sensors 159 and actuate the firing event prior to the operator feeling the end of travel of a mechanical trigger when using the actuator in a firing mechanism release role as further described herein. This would enhance trigger follow-through and greatly reduce the operator effects of flinching as the firing event approaches. Additionally, since precise trigger event timing can be provided independent of the firing actuation event, the same firing actuator can be used with many different trigger force and displacement profiles.
One enhancement to the control system disclosed herein is the inclusion of one or more wireless communications options in some embodiments such as Bluetooth® (BLE), Near-Field Communication (NFC), LoRa, Wifi, etc. implemented via communications module 209 (see, e.g.
Referring now to
As the trigger 121 moves rearward and is displaced against the mechanical Hooke's law force of the spring 125, the trigger 121 (defined by rotating trigger member 104) can be released at any point during its travel by energizing the electromagnetic trigger mechanism 100 through the use of feedback to the microcontroller 200 provided by a trigger displacement sensor 159 operably and communicably coupled to the microcontroller. As the desired preprogrammed set-point is reached which is sensed by displacement sensor 159 and received by microcontroller 200, the trigger 121 is released via the microcontroller energizing the electro magnetic coil 106 in a fast snap-like action that initiates the trigger movement transfer means to activate the firing mechanism such as by releasing the striking member 130 directly engaged by the trigger mechanism 100 (see, e.g.
It should be noted that spring 125 if provided affects and establishes a mechanically-based component of the force/displacement profile for the trigger 121. Permanent magnet 108 may be considered to establish a magnetically-based component of the force/displacement profile. In one embodiment, spring 125 acts in a biasing direction counter to the holding force created by permanent magnet 108. Spring 125 therefore acts in such an arrangement to assist the user in pulling the trigger against the static magnet holding field of the magnet 108. Permanent magnet 108 acts to reset the rotating trigger member to the vertical unactuated position after a trigger pull event even in embodiments without a spring which may be sufficiently fast acting to support multiple trigger pulls in rapid succession. As a corollary, it bears noting that the trigger 121 of the snap actuator trigger mechanism 100 is not returned to the unactuated position by the microcontroller 200 and power source 122. Instead, the magnet 108 and/or other mechanical means (e.g. springs) that might be provided are used to reset the trigger. This allows the actuator coil 106 to be de-energized at the end of the full trigger travel or displacement until needed during the next trigger pull event, which conserves battery power.
Additional enhancements can be combined to alter and/or improve the trigger feel. In one embodiment, a segmented trigger design shown in
In operation, as the trigger (i.e. lower portion 118) is displaced against the biasing force of spring 126 with the separately pivotable upper portion 120 remaining stationary and engaged with permanent magnet 108, a displacement sensor 159 determines the threshold position during trigger travel (i.e. displacement distance) for energizing the electromagnet coil 106 in the snap actuator. At this point, the electromagnet coil is electrically energized to cancel out the permanent magnet 108 generated static holding force or primary resistance and creates a crisp snap-like final movement of the trigger linkage. The final trip force is selectable by sensing the desired displacement/force point to electrically break-over the electromagnetic snap actuator prior to reaching the magnetic flux open-loop break-over point of the permanent magnet.
In
The trigger member 104 in
Referring to any of the foregoing embodiments of
In the un-energized state of the actuator 123, an operator can apply pressure to the rotating trigger member 104 until it exceeds the fixed holding force of the permanent magnet 108 at which time the trigger and its integral sear 131 will move, thereby releasing the striking member 130 (e.g. hammer or striker) to strike a chambered round and discharge the firearm. Ideally, the fixed un-energized holding force provided by the permanent magnet108 may be chosen to product a heavy trigger pull force that would be acceptable as a manual default should battery power or a failure of the magnetic coil or control logic result in a failure to operate properly electronically. An example of this open-loop breakover trigger force profile is shown in
In normal operation, a range of trigger release forces can be chosen by applying electricity to the magnetic coil via microcontroller 200 to add to or subtract from the fixed holding force of the permanent magnet. An example of this new electrically adjusted breakover trigger force profile is also shown in
A simple mechanical switch could be used for trigger sensor 159 in its most basic form to sense the movement of the trigger initiated by the user or shooter. Other means such as a displacement and/or force sensor can be used instead of or in combination with a mechanical switch as previously described herein to determine that an operator has taken a positive action to pull and actuate the trigger.
In its simplest form, a potentiometer 371 as shown in
Alternatively, a simple basic electronic logic circuit or instructions implemented by microcontroller 200 and associated circuitry could be used to control precisely the polarity, the amount of voltage, and timing of the electrical energy pulse sent to the magnetic coil 106 by the microcontroller for energizing the actuator 123 of trigger mechanism 100. This allows the user to highly customize the trigger pull force-displacement profile. Actuation control circuit 202 (see, e.g.
Referring now to
To achieve a crisp fast acting trigger release feel with a reliable means for varying the trigger force, one embodiment may include force or displacement type sensor 159 monitored by microcontroller 200 that determines, in real time, when the desired degree of actual trigger force or displacement is applied to the trigger by the user during a trigger pull event. At this point, a pulse of electrical energy is applied to the magnetic coil 106 by the microcontroller to quickly lower the static magnetic holding force breakover point for actuating the trigger mechanism 100 and releasing its integral sear 131 to discharge the firearm.
Control and adjustment of the dynamically variable force electromagnetic actuator trigger mechanism would ideally be through the use of microcontroller 200. Such a control system could easily be configured with a wireless communication capability such as Bluetooth BLE, NFC, LoRa, WiFi or other commercial or custom communications means (see, e.g.
Dual Closed Magnetic Flux Loop Path Embodiment
Trigger mechanism 300 includes an electromagnetic snap actuator 350 configured to form the dual closed magnetic flux loop or paths. Actuator 350 may be a non-bistable release type electromagnetic actuator in which the actuator is not energized to change position for either initiating movement or to reset the actuator similar to trigger mechanism snap actuator 123 previously described herein. Instead, similarly to actuator 123 previously described herein, microcontroller 200 may be programmed and configured to energize the present actuator 350 of the dual flux loop design only in response to a manual trigger pull. This generates the secondary dynamic or active magnetic field which interacts with the primary fixed or static magnetic field generated by the permanent magnet 308 in either an additive or subtractive operating mode depending on the polarity of the power source 122 established via the microcontroller. The present actuator 350 is configurable by the user or shooter via the microcontroller 200 to change the trigger pull force and displacement profile in the same manner described above for single flux loop electromagnetic actuator 123.
Referring to
Yoke 302 includes an outer yoke portion 305 and a central inner yoke portion 307. The outer yoke portion 305 has a circular annular and circumferentially extending body which may be considered generally O-shaped in configuration. Outer yoke portion 305 circumscribes a central space 303. Inner yoke portion 307 is nested inside the outer yoke 305 in the central space 603. Outer yoke portion 305 generally comprises a common horizontal bottom section 305A, upwardly extending rear and front vertical sections 305B, 305C spaced laterally apart, and a pair of inwardly-turned top sections 305D, 305E having a horizontal orientation. Each top section 305D, 305E is removably attached directly to a respective one of the vertical sections 305B and 305C to facilitate assembly of the actuator 350. In one embodiment, each top section 305D, 305E may be attached to a vertical section by a pair of laterally spaced apart longitudinal fasteners such as cap screws 316 which extend through axial bores 318 in vertical sections 305B, 305C and engage corresponding threaded sockets 319 formed in the top sections. The top sections 305D, 305E when mounted to each of the vertical sections 305B, 305C are horizontally and longitudinally spaced apart to define a top gap or opening 309 therebetween which communicates with the central space 303 of the outer yoke. A working end portion 304A of the rotating member 304 is received between the top sections 305D, 305E in opening 309 and movable therein when the actuator 350 is actuated, as further described herein.
The inner yoke portion 307 is generally straight and vertically elongated forming a substantially hollow structure defining an internal upper cavity 330 which movably and pivotably receives rotating member 304 therein. Inner yoke portion 307 may be formed as integral unitary structural part of the outer yoke portion 305as shown in the figures and extends upwards from the horizontal bottom section 305A thereof into central space 303. Inner yoke portion 307 is cantilevered from the outer yoke portion 305 in this construction. In other embodiments, inner yoke portion 307 may be formed as a separate component attached to bottom section 305A of outer yoke portion 305 such as via fasteners, adhesives, welding, soldering, etc. Inner yoke portion 307 is orientated parallel to the rear and front vertical sections 305B, 305C of the outer yoke portion 305. The inner yoke portion 307 may be spaced approximately equidistant between the rear and front vertical sections 305B, 305C to facilitate winding coil 306 around the inner yoke portion in the central space 303 of actuator 350.
Because the rotating member 304 is sheathed or shrouded by inner yoke portion 304 for a majority of its length in one embodiment as best shown in
In one embodiment, yoke 302 comprising the outer yoke portion 305 and integral inner yoke portion 307 may be split longitudinally (i.e. lengthwise) front a right half-section 305RH and left half-section 305LH. This split casing arrangement facilitates assembly of the rotating member 304 inside the inner and outer yoke portions. The half-sections 305RH and 305LH may be mechanically coupled tougher by any suitable means, including for example without limitation fasteners including screws and rivets, adhesives, welding, soldering, etc. In one embodiment, threaded fasteners such as transverse cap screws 317 may be used.
Each half-section 305RH, 305LH defines a portion of the vertically elongated upper cavity 330 in inner yoke portion 307 which pivotably receives rotating member 304 partially therein. The cavity 330 communicates with a downwardly and rearwardly open internal lower cavity 331 of the actuator 350 formed in outer yoke portion 305. Lower cavity 331 pivotably receives bottom actuating section 304B of rotating member 304 therein. Lower cavity extends rearward from the central pivot region of the outer yoke portion 305 (containing pivot pin 335) to the rear side of the actuator 350 and bottom section 305A of the outer yoke potion. Upper cavity 330 extends vertically from the lower cavity 331 and penetrates the top and bottom ends of the central inner yoke portion 307.
Referring particularly to
Rotating member 304 has a vertically elongated body including a top or upper operating end section 304A, bottom or lower actuating end section 304B, and intermediate section 304C extending therebetween. Both top operating end section 304A and bottom actuating end section 304B may be enlarged and longitudinally/horizontally elongated in the front to rear direction relative to intermediate section 304C in one embodiment as shown to achieve their intended functionality. In one embodiment, intermediate section 304C may have parallel sides and be generally rectilinear in configuration and cross-sectional shape. Operating end section 304A is configured to operably interface with the both the outer yoke portion 305 of yoke 302 and the firing mechanism of the firearm as further described herein. When the electromagnetic actuator 350 is fully assembled, the operating end section 304A protrudes upwards beyond the inner yoke portion 307 of yoke 302 and is exposed to engage both the outer yoke portion 305 and a firing mechanism component or mechanical linkage.
The top operating end section 304A of rotating member 304 may be generally cruciform-shaped in one embodiment defining horizontally/longitudinally protruding front and rear extensions 332. This portion of operating end section 304A may be considered to generally resemble double-faced hammer in configuration and defines two opposite and outwardly facing front and rear actuation surfaces 334F, 334R (see, e.g.
Actuator 350 may further include an engagement feature strategically located on the upper portion of central rotating member 304 and configured to interface with a component of the firearm's firing mechanism in release-type operational role. In various embodiments, the engagement feature may be an operating extension or protrusion 333 of the rotating member 304 as illustrated in
Operating protrusion 333 extends upwards from between the front and rear extensions 332 at the top of the rotating member 304. Operating protrusion 333 may be approximately centered between actuation surfaces 334F, 334R in one embodiment; however, other positions of the operating protrusion may be used depending on the interface required with the firing mechanism component acted upon by the operating protrusion 333. The operating protrusion 333 may be configured to releasably engage a firing mechanism component or linkage in a direct release role or an indirect release role. Accordingly, operating protrusion 333 may be configured and operable to act directly on the energy storage device such as the spring-biased striking member 130 shown in
Permanent magnet 308 may be fixedly attached to rear top section 305D of outer yoke portion 305 in a position between the top section 305D and the rotating member 304. Rear top section 305D may include a flat forward facing surface 308a for mounting the permanent magnet 308. This arrangement advantageously magnetically attracts and engages rotating member 304 to create a static holding force on the rotating member. Rotating member 304 is magnetically biased rearwards towards its rearward unactuated position associated with a corresponding unactuated forward position of the trigger member 320 when not pulled by the user. Any suitable mechanical coupling means may be used to affix magnet 308 to the outer yoke portion 304, including for example without limitation adhesives, fasteners, welding, soldering, etc.
The enlarged bottom actuating end section 304B of the rotating member 304 may be completely disposed in lower cavity 331 of outer yoke portion 305 in one configuration and enclosed therein by the yoke 302. Actuating end section 304B includes a horizontally/longitudinally elongated cantilevered rear actuating arm or extension 340 used to manually actuate the rotating member 304 via a trigger pull by the user. This may be considered to give the rotating member 304 a generally L-shaped body configuration. Actuating extension 340 extends rearward from the central pivot region of the bottom actuating end section 304B towards the rear side 311 of the actuator 350. In one embodiment, the actuating extension 340 may be formed integrally with the rotating member body as a unitary monolithic structural part thereof. Actuating extension 340 may be obliquely angled to the vertical central axis CA of actuator 350 and may extend completely to the rear side 311 of the actuator such that the free terminal rear end of the actuating extension is exposed for attachment of monitoring or sensing devices, as further described herein.
The rear actuating extension 340 includes an upwardly facing spring seating surface 341 and downwardly facing actuation surface 342. Each surface may be substantially flat or planar in one configuration. Surfaces 341 and 342 may be formed on a laterally widened paddle-shaped portion of actuating extension 340 at the terminal rear end of the extension as shown (best seen in
Spring seating surface 341 of the rear actuating extension 340 is engaged by one end of an operating or trigger return spring 344 disposed in vertical spring socket 345 formed in yoke 302. In one embodiment, spring socket 345 may be formed in rear vertical section 305B of the outer yoke portion 305 as shown. Spring 344 may be a helical coil compression spring in one embodiment; however, other type springs may be used. Spring 344 acts to bias the rear actuating extension 340 downward, which in turn rotates the rotating member 304 about pivot pin 335 to bias the top operating end section 304A into engagement with the permanent magnet 308 when the trigger member is not pulled and actuated (e.g. ready-to-fire position).
Rotating member 304 may be pivotably mounted to yoke 302 via a pivot protuberance such as pivot pin 335 which defines a pivot axis PAL Rotating member 304 is movable between a rearward unactuated position magnetically engaged with permanent magnet 308 (or yoke 302 in other embodiments depending on placement of the magnet), and a forward actuated position disengaged from the permanent magnet. It bears noting that the rotating member 304 may be moved between the two positions by sensing user action on the trigger member 320 which then energizes the actuator 350. Movement of the rotating member 304 then comes under the influence of the secondary electromagnetic field generated by the electromagnetic actuator 350 when energized by the microcontroller 200, which can either assist with completing the trigger pull for the user, or retard trigger travel/displacement by creating a resistance force on the trigger as previously described herein.
In one embodiment pivot axis PA1 may define a common pivot axis for mounting both the rotating member and trigger member 320 to yoke 302 of snap actuator 350 in one embodiment. Pivot pin 335 therefore defines a common center of rotation about which both the rotating member 304 and trigger member 320 each pivot or rotate independently of each other Common pivot axis PA1 is aligned with central axis CA of the actuator 350 which passes through this pivot axis. In one embodiment, pivot pin 335 is disposed inside lower cavity 331 of the outer yoke portion 305 which serves as the mounting point for the rotating member and trigger member. Rotating member 304 and trigger member 320 each include laterally open pivot holes 336 and 337 respectively for inserting pivot pin 335 therethrough. Holes 336 and 337 are concentrically aligned when the trigger mechanism 300 is fully assembled.
In one construction, as shown, pivot pin 335 may comprise two right and left half-pin sections 335R, 335L each fixedly disposed on a respective right and left yoke half section 305RH, 305LH. In one embodiment, half-pin sections may be integrally formed with the right and left yoke half sections. Each half-pin section collectively forms a complete pin extending from the right to left yoke half-section when assembled together to capture both the rotating member 304 and trigger member 320 thereon and therebetween the yoke half sections. In an alternative embodiment, a single one-piece pivot pin may instead be used which extends completely through lower cavity 331 of outer yoke portion 305 from right to left. In one embodiment, pivot pin 335 is preferably circular in cross section.
Referring to the exploded views of electromagnetic actuator 350 in
The trigger member 320 will now be described in further detail. With continuing reference to
The outer trigger 321 includes an upper mounting portion 362 and a lower blade portion 363 depending downwards therefrom. The blade portion includes a vertical slot 364 for movably receiving the inner safety trigger 322 therethrough when actuated by the user. Blade portion 363 may have an arcuately concave front surface configured for engagement by the user's finger. The mounting portion 362 of outer trigger 321 may have a U-shaped body in one embodiment defining a forwardly and upwardly open channel 361 which movably receives the lower actuating section 304B of rotating member 304 therein. The rear actuating extension 340 of rotating member 304 also extends through channel 361. The actuating section 304B of the rotating member is therefore nested inside the mounting portion 362 of the outer trigger 321.
Outer trigger 321 further includes a cantilevered rear operating arm or extension 360 arranged to engage the rear actuating extension 340 of the rotating member 304. In one embodiment, operating extension 360 protrudes rearwardly from the mounting portion 362 of outer trigger 321. Operating extension 360 defines a flat or planar upwardly facing operating surface 343 configured and arranged to abuttingly engage downwardly facing actuation surface 342 of rotating member 304. The interface between the operating surface 343 and actuation surface 342 is one of a flat-to-flat interface in one embodiment as shown (see, e.g.
In one embodiment, a force/displacement sensor such as a thin film force sensing resistor 370 may be interposed at the interface between the operating surface 343 of the operating extension 360 of outer trigger 321 and actuation surface 342 of the rear actuating extension 340 of rotating member 304. Force sensing resistors measure an applied pressure or force between two mating surfaces and are commercially available from numerous suppliers. Force sensing resistor 370 is operably and communicably coupled to microcontroller 200. Force sensing resistor 370 is configured to detect and measure a trigger force F exerted by the user on the outer trigger 321 when pulled to fire the firearm 20. When paired with trigger force setpoint preprogrammed into microcontroller 200, this serves as a basis for intermittently energizing the electromagnetic snap actuator 350 based on trigger force, as further described herein.
Inner trigger 322 is biased toward its substantially vertical forward position (see, e.g.
In operation, the trigger mechanism 300 will be in the ready-to-fire condition shown in
The stationary yoke 302 and the rotating member 304 may be formed of any suitable magnetic metal capable of being magnetized, such as without limitation iron, low-carbon steel, nickel-iron, cobalt-iron, etc. Suitable fabrication methods include for example without limitation metal injection molding, casting, forging, machining, extrusion, laminated stamping, and combinations of these or other methods. The method is not limiting of the invention.
The operating theory of the electromagnetic trigger mechanism 300 with snap actuator 350 is as follows. The central rotating trigger armature or rotating member 304 is surrounded by the magnetically conductive yoke 302 configured to form two possible flux loop paths. A primary fixed or static magnetic flux and associated holding force is established using the permanent magnet 308 in the right hand flux loop or path to hold the central rotating member 304 firmly to the right side of its pivotal range of motion within the yoke 302. The primary magnetic flux path generated by the permanent magnet 308 is shown in
Under normal operation to discharge the firearm, the operator or user pulls the outer trigger 321 which applies a trigger pull force F thereon that acts in an opposite direction counter to the primary fixed or static magnetic field flux and holding force generated by the permanent magnet 308. This creates pressure on and pivotably displaces the outer trigger 321 rearwards. This applied pressure and trigger displacement provides the means for sensing physical activity with the trigger sensor 370 as input for Step 504 in the control logic process of
In one embodiment, the sensor 370 may be a thin film force sensing resistor as previously described herein which measures the magnitude of the trigger pull force F. Alternative approaches such as load cells, piezo-electric force sensors, displacement sensors such as hall effect sensors, GMR sensors, and optical or mechanical switches or sensors could also be used. When the force (or displacement) reaches a preset desired trigger trip or setpoint preprogrammed into microcontroller 200 for the variable force trigger, the control system applies electrical energy to the magnetic coil 306.
At the preset desired force or displacement trip or setpoint, the pulse of electrical energy applied to the electromagnet coil 306 by microcontroller 200 generates user-selectable and adjustable dynamic secondary dual magnetic field fluxes. The two flux loop or paths for the right-hand side and left-hand side magnetic fluxes M2 and M3 are shown in
When electrical energy is removed from the magnetic coil by microcontroller 200, the left-hand flux path collapses and the static permanent magnet 308 attractive force takes back over and pulls the rotating member 304 back to the right-hand side of the yoke 302 as shown in
Under conditions when the electromagnet coil 306 is not energized, either by intentional design or failure of components or weak batteries, the operator can still cycle the firearm by applying force/displacement to the outer trigger 302 that exceeds the fixed or static holding force of the permanent magnet 308.
An alternate embodiment and application can be envisioned where the static holding force of the permanent magnet 308 is increased by applying electrical energy to the magnetic coil 306 in an “additive” manner instead that reinforces the permanent magnet's holding force. In this instance, the microcontroller 200 is configured to apply the electric pulse to electromagnet coil 306 with an opposite second polarity. The secondary dynamic right-side flux M2 would therefore act in the same clockwise direction as the static flux M1 seen in
One key feature of the present variable force trigger mechanisms 100 or 300 disclosed herein is the ability to select a desired trigger pull force-based release breakpoint or breakover setpoint for the trigger that is optimal for the user's experience and shooting situation. In one embodiment, the setpoint may be preprogrammed into microcontroller 200 for use in the control logic shown in
The cellphone microprocessor runs a local software application or “app” comprising program instructions or control logic that allows adjustment of the trigger release profile. Two application screens which may be presented to the user on the cellphone visual touchscreen are shown in
It will be appreciated that numerous variations in the configuration of the trigger profile software application are possible. The trigger profile software may also be implemented in other external electronic devices, such as a laptop, notebook, electronic pad, desktop computer, or other processor-based devices capable of communication with the onboard microcontroller 200 of the firearm.
It bears noting that particularly the electromagnetic trigger mechanism 300 is substantially immune to external magnetic field which could interfere with proper operation of the trigger mechanism electromagnetic actuator 350. The permanent magnet 308 in the embodiment presented herein provides a fixed or static holding force for a trigger-sear release system in a closed flux loop that limits susceptibility to external magnetic fields. With the exception of the small air gap created between the rotating member 304 and stationary yoke 302, that allows for the motion of the rotating central trigger/armature (rotating member 304), the magnetic yoke cross sectional area, and soft magnetic material properties of the yoke and rotating member to provide a low reluctance path that captures almost all of the magnetic flux generated by energizing the magnetic coil and from the permanent magnet.
Since magnetic force within the air gap increases with magnetic cross-sectional area and decreases with the square of the air gap length or width, practical designs which are optimized for force and speed tend to minimize the length or width relative to the cross-sectional area of the yoke. A consequence of this is that variable force trigger designs based on these design principles are inherently immune to external magnetic field interference. In practice, it is virtually impossible to change the state of the variable force trigger using an external magnet (and optional soft magnetic material yoke) provided the rotating member is physically isolated from the external magnet by at least one air gap distance. This will virtually always be the case in practical firearm embodiments.
In the present firearm embodiment, electromagnetic snap actuator 350 operably interacts with and releases the energy storage device such as movable striking member 130 in an indirect manner via an intermediate firing mechanism component. The central rotating member 304 of the electromagnetic snap actuator 350 in this case operably interacts with a sear 375 operably interposed in the firing linkage between actuator 350 and striking member 130 (see also
In one embodiment, the firearm 20 may be a semi-automatic pistol recognizing that the trigger mechanism 300 with electromagnetic actuator 350 may be used in any type firearm having a pivotably or linearly movable striking member 130 and optionally a sear 375 or other intermediate component in some designs which operate to hold and selectively release the energy storage device (e.g. hammer or striker). Accordingly, the trigger mechanism 300 may be variously embodied in firearms including for example without limitation rifles, carbines, shotguns, revolvers, or other small arms.
Firearm 20 generally includes a frame 22, trigger guard 23 formed as a unitary structural part of the frame or a discrete guard separately attached thereto, reciprocating slide 24, barrel 26 mounted to the frame and/or slide 24, and a movable energy storage device such as striking member 130. Slide 24 is slideably mounted on frame 22 for movement in a known axially reciprocating manner between rearward open breech and forward closed breech positions under recoil after the pistol is fired. A recoil spring 29 compressed by rearward movement of the slide acts to automatically return the slide forward to reclose the breech after firing. Slide 24 may be also considered to define an axially movable receiver, in contrast to a fixed receiver mounted rigidly to the frame or chassis of a long gun such as for example a rifle, carbine, or shotgun (see, e.g.
Barrel 26 is axially elongated and includes rear breech end 30, front muzzle end 31, and an axially extending bore 25 extending therebetween. Bore 25 defines a projectile pathway and a longitudinal axis LA of the firearm which defines an axial direction; a transverse direction being defined angularly with respect to the longitudinal axis. The breech end 30 defines a chamber 32 configured for holding an ammunition cartridge C. The slide 24 defines a vertical breech face 34 movable with the slide and arranged to abuttingly engage the rear breech end 30 of barrel 26 to form the openable/closeable breech in a well known manner. The vertically elongated rear grip portion of frame 22 comprises a downwardly open magazine well which receives a removable ammunition magazine 136 therein for uploading cartridges automatically into breech area after the firearm is discharged which are chambered into the barrel via operation of the slide 24. All of the foregoing components and operation of semi-automatic pistols are well known in the art without requiring further elaboration.
With continuing reference to
Sear 375 is pivotably movable between an upward standby position in which sear protrusion 44 engages catch protrusion 42 of striker 40, and a downward fire position in which the sear protrusion disengages the catch protrusion to release the striker for firing the firearm 20. Sear 375 is held in the upward position by engagement with upstanding operating protrusion 333 on the central rotating member 304 of electromagnetic actuator 350 of the trigger mechanism 300 (see, e.g.
In operation, the firing mechanism is initially in the ready-to-fire condition or state shown in
To fire the firearm 20, the operator or user pulls the trigger member 320 thereby applying a trigger pull force F which is sensed and measured by the trigger sensor such as thin film force sensing resistor 370. The electromagnet coil 306 is then energized by microcontroller 200 in accordance with the control logic of
Fire-by-Wire Dynamic Variable Force and Displacement Trigger Embodiment
Expanding on the variable force trigger concept disclosed herein, it may be ideal if both the trigger force and trigger displacement could be dynamically changed during the trigger pull and firing sequence. One way to accomplish this would be to completely separate the trigger function from the firing event. The trigger event would generate an electrical signal that would be sent by wire to a separate electromechanical actuator to fire the firearm. In this embodiment, the trigger force could be dynamically adjusted as before; but the displacement could also be dynamically adjusted. This can be accomplished by a pre-defined effect or with feedback using a displacement sensor 159 of a flux measurement type such as a hall-effect or alternatively a GMR (Giant Magnetoresistance Effect) sensor operably incorporated with the trigger mechanisms 100 (with single flux loop actuator 123) or 300 (with double flux loop actuator 350). Such a sensor could be placed near the air gap A (see, e.g.
Force feedback could be combined with the dynamic adjustment of displacement and force in trigger feel to indicate the firing point. At the point of firing, the trigger force could be dynamically changed to give the operator haptic or kinesthetic feedback of the fire decision being reached. Optionally, the kinesthetic feedback could be supplied slightly after the actual firing event to minimize the possibility of the user staging or anticipating the firing event and minimizing flinching which could adversely affect point of aim.
The fire-by-wire concept has one potential weak spot in that a single fire signal could result in a single point of failure. A false positive or negative signal resulting from a short, open, or other failure could result in a failure to function or unintended trigger event. One of several concepts that would mitigate this is to have the trigger event generate two redundant triggering signals, an armed and a fire event signal. Using the displacement sensor 159, a minimum displacement of the trigger could be used as a signal to arm the firing system. The final fire decision could be an electrical contact or optical switch. Using two or more sensors, with different failure mechanisms, should ensure no single failure point. By adding intelligence to the relationship of the two signals, the reliability can be enhanced further. For example, it should not be possible to arm the firing sequence unless the trigger displacement has recovered to a predetermined position and the electro-mechanical switch is in an open state. The displacement sensor could be used to arm the firing signal as displacement is increased but before the mechanical switch closes. The actual closing of the mechanical switch would need to happen within a predefined time window or the arm signal would time out. This would ensure that the trigger pull event is representative of an actual firing event and would not be duplicable as a random failure of several components at the same time.
It can be envisioned that by incorporating the additional system sensors shown in
The fire-by-wire electronic firing system may still incorporate a modified version of either trigger mechanisms 100 or 300. In such an application, electromagnetic actuators 123 or 350 of trigger mechanism 100 or 300 respectively would not physically engage/disengage a component of the firing mechanism as previously described herein. Instead, the actuators would simply be used to adjust the trigger release profile and breakpoint of the trigger member 104 or 320 in the manner previously described herein in accordance with the control logic of
Referring to
If however the Step 404 test is positive, the microcontroller 200 will arm the firearm and continuously monitor for a trigger event and a number of other possible state change events in Step 408; some examples of which are indicated in
An example of one state change event that would effect authorization is the detection of loss of intent-to-fire grip that would indicate the user no longer has control of the firearm (Step 412). Another example would be the detection of an unsafe acceleration force detected by motion sensor 207 (Step 411), which is associated with falling or being bumped or jarred while holding the firearm. In the presence of a high acceleration force, the system disables the firing due to unsafe conditions. Another example of state-change events would be the detection of a system error or the detection that the battery might not have sufficient remaining power to reliably actuate the magnetic actuator (Step 416). These types of faults and warning would also drop the firearm out of the arm state and indicate a warning to the user.
An actuation event cycle also starts if a trigger event is detected by trigger sensors in Step 410, and the firearm is in an armed state and no state change event (Steps 411, 412, or 416) has occurred to disarm the firing mechanism as indicated above. Steps 422 through 430 represent a firing sequence for the firearm implemented by microcontroller 200. For added safety, two independent trigger events, “Trigger Event 1” based a signal from mechanical trigger sensor 160 and “Trigger Event 2” based on a signal from the electronic sensor 159 or 370 may be used to initiate a valid trigger event. However, a single trigger sensor and event may be used in other embodiments. After the system detects Trigger Event 1 has occurred, the system then confirms that the firearm is still under the users physical control with an intent-to-fire grip (Step 422). Next, the system detects whether an intent-to-fire Trigger Event 2 is activated. This provides the double layer of firing security. Assuming Steps 422 and 426 are positive, the electronic safety shorting clamp 251 is lifted (Step 428) to enable the firing mechanism. A high voltage electric pulse or signal from circuit 250 is sent by the microcontroller 200 via actuation control circuit 202 to the E-sear piezo actuator 252 which discharges the firearm (Step 430). The firing system is then reset for the next firing event.
During the preceding firing sequence of the fire-by-wire firing mechanism, it bears noting that the control logic of
Magnetically Variable Trigger Mechanisms
The following disclosure describes non-electrically operated trigger mechanisms which are magnetically variable by manually adjusting the static magnetic field of the mechanism. These trigger mechanisms function without an electric power source or electromagnet to release a spring-loaded striking member for striking a chambered round of ammunition, but embody some of the same general magnetic operating principles of the electromagnetically operated trigger mechanisms described heretofore.
Traditional triggers for firearms provide a decisive intent-to-fire signal through mechanical motion that utilizes a displacement and force profile developed by using mechanical linkages, springs and the release of energy stored in a spring-biased hammer, striker, or sear. The trigger force and displacement curve or profile is normally fixed by these mechanical linkages and springs. A number of designs exist that provide adjustable characteristics for the force and displacement of the trigger using set screws, additional springs and other parts, or by completely changing components in order to customize the force-displacement profile of firearm triggers. Such adjustment techniques, however, modify the trigger pull force resistance in a purely mechanical manner which is limited by the physical interaction of trigger parts and associated linkages alone. To provide adjustment of the trigger pull force, these trigger mechanical linkages may therefore become quite complex, require multiple individual mechanical components, and hence are susceptible to wear and failure.
Exemplary embodiments of the present invention provide a trigger mechanism for a firing system of a firearm which is magnetically adjustable and variable, thereby providing quick and easy user-adjustment of the trigger pull force. Both closed and open magnetic flux loop designs are provided. In one implementation, the combination of a closed magnetic flux loop design and a manually translatable magnetic control device or insert configured and constructed to adjustably vary the magnetic field in the trigger mechanism produced by a permanent magnet disposed in the loop overcomes the deficiencies of purely mechanical and often complex adjustable trigger designs comprising multiple parts, springs, and linkages. The control device may comprise a “soft” magnetic material—a material preferably having a large relative magnetic permeability (i.e. the ability to support formation of a magnetic field in the material). As used in the art, “soft” magnetic materials refer to materials which are easily magnetized and demagnetized. Non-limiting examples include iron, low-carbon steel, nickel-iron, cobalt-iron, etc. The control device or insert in some embodiments is selectively and variably insertable into and retractable from a control recess or air gap (B) formed in the magnetic flux loop by varying degrees to adjust the trigger force. The control air gap B, formed by removing material from the stationary yoke, attenuates (i.e. decreases or diminishes) the maximum magnetic flux available in the loop at a working air gap (A) between the yoke and a movable trigger member which retains the trigger member magnetically to the yoke until the trigger member is pulled. Inserting the control device or insert into the control air gap B increases the magnetic flux in the closed loop at air gap A. Conversely, retracting the control device or insert from the control air gap B decreases the magnetic flux in the loop at air gap A. In some embodiments, the control device or insert may comprise the permanent magnet for the closed magnetic loop and inserting/retracting, or rotating the insert relative to the control air gap B changes the magnetic flux in the loop at air gap A. In another implementation, the combination of an open flux loop design and a manually translatable magnet configured to adjustably vary the proximity of a magnet to the trigger body provides adjustment of the trigger pull force. Each trigger mechanism design is further described herein.
In one aspect, embodiments of the magnetic trigger mechanism disclosed herein represent adjustable variable force magnetic air gap trigger designs. A permanent magnet in the closed flux loop generates a primary static magnetic field producing a fixed or static holding force for a trigger-sear release system which limits susceptibility to external magnetic fields that might affect the trigger force. By adjusting the control air gap in the closed magnetic flux loop via the magnetic control device, the fixed or static holding force can be increased or decreased to provide a variable range of trigger force breakpoints or setpoints that provide a crisp feel as the trigger pull force applied by the user to the trigger meets or crosses the fixed magnetic holding force set point during a trigger pull event. The fixed or static magnetic field generated by the permanent magnet in the closed flux loop creates a primary resistance force opposing movement of the trigger when pulled by the user. The trigger mechanism operates to release the movable sear of the firing system, which in turn releases a cocked energy storage device to discharge the firearm. The energy storage device may be a spring-biased striking member such as a pivotable hammer or linearly movable striker configured to strike and detonate a chambered ammunition cartridge; each of which is described herein.
The different examples of trigger mechanisms presented hereafter illustrate the relative features of the design strategies used in each design embodiment. The full analysis is not included; however, important summary performance is presented. It will be clear to those in the field that these examples are not exhaustive, but merely a sample of differing design strategies which can be implemented. It should also be clear that desirable design features of a trigger mechanism include a wide range of adjustable trigger pull force, an adjustment means that is relatively linear in response, and an adjustment means being relatively insensitive to normal mechanical tolerances.
Closed Magnetic Loop Designs
It bears noting that the magnet only trigger mechanisms described in this section of the application may also be used with any of the trigger assemblies shown in
Referring to
Rotating trigger member 104 of the trigger mechanism 1000 includes vertically elongated upper working extension or portion 120 and lower trigger portion 118 each mounted about pivot 101, as previously described herein with respect to
The permanent magnet 108 may be disposed and arranged on or within the yoke 102 (see, e.g.
Permanent magnet 108 preferably has dimensions and a cross-sectional area commensurate in dimensions and cross-sectional area to the cross section of the yoke 102, as shown (or alternatively the upper working portion 120 of trigger member 104 if mounted thereto as shown for example by magnet 108′. Optimal coupling of the flux lines of the magnet to the closed loop of magnetic material is achieved by such an arrangement and dimensions. If the magnet is smaller than the yoke in cross section, then flux lines will short across the gap B formed between the two yoke separated pieces in which there is no magnet, reducing the closed-loop flux in the circuit.
The yoke 102 and rotating member 104 are configured to collectively form an annular-shaped closed flux loop resistant to external magnetic fields. Yoke 102 and trigger member 104 define an enclosed open central space 1003 therebetween (see, e.g.
A completely openable/closeable air gap A is formed between the yoke and rotating member. The air gap A may be vertically oriented and normally held closed by the static holding force created by the permanent magnet 108, and opened when the trigger is pulled by the user to overcome the static holding force and discharge the firearm.
The preferably strong permanent magnet 108 arranged in the closed magnetic flux loop maintains a high static holding force threshold inhibiting the movement of the trigger portion 104 (e.g. “trigger” alternatively) around the pivot point 101.
The magnetic control device used to alter the static magnetic field and establish a trigger force breakpoint or setpoint comprises the adjustably translatable soft magnetic material control insert 1001. In one embodiment, the control insert 1001 may be in the form of a triangular or V-shaped wedge formed of a magnetically conductive material such as without limitation a suitable soft magnetic metal capable of being magnetized by a magnet, such as without limitation iron, low-carbon steel, nickel-iron, cobalt-iron, etc. This same material may be used for the yoke 102 and rotating trigger member 104. The control insert 1001 is linearly translatable to project into or retract from a secondary control air gap B formed in the yoke 102 to change the reluctance. Air gap B may comprise an outwardly open and angled wedge-shaped (e.g. triangular) control recess 1002 in one embodiment as shown which may be formed in the yoke 102 by partially removing some material such that the recess does not completely sever the cross section of the yoke (see, e.g.
To linearly translate or move the soft magnetic material control insert, a manually operable actuator 1004 may be operably coupled to the wedge-shaped control insert 1001. The actuator 1004 may be movably mounted to the firearm frame 22, receiver 39, or alternatively a trigger housing 1220 (see, e.g.
The actuator 1004 in one non-limiting example may be comprise an insert adjustment screw 1005 which acts on the wedge-shaped control insert 1001 as shown in
The position of the wedge-shaped control insert 1001 relative to the angled control air gap B and concomitantly the yoke 102 increases or decreases the static holding force in the closed magnetic loop of the trigger mechanism, which holds the upper working portion 120 of trigger member 104 against the yoke 102. This in turn creates the user-adjustable trigger pull force which must be overcome by the user in order to pivot the trigger member about pivot 101 and open the air gap A for releasing the striking member, such as for example without limitation the spring-biased hammer 130 shown in
In sum, rotating and linearly moving actuator 1004 accordingly moves the control insert 1001 between a first position relative to the control air gap B producing a first magnetic static holding force in the closed magnetic loop, and a second position relative to the control air gap B producing a second magnetic static holding force different than the first force (e.g. more or less).
An alternate actuator 1007 for linearly translating the wedge-shaped control insert 1001 of trigger mechanism 1000 is shown in
By adjusting the displacement and position of a wedge control insert 1001 of magnetically conductive material relative to control air gap 1002, the effective length of the control air gap 1002 (the distance magnetic flux lines have to travel in air) can be varied. As the effective length is shortened, the total magnetic flux in the closed loop magnetic circuit increases, and hence the flux density in the air gap A is increased resulting in greater trigger holding force (torque). An increase in the effective length of control air gap 1002 has the opposite effect. Adjusting the displacement and position of control insert 1001 therefore adjusts and changes the resulting strength of the trigger static magnetic field and holding force that creates a primary resistance force opposing movement of the trigger member when pulled by the user that must be overcome. Inserting the wedge control insert 1001 farther into control air gap B increases the static magnetic holding force to increase the required trigger pull force. Conversely, withdrawing control insert 1001 from the control air gap B decreases the static magnetic holding force to lessen the required trigger pull force.
In alternative embodiment shown in
The present closed-loop sliding plate design is based on a principle which allows the magnetic flux to be choked off by introducing a restriction in the magnetic loop. By contrast, it bears mention here that both the sliding magnet design and the rotating magnet design as further described below are based on varying the amount of total flux coupled from the magnet 108 into the magnetic yoke 102.
Another alternative embodiment to achieve the variable coupling of the magnetic flux comprising a closed loop rotating permanent magnet control insert 1040 whose rotational position is adjustable by the user is shown in
It bears noting that since magnetic force within the air gap increases with magnetic cross-sectional area and decreases with the square of the air gap length, practical designs which are optimized for force and speed tend to minimize the length relative to the cross-sectional area. A consequence of this is that actuator designs based on these design principles are advantageously inherently immune to external magnetic field interference. In practice, it is impossible to change the state of the actuator using an external magnet (and optional soft magnetic material yoke) provided the rotating trigger member 104 is physically isolated from the external magnet by at least one air gap distance. This preferably should always be the case in practical firearm embodiments utilizing the trigger mechanisms disclosed herein.
The trigger pull force in all design magnetic embodiments is adjusted by varying the magnetic flux density in the control air gap B acting on the rotating trigger bar or member 104. Ultimately the breakpoint of the trigger is determined by the magnetic flux density in the air-gap A controlled by manipulation of control air gap B via the various control inserts described herein. Even though A is very small, the holding force is determined by the flux density in this space. In general, the flux density at air gap A is varied by either changing the flux density at control air gap B, or by changing the effective coupling of flux from the magnet into the yoke. These two principles are used independently or together in each of the designs. In the case of
For open-loop designs, the flux density is dependent on the magnetic properties of the permanent magnet 108, the physical geometry of the magnet, and the displacement between the magnet and the rotating trigger member 104. For closed-loop designs, the flux density is dependent on the magnetic properties of the permanent magnet 108, the geometry of the magnet, the physical placement of the magnet within the magnetic yoke 102 and the geometry of the control air gap B. In general, the breakpoint force of the trigger mechanism is determined by the flux density at air gap A, but this flux density is varied only by (1) changing the flux using the properties of control air gap B, or (2) changing the coupled flux into the yoke by varying the position or angle of the magnet relative to the yoke at control air gap B.
In general, the magnetic flux density in closed-loop designs can be changed by a combination of changing the reluctance in the magnetic circuit and changing the described below coupling of the permanent magnet 108 into the yoke 102. In open-loop designs discussed below, the magnetic flux density is adjusted by changing the displacement of the magnet 108 relative to the rotating trigger member 104.
Open-Loop Magnetic Design
Summary of Closed and Open Loop Design Comparison Results
Based on the comparative results of the design and performance analysis for each magnetic only trigger mechanism describe above, a few summary conclusions can be offered. Each design disclosed herein is capable of achieving the design goals for a magnetically adjustable trigger mechanism, which are a wide range of adjustable trigger pull force, an adjustment means that is relatively linear, and an adjustment means that is relatively insensitive to normal mechanical tolerances.
The rotating magnet and sliding magnet have similar torque/response curves and similar holding torques. The rotating magnet and sliding magnet designs offer an optimal way of varying holding torque while being least affected by mechanical adjustment tolerances when the user manually adjusts the trigger pull force. A major advantage of the sliding magnet and rotating magnet designs in contrast to just adjusting the width of the control air gap B (via the sliding soft magnetic material plate or wedge control insert designs) is the required precision of the movement over the range necessary to change the torque. When adjusting the reluctance by opening or narrowing the control air gap B via the sliding plate or wedge, it will take a precision adjustment by the user to control the small changes in width of the air gap. Very slight precision changes in control air cap B width have a large impact on the torque. This will require a very tight manufacturing tolerance of the adjustment means to make a reliable and repeatable adjustment. Even with a fine threaded lead-screw, for example, it might only be a fraction of a turn to make a significant adjustment in the effects of the airgap. With the sliding magnet, however, the effective change in magnetic coupling is distributed over a much longer movement from totally open to completely centered in the yoke. Similarly in the rotating magnet design, the adjustment range is from 0 to 90 degrees. The sliding or rotating magnet designs are therefore offer a much less sensitive adjustment that does not require the same great degree of precision adjustment tolerance. The rotating magnet design has the added advantage of occupying less physical space, thereby advantageously allowing for a more compact trigger mechanism construction for placement in the firearm.
The open loop and closed loop sliding wedge designs both have similar torque-displacement curve shapes (i.e. high initial trigger pull holding torque requirement which diminishes over the remainder of the trigger displacement when firing the firearm). The open-loop design though has much lower holding torque due to the magnetic losses in the air which is less desirable, but nonetheless still offers an acceptable magnetic trigger mechanism design.
The analysis confirms that all the closed magnetic loop embodiments documented herein meet the magnetically adjustable trigger design goals of a wide range of adjustable trigger pull force, an adjustment means that is relatively linear, and an adjustment means that is relatively insensitive to normal mechanical tolerances. The magnetic field open loop design mentioned above provides an acceptable means for achieving a viable adjustable trigger. While not optimal in performance, the open loop design is compact and mechanically simple to construct and implement offering certain advantages.
A major feature of one non-limiting preferred closed magnetic loop design of a sliding magnet shown in
Mechanically detailed preferred embodiments of closed and open magnetic loop trigger mechanism designs will now be described in further detail below, respectively.
Closed Loop Sliding Magnetic Trigger Mechanism
The sliding magnet trigger mechanism 1200 includes a front 1230, rear 1231, opposing right and left lateral sides 1232 (side designations when the trigger unit is mounted in a firearm), top 1233, and bottom 1234. Trigger mechanism 1200 generally comprises stationary yoke 102, rotatable trigger member 104, sear 375, and a movable sliding magnet control insert 1031 (a basic version of which is shown in
Yoke 102 includes horizontal upper portion 110, horizontal lower portion 111 oriented parallel to the upper portion, and vertical intermediate portion 114 extending therebetween. Control air gap B is formed in intermediate portion 114 and extends completely through the portion. The lower portion 111 may be bifurcated as shown forming a pair of laterally spaced apart arms defining a vertical through opening 1214 therebetween in which the trigger member 104 is pivotably mounted thereto by transverse trigger pivot pin 1205. Yoke 102 is fixedly mounted to the firearm frame 22, receiver 39, or a trigger housing 1220 as shown in the illustrated embodiment so as to remain stationary when the trigger is pulled.
In the embodiment shown in
Rotating trigger member 104 includes upper working portion 120 and lower trigger portion 118. Trigger member 104 has a vertically elongated body. Working portion 120 may be linearly straight and have rectilinear transverse cross section (e.g. square or rectangular) in one non-limiting configuration as shown. Lower trigger portion 118 may have an arcuately curved profile by contrast.
Trigger assembly 1202 defined in part by lower trigger portion 118 of trigger member 104 may include an outer trigger 1201 and inner safety trigger 1203 movable relative to the outer trigger. Outer trigger 1201 is pivotably mounted to yoke 102 via first transverse pivot pin 1205 which defines a first pivot axis. Inner safety trigger 1203 includes an enlarged upper mounting portion 1203-1 pivotably mounted to outer trigger 1201 via a second transverse pivot pin 1206 which defines a second pivot axis parallel to the first pivot axis. The safety trigger further includes a lower blade portion 1203-2 depending downwards therefrom for actuation by a shooter or user. The blade portion 1203-2 may have a solid or an open framework construction as shown including an arcuately concave front surface configured to facilitate engagement by the shooter or user's finger. Safety trigger 1203 is pivotable independently of both the outer trigger 1201 between forward and rearward positions. A spring 1204 biases the safety trigger 1203 towards the forward position projecting forward from the vertical slot 1201-1 formed in outer trigger 1201 in which the inner safety trigger 1203 nests. The second pivot axis defined by pivot pin 1206 may be positioned below and behind the first pivot axis defined by pivot pin 1205. A vertical central axis CA and horizontal central axis HA of the trigger mechanism 1200 are defined for convenience of reference which pass through pivot pin 1205 and perpendicularly intersect each other (see, e.g.
A transversely oriented split trigger safety blocking pin 1207 is fixedly coupled to the trigger housing 1220 and arranged to selectively engage or disengage a cam surface 1203-3 on top of the upper mounting portion 1203-1 of the safety trigger 1203. Safety blocking pin 1207 may have a cylindrical configuration in one embodiment; however, other shapes may be used.
The trigger member 104 may have a one-piece unitary construction such that the lower trigger portion 118 which defines the main outer trigger 1201 of the trigger member is a unitary structural part of the upper working portion 120 which engages the sear 375. Rotating the trigger 1201 about pivot pin 1205 therefore concomitantly rotates the upper working portion 120 in the same direction in unison to open air gap A and release the sear 375 to discharge the firearm. In other embodiment, the lower and upper portions 118, 120 may be separate components which are rigidly coupled together to provide the same action.
An adjustable trigger member travel stop comprises a mounting block 1213 having an internally threaded bore which rotatably receives adjustment screw 1212 therethrough. Block 1213 may be fixedly mounted to the trigger housing 1220 and spaced forward from upper working portion 120 of rotatable trigger member 104 when in the upright un-pulled condition. The shaft end of adjustment screw 1212 opposite its enlarged head used to rotate the screw is variably positionable to selectively engage and bear against the upper working portion 120 of trigger member 104 when rotated forward via a trigger pull. This manually adjustable physical stop limits the travel of the rotating trigger body after release of the sear to ensure the trigger mechanism can properly reset to ready-to-fire condition. One advantageous feature of the magnetic design is that the need for the trigger return spring may be eliminated since the magnet 108 will always be drawn into the control air gap B magnetically, as previously noted. The adjustable stop may alternatively be replaced with a fixed stop in some embodiments that is not adjustable using the mounting block alone or a pin fixedly attached to the trigger housing, frame, or receiver. Based on performance and tolerances, it may be desirable to add a small trigger return spring to account for tolerances of a fixed stop. A trigger return spring may, or may not, be necessary, but if needed would still be smaller and less critical than conventional trigger return spring designs and less noticeable to the operator during trigger recovery.
The sliding magnet control insert 1031 in this embodiment shown in
A vertically and forwardly open cavity 1036 is formed by the sidewalls 1035 and front wall 1034 of carrier 1030. Permanent magnet 108 is mounted in cavity 1036. To assist in retaining the magnet 108 in the cavity 1036, a cross bar 1033 may be molded into the carrier which extends horizontally between the sidewalls 1035 at the front of the carrier body. Cross bar 1033 is insertable into control air gap B, but has no effect on the static magnetic field since the carrier is formed of a non-magnetic material.
Carrier 1030 is slideably mounted between the right and left side plates 1220-1 of trigger housing 1220 in a rearwardly open channel 1210 formed in each side plate.
Adjustment screw 1211 is fixed in horizontal position in the trigger housing 1220 but rotatable. This can be accomplished by providing a plain unthreaded hole in a rear plate 1220-2 of the trigger housing (shown schematically in dashed lined in
The control insert 1031 can be slideably adjusted along the horizontal central axis HA to move the magnet 108 in carrier 1030 into and out of the control air gap B in the closed-loop magnetic trigger circuit. Rotating screw 1211 in a first direction translates the carrier 1030 forward for increasing the insertion of the permanent magnet 108 in control air gap B of yoke 102 in order to increase the magnet static holding force or torque. Rotating screw 1211 in an opposite second direction withdraws the carrier 1030 rearward for decreasing the insertion of the permanent magnet 108 in control air gap B of yoke 102 to decrease the magnet static holding force or torque. This provides a user selectable adjustment of the trigger pull force or holding torque to suit personal preferences.
It bears noting that other suitable shapes of non-magnetic carriers may be used so long as the permanent magnet 108 may be linearly translated into or out of the control air gap B of yoke 102. Although the magnet 108 is insertable into control air gap B from the rear 1231 of the trigger mechanism 1200, in other possible embodiment the trigger mechanism may be designed to insert the magnet from either two of the lateral sides 1232 into air gap B with equal results. This may be more convenient in some firearm designs and allows the adjustment screw 1211 to be accessible through the trigger housing 1220 from either the right or left sides of the firearm for the user.
It bears noting that the magnet 108 in the control insert 1031 will always try to pull itself into full engagement centered in the control air gap B via the magnetic attraction forces created in the closed loop, which acts like a magnetic biasing spring against the adjustment means. By turning the threaded adjustment screw 1211, the magnet 108 can slide outward from the control air gap B, or allowed to be drawn inward into the air gap. By moving the magnet into and out off the control air gap B, the magnetic flux density in the air gap will approximately vary as a linear function. This is due to the magnetic field strength times the area being preserved across the boundaries. By changing the engagement position of the magnet 108 with yoke 102, the magnetic static holding force at the air gap B between the yoke 102 and the trigger member 104 can be selectively varied by the user.
Sear 375 has already been fully described herein and will not be discussed again in depth for sake of brevity. In general, sear 375 is mounted to trigger housing 1220 via transverse cross pin 377 that defines the pivot axis 376 of the sear. Sear protrusion 44 may be formed on one forward end of sear 375 opposite a rear end having a transverse opening which receives a cross pin 377 that defines pivot axis 376. A rear facing vertical surface on sear protrusion 44 engages a mating front facing surface of catch protrusion 42 on striker 40 to hold the striker in the rearward cocked position (see, e.g.
In operation, with additional reference to
It bear noting that the sear pin 377, rotatable trigger member pin 1205, safety trigger pin 1206, and the safety blocking pin 1207 are mounted in complementary configured mounting holes formed in the inner surfaces of the trigger housing 1220 right side plate 1220-1 and left side plate (not shown).
A method for adjusting the closed loop magnetic trigger mechanism 1200 described above will now be briefly summarized. The method comprises providing stationary yoke 102 configured for mounting in the firearm, a rotating trigger member 104 pivotably movable about a pivot axis relative to the stationary yoke, the trigger member and stationary yoke collectively configured to form a closed magnetic loop, and an openable and closeable first air gap A being formed between the trigger member and the stationary yoke. The method further includes providing a control insert 1031 comprising a non-magnetic carrier 1030 and a permanent magnet 108 operable to generate a static magnetic field in the closed magnetic loop, the static magnetic field creating a primary resistance force opposing movement of the trigger member 104 when pulled by the user. The method includes: rotating an actuator such as screw 1211 operably coupled to the control insert in a first direction to advance the permanent magnet 108 into a second control air gap B formed in the stationary yoke 102, the magnet creating a first static magnetic field strength in the closed magnetic loop; and rotating the actuator in an opposite second direction to withdraw the magnet from the second control air gap, the magnet creating a second static magnetic field strength in the closed magnetic loop less than the first magnetic field strength. The strength of the static magnetic field is changeable via varying position of the permanent magnet in the control insert relative to the second control air gap to adjust a trigger pull force of trigger mechanism.
Open Loop Magnetic Trigger Mechanism
With continuing reference to
Magnet holder mounting block 1304 includes an elongated internally threaded bore 1305 which opens forward and rearward. Bore 1305 extends horizontally parallel to horizontal central axis HA. The magnet holder 1302 may comprise an elongated threaded rod which threadably engages the bore 1305. Holder 1302 includes a first inboard end including a forwardly open receptacle 1310 and a second outboard end which may include a tooling recess 1311 configured for engaging a tool used to turn the holder. Tooling recess 1311 may have any suitable tooling configuration, such as for example without limitation a hex shape for engaging an Allen wrench as shown, or a Philips, slotted, torx, star, square, or other shaped tooling recess for engaging a complementary configured screwdriver.
Permanent magnet 108 is insertably mounted in receptacle 1310. Magnet 108 may be retained in the receptacle by any suitable means, such as adhesives, fasteners, threaded caps, or other techniques. In the illustrated embodiment, magnet 108 may be cylindrical in shape and receptacle 1310 has a complementary configuration. Preferably, the front free end of the magnet 108 protrudes outwards beyond the holder 1302 and receptacle 1310 to directly engage the rear face of the upper working portion 120 of trigger member 104 as shown.
Magnet holder 1302 may be made of any suitable magnetic material or non-magnetic material. In one embodiment, the holder preferably may be made of a non-magnetic, non-ferrous metal such as brass. Non-magnetic material are essentially transparent to the magnet as long as it does not magnetically interfere into control air gap B to limit the range of motion of the magnet into the gap. Magnetic holder materials are less preferred, but may be acceptable as long as the geometry does not allow a magnetic path that would shunt magnetic flux away from the air gap B. In other possible embodiments, holder 1302 may be made of a suitably strong polymeric material.
Rotating magnet holder 1302 alternatingly in opposing directions advances the holder and magnet 108 towards the working portion 120, or retracts the holder and magnet from the working portion of the trigger member. By adjusting the displacement of the magnet 108 with respect to the main rotating upper working portion 120 of the trigger member body, the static magnetic holding force of the magnet can be adjusted by increasing or decreasing the control air gap B between the magnet and the rotating trigger body.
As the trigger assembly 1202 of the open magnetic loop trigger mechanism 1300 is initially pulled and displaced by the user to the right, the top trigger safety cam surface 1203-3 of the rotating inner safety trigger 1203 engages and the moves past the safety blocking pin 1207, thereby providing the initial take-up travel of the trigger. As the user continues to pull the full trigger assembly 1202 (outer trigger 1201 and safety trigger 1203), the final release force to rotate the trigger member 104 body and release the firing sear 375 is dependent on the magnetic flux density created between the magnet 108 and the rotating upper working portion 120 of the trigger body. The flux density is dependent on the magnetic properties of the permanent magnet, the physical geometry of the magnet, and the displacement between the magnet and the rotating trigger body. In general, the trigger release magnetic static holding force is adjusted by changing the displacement and position of the magnet 108 relative to the rotating trigger body at control air gap B, which in turn changes the magnetic flux contribution to the trigger release holding force.
When the trigger is reset after releasing the sear 375, the movement of the safety trigger 1203 cams down as it resets past the safety blocking pin 1207 and applies a leveraged pressure on the rotating trigger body upper mounting portion 120 to help position the trigger body closer to the magnet. This camming action assists in driving the rotating trigger body back into the reset position where the magnetic forces are re-established and accelerates the re-establishment of the magnetic pull strength necessary to reset the sear 375. The combination of the trigger safety camming force and the magnetic pull forces of the magnet will advantageously allow for the potential removal of the traditional trigger return spring. The elimination of the trigger return spring allows a much crisper trigger reaction when the sear releases and more range of possible trigger pull adjustment, which is considered a significant advantage of both this open magnetic loop design and the closed magnetic loop designs.
It bears mention that the foregoing camming force of the split trigger safety and the leveraging of the magnetic attraction force at control air gap B to reset the rotating trigger arm 104 and potentially eliminate the need for a trigger return spring is a significant advantage of both the open and closed loop magnetic designs.
In other possible embodiments, the closed or open loop trigger mechanisms 1200 or 1300 may instead be mounted in a handgun such as firearm 20 shown in
It bear noting that the sear pin 377, rotatable trigger member pin 1205, safety trigger pin 1206, and the safety blocking pin 1207 are mounted in complementary configured mounting holes formed in the inner surfaces of the trigger housing 1220 right side plate 1220-1 and left side plate (not shown).
A method for adjusting the open loop magnetic trigger mechanism 1300 described above will now be briefly summarized. The method comprises providing a rotating trigger member 104 pivotably movable about a pivot axis relative to a frame 22, receiver 39, or trigger housing 1220 of a firearm 20 or 20-1, and a threaded magnet holder 1302 holding a permanent magnet 108 in proximity to the trigger member. The permanent magnet 108 is operable to generate a static magnetic field attracting the trigger member to the magnet 108, the static magnetic field creating a primary resistance force opposing movement of the trigger member 104 when pulled by the user. The method includes: rotating the magnet holder 1302 in a first direction to advance the permanent magnet 108 towards the trigger member at a control air gap B formed between the magnet and trigger member, the magnet creating a first static magnetic field strength; and rotating the magnet holder in an opposite second direction to withdraw the magnet from trigger member, the magnet now creating a second static magnetic field strength less than the first magnetic field strength. The strength of the static magnetic field is changeable via varying position of the permanent magnet relative to the trigger member at the control air gap to adjust a trigger pull force of trigger mechanism.
The trigger mechanisms disclosed herein are all generally amenable for use in any type of small arms or light weapons using a trigger mechanism, including for example handguns (pistols and revolvers), rifles, carbines, shotguns, grenade launchers, etc.
Firing Event Tracking and Associated Event Characterization
According to another aspect of the present disclosure, the microcontroller-operated firing system with electromagnetic actuator-based trigger mechanism may be configured to provide a tracking system comprising a firing event/shot counter, and in some embodiments execute an associated post-event processing routine to characterize the type of firing event detected. One attribute of the present electromagnetic trigger system unique to microprocessor controlled firing actuation is the unique ability to electronically sense the precise moment in time that the electromagnetic actuator trigger mechanism of the firearm is directed to trip and discharge the firearm based on receiving the electric pulse or signal from the microcontroller, as previously described herein. This unique electronic trigger actuation information presents an extremely accurate timing of shots fired and can be used as a metric for firing event/shot counter that is integrated within the variable force trigger enabled firearm. This type information is especially of interest to shooters who engage in competitive shooting events. This precise timing information allows the microcontroller to track and store a running total of the cumulative number of shots fired and record an associated time/date stamp, thereby allowing the shooter to practice and improve the cadence of firing (time interval between shots). Another use of this precise firing information is the ability to use the running total of shots as an odometer to determine when maintenance of the firearm is required for parts replacements (e.g. changing barrels, etc.), routine cleaning, lubrication, or other needs.
The industry has developed versions of shot counter accessories that are standalone, attached onto the firearm, or installed within the firearm. There are multiple drawbacks with these commercial devices however which hinder their accuracy. All of these devices do not directly observe the trigger force/displacement event by the user to discharge the firearm. Instead, these shot counters generally rely on various types of sensors mounted in the firearm as the sole means for detecting a trigger pull on a “second hand” basis after the fact of an actual firing event, not simultaneously or concurrently with the occurrence of the event. These commercial shot counters typically observe the resulting effects created by the firing event (e.g. blast noise, vibrations, etc.) and must interpret those effects to determine if a shot was in fact actually fired. This presents significant difficulties in differentiating between firing events and other events that may not be related to actual firings (e.g. dropping, bumping, or manually manipulating the action of the firearm). Events such as dropping the firearm on a table, charging the firearm by chambering ammunition, extracting ammunition from the chamber, or loading or extracting an ammunition magazine could be confused with a firing event by these shot counters. Additionally, firearms that are discharged nearby such as at a shooting range during a shooting competition or the presence of other background noises may adversely affect the accuracy of sensor data, thereby making it more difficult to accurately predict if the event is a firing event associated with the specific firearm of interest.
The variable force electromagnetic trigger mechanism with microcontroller disclosed herein has the unique ability to precisely know electronically when the operator has intentionally pulled the trigger of the firearm without the deficiencies inherent with conventional shot sensing means and counters. This precise firing information provided by the present electromagnetic actuator trigger mechanism advantageously is unaffected by background and ambient noise, such as at shooting ranges or in other loud environments, thereby eliminating the need to differentiate which firearm has been fired and when with precision. This advantage is attributable to a shot firing event tracking system which is entirely based on the direct firing signal transmitted by the microprocessor to the electromagnetic actuator in the form of an electric pulse which activates the actuator and fires the firearm. This provides a unique advantage over existing shot counting accessories that rely on indirect and “second hand” detection of the firing event via the blast generated by firing the firearms, and which cannot reliably differentiate between blasts generated by other shooters in close proximity in some situations such as at a shooting range. In some embodiments, the microcontroller according to the present disclosure may be further configured to automatically discriminate between and classify a firing event as a “live fire” event resulting in discharge of the firearm, or a “non-fire” event which does not result in discharge (e.g. dry fire/trigger pull event or an attempted discharge event).
Referring initially now to
In some embodiments, the microcontroller also simultaneously records/stores a time/date stamp associated with the firing event. Each time an electric control pulse is subsequently transmitted to the actuator, the microcontroller records another firing event, and so on. The microcontroller stores each of the firing events and associated time/date stamp in memory, and further maintains a running cumulative total of the number of firing events occurring. This could be a real-time date/time stamp provided by a real-time clock accessible to the microcontroller 200 in its associated circuitry. An alternate embodiment could utilize a pseudo time stamp that simply provides only a relative time stamp between firing events. This pseudo time stamp has the advantage of providing privacy to the user, and also eliminates the need to utilize a real-time clock which can result in on-firearm power savings.
In addition to recording a running total of cumulative number of rounds fired for maintenance purposes, the rate of fire which may be the timing between rounds fired or total rounds fired over a selected interval of time (may be derived by microcontroller 200 processing the foregoing recorded firing event data and its associated time/date stamps. This provides the cadence of firing or timing between firing events (shots). Timing interval scoring is used in some competitive shooting matches as a metric.
It bears noting that the trigger/firing events (e.g. number and associated time/date stamps) are recorded by the microcontroller 200 in the present embodiment based solely direct detection of the transmission of the electric control pulse or signal to the trigger mechanism actuator without reliance on any input from other secondary sensors as in know shot counters which rely the after-effects of firing (e.g. sound, vibration, motion, etc.) as an indication of a firing event. By contrast, such secondary sensor data however may be drilled down and used in the present firing event tracking process 520 as an adjunct to the direct firing event data to further characterize or classify the type of firing event which has just been detected and recorded by microcontroller 200 (e.g. live fire event or non-fire event).
The precision firing timing information recorded by the microcontroller 200 in the present firing event tracking process 520 (i.e. transmission of electric pulse to trigger mechanism actuator) may be used to help interpret the external firing-effect stimulus observed and detected by a firing event sensor 530 to differentiate between live fire events which result in discharge of the firearm, non-fire events which do not result in discharge. Since the microcontroller 200 knows precisely when the electric control signal is sent to the actuator to fire the ammunition, the microcontroller accordingly knows with precision when to poll or look for external confirmation that the actual firing event has occurred and can discriminate the beginning point of a characteristic signature of the event which should follow (e.g. acoustic, motion, etc.). Accordingly, microcontroller 200 knows exactly when the start of an acoustic, motion, or acceleration event created in reaction to tripping the trigger electronically can be expected and detected by the firing event sensor 530 due to electronic sensing of the firing event electric control pulse transmission. This greatly simplifies the complexity of parsing the detected signature or signal indicative of an after-effect observed in the firearm from an actual firing event which results in discharge of the firearm by the microcontroller 200. One of the most difficult and electrical power consuming aspects of known secondary external stimulus based shot counters previously described herein is the necessity for the microprocessor to be “always on” to continually search for and evaluate if a possible trigger actuation event has started, and then making sure it is interpreted correctly as a start of an actual discharge-related firing event and not another non-discharge event (e.g. firearm jarred/dropped, dry fire event (trigger pull), magazine inserted/ejected, etc.). This requires complex algorithms which inherently reduces reliability of known shot counters.
The foregoing processing complexity and algorithms used by convention shot counters is completely eliminated with the present firing event tracking process 520. Because the microcontroller 200 does not use the firing event sensor 530 according to the present disclosure as the primary means for detecting a trigger pull/firing event, the microcontroller need only initiate search for a signal from the firing event sensor as a secondary processing routine to characterize the event as a live fire event or non-fire event. Transmission of the electric control pulse to the trigger mechanism electromagnetic actuator provides the detection of the firing event. Accordingly, the microcontroller may include a predetermined and preprogrammed window or interval of time to actively search for confirmation of the firing event after the microcontroller senses the electric control pulse transmission to the trigger mechanism electromagnetic actuator. During this window of time, the microcontroller 200 looks for confirmation of the expected firing event characteristic/signature indicative of a live fire event detected by the firing event sensor 530. Because there is no need to guess if the detected firing event signature is the start of an actual event versus some other background or non-fire event noise, the computational analysis is greatly simplified and can result in the use of cheaper less precision sensors, lower power consumption, faster response times, and much more accurate interpretation of the data than known shot counters.
With reference to
If the answer is “Yes” in Step 526, control passes to Step 528. In Step 528, the microprocessor compares the detected real-time firing characteristic sensed by firing event sensor 530 to a preprogrammed firing characteristic/signature indicative of the live fire event (examples of which are shown in
As shown in
The firing event sensor 530 may be various types of commercially-available sensors which are capable of detecting a firing characteristic/signature indicative of a live fire event. A few non-limiting examples will now be further described.
In one embodiment, firing event sensor 530 may be a simple acoustic sensor with the range and bandwidth to differentiate the sound of a shot fired can be added to the electromagnetically variable force trigger mechanism. This can be an inexpensive piezoelectric sensor or microphone. Since the microcontroller 200 already knows the precise time when the operator pulled the trigger sufficiently to discharge the firearm and the electric control pulse was transmitted to energize the trigger mechanism actuator (
To illustrate the above point,
Note that the timing of the trigger pull and trigger mechanism actuator activation event to the subsequent acoustic firing event noise pickup is very short; in the order a microseconds. Accordingly, the preprogrammed observation window/interval of time may be less than 1 second, and preferably preset and measured in fractions of a second or microseconds in some embodiments based on the typical cycle rate time for the action of the particular firearm involved. The cycle rate for the action of a firearm is generally the time required to open the breech after firing the ammunition, extract and eject the spent cartridge case from the barrel assembly chamber via translating the bolt or slide rearward, strip a fresh cartridge from the magazine, and chamber the fresh cartridge while reclosing the breech for the next firing event. Accordingly, the preprogrammed observation window would ideally be no longer in duration than the typical action cycle rate of the particular firing system involved so that the firing event tracking system is rapidly reset and ready to track the next firing event. This ensures that each observation window, during which time the microcontroller 200 monitors and acquires a firing characteristic detected by the firing event sensor 530, does not overlap the subsequent firing event to maintain the integrity of the firing event count. As examples, a very fast shooter using a semi-automatic pistol could fire up to about 5 rounds per second. The fastest fully automatic mode machine gun can come close to 100 rounds per second. Thus the preprogrammed observation window must be preset to take into consideration the type of firearm involved and firing mode (semi-automatic or fully automatic). In one non-limiting embodiment, the observation time window may be equal to or less than approximately 1.5 times a total cycle time to cycle an action of the firearm for a semi-automatic or automatic firearm. In one non-limiting example, the preprogrammed duration of the observation window may be about 100 milliseconds maximum for a semi-automatic firearm. It bears noting that for bolt-action rifles in which the bolt is manually retracted to open the breech after each shot, the preprogrammed observation window duration would be limited to the firing event only and not include the manual racking of the bolt. Accordingly, the observation window duration would not include cycle time to retract the bolt and open breech, and closing the breech to chamber of the next round as this is a manual operation and not deterministic. For bolt-action rifles, the preprogrammed duration of the observation window of about 100 milliseconds maximum would generally also suffice for the firing event timing only for these manually operated firearms.
In another embodiment, firing event sensor 530 may be a motion type sensor. The use of commercially-available motion sensors with one, two, three or more degrees of freedom and MEMS micro-miniature single axis and multi-axis accelerometers may be used and provides the opportunity to capture a rich data signature of events during the shooting of a firearm. Motion sensors look for motion and/or acceleration of the firearm that occurs during the recoil shock of live-firing. There are a number of types of motion sensors that may be used with the present firing event tracking system 520 to discriminate between the typical slow motion changes in position or velocity of the firearm during normal handling and use, and the sudden high speed change in motion/acceleration from firing ammunition. Typically piezoelectric, piezoresistive, variable capacitance, or variable reluctance acceleration sensors (accelerometers) may be used to provide the type of high speed sensing for good motion/acceleration event discrimination in the present application. Alternatively numerous other types of motion sensors such as magnetometers, gyroscopes, inertia and position sensors may be used. Some simplistic very low cost motion sensors that simply register the movement of weighted mass or liquid can be used as the firing event sensor 530 to register the presence of the high speed motion of firing event as well. The prior knowledge of the precise timing of the firing event by the microcontroller 200 (i.e. electric control pulse transmission to trigger mechanism electromagnetic actuator) herein advantageously allows for the use of less precise in the type of sensor needed since the microcontroller is only interested in a gross measure that confirms the firing event has occurred during the observation window or interval of time as previously described. Accordingly, the term “motion sensor” for use as the firing event sensor 530 should be broadly construed to include any of the foregoing types of motions sensors and those similar.
It bears noting that the firing event tracking system may be used with any of the actuators disclosed herein, including embodiments of the fire-by-wire trigger mechanism having an electronic sear (E-sear) shown in
Advanced Fire Control System Interface
According to another aspect of the present disclosure, the present microcontroller-operated trigger system disclosed herein with user-adjustable electromagnetic actuator variable force trigger mechanism may be configured to cooperate and interface with an external optical-based advanced fire control targeting system also mounted onboard the firearm, such as without limitation embodiments of the Next Generation Squad Weapons Fire Control (NGSW-FC). This government initiative is intended to develop the next generation of military combat rifles which incorporates an electronic adaptive optical fire control system mountable on the rifle. The U.S. Military, through programs such as the NGSW-FC program and testing of the Israeli Smart Shooter SMASH 2000 fire control system for small arms, is evaluating the viability of integrating adaptive direct view optics with ballistic calculators, environmental/atmospheric sensors, and laser range finding devices into the next generation of firearms. The fire control system essentially assists the user with aiming the firearm and targeting for increased shot accuracy by employing a microprocessor and associated input sensors and devices. The optical-based fire control targeting system automatically compensates for user skill and a host of field variables and factors all of which affect point of aim in real-time based on the sensor data and information relayed to and processed by the on-board microcontroller.
One beneficial attribute of the present variable force electromagnetic actuator trigger system unique to microprocessor-controlled firing actuation previously described herein is the provision of an electronically interruptible trigger platform which can receive and process a shot authorization signal generated by an adaptive optics unit of the external advanced fire control targeting system which is mounted onboard the weapon. Accordingly, following a trigger pull event, the trigger unit microcontroller of the present electromagnetic trigger system in one programmed configuration may delay actual firing of the weapon until the shot authorization signal is received and detected, thereby indicating that the user has accurately acquired the target with the guidance of the advanced fire control targeting system. A critical component for integrating the intelligent adaptive optics package with a base firearm is the need for a reliable interruptible electro-mechanical trigger mechanism as disclosed herein which provides the electrical input/output control capable of operable cooperation and integration with the optics package, while doubly providing a simplistic backup manual override to default to a standard mechanical trigger means in the event of an electronics or power supply failure. Numerous operational scenarios may be preprogrammed into the interruptible electromagnetic actuator trigger mechanism disclosed herein. Embodiments of the present electromagnetic trigger mechanism disclosed herein advantageously allow the firearm to still be fired manually in exigent circumstances until such time that the electronics operating problems can be rectified.
It bears noting that the term “external” as used herein in reference to the advanced fire control targeting system merely connotes that the targeting system is separate from and hence external to the electromagnetic actuator trigger mechanism and system in that sense. Both the trigger and targeting systems may therefore still be mounted to and onboard the firearm. In other possible embodiments, it is possible that the advanced fire control targeting system may be another type of targeting system which is physically removed from the firearm and may communicate with the trigger system via any suitable wireless communication protocols.
The electronic adaptive optics unit 701 comprises a control module 711 which includes control circuitry comprising programmable targeting microcontroller 712. Microcontroller 712 is operably coupled to the trigger unit microcontroller 200 of the electromagnetic trigger mechanism and configured for establishing two-way communications between the microcontrollers.
Control module 711 (e.g. microcontroller 712) is operably coupled via wired and/or wireless two-way communication links to a targeting reticle display 702, range-finding sub-module 703, ballistics computation sub-module 704, environmental sensing sub-module 705, and point of aim sensing sub-module 706. The foregoing sub-modules may each include dedicated circuitry including microprocessors, memory, application-specific integrated circuits (ASIC) chips, or other electronic or semiconductor devices configured via programming and design for performing the desired function of each sub-module. The reticle display 702 may be controlled by the control module targeting microcontroller 711. Each of the sub-modules may be operably/communicably interlinked together to each other as shown and to the main adaptive optics unit control module 711.
It bears noting that the term “sub-module” does not necessarily refer to discrete physical modules with individual housings separate from the optics unit control module 711, but rather is intended to connote a grouping of electronic components (i.e. dedicated circuitry and devices as described above) organized by function which may be different parts of the main control module. Accordingly, the adaptive optics unit control module 711 may be configured and operable to perform all of the functions of the sub-modules which are further delineated below.
Range-finding sub-module 703 comprises circuity configured to at least find the distance from the firearm to the target. Sub-module 703 therefore includes electronic devices including sensors 707 necessary to perform the intended function such as without limitation sensors including laser range finders and other devices, etc. For active range finding, methods which may be used include laser, LIDAR, radar, sonar and ultrasonic range finding. Basically, any method may be used employing the time it takes for light, radio waves, sound and ultrasonic sound waves to travel to and return from the target to measure distance to target; all with similar sensor data results.
Environmental sensing sub-module 705 comprises circuity configured to adjust the point of aim based on factors that an expert marksman (e.g. sniper) would normally obtain and take into consideration. Sub-module 704 therefore includes electronic devices including sensors 709 necessary to perform the intended function such as without limitation sensors configured for sensing and obtaining various data and information relevant to the ambient atmospheric environment around the firearm and user which may affect point of aim. Such sensors may include for example without limitation ambient temperature, humidity, air density, wind direction and speed, altitude/elevation above sea level, etc.
Point of aim sensing sub-module 706 comprises circuity configured to collect multi-axis positional and motion/acceleration data on the aiming of the firearm and adjust the point of aim via reticle display system 702 based on the three-dimensional (3D)/three-axis angular position of the firearm barrel in space as held by the user when aiming at the target (e.g. barrel 23-1 of firearm 20-1 in
Examples of barrel positional and motion sensors which could be used include without limitation several MEM-based high precision fast acting accelerometers, such as the ADL001 from Analog Devices iMEMs® high-performance, high-bandwidth accelerometer line, that can give detailed acceleration and velocity data during the trigger pull event. Additionally, 3D orientation information can be acquired using off-the-shelf solutions such as a three axis orientation sensor from BOSCH (Model BMX055 or similar) that combines a MEMS (Micro-Electro-Mechanical Systems) accelerometer, magnetometer, and gyroscope on a single die with high speed ARM micro-controller and software algorithms to provide accurate real-time orientation information. By analyzing the motion and acceleration of the firearm barrel collected by the positional/motions sensors of sub-module 704 during the trigger pull event, the aimpoint of the firearm can be acquired as the user applies pressure and squeezes the trigger. This firearm barrel positional information can then be used by the trigger unit microcontroller 200 to control the timing of the actual firing event.
Ballistics computation sub-module 704 comprises circuity configured to adjust the point of aim (or aimpoint) based on factors that an expert marksman (e.g. sniper) would normally obtain and take into consideration to improve shot accuracy. Sub-module 704 therefore includes circuitry comprising associated related electronic devices 708 configured to automatically calculate point of aim adjustments necessary to accurately sight the target through the adaptive optics unit based on receiving data obtained by the sensors associated with range-finding sub-module 703, environmental sensing sub-module 705, and point of aim sensing sub-module 706. The ballistics computation sub-module 704 may also integrate characteristics of the ammunition being used (e.g. powder charge/load, projectile/bullet weight and length, etc.) to adjust the point of aim. Other sensor data used by the ballistics computation sub-module may include muzzle velocity, ballistic coefficient, and other ammunition and rifle specific inputs.
The electronic adaptive optics unit 701 comprises an optical sight including an integrated reticle display system 702. The reticle display system may be an electronic system configured and operable to generate a digitally displayed reticle 714 of certain shape (e.g. red, green, or other color dot, cross-hairs, etc.). The adaptive optics unit 701 may be in the form of a scope or sight having a housing configured for mounting on the firearm frame, receiver, barrel, or accessory mounting rail/system in a top position normally used for mounting firearm sights via any suitable mounting interface commonly used in the art. Adaptive optics unit 701 may comprise at least one transparent sighting lens 713 usable by the user as a direct view optic for visually sighting a target downfield therethrough. The digitally displayed reticle 714 is projected and overlaid onto the sighting lens 713.
To improve the speed of acquiring the target and shot accuracy, the programmable targeting microcontroller 712 of the adaptive optics unit control module 711 may be configured and operable to control and adjust the position of the digitally displayed reticle 714 on sighting lens 713 based on the sensor and other data obtained and/or calculated by the sub-modules 703-706 described above. Control module 711 (e.g. targeting microcontroller 712) is configured via programming to display a corrected reticle 714 at a position which compensates for all of the variables and parameter obtained by the sub-modules. The displayed reticle is therefore actually an electronically corrected digital reticle which accurately aligns the point of aim on the intended target.
It bears noting that all of the foregoing features of the advanced optics-based fire control targeting system 700 may all be integrated with and onboard the housing of the adaptive optics unit 701, which is configured for mounting directly on the firearm such as for example firearm 20-1 shown in
Interruptible Electromagnetic Trigger Mechanism Operation
Targeting microcontroller 712 of adaptive optics unit 701 may be configured and operable to generate and then transmit a “fire” (shot authorization) signal to the trigger unit microcontroller 200 of the variable force electromagnetic actuator trigger mechanism. The trigger unit microcontroller 200 may be programmed to time electrically discharging the firearm subsequent to a trigger pull event based on the receipt and detection of the valid shot authorization signal from the advanced fire control targeting system 700, thereby configuring the trigger mechanism to interrupt the normal firing sequence pending the shot authorization signal. Firing of the firearm is there contingent upon satisfying trigger setpoint operating parameters preprogrammed into the trigger unit microcontroller 200 and detection of the shot authorization signal from the targeting microcontroller 712.
Numerous electronic control scenarios via programming trigger unit microcontroller 200 with appropriate control logic to operate the electromagnetic actuator trigger mechanism in an interruptible mode in conjunction with the advanced fire control targeting system 700 to discharge the firearm are possible. Several non-limiting examples of control scenarios are described below. It will be appreciated that numerous variations of the following control scenarios are possible which fall substantially within the scope of the present disclosure.
In the interruptible trigger control scenarios presented below, any of the trigger mechanisms with bistable or non-bistable design electromagnetic actuators previously described herein may be used. As one non-limiting example, electromagnetic actuator trigger mechanism 300 of the electronic trigger system shown in
As previously described, trigger mechanism 300 includes electromagnetic snap actuator 350 configured to form the dual closed magnetic flux loop or paths. To briefly reiterate for convenience of reference, actuator 350 may be a non-bistable release type electromagnetic actuator in which the actuator is not energized to change position for either initiating movement or to reset the actuator similar to trigger mechanism snap actuator 123 previously described herein. Instead, similarly to actuator 123, microcontroller 200 may be programmed and configured to energize the present actuator 350 of the dual flux loop design via electromagnetic coil 306 in response to a manual trigger pull. This generates the secondary dynamic or active magnetic field which interacts with the primary fixed or static magnetic field generated by the permanent magnet 308 in either an additive or subtractive operating mode depending on the polarity of the power source 122 established via the microcontroller. The present electromagnetic actuator 350 is configurable by the user or shooter via programming the trigger unit microcontroller 200 to change the trigger pull force and displacement profile in the same manner described above for single flux loop electromagnetic actuator 123. The preprogrammed trigger setpoint(s) in the interruptible trigger mechanism control scenarios below may be based on sensed trigger pull force applied by the user or measured trigger displacement via the sensors previously described herein. Trigger pull force and displacement may be characterized as trigger activity in a broad sense for brevity and includes either pull force or displacement.
As a general high-level overview of the single stage interruptible electronic trigger system control process, the trigger unit microcontroller 200 initiates the firing or shot as the user commits to firing by increasing the pull force manually applied on the trigger (e.g. trigger member 320 in
Referring to
In step 736, the trigger unit microcontroller 200 transmits/sends a “shot initiation” signal to the external adaptive optics unit control module 711 of the advanced fire control targeting system (reference system architecture schematic diagram of
In Step 738, trigger unit microcontroller 200 performs a test to search for both receipt of the “fire” signal from the adaptive optics unit microcontroller 712 and continued sensed activity on the trigger 320 by the user above the preprogrammed setpoint from Step 735, which would be indicative of the user's continued intent to discharge the firearm. If both signals are present and detected by trigger unit microcontroller 200 (yes), control passes to Step 739 to initiate electrical actuation of the firing event. With additional reference to
If in Step 738 a negative (no) response is returned, control instead passes to Step 741. The negative response indicates that the “shot initiation” signal has been sent to the adaptive optics unit control module 711, but a “fire” signal has not yet been returned to the trigger unit microcontroller 200 upon searching for receipt of this signal. The test of Step 741 performed by trigger unit microcontroller 200 confirms whether or not the trigger is still being pulled to fire the firearm. If a negative (no) response is returned, control passes to Step 740 to reset the trigger mechanism for the next trigger pull event. If the result is positive (yes) indicating that the user is still pulling the trigger, control passes to Step 742.
In Step 742, a test is performed to compare and determine if the trigger activity (i.e. trigger pull force or displacement) applied by the user exceeds a preprogrammed maximum allowed trigger pull force/displacement limit. This limit is indicative of the user's intent to apply sufficient force on the trigger to manually override the trigger system electronics and fire control targeting system 700 and discharge the firearm. Such a situation may occur in exigent combat circumstances where immediate firing is necessary. If the test answer is negative (“no”), control passes to Step 743 to initiate a firing sequence timer of predetermined duration preprogrammed into trigger unit microcontroller 200. Any suitable duration of time may be used. In Step 743, the microcontroller 200 further performs a test to determine if the timer has expired. If not (i.e. “no” response), control passes back to Step 738 for the trigger unit microcontroller 200 to continue searching for a valid “fire” signal from the adaptive optics unit control module 711. A control loop is implemented by microcontroller 200 to repeat Steps 738, 741, 742, and 743 until the “fire” signal is detected by the trigger unit microcontroller.
If in Step 742 a positive response (“yes”) results indicating that the applied actual trigger pull force/displacement imparted by the user to the trigger exceeds the preprogrammed maximum allowable trigger pull force/displacement limit, control instead bypasses the decision block in Step 743 and timer to proceed to Step 744. In Step 744, the trigger system defaults to a non-powered manual “override” condition and enters manual firing mode operably detached from electrical firing assistance normally provided by the electromagnetic actuator trigger unit. The electromagnetic actuator trigger unit acts as a conventional manually fired trigger unit for mechanically firing the firearm. Accordingly, the trigger unit microcontroller 200 electrically deactivates the electronic firing system and power to the electromagnetic actuator trigger mechanism. The increased pressure applied to the trigger by the user in excess of the preprogrammed maximum allowable trigger pull force/displacement limit indicates that the user wishes to discharge the firearm despite the absence of a valid “fire” signal from the adaptive optics unit control module 711. This condition may possibly occur: (1) if there is a malfunction with the advanced fire control targeting system electronics (e.g. dead power source onboard battery 715 (see, e.g.
As an overview of the two stage control process 750 embodiment, the trigger pull event initiated by the user is broken into a “shot initiated” and “shot confirmed” trigger force setpoints. The “shot initiated” state of the electronic trigger system indicates that the user has initially selected an aimpoint (point of aim) for firing without yet fully committing to discharge the firearm. The “shot confirmed” state of the electronic trigger system indicates the user has adjusted the aimpoint based on corrections made by the external fire control targeting system 700 and is now fully committing to the firing the shot at an accurately acquired target. To be clear, the “shot confirmed” signal does not indicate that the firearm has been discharged and the shot taken yet. Both the “shot initiated” and “shot confirmed” signals are control signals each associated with a respective trigger pull setpoint (Setpoint 1 and Setpoint 2) preprogrammed into trigger unit microcontroller 200. Setpoint 1 may be associated with a partial trigger pull to activate the electromagnetic trigger mechanism for aiming in preparation for firing. Setpoint 2 may be associated with the trigger activity comprising a full trigger pull for discharging the firearm via fully actuating the electromagnetic actuator trigger mechanism in the manner previously described herein after the target has been accurately acquired. Both of the “shot initiated” and “shot confirmed” signals are sent/transmitted to the external advanced fire control targeting system 700 system. Between receipt of these two control signals, the external fire control targeting system could calculate new ballistic solutions and modify an adaptive optics unit sight, confirm authorization with another entity approving authorization to take the shot, or other intelligent adjustments or control criteria such as waiting for the operator to position and align the aimpoint more precisely on target via a corrected reticle displayed on the optics unit sight before authorizing the firing event via transmitting the “fire” signal to the trigger system as a response.
Referring now to
In step 753, the trigger unit microcontroller 200 transmits/sends a “shot initiation” signal to the external adaptive optics unit control module 711 of the advanced fire control targeting system (reference system architecture schematic diagram of
In Step 755, the trigger unit microcontroller 200 compares the actual sensed trigger pull force or displacement (dependent on what type trigger sensing design is used) to the associated preprogrammed trigger pull Setpoint 2. Setpoint 2 will be greater than Setpoint 1 (force or displacement) since Setpoint 2 is associated with a greater threshold parameter corresponding to the user's intent to fire the firearm rather than a partial trigger pull used for aiming the firearm only. If the actual sensed trigger pull force or displacement is less than Setpoint 2, control passes to Step 756 to check if there is still actual user-applied activity on the trigger (e.g. trigger force or displacement) that exceeds Setpoint 1. If not (indicating the user has backed off on or released the trigger), the shot is aborted and the system is reset for the next firing event (Step 764,
Returning to the decision block in Step 755, if the user-applied trigger activity (trigger pull force or displacement) exceeds Setpoint 2 (“yes” response to test), control passes to Step 758. The trigger unit microcontroller 200 sends a “Shot Confirmed” signal to adaptive optics unit control module 711 (microcontroller 714) indicating that the user has acquired the target with guidance from the optics unit to correct point of aim, and intends now to fire the firearm. Targeting microcontroller 712 generates and transmits a “fire” signal to trigger unit microcontroller 200 as the operator pulls the trigger smoothly and hovers aim around the intended target location when the corrected point of aim coincides with the ballistics calculation of correction indicating the user has locked onto the target.
In Step 759, the trigger unit microcontroller 200 checks for the receipt of both the “fire” signal from targeting microcontroller 712 and user trigger activity still exceeding setpoint 2 indicative of a positive intent to still discharge the firearm. If both signals are received and detected (“yes” response), the firearm is discharged (Step 760) and the electromagnetic actuator trigger unit is reset from the next firing event (Step 764).
Conversely, if both the “fire” signal and trigger activity exceeding setpoint 2 are not detected by trigger unit microcontroller 200 in Step 759, control passes to Step 761. The “fire” signal will have been generate by adaptive optics unit control module 711 and received by the trigger unit microcontroller 200; however, the user may have decided not to take the shot in the interim and backed off on the trigger. If trigger Setpoint 1 is not still exceeded by the user activity on the trigger indicating a released trigger (“no” response), the shot abort and the electromagnetic trigger mechanism is reset for the next firing event (Step 764). Conversely, if the use-applied trigger force or displacement exceeds Setpoint 1, control passes to Step 762.
In Step 762, a test is performed by trigger unit microcontroller 200 to determine if the trigger pull force/displacement applied to the trigger by the user exceeds the preprogrammed maximum allowable trigger activity limit (trigger pull force/displacement limit). If the test answer is negative, control passes to back to stop 759 and a control loop and timer are initiated via Step 763 for a preprogrammed duration of time. Any suitable duration of time may be used. If the timer expires in Step 763, control passes to Step 765 described above. The electronic trigger system ignores the trigger pull event and defaults to a non-powered manual fire state at maximum force/displacement to permit manual firing of the firearm until the user-applied force on the trigger is removed which resets the system.
If instead in Step 762 a positive response (yes) results indicating that the applied trigger pull force imparted by the user to the trigger exceeds the preprogrammed maximum allowable trigger pull force/displacement limit, control instead bypasses the decision block in Step 763 and timer, and proceeds to Step 765. The trigger system ignores initiation of the electronically-assisted trigger event and defaults now to the non-powered manual “override” condition previously described herein by entering the manual firing mode without electrical assistance of the electronic trigger unit. The increased pressure and displacement applied to the trigger by the user indicates that the user intends to discharge the firearm despite the absence of a valid “fire” signal from the adaptive optics unit control module 711. This condition may possibly occur: (1) if there is a malfunction with the advanced fire control targeting system electronics (e.g. dead power source onboard battery 715 (see, e.g.
In summary of the foregoing two stage interruptible trigger control logic process 750, it will be appreciated that if user-applied trigger force is removed (below preprogrammed trigger Setpoint 1), after passing through Setpoint 2, the firing attempt is aborted, the system reset, and a new firing attempt can be made. If the applied trigger force is lowered from trigger Setpoint 2 back to Setpoint 1 during the trigger pull event after a firing attempt is started, the electronic electromagnetic actuator trigger system will stay in a ready-to-fire state until (1) both the “fire” signal from adaptive optics unit control module 711 and the preprogrammed trigger Setpoint 2 force or displacement profile are detected and met for the firing solution; or (2) until a preset error timeout is reached. In the event of this timeout error, the electromagnetic trigger system ignores the trigger pull event and defaults to a non-powered manual fire state at maximum force/displacement until the force on the trigger is removed. This allows the firearm to be used as regular non-electronic firearm and discharged manually without electromagnetic assistance from the electronic trigger system or the advanced fire control targeting system input. This default manual override capability is a unique and significant advantage of the present electromagnetic actuator trigger system for user safety as the firearm may still be discharged in the event of an electronics failure in exigent circumstances.
Accordingly, if during the firing sequence the trigger pull exceeds the maximum allowed adjustable trigger pull force threshold, the electromagnetic trigger system will default to the manual override mode. If the operator choices to override the electronic/electric trigger system by increasing pressure on the trigger, before the enabling “fire” signal is received from adaptive optics unit control module 711, the trigger system defaults to a non-powered state at maximum Force/Displacement at the point that the user-applied trigger pull force exceeds the predefined preprogrammed maximum trigger pull force. The system will stay in this manual override mode until the force on the trigger is completely removed, at which time the trigger system will reset and return to electronic trigger mode.
The three stage interruptible trigger control logic process 800 is essentially the same as the two stage process 750 of
The three-stage trigger control logic process 800 embodiment adds a third level of trigger pull force associated with a preprogrammed third trigger activity (pull force/displacement) Setpoint 3 (Step 801,
If during the firing sequence the trigger pull force exceeds the previously described maximum allowed trigger activity (trigger pull force/displacement) limit preprogrammed into trigger unit microcontroller 200, the electronic trigger system will default to the manual override mode. If the operator chooses to override the system by increasing pressure on the trigger, before the enabling “fire” signal is received from the adaptive optics unit control module 711, the trigger system defaults to the non-powered state manual firing mode or state when the user-applied trigger force/displacement exceeds the predefined preprogrammed maximum allowable limit. The trigger system will stay in this manual override mode until the force on the trigger is completely removed at which time the system will reset and return to electronic trigger firing mode.
Accordingly, in Step 801 of the three stage trigger control logic process 800, a signal is received from the decision block of Step 759 (
It bears noting that in all of the foregoing firing control schemes of the interruptible electronic trigger system (e.g. single, two, or three stage), the trigger unit actuator is changeable between a non-powered ready-to-fire unactuated position and powered actuated firing position when the electromagnetic coil is energized, as previously described herein. User-activity sensed on the trigger unit by microcontroller 200 may awaken and activate the electronic trigger system from a sleep mode which conserves battery life. The activated trigger system is now readied to implement the foregoing firing schemes in operable cooperation with the advance fire control targeting system 700.
It further bears noting that certain steps of the foregoing control logic processes may occur rapidly within a fraction of a second, which is only made possible by bi-directional communications and cooperation between the trigger unit microcontroller 200 and targeting microcontroller 712 onboard the adaptive optics unit 701. Numerous variations of the foregoing interruptible electronic trigger system are possible within the scope of the invention. The electromagnetic actuator trigger unit retains it user-adjustable variable trigger pull force characteristics previously described herein in detail, which allows the user to customize and control at least some of the foregoing trigger Setpoints 1, 2, or 3 via programming the trigger unit microcontroller 200 to adjust the trigger.
In the two stage trigger control mode shown in
While the foregoing description and drawings represent exemplary (i.e. example) embodiments of the present disclosure, it will be understood that various additions, modifications and substitutions may be made therein without departing from the spirit and scope and range of equivalents of the accompanying claims. In particular, it will be clear to those skilled in the art that the present invention may be embodied in other forms, structures, arrangements, proportions, sizes, and with other elements, materials, and components, without departing from the spirit or essential characteristics thereof. In addition, numerous variations in the methods/processes described herein may be made within the scope of the present disclosure. One skilled in the art will further appreciate that the embodiments may be used with many modifications of structure, arrangement, proportions, sizes, materials, and components and otherwise, used in the practice of the disclosure, which are particularly adapted to specific environments and operative requirements without departing from the principles described herein. The presently disclosed embodiments are therefore to be considered in all respects as illustrative and not restrictive. The appended claims should be construed broadly, to include other variants and embodiments of the disclosure, which may be made by those skilled in the art without departing from the scope and range of equivalents.
The present application is a continuation-in-part of U.S. patent application Ser. No. 16/909,577 filed Jun. 23, 2020; which is a continuation-in-part of U.S. patent application Ser. No. 16/530,545 filed Aug. 2, 2019 (now U.S. Pat. No. 10,690,430), which is a continuation of U.S. patent application Ser. No. 16/283,338 filed Feb. 22, 2019 (now U.S. Pat. No. 10,458,736), which: (1) claims priority to U.S. Provisional Application No. 62/635,598 filed Feb. 27, 2018; and (2) is a continuation-in-part of U.S. patent application Ser. No. 15/908,883 filed Mar. 1, 2018 (now U.S. Pat. No. 10,228,208), which claims the benefit of priority to U.S. Provisional Application No. 62/468,632 filed Mar. 8, 2017. The foregoing applications/patents are incorporated herein by reference in their entireties.
| Number | Date | Country | |
|---|---|---|---|
| 62635598 | Feb 2018 | US | |
| 62468632 | Mar 2017 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 16283338 | Feb 2019 | US |
| Child | 16530545 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 16909577 | Jun 2020 | US |
| Child | 17158139 | US | |
| Parent | 16530545 | Aug 2019 | US |
| Child | 16909577 | US | |
| Parent | 15908883 | Mar 2018 | US |
| Child | 16283338 | US |
