Dynamic variable force trigger mechanism for firearms

BACKGROUND OF THE DISCLOSURE

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.

SUMMARY OF THE DISCLOSURE

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.

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.

BRIEF DESCRIPTION OF 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:

FIG. 1 is a graph depicting variation in trigger pull force versus displacement (distance) for two different trigger actions or mechanisms;

FIG. 2A is a side cross-sectional view of a control device comprising an electromagnetic magnetorheological fluid piston assembly for a trigger mechanism of a firearm;

FIGS. 2B-D show sequential views of the piston assembly thereof embodied in a variable force trigger mechanism during different stages in the process of pulling the trigger, wherein FIG. 2B shows a first position, FIG. 2C shows a second position, and FIG. 2D shows a third position of the piston assembly;

FIG. 3 is a side cross-sectional view thereof including an alternative embodiment of a user-adjustable magnetic control device for altering the trigger pull force comprised of a permanent magnet control linkage that provides the magnetic field in lieu of an electromagnetic shown in FIGS. 2A-D;

FIG. 4A is a perspective view of a housing incorporating the foregoing magnetorheological fluid piston assembly and a user-adjustable electromagnetic control device for altering the trigger pull force;

FIG. 4B is a partial cutaway view thereof showing the coiled electromagnetic device which includes a permanent magnet in greater detail;

FIG. 4C is an end view thereof showing a closed loop magnetic flux path or circuit formed by the electromagnetic device incorporated with the magnetorheological fluid piston assembly;

FIG. 5 is a perspective view showing the magnetorheological fluid piston assembly and electromagnetic control device incorporated in a firing mechanism or system of a firearm;

FIG. 6 is a perspective view of an electrically variable and adjustable electromagnetic trigger mechanism comprising an electromagnetic control device in the form of an electromagnetic actuator designed with a single magnetic flux loop;

FIG. 7 is a perspective view of a second embodiment thereof adding spring assist and control feedback from a trigger displacement sensor;

FIG. 8 is a control logic diagram of a process implemented by a programmable microprocessor-based microcontroller for controlling operation of the electromagnetic trigger mechanism;

FIG. 9 is a system block diagram of the programmable microcontroller based control system for monitoring and operating the electromagnetic trigger mechanism;

FIG. 10A is a diagram showing a wireless communication and control system interfacing with the microcontroller for use with the electromagnetic trigger mechanism which is programmable via an external/remote electronic device;

FIG. 10B is a graph of an example trigger pull force versus displacement (travel) curve showing various stages trigger force during a trigger pull sequence and an illustrating a breakpoint in the trigger release profile;

FIG. 11 is a diagram showing a variable force trigger wireless data collection and communication smart application;

FIG. 12 is a graph of trigger pull force versus displacement (travel or distance) of a non-linear force displacement curve for a segmented trigger design;

FIG. 13A is a perspective view of an electrically variable and adjustable electromagnetic trigger mechanism comprising an electromagnetic control device and including a non-linear leaf spring;

FIG. 13B is a side view thereof;

FIG. 14A is a perspective view thereof including a secondary spring flexing member joining an upper rotating member of the trigger mechanism with a lower trigger member;

FIG. 14B is a side view thereof;

FIG. 15 is a perspective view thereof with the upper rotating member of the electromagnetic trigger mechanism configured as a sear for interacting with a firing system component for discharging the firearm;

FIGS. 16 and 17 are front and rear top perspective views respectively of a second embodiment of an electromagnetic trigger mechanism comprising an electromagnetic actuator designed with a dual closed magnetic flux loop;

FIGS. 18 and 19 are front and rear bottom perspective views respectively thereof;

FIGS. 20 and 21 are exploded top and bottom perspective views respectively thereof;

FIGS. 22 and 23 are front and rear end views respectively thereof;

FIG. 24 is a right side view thereof;

FIGS. 25 and 26 are top and bottom views respectively thereof;

FIG. 27 is a first left side cross-sectional view thereof showing the electromagnetic actuator trigger mechanism in an unactuated ready-to-fire position or state;

FIG. 28 is a second left side cross-sectional view thereof showing the same;

FIG. 29 is a side view thereof showing the electromagnetic actuator trigger mechanism in an actuated fire position or state;

FIG. 30 is a right side view of a firearm in the form of a pistol incorporating the electromagnetic actuator trigger mechanism;

FIGS. 31 and 32 show magnetic flux paths in the electromagnetic actuator trigger mechanism in a de-energized state (FIG. 31) and energized state (FIG. 32);

FIG. 33 is a schematic diagram of a manually adjustable potentiometer which may be used to control operation of the electromagnetic actuator;

FIG. 34 is a control logic diagram of a fire-by-wire electric firing system for a firearm implemented by the microcontroller; and

FIG. 35 is a system block diagram of the programmable microcontroller based control system for monitoring and operating the fire-by-wire firing system.

All drawings are schematic and not necessarily to scale. Any reference herein to a whole figure number (e.g. FIG. 1) which may include several subpart figures All drawings are schematic and not necessarily to scale. Any reference herein to a whole figure number (e.g. FIG. 1) which may include several subpart figures (e.g. FIGS. 1A, 1B, 1C, etc.) shall be construed as a reference to all subpart figures unless explicitly noted otherwise.

DETAILED DESCRIPTION

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. FIG. 1 shows a comparison of a conventional military spec trigger pull force profile versus a modified version of an AR type rifle trigger exhibiting a lower pull force profile over the range from the initial trigger pull through release of the hammer or striker of the firearm.

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.

FIGS. 2A-D and 4-5 depict one embodiment of an electromagnetic MR fluid actuator 600 comprising an MR fluid-filled piston assembly 602 comprising a disk-shaped piston 612 movably disposed inside an MR fluid-filled cylinder 601. An electromagnet coil 614 is wound around a portion of the cylinder 601 and operably coupled to an electric power source 122 onboard the firearm and further described herein. The piston 612 is spring loaded so that the trigger linkage 610 would have a low return spring force sufficient to reliably return the trigger to it's original vertical ready-to-fire position with the MR fluid in it's free-flowing most liquid state (i.e. lowest viscosity condition). Approximately 1.0 lbs. might be a good baseline in one example for spring force imparted by piston spring 604. By increasing a magnetic field via the electromagnet coil 614 operably coupled to a power source 122, applied in such a way as to change the viscosity of the MR fluid, the force necessary to move the trigger bar could be adjusted upward to as much as 10-15 lbs. force in some embodiments. The trigger linkage 610 may comprise an elongated rod 611 pivotably coupled to a trigger member 608 rotatable about a transverse pivot axis 606 formed by a pin. Trigger member 608 may be mounted to a frame of a firearm.

In a basic implementation of a simple non-electromagnetic MR fluid actuator shown in FIG. 3, the magnetic field may be created by a spatially adjustable permanent magnet 615 mounted in close proximity to the piston cylinder 601 via an adjustable mechanical linkage 616. The linkage 616 may comprise a permanent magnet 615 slideably disposed inside a guide tube 616 and acted upon by a pair of springs 613a and 613b. One spring is disposed on each side of the permanent magnet. By adjusting the linkage up or down using a rotary adjustment device 618 such as set-screw or other manual device, the position of the permanent magnet 615 relative to the piston cylinder 601 can be adjusted. In one embodiment, the guide tube 616 may be disposed perpendicularly to the piston cylinder 601. Other arrangements are possible. This allows the relationship of the magnetic field in respect to the MR fluid filled spring-loaded piston to be changed for increasing or decreasing the viscosity of the MR fluid (i.e. viscosity increasing with decreasing proximity to cylinder). This simple non-electromagnetic adjustment means can be used by the user to increase or decrease the trigger pull force required to actuate the firing mechanism of the firearm (e.g. trigger linkage 610). This would allow for a user selectable fixed trigger force profile.

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 FIG. 1. This would allow a number of force profiles to be defined, selected, and implemented under electrical control. For example, one might want a very high trigger force when used in a self-defense, holstered, or concealed carry situation. Or one might choose a very light trigger force when target shooting, something in between when recreational shooting, or perhaps a different trigger force for the first round and lighter trigger profile for subsequent shots.

FIGS. 4A-C depicts an embodiment of a complete electromagnetic MR fluid actuator 600 assembly according to one embodiment. The actuator 600 may be mounted at least partially or fully inside a housing 619 which is configured for mounting to a frame of a firearm. Actuator 600 further comprises a stationary magnetic yoke 620 around which the electromagnet coil 614 (shown only schematically in FIGS. 2A-D) may be wound. Coil 614 is operably connected to the power source 122, which may be a battery. In this embodiment, a permanent magnet 615 is mounted to the yoke 620 to create a static or fixed magnetic field which may be biased to automatically maintain the trigger in the upright ready-to-fire position shown in FIG. 2B when the trigger is not pulled by the user. The yoke 602 is configured to form a single closed flux loop with lines of flux represented by flux arrows 622. When energized, the coil 614 creates a secondary electromagnetic field which interacts with the static magnetic field and dynamically changes the viscosity of the MR fluid and trigger pull force required to move the trigger 608.

FIG. 5 shows the complete electromagnetic MR fluid actuator 600 embodied in a firing mechanism of a firearm. The firing mechanism may comprise a movable spring-biased striking member 130 which may be a rotatable hammer as shown or alternatively a linear movable striker (not shown). The striking member 130 is arranged to strike the rear end of a firing pin 630 which in turn strikes a chambered ammunition cartridge C held in the barrel of the firearm. The striking member 130 is movable between a rearward cocked and forward firing position. A sear 632 is releasably engaged with the striking member 130 which is held in the cocked position by sear. The sear 632 is operably coupled to the trigger rod 611 at a rear end opposite the front end of the rod which is pivotably coupled to the trigger 608. Pulling the trigger which has a trigger pull force-displacement profile created by energizing the coil 614 moves the sear, which releases the striking member 130 to strike the firing pin and discharge the firearm. Variations of the firing mechanism are possible for use with the electromagnetic MR fluid actuator 600. The actuator 600 and its operation to energize and adjust the MR fluid viscosity and trigger pull force may be adjusted and control via a suitable programmed microcontroller 200; an example of which is discussed elsewhere herein. In some embodiments, the electromagnetic MR fluid actuator 600 may be configured to be additive during one portion or phase of the trigger pull, and changed to subtractive over another portion or phase of the pull based on the trigger displacement distance via properly configuring the control logic executed by the microcontroller which controls the electric power supplied to the electromagnet coil 614. For example, a higher initial trigger pull force may be desired for the initial portion or phase of the trigger pull and a lower pull force for the remaining portion or phase of the trigger pull as the trigger continues to move rearward. The timing of when each phase is initiated, its duration, and change in value or magnitude of the pull force required may be selected via appropriately programming and configuring the microcontroller 200.

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 FIG. 5).

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. FIGS. 6 and 7 depict non-limiting examples of an electrically-variable electromagnetic trigger release mechanism or simply “electromagnetic trigger mechanism” is presented. FIG. 6 depicts a one-piece rotating trigger member whereas FIG. 7 depicts a trigger member in which an upper portion is pivotably movable relative to the lower portion.

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 FIG. 15, then the actuator is directly releasing the hammer or striker. If the sear is a separate secondary component as shown in FIGS. 16-29, then the release actuator can release the sear which in turn releases the hammer or striker. In either case, energy applied to the actuator directly results in the firing of the weapon.

Referring now again to FIGS. 6 and 7, trigger mechanism 100 includes a magnetic stationary yoke 102, a rotating trigger member 104, and an electromagnet coil 106 disposed and wound around a portion of the stationary yoke. The yoke 102 may be fixedly and rigidly but removably attached to the frame 22 of the firearm 20 (see, e.g. FIG. 30) by any suitable manner, including for example without limitation entrapment in an open trigger unit receptacle of the frame, fasteners, couplers, pins, interlocking features, etc. The mode of attachment is not limiting of the invention. The trigger mechanism 100 may have a generally annular shape in one embodiment which is collectively formed in part by the yoke 102 and in the remaining part by the rotating trigger member 104 to form the annulus. An open central space 103 is defined by the trigger mechanism 100. This space 103 provides room for receiving a portion of the coil 106 when wound around the trigger mechanism.

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 which defines a pivot axis PA of rotation oriented transversely to the longitudinal axis of the firearm. As shown in FIGS. 6 and 7, rotating trigger member 104 may be pivotably coupled to the lower portion 112 of yoke 102 at a terminal end thereof. The rotating trigger member 104 and lower portion 112 are thus each configured to receive pivot 101 therethrough for forming the pivotable coupling. Any suitable type of pivot connection may be used for pivot 101, such as without limitation a pin or rod as some examples so long as the rotating trigger member 104 may be moved relative to the yoke 102. The rotating trigger member 104 defines an axis of tilt TA which is angularly movable with respect to a stationary axis SA defined by the vertical portion 114 of yoke 102 when the trigger mechanism is activated.

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 FIGS. 6 and 7, the rotating trigger member 104 includes a lower trigger segment or portion 118 below pivot 101 and an upper working segment or portion 120 above pivot 101. These portions may simply be referred to herein as lower and upper portions 118, 120 for brevity. In the case of FIG. 7, the lower portion 118 is pivotably movable relative to the upper portion. The lower portion 118 is configured to define a trigger 121 in one embodiment, and may include an arcuately curved shape typical of some forms of a firearm trigger for better engaging a user's finger. The upper portion 120 forms part of the magnetic flux circuit of the electromagnetic trigger mechanism 100 and is arranged to selectively and releasably engage the stationary yoke 102. In one embodiment, the rear surface of the upper portion 102 is engageable with the upper portion 110 of the yoke 102 as shown. The combination of the C-shaped yoke 102 and upper portion 120 of the rotating trigger member 104 including the pivot portion including the pivot 101 collectively define an openable and closeable annulus and magnetic flux loop via operation of the trigger (see magnetic flux path arrows). The lower portion 118 therefore may be considered to extend downwards from the annulus.

In one embodiment, as shown in FIG. 15, the upper portion 120 of the rotating trigger member 104 may be vertically elongated forming an extension that projects upwards beyond the upper portion 110 of yoke 102. This extension defines a sear 131 integrally formed with the trigger member. A sear surface 132 formed on the sear 131 is operably engageable with the striking member 130 (a pivotable hammer in the illustrated embodiment) to selectively hold or release the striking member 130 in/from the rearward cocked position for discharging the firearm. The sear surface 132 may be formed on the upward facing top surface on the top end of the sear 131 in one embodiment. In this example embodiment, the striking member 130 is a pivotable hammer. In other embodiments, the striking member 130 may be linearly movable and cockable striker well known in the art which operably interfaces with the sear 131. In yet other possible implementations, the sear surface 132 may operably interface with a separately rotatable sear disposed in the firearm frame which in turn interfaces with the striking member 130 similarly to that shown in FIG. 30. Numerous other variations and locations and configurations of sears and sear surfaces on the rotating trigger member 104 may of course be used. It bears noting that the vertically elongated extension of the upper portion 120 of trigger member 104 to form sear 131 may of course be provided in any of the trigger mechanisms 100 shown in FIGS. 6, 7, 13, and 14.

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 FIGS. 6 and 7, the electromagnet coil 103 of the trigger mechanism 100 is electrically coupled to and energized by an electric power source 122 (see, e.g. FIG. 1) of suitable voltage and current to control operation of the trigger mechanism for adjusting the trigger pull force and profile. The power source 122 is preferably mounted to the firearm and may comprise a single use or rechargeable replaceable battery in some embodiments. In one embodiment, an electric coil 106 wound primarily around and supported by the upright or vertical intermediate portion 114 of the stationary yoke 102 may be provided as shown which collectively forms an electromagnet. Operation of the trigger mechanism 100 such as for controlling the firing mechanism of a firearm or other applications is further described herein. In one embodiment, a protective casing such as an electrical resin encapsulate or potting compound may be provided to at least partially enclose and protect the coil 106.

The stationary yoke 102 and rotating trigger member 104 may be formed of any suitable soft ferromagnetic metal capable of being magnetized, such as without limitation iron, steel, nickel, 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.

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 FIG. 9). This results in either a decrease or increase in the peak trigger pull force required to be exerted on the rotating trigger member 104 by the user to pull and fully actuate the trigger mechanism 100. This parameter may be configured in conjunction with preprogramming the actuator 123 to operate the secondary electromagnetic field in either the additive or subtractive mode described above, thereby advantageously creating a highly customized the trigger pull force-displacement profile or curve in accord with user preferences.

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 FIG. 7, the stationary yoke 102 and rotating trigger member 104 of the snap actuator 123 are configured to create a magnetic circuit having a single closed flux loop or path. By orienting the north pole N and south pole S of permanent magnet 108 in any direction, a magnetic static holding force is created which draws the rotating member 104 to the stationary yoke 102. As one non-limiting example, assuming the north pole N were facing towards the rotating trigger member 104 as illustrated, the static magnetic flux circulates or flows through the flux circuit between the north and south magnetic poles in the clockwise direction indicated by solid static magnetic flux field arrows Ms. This draws the rotating member 104 and yoke 102 together at permanent magnet 108 to hold the trigger mechanism in the unactuated ready-to-fire position shown. When the power source 122 is configured via microcontroller 200 to operate in the “additive” mode as previously described (based on the polarity of the electric pulse sent to the actuator), the dynamic or active magnetic flux circulates or flows through the flux circuit when energized in the same clockwise direction indicated by dashed dynamic magnetic flux arrows “Md+”. This intensifies and increases the magnetic field and attraction between the yoke 102 and rotating member 104 which equates to a greater trigger pull force requirement to fully actuate the trigger mechanism. Conversely, when the power source 122 is configured by microcontroller 200 to operate in the “subtractive” mode as previously described (based on a reverse polarity of the electric pulse sent to the actuator), the dynamic or active magnetic flux circulates or flows through the flux circuit when energized in the opposite counterclockwise direction indicated by dashed dynamic magnetic flux arrows “Md−”. This lessens or decreases the magnetic field and attraction between the yoke 102 and rotating member 104, which equates to a lesser trigger pull force (i.e. resistance) required by the user to fully actuate the trigger mechanism. In some embodiments, the active magazine flux field can complete the trigger pull for the user upon detection of a trigger pull event. It bears noting that the actuator 123 would still operate in a similar manner if the north N and south S poles of permanent magnet 108 were reversed from the illustrated position which still creates a magnetic attractive force pulling the rotating member 104 to the yoke 102.

FIG. 9 shows one non-limiting embodiment of a control system which enables user selectable, programmable, and precisely timed adjustment of the trigger pull force/displacement profile during a trigger pull event via application of electric control current to the electromagnetic actuator 123 of the trigger mechanism 100. The control system includes programmable microcontroller 200 for monitoring and controlling operation of the electromagnetic trigger mechanism snap actuator and other aspect of the firearm operation in general. An actuation control circuit 202 operably coupled to power source 122 forms a control interface between the microcontroller 200 and electromagnetic actuator 123. In some configurations, the microcontroller 200 may actually from an integral part of the actuation control circuit 202 which is mounted on the same circuit board as opposed to being a separate component electrically coupled to the control circuit. This creates a “smart” control circuit 202.

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 FIG. 8).

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 FIG. 9).

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 a 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 FIG. 8).

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. FIGS. 9 and 10A). This would allow the collection of data such as rounds fired, attempted fires, acceleration forces, performance data, maintenance data, and timing and authorization events. This data could be wirelessly shared with a cellphone or other external electronic data processing/communication device, or even directly through a WiFi hub as shown in FIG. 11. In addition, operation of the electromagnetic actuator system including programming of the trigger pull force and displacement profile in the microcontroller 200 on the firearm may be programmed and controlled via the remote device.

Referring now to FIG. 7, further energy conservation and repeatability enhancements can be achieved by adding a spring 125 or other resiliently flexible member to the system, and the addition of a trigger displacement sensor 159. Spring 125 may be configured and arranged to bias the lower portion 118 (i.e. trigger 121) upper portion 120 of the rotating trigger member 104 forward to the ready-to-fire (unactuated) position relative to the upper portion 120. The static magnetic field generated by the permanent magnet 108 conversely holds the separately pivotable upper portion 120 of rotating trigger member 104 rearward towards the yoke 102 in the unactuated position. In various embodiments, the spring 125 may be a linear spring having a linear relationship between force and displacement, or a non-linear spring which changes spring force during trigger travel as further described herein elsewhere with respect to alternate spring 126. The spring 125 acts as a “buffer” for the magnetically-applied force on the upper member. The spring also provides the uniform feel of the trigger pull. Spring 125 may be a linear torsion spring in one embodiment as illustrated. The force “F” needed to extend or compress the spring 125, or other flexible member, by a distance “X” is proportional to that distance multiplied by the spring constant “k” (per Hooke's Law) and provides an additional force opposed to the permanent magnet 108 static holding force. In operation, as the trigger 121 (i.e. lower portion 118) is pulled and displaced against the biasing force of spring 125 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 of the snap actuator 123. At this point, the electromagnet coil is electrically energized to cancel out the static holding force or primary resistance created by permanent magnet 108 and creates a crisp snap-like final movement of the trigger linkage. As described elsewhere herein, permanent magnet 108 provides the primary or static magnetic field that directly constrains the movement of the trigger linkage at the beginning of the trigger travel. In this present embodiment, the final trip force is selectable by sensing the desired displacement/force point to electrically break-over the electromagnetic snap actuator 123 prior to reaching the magnetic flux open-loop break-over point of the permanent magnet.

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. FIG. 15), or an intermediate sear operably linked between the trigger mechanism 100 and striking member which holds the striking member in the rearward cocked position (see, e.g. FIG. 30).

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 FIGS. 13A-B may be used to create a non-linear trigger force displacement curve using a non-linear spring 126 or other resiliently flexible member and the electromagnetic snap actuator 123 of trigger mechanism. In this embodiment, the upper segment or portion 120 of the rotating trigger member 104 is pivotably coupled to and independently movable relative to the lower segment or portion 118. Spring 126 has a fixed end rigidly attached to or formed integral with the lower portion 118 of trigger member 104 and a free end engaged with the upper portion 120 of the trigger member. Spring 126 engages the rear surfaces of the upper and lower portions 120, 118 which acts to bias the trigger forward to the ready-to-fire vertical position.

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.

FIG. 12 shows a representative non-linear force-displacement curve for the proposed segmented trigger design of FIGS. 13A-B. A non-linear means or mechanism such as a combination of springs, flexible members and linkages is used to create the trigger displacement profile shown and the displacement sensor 159 is used to adjust the point at which the electrical trigger's break-over point in tripped. In the event of a failure of the electrical system, the default open-loop break-over point will provide a higher force trip point as a default operating point for the trigger. Many variations of the force-displacement curve could be possible using different springs, flexible members, and linkages.

In FIGS. 13A-B, the non-linear displacement force curve characteristics are achieved using a non-linear leaf spring 126. The first portion of the segmented trigger force-displacement curve is defined by the characteristics of the deformation of the non-linear leaf spring. When the trigger travel or displacement reaches and crosses the desired set-point, as measured using the trigger displacement trigger sensor 159 and relayed to the microcontroller 200, an electrical signal to the actuator triggered by the microcontroller snaps the upper segment of the trigger forward to interact with a traditional trigger bar linkage, sear, or alternative firing means. Although a leaf spring 126 is disclosed herein as an example of a spring exhibiting a non-linear relationship between force and displacement, other types of non-linear springs may be used such as for example without limitation a non-linear dual pitch helical coil springs, conical/tapered springs, barrel compression springs, etc.

FIGS. 14A-B shows another possible embodiment of the invention where the non-linear displacement force curve characteristics are achieved using a flexing member 127 combined with a secondary non-linear leaf spring 126. In this construction, the upper segment or portion 120 of rotating trigger member 104 is hingedly connected to the lower segment or portion 118 by a structurally integral portion of the trigger member body have a reduced transverse cross section in comparison to the upper and lower portions. The cross-sectional shape may be rectilinear in one embodiment. This creates a resiliently flexible and spring-like connection between the upper and lower portions of the rotating trigger member 104. Flexing member 127 acts as a elastically deformable living hinge. Other optional means for creating different force-displacement trigger profiles, before the magnetic break-over trip point, can be easily integrated with the magnetic snap actuation of the trigger mechanism 100 to those skilled in firearm trigger design. This could include the novel application of the magnetic snap actuation combined with mechanical trigger means used in traditional non-adjustable trigger designs. An apparent extension of the embodiment would include the application of the magnetic snap actuation combined with adjustable traditional mechanical trigger designs in a hybrid trigger design.

FIG. 15 shows the non-linear segmented trigger mechanism 100 with snap action magnetic break-over design used as a low-force sear surface and integrated into the release of a firearm striking member 130 in the form of a pivotable hammer, already described in detail above. This represents one non-limiting example of how the variable force trigger actuator could interface with existing firearm firing mechanism designs. Those skilled in firearm design can easily adapt this modular design to interface with other firing mechanisms as a direct replacement for the trigger mechanism.

The trigger member 104 in FIGS. 7 and 13-15 commonly share the design feature that the upper portion 120 of the trigger member is moveable independently of the lower portion 118 below the pivot 101 which is configured for a user's finger grip. Accordingly, in such a case, the upper portion 120 may alternatively be considered as simply a rotating member of the electromagnetic actuator 123 which is coupled to the trigger formed by the lower portion 118.

Referring to any of the foregoing embodiments of FIGS. 6, 7, and 13-15, an overview of basic theory of operation for the trigger mechanism 100 will now be described. The permanent magnet 108 contained within a closed loop magnetic yoke arrangement provides the fixed or static holding force for resisting movement of the trigger and associated sear 131. The holding force acts on the movable upper portion 120 of rotating trigger member 104. The magnetic yoke cross-sectional area and soft magnetic properties are chosen to maximize the efficiency of conducting the magnetic flux lines and provide inherent immunity to external magnetic field interference. The magnetic coil 106 can be energized, in either polarity, to add to or subtract from the fixed holding force of the permanent magnet which will result in changing the release force necessary to move the trigger and release the sear formed thereon.

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 magnet 108 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 FIG. 12.

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 FIG. 12 (dashed line curve). Because it is impractical to have the magnetic coil 106 energized at all times to extend battery life, the preprogrammed control logic executed by microcontroller 200 is used to determine the exact timing when to energize the magnetic coil, by how much (i.e. magnitude of electric voltage applied), and in what polarity (i.e. additive or subtractive).

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 FIG. 33 and electrically coupled between the power source 122 and snap actuator 123 could be used as the electronic control system to mechanically adjust and select a desired amount of voltage from a battery source to be applied to the magnetic coil 106. Potentiometer 371 provides a manually adjustable output voltage which is directed to the actuator 123 to either add to or subtract from the permanent magnetic holding force applied by permanent magnet 108. This allows the user to select the desired static magnetic holding force and concomitantly trigger force necessary to actuate the trigger mechanism. Potentiometer includes a manually rotatable or linearly movable slider or wiper allowing the user to adjust the output voltage. Potentiometers are commercially available.

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. FIG. 9) may be configured to include a digital potentiometer which is well known in the art. This provides adjustment of the magnitude of output voltage provided to actuator 123, thereby concomitantly allowing the magnitude of the required peak trigger pull force to be selected in addition to the other parameters such as polarity and timing of the electric signal pulse. FIG. 8 depicts one embodiment of a core or basic control logic which may be preprogrammed into microcontroller 200 to configure operation of the microcontroller and control snap actuator 123 of trigger mechanism 100. This control logic process may be used alone, or as the core for a more complex and detailed logic process used to control operation of the electromagnetic actuator 123 of trigger mechanism 100.

Referring now to FIG. 8, the control logic process 500 used to operate trigger mechanism 100 in one embodiment may start with activating and initializing the microcontroller 200 in Step 502. This may be initiated automatically in one embodiment via a wakeup signal from the grip force sensor 206 (see, e.g. FIG. 9) or other means. In Step 504, user activity on the trigger is sensed and measured by the trigger sensor 159 (e.g. a trigger pull) and a corresponding real-time data signal is transmitted to microcontroller 200. The sensor 159 may be a force or displacement type sensor in some embodiments, and the real-time data relayed to microcontroller 200 contains a respective type of information associated with the type of sensor being used (e.g. applied actual trigger pull force F or actual displacement distance of the trigger during its rearward travel). In one implementation, the displacement type sensor may be configured in its simplest form to merely measure movement of the trigger. The trigger activity real-time data may change over time during the trigger pull as the user further applies force or pressure on the trigger which is displaced by an increasingly greater distance. In Step 506, a test is performed by the microcontroller 200 which compares the real-time trigger activity data to a force or displacement setpoint preprogrammed into the microcontroller 200 by the user. If the microcontroller determines the measured real-time actual trigger force or displacement is less than the setpoint, control passes back to Step 504 to be repeat Steps 504 and 506. If the microcontroller determines that the measured real-time actual trigger force or displacement is greater than or equal to the preprogrammed setpoint, control passes forward to Step 508 in which the microcontroller sends an electric control pulse to actuator electromagnet coil 106. The actuator 123 becomes energized to implement the trigger force and release profile or curve having the characteristics preset by the user in the microcontroller 200. In Step 510, the process circuitry is reset in anticipation of the next trigger pull event.

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. FIG. 10A). Additionally, wireless communications, applications using an external electronic device 372 such as smartphone, tablets, personal wearable devices, or other custom external devices could be used to control the variability of the trigger feel. Additionally, the direct sensing of the trigger means provides a rich area 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 wired or wireless connections to the external electronic device (see, e.g. FIG. 11).

Dual Closed Magnetic Flux Loop Path Embodiment

FIGS. 16-30 depict an electromagnetically adjustable firing system of a firearm having an alternative non-limiting embodiment of an electromagnetic trigger mechanism 300 using a second magnetic flux loop. The second magnetic flux loop or path provides additional design features that provide faster snap action at the trigger breakover point and the ability to actively pull the trigger through its full range of travel on its own under magnetic power without additional external force or displacement from the operator's finger on the trigger. This advantageously provides essentially a powered follow through motion of the trigger and elimination of the operator feeling any of the remaining resistance of movement of the sear release linkages and parts. A principle advantage of the dual loop design is that it makes the operation of the trigger less susceptible to tolerance variations in the magnetic circuits. Trying to “buck” the magnetic holding force to exactly zero in a single loop design is generally not practical.

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 FIGS. 16-29, trigger mechanism 300 generally comprises electromagnetic snap actuator 350 and a trigger member 320 which may be pivotably coupled to the actuator in one embodiment. Viewed from the perspective of being mounted in a firearm held by a user or shooter (see, e.g. FIG. 30), actuator 350 includes a front side 310, rear side 311, right and left lateral sides 312, 313, bottom 314, and top 315. Actuator 350 comprises a stationary magnetic yoke 302, movable central rotating member 304, and electromagnet coil 306 which is operably connected to an electric source of power such as power source 122 onboard the firearm, as previously described herein. Yoke 302 defines mechanically robust main body or housing of the actuator, which is configured for removable mounting to a chassis or frame 22 of the firearm (see, e.g. FIG. 30) by any suitable mechanical coupling means, such as for example without limitation fasteners, interference or press fit, mechanically interlocked surfaces, combinations thereof, or other. The yoke 302 is 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.

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 305 as 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 FIGS. 28 and 29, possible physical interference between the coil 306 windings on the actuator and the rotating member is avoided. This arrangement therefore advantageously prevents impeded movement and response time or speed of the rotating member when actuated which might create undue pull resistance on the trigger member 320.

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 FIG. 28, upper cavity 330 in inner yoke portion 307 of yoke 302 defines a pair of opposing front and rear inner wall surfaces 307A, 307B on the front and rear of the cavity. Cavity 330 is configured to allow full pivotable actuation movement or action of the rotating member 304 about its pivot axis PAL To achieve this functionality, the inner wall surfaces 307A-B have a non-parallel converging-diverging relationship in so far that these wall surfaces converge moving downwards in cavity 330 towards the pivot axis PA1 of the rotating member 304 and diverge moving upwards towards the top open end of the inner yoke portion 307. The front inner wall surface 307A is obliquely angled to the rear inner wall surface 307B such that upper cavity 330 of inner yoke portion 307 is wider at the top and narrower at the bottom from front to rear. In one embodiment, the front inner wall surface 307A may be obliquely angled to the vertical central axis CA of actuator 350 and rear inner wall surface 307B may be parallel to central axis CA. The foregoing arrangement permits pivotable motion of the rotating member 304 forward and rearward in the upper cavity 330.

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. FIG. 28). When the actuator 350 is cycled between its two actuation positions by a user via a trigger pull, the actuation surfaces 334F, 334R are arranged to alternatingly engage the top sections 305D, 305E of the outer yoke portion 305. In one embodiment, rear actuation surface 334R engages permanent magnet 308 affixed to the rear top section 305D of outer yoke portion 305.

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 FIGS. 16-29, a socket or recess formed in the rotating member (not shown), or other element of other type and/or configuration (not shown) capable of mechanically interfacing with the firing mechanism. Although the engagement feature may be described herein for convenience of description and not limitation as an operating protrusion 333, any other form of engagement feature may be provided so long as the feature is capable of mechanically interfacing with a portion of the firing mechanism.

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 FIG. 15, or indirectly by acting on a separately mounted pivotable sear 375 which in turn is releasably engaged with the striking member (see, e.g. FIGS. 16-30).

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 FIGS. 20 and 21). This increases the surface area of the seating and actuation surfaces 341, 342 in contrast to portions of the actuating extension 340 extending forward from the paddle-shaped region.

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 FIGS. 20 and 21, the foregoing split construction of yoke 302 facilitates preassembly of the rotating member 304, electromagnet coil 306, and the trigger assembly or member 320 to the yoke to form a self-supporting electromagnetic trigger unit which is configured for mounting to the firearm via any suitable mechanical manner. Because the rotating member 304 and trigger member 320 (i.e. outer trigger 321) are pivotably mounted on pin 335 inside cavity 330 of the central section or portion 307 of yoke 302, these components require mounting before the right and left half-sections 305RH, 305LH of the yoke are assembled and fastened together. A general method for assembling actuator 350 in one non-limiting scenario may therefore comprise the sequential steps of: inserting trigger spring 344 into the downwardly open spring socket 345 of the yoke 302; inserting the inner trigger 322 into the outer trigger 321; inserting the pivot pin 323 transversely through the outer and inner triggers to complete assembly of these components; inserting the bottom actuating section 304B of rotating member 304 into the U-shaped channel 361 of the outer trigger 321 (inner trigger spring 365 being pre-mounted to the underside of bottom actuating section 304B using fastener 366); pivotably mounted the rotating member 304 and trigger member 320 on pivot pins 335R or 335L on the yoke 302 inside cavity 330; assembling or joining the right and left half-sections 305RH and 305LH of yoke 302 together using fasteners 317; winding the electromagnet coil 306 around central inner yoke portion 307; and attaching and mounting each rear and front top section 305D, 305E to its respective one of the vertical sections 305B and 305C of the outer yoke portion 305 using fasteners 316 (the permanent magnet 308 being pre-mounted on the rear top section 305D). Variations of the assembly sequence are possible and not limiting of the invention. In one embodiment, the assembled electromagnetic actuator trigger unit may be dropped into an upwardly open receptacle of the firearm frame 22 (see, e.g. FIG. 30) for securing the unit to the firearm. The electromagnetic trigger unit may alternatively be mounted to the firearm frame via fasteners or other methods.

The trigger member 320 will now be described in further detail. With continuing reference to FIGS. 16-29, trigger member 320 may include an outer trigger 321 and inner safety trigger 322 movable relative to the outer trigger. Inner safety trigger 322 includes an enlarged upper mounting portion 324 and lower blade portion 326 depending downwards therefrom for actuation by a shooter or user. The blade portion 326 may have an open framework construction including an arcuately concave front surface configured to facilitate engagement by the shooter or user's finger. The mounting portion 324 is pivotably mounted to outer trigger 321 via a second pivot pin 323 which defines a transverse second pivot axis PA2. Pivot pin 323 extends transversely through laterally open mounting holes 329 and 328 formed in the mounting portion 324 and outer trigger 321 respectively. Safety trigger 322 is pivotable independently of both the outer trigger 321 and rotating member 304 between forward and rearward positions. Pivot axis PA2 may be parallel to transverse pivot axis PA1 about which the trigger member 320 and rotating member 304 rotate. Pivot axis PA2 may be below pivot axis PA1 and is offset rearwards from the vertical central axis CA of the actuator. A transversely oriented safety bar 325 is carried by the upper mounting portion 324 and is arranged to selectively engage or disengage an upwardly open safety notch 327 formed in the cantilevered rear actuating extension 340 of the rotating member 304. In one embodiment, actuating extension 340 runs through a an upwardly open longitudinal slot formed in the upper mounting portion 324 of safety trigger 322 and is captured beneath the safety bar 325, but movable up/down when the rotating member 304 is actuated.

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. FIGS. 27-29). Operating extension 360 of outer trigger 321 is biased downward by trigger return spring 344 via rear actuating extension 340 of the rotating member (which acts on the operating extension). This in turn biases outer trigger 321 forward towards the ready-to-fire position. The spring 34 maintains continuous mutual engagement between the outer trigger 321 and the rotating member 304. Outer trigger 321 is manually movable by the shooter or user between the substantially vertical forward ready-to-fire position and pulled rearward fire position.

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. FIGS. 27 and 28) by a spring 365. In one embodiment, spring 365 may be in the form of a spring clip having a flat thin body with an upwardly angled central arm which engages a bottom surface of the inner trigger mounting portion 324 and a pair of downwardly angled legs which engage the lower trigger within channel 361. The central arm acts on the mounting portion 324 to bias the blade portion 326 of inner trigger 322 forward. The spring clip may be mounted to the underside of rotating member 304 in one embodiment by a threaded fastener 366 received in a threaded socket in the bottom actuating section 304B of rotating member 304. The bottom of rotating member 304 may comprise a recess configured to receive the spring clip. In the forward position, the blade portion 326 of inner trigger 322 protrudes forward from the outer trigger 321(see, e.g. FIGS. 27 and 28). In the rearward position, the blade portion protrudes rearward from the outer trigger when the inner trigger is fully depressed by the user (see, e.g. FIG. 29).

In operation, the trigger mechanism 300 will be in the ready-to-fire condition shown in FIGS. 27 and 28. Both the inner safety and outer triggers 322, 321 are in their vertical forward ready-to-fire positions via the biasing action of springs 365 and 344, respectively. In this position, the safety bar 325 on the inner trigger is engaged with the rear actuating extension 340 of the rotating member 304, thereby blocking its upward movement and preventing the firearm from being fired (best shown in FIG. 27). To discharge the firearm, the shooter or user initially applies a trigger pull force F on first the safety trigger 322 which rotates rearward to its rearward position shown in FIG. 29. The safety bar 325 seen in FIG. 27 rotates forward from the position shown and becomes vertically aligned with safety notch 327 in the rear actuating extension 340 of rotating member 304. The user's trigger finger may then fully engage and rotate the trigger member 320 (i.e. collectively outer trigger 321 with inner trigger 322) rearward to the rearward fire position. This fully actuates the trigger mechanism 300 to discharge the firearm, as further described herein. Because the safety bar 325 is aligned with safety notch 327, upward movement of rear actuating extension 340 of the rotating member 304 is no longer blocked, thereby allowing the firearm to be discharged either manually or when the snap actuator 350 is energized via normal operation.

The stationary yoke 302 and the rotating member 304 may be formed of any suitable ferromagnetic metal capable of being magnetized, such as without limitation iron, steel, nickel, 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 FIG. 31 (see flux arrows representing the primary static flux M1). The rotating member 304 is held firmly against and abuttingly engages the permanent magnet 308 as shown in FIGS. 27 and 28. The air gap B on the left side of the top of the rotating member 304 ensures that the left hand magnetic flux path is sufficiently high in magnetic reluctance that essentially all of the magnetic flux from the permanent magnet 308 is contained within the right hand loop (see, e.g. FIG. 28). A magnetic coil 306 surrounds the rotating member and when energized, the coil will generate and provide a secondary dynamically variable magnetic flux that adds to, or subtracts from, the primary fixed or static magnetic flux generated by permanent magnet 308 depending on the polarity of the electricity provided to the coil.

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 FIG. 31. In various embodiments, the trigger sensor(s) may be a force type sensor that measures applied force in real-time, a displacement type sensor that measures displacement distance in real-time, or a combination of force and displacement sensors may be used to provide both force and displacement information relayed to the microcontroller 200 for use in activating the snap actuator 350 in accordance with the preprogrammed trigger release profile created by the user. The force type sensor senses and provides information to the microcontroller relevant to actual trigger pull force F being applied on the trigger by the user. This serves as a basis for comparison to the preprogrammed breakpoint or setpoint trigger pull force used to time energizing the electromagnetic actuator 350 to alter the trigger pull force-displacement profile (see, e.g. FIG. 10B). The displacement type sensor senses and provides information relevant to the displacement distance of the trigger which may be used as the basis by the microcontroller for energizing the actuator 350 when a displacement setpoint is preprogrammed into the control system.

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 FIG. 32 and represented by the flux line arrows indicated. In one implementation, as depicted, the secondary flux M2 opposes the static magnetic flux M1 generated by the permanent magnet 308 in the right-hand side circuit when the electric pulse from power source 122 has a first polarity as controlled by microcontroller 200. Note that the dynamic secondary right-hand side flux M2 generated by energizing the coil is shown to circulate in a counterclockwise direction opposite to the static clockwise flux M1 generated by permanent magnet 308 shown in FIG. 31. The right-hand side secondary flux M2 created by the electromagnet coil 306 is therefore considered “subtractive” and decreases the clockwise static magnetic flux M1 in the right-hand side of the flux circuit. The energized coil 306 also simultaneously creates the additional clockwise flux M3 in the left-hand side of the circuit. If the current in the magnetic coil 306 is sufficiently large as in the present embodiment, then the force resulting from the magnetic flux M3 in the left-hand circuit air gap B will be greater than the force in the right-hand circuit, and the central rotating member 304 will snap to the left very quickly under magnetic force without any additional pull force F applied to the trigger by the operator or user. As the size of the air gap B on the left-hand side flux loop closes, an air gap A opens on the opposite right-hand side flux loop between the top of the rotating member 304 and permanent magnet 308 at right (see, e.g. FIG. 29). The magnetic reluctance of the left-hand side flux loop decreases and the magnetic reluctance of the right-hand side flux loop increases causing a rapidly increasing magnetic force of attraction pulling the central rotating member 304 to the left-most position allowed by the yoke 302 shown in FIG. 29.

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 FIG. 28. The trigger return spring 344 provides a preferably light biasing force ensuring the positive return of the rotating member 304 to the right-side starting or ready-to-fire position in the event the permanent magnet 308 fails to positively reset the actuator 350 or another unanticipated failure of the trigger mechanism occurs. The trigger spring, however, is not an essential component in the design in all embodiments but does provide a backup system for operating the trigger mechanism 300 completely by manual means particularly in exigent circumstances if the battery charge is lost or the microcontroller 200 malfunctions.

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 FIG. 31. This could be used to greatly increase the adjustable range of the trigger setpoint. This could also be used as a safety measure to increase the trigger holding force significantly in the event of some outside influence where it would be desirable to require a much higher trigger pull such as under high acceleration, drops, or shocks applications. This may be done with certain firearm configurations to ensure compliance with gun safety drop tests which is a well known test procedure in the art to confirm a firearm does not fire when accidentally dropped.

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 FIG. 8. In other embodiments, the selection of the setpoint can be as simple as a manual adjustment screw or knob of the potentiometer shown in FIG. 33 that interfaces with the microcontroller 200 and its basic control logic shown in FIG. 8. Or it can be any range of options from pre-programed to provide preset features, or totally programmable using controls mounted on the firearm, computer, or an external electronic device such as even a cellphone application that interface with the control logic unit or microcontroller 200. Examples of implementations that can be used include: (1) a Trigger Setpoint that is selected by manually adjusting a screw, knob, or switches of a potentiometer 371 to select either a continuous range of trigger release forces or a preset number of fixed release levels; (2) a user interface using switches, knobs, buttons, touch screen or other control interface on the firearm to set the trigger setpoint parameters and communicate them to the logic control unit or microprocessor 200 shown in FIG. 9; and (3) a wired or wireless programming device that communications to the firearm control logic via either a cable such as a USB cable, or wireless network connection such as Bluetooth, Wi-Fi, NFC, etc. The programming device could be a simple discrete remote control device or key fob, a computer, laptop, tablet, or cellphone running a software application which communicably interfaces with microcontroller 200 and its control logic or program instructions.

FIG. 10A graphically shows how an external electronic device 372 such as a cellphone for example could be used to select and program microcontroller 200 located onboard the firearm 20 with a trigger release profile via wireless Bluetooth communications. The wireless communications is enabled via the communication interface or module 209 in the microcontroller 200 (see, e.g. FIG. 9). The trigger profile parameters which may be accessed and selectively adjusted by the user in this non-limiting example may include both a trigger force breakpoint or setpoint (i.e. magnitude or value of holding or breakover trigger force F necessary to release the trigger) and timing of which point during the travel or displacement of the trigger that the trigger mechanism actuator 123 or 350 will be energized by the microcontroller 200. An example of the breakpoint or setpoint is shown in the trigger release profile of FIG. 10B.

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 FIG. 10A as examples. When the trigger profile setting software application is launched, a first security access screen 373 may be presented which prompts the user to enter a preselected personal identification number (PIN) in a similar manner to the security PIN required by the cellphone to change some of its core user settings. The user is then presented with a second trigger settings screen 374 containing input fields such as active icons, adjustment sliders, or other type input fields. This the user to select/enter the desired trigger breakpoint or breakover setpoint force (“Trigger Force” icon) for energizing the actuator 350 and/or timing for energizing the actuator based instead on trigger displacement (“Displacement” icon) depending on which type sensor is used. Alternatively, both type sensors may be used in some embodiments. These input fields provide the user interface which allow adjustment of the trigger force-displacement curve (FIG. 10B) to suit the user's preferences. In one embodiment, an active trigger release profile may be displayed in screen 374 which changes in real-time to reflect the corresponding settings for the setpoint and timing being input by the user. The external electronic device 372 then wirelessly communicates the selected changed trigger settings to the microcontroller 200 which becomes programmed with the trigger parameters entered in the cellphone trigger software application. Once the setting are complete, the user may close the trigger software application on the cellphone.

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 iron 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.

FIG. 30 shows one embodiment of a firearm 20 incorporating the electromagnetic trigger mechanism 300 with dual flux loop electromagnetic snap actuator 350 shown in FIGS. 16-29. It bears repeating that actuator 350 does not act like a non-bistable actuator characterized by the presence of a single permanent magnet 308 in the dual flux loops. Instead, the present trigger mechanism 300 and controller in this embodiment are mutually configured and operable to use a sensed externally applied force F on the trigger member as the impetus to energize the coil of the actuator 350. Energizing actuator 350 alters the force F required to be applied by the user to pull the trigger in accordance with the trigger release profile preprogrammed into microcontroller 200 (e.g. trigger breakpoint or breakover point previously described herein). In some configurations, the actuator 350 may actually complete the full trigger pull or travel without application of additional force by the user.

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 FIGS. 27-29).

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, 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.

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 FIGS. 27-30, firearm 20 in the present embodiment includes a striking member 130 in the form of a spring-biased and linearly movable striker 40. Striker 40 is movable in a forward linear path P for striking a chambered cartridge C. Spring 28 biases the striker 40 forwards such that when the striker is released from a rearward cocked position, the spring drives the striker forward to strike and detonate the charge in the cartridge C. Striker 40 has a horizontally-axially elongated body including a downwardly depending catch protrusion 42 which is engageable with an upstanding sear protrusion 44 of the sear 375 to hold the striker in the rearward cocked position. Sear 375 is pivotably mounted to the firearm frame 22 about a separate transverse sear pivot axis 376. 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. In one embodiment, 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. Striker 44 is movable in forward path P via a trigger pull between a rearward cocked position and a forwarding firing position contacting and detonating a chambered cartridge C to discharge the firearm.

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. FIGS. 27-28). In one embodiment, the front end of sear 375 may include a downward facing engagement surface 46 formed on a forwardly extending ledge-like protrusion of the sear which is selectively engageable with an upward facing engagement surface 48 formed on operating protrusion 333 of rotating member 304. Mutual engagement between surfaces 46 and 48 maintains the sear 375 in the upward position. Sear 375 may be biased towards the downward fire position by a spring 45 (shown schematically in FIGS. 28 and 29).

In operation, the firing mechanism is initially in the ready-to-fire condition or state shown in FIGS. 24, 27, 28, and 30. The striker 40 is held in the rearward cocked position by sear 375 which is in the upward standby position. Engagement surface 46 of the sear is engaged with engagement surface 48 of the actuator 350 (i.e. central rotating member 304). The trigger member 320 is not yet pulled. The microcontroller 200 is programmed with the control logic shown in FIG. 8 and may be initialized and active (Step 502), such as via the microcontroller detecting user activity on the firearm, such as the user's positive grip on the frame 22 sensed by grip force sensor 206 mounted to the frame, and/or motion of the firearm sensed by motion sensor 207 (see also FIG. 9). The rotating member is in the rearward unactuated position magnetically engaged with permanent magnet 308.

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 FIG. 8 in the manner previously described herein. The preprogrammed trigger force and displacement profile (e.g. breakpoint or breakover setpoint) is implemented in which the microcontroller energizes the electromagnetic actuator 350 and automatically adjusts the trigger activation force according to the preprogrammed profile created by the user. The user continues to pull the trigger until the central rotating member 304 of the actuator pivots forwards to the actuated position and breaks engagement with the sear 375 as shown in FIG. 29. Sear 375 then in turn drops and pivots downward thereby releasing the striker 40 which moves along path P to strike the chambered cartridge C and discharge the firearm 20. After firing, actuator 350 is de-energized by the microcontroller 200 as the user completely or partially releases the trigger which resets to the ready-to-fire position for the next firing cycle. In some embodiments, the microcontroller via actuation control circuit 202 transmits merely a short momentary pulse of electric current to the coil 306 which is sufficient to change state of the electromagnetic actuator 350 for implementing the trigger release profile and alter the primary resistance force generated by the permanent magnet 308 in the flux loop. The control circuit therefore performs a quick on/off switching of the power supply to the actuator. Accordingly, no feedback control is required for the microcontroller 200 to terminate electric power to the actuator 350.

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. FIG. 7 or 29) to measure leakage flux at the air gap as the rotating trigger member 104/304 are moved. This measurement could be relayed to the microcontroller 200 and used to deduce the state of the electromagnetic actuator. The flux measurement displacement sensor would allow for the dynamic variation of trigger pull force based on travel or displacement and the trigger decision event could be defined as a specific displacement threshold. The possible force profiles to be defined, selected, and implemented under electrical control could be expanded to include any number of force/displacement curves with the displacement to firing being a new dynamic variable. A long easy trigger pull, verses a short heavy pull, or a long heavy pull, or even a short light hair trigger could be created by appropriately programming the microcontroller 200. The force and displacement could conceptually be fully programmable over a plurality of all possible ranges using the control system shown in FIG. 9.

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 FIG. 9 beyond a trigger sensor(s), a series of operating conditions could be incorporated into the control logic used to enhance operation of an electronic fire-by-wire firing mechanism. Referring to FIG. 9, some possibilities could include grip force sensors 206 to ensure a ready-to-fire secure grip of the firearm by the user preceding the firing event, to inertia or motion sensors 207 that would preclude the firearm to function under dropping or accidental movement due to a fall, trip, or other similar incident, to the incorporation of other sensors operable to confirm suitable firing conditions based on the user, location, time of day, or environment.

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 FIG. 8.

FIG. 34 shows an exemplary control logic process 400 which may be implemented by microcontroller 200 to control a fire-by-wire trigger mechanism having an electronic sear (E-sear) such as a piezo-electric actuator to detonate the cartridge. Such a system may be incorporated into any type of firearm, such as the pistol shown in FIG. 30 as one non-limiting example. FIG. 35 shows a modified control system amenable for use with such an electronic E-sear trigger mechanism. The trigger mechanism 400 may include a second mechanical trigger sensor 160 such as a mechanical switch in conjunction with a force or displacement trigger sensor 159/370 associated with the electromagnetic actuators 123/350 of firing mechanisms 100/300 depending on which firing mechanism is used with the fire-by-wire system.

Referring to FIGS. 34 and 35, the microcontroller 200 would awaken when it detects a wake-up signal generated from gripping the gun which is sensed by grip sensor 206 and communicated to microcontroller 200 (Step 402). Alternatively, this could be a motion detection wake-up signal sensed by motion sensor 207 instead of a grip sensor. On wake-up, a quick check that sufficient battery power is available and that the system is functioning is performed in the form of a self-test (Step 404). A failure of this self-test or battery check would result in aborting the start-up sequence and informing the operator of the error/warning so that corrective action can be taken.

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 FIG. 34. Alternatively, these state change events could be polled periodically on a reasonable preprogrammed time schedule to ensure reliable and timely detection.

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 FIG. 8 is simultaneously performed and implemented by the microcontroller 200 to adjust the trigger release profile according to the preprogrammed trigger breakpoint/breakover setpoint or displacement in the manner previously described herein. The trigger release settings and electric pulse sent to actuator 123 or 350 to activate the same (depending on whether the single or double loop actuator firing mechanism is used) is represented by block 253 in FIG. 35.

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.

Number	Name	Date	Kind
1875941	Schwartz	Sep 1932	A
2424247	Mccaslin	Jul 1947	A
2702841	Bernstein	Feb 1955	A
2780882	Temple	Feb 1957	A
2957391	Lovercheck	Oct 1960	A
2978825	Tichenor	Apr 1961	A
3065560	Bumiller	Nov 1962	A
3184651	Albosta	May 1965	A
3208181	Calhoun et al.	Sep 1965	A
3250034	Simmons	May 1966	A
3650174	Nelsen	Mar 1972	A
3854231	Broyles	Dec 1974	A
3982347	Brandl et al.	Sep 1976	A
4009536	Wolff	Mar 1977	A
4134223	Hillenbrandt	Jan 1979	A
4236132	Zissimopoulos	Nov 1980	A
4275521	Gerstenberger et al.	Jun 1981	A
4329803	Johnson et al.	May 1982	A
4347679	Grunig	Sep 1982	A
4510844	Fritz et al.	Apr 1985	A
4727670	Krouse	Mar 1988	A
4730407	DeCarlo	Mar 1988	A
4793085	Surawski et al.	Dec 1988	A
5074189	Kurtz	Dec 1991	A
5083392	Bookstaber	Jan 1992	A
5272828	Petrick et al.	Dec 1993	A
5303495	Harthcock	Apr 1994	A
5544439	Grember et al.	Aug 1996	A
5625972	King et al.	May 1997	A
5713150	Ealovega	Feb 1998	A
5755056	Danner et al.	May 1998	A
5784821	Gerard	Jul 1998	A
5901488	Oberlin	May 1999	A
6286241	Constant	Sep 2001	B1
6354033	Findley	Mar 2002	B1
6360469	Mikuta et al.	Mar 2002	B1
6374525	Thomas	Apr 2002	B1
6425199	Vaid	Jul 2002	B1
6430861	Ayers et al.	Aug 2002	B1
6442880	Allan	Sep 2002	B1
6668700	Danner et al.	Dec 2003	B1
6694963	Taylor	Feb 2004	B1
6732464	Kurvinen	May 2004	B2
6802305	Hatcher	Oct 2004	B1
6951071	Acosta	Oct 2005	B1
7049915	Delamare et al.	May 2006	B2
7231911	Hatcher	Jun 2007	B2
7441362	Kley	Oct 2008	B1
7457096	Brundula	Nov 2008	B2
7819051	Beckmann et al.	Oct 2010	B1
8015911	Hellstrøm et al.	Sep 2011	B2
8109024	Abst	Feb 2012	B2
8113103	Beckmann et al.	Feb 2012	B2
8234969	Beckmann	Aug 2012	B2
8336438	Compton	Dec 2012	B2
8461951	Gassmann et al.	Jun 2013	B2
8522466	Arduini	Sep 2013	B2
8677665	Huber	Mar 2014	B1
8692636	Reuber	Apr 2014	B2
8807007	Alicea	Aug 2014	B2
9011151	Jones et al.	Apr 2015	B1
9190234	Reuber	Nov 2015	B2
9347726	Thomas	May 2016	B1
9395134	Swensen	Jul 2016	B2
20010039751	Kurvinen	Nov 2001	A1
20060005447	Lenner	Jan 2006	A1
20090300961	Ruhland et al.	Dec 2009	A1
20120131832	Arduini	May 2012	A1
20150107567	Vera et al.	Apr 2015	A1
20150377574	Cooke et al.	Dec 2015	A1
20160061549	Patterson	Mar 2016	A1
20160233012	Lubinski et al.	Aug 2016	A1

Number	Date	Country
2701446	Oct 2011	CA
204301599	Apr 2015	CN
2926559	Jan 1981	DE
9301009	May 1994	DE
202013005117	Jul 2013	DE
1132929	Jul 2008	EP
2887003	Dec 2016	EP
2887002	Jan 2017	EP
2313655	Dec 1997	GB
2000133091	Jul 2001	JP
2001250716	Sep 2001	JP
3240351	Dec 2001	JP
4887993	Feb 2012	JP
5613731	Oct 2014	JP
20010035913	May 2001	KR
2101839	Jan 1998	RU
1133960	Sep 1987	SU
1830443	Sep 1987	SU
WO2005116567	Dec 2005	WO

Dynamic variable force trigger mechanism for firearms

Information

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Date Filed

Date Issued

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CPC

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US

CPC

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Abstract

Description

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CROSS-REFERENCE TO RELATED APPLICATIONS

US Referenced Citations (72)

Foreign Referenced Citations (19)

Non-Patent Literature Citations (2)

Related Publications (1)

Provisional Applications (1)

Entry
Corresponding International Search Report for Application No. PCT/US2018/020355, dated May 21, 2018.
Author: Moving Magnet Technologies SA, Bistable Actuators Actuators and Solenoids for stable positions without current; See description and rotary actuator figure. Internet site: http://www.movingmanget.com/en/bistable-actuators-rotary-solenoids/ printed Jun. 19, 2018.