Aircraft bomb racks have long had safety locks to prevent unintentional discharge of bombs from the racks. Current bomb rack safety locks can provide for remote locking and unlocking while the aircraft is in flight. However, due to the function bomb rack safety locks perform, safety and reliability considerations have caused current designs to be rather heavy, complicated and costly to implement. Additionally, some bomb rack safety locks are associated with pneumatically actuated bomb racks, which introduces additional challenges in bomb rack safety lock design and usage. Moreover, small bomb racks are typically not designed to use bomb rack locks and devices designed for larger bomb racks, thus leading to multiple designs on which in flight operators and ground crew must be trained.
Features and advantages of the invention will be apparent from the detailed description which follows, taken in conjunction with the accompanying drawings, which together illustrate, by way of example, features of the invention; and, wherein:
Reference will now be made to the exemplary embodiments illustrated, and specific language will be used herein to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended.
As used herein, the term “substantially” refers to the complete or nearly complete extent or degree of an action, characteristic, property, state, structure, item, or result. For example, an object that is “substantially” enclosed would mean that the object is either completely enclosed or nearly completely enclosed. The exact allowable degree of deviation from absolute completeness may in some cases depend on the specific context. However, generally speaking the nearness of completion will be so as to have the same overall result as if absolute and total completion were obtained. The use of “substantially” is equally applicable when used in a negative connotation to refer to the complete or near complete lack of an action, characteristic, property, state, structure, item, or result.
An initial overview of technology embodiments is provided below and then specific technology embodiments are described in further detail later. This initial summary is intended to aid readers in understanding the technology more quickly but is not intended to identify key features or essential features of the technology nor is it intended to limit the scope of the claimed subject matter.
Although the current bomb rack lock designs are indeed functional, they can be overly complex, large, and expensive, usually requiring a multitude of sensors and electronics. Additionally, current bomb rack lock designs are also typically single task devices that only lock/unlock a bomb rack.
A bomb rack lock as part of and for a bomb rack is disclosed that is easy to use, scalable to a small size, and combines operational functions into single components. In one aspect, the bomb rack lock can include features that eliminate common operator error associated with loading bombs, thus improving operational safety. The bomb rack lock can include a plunger movable to engage a bomb rack linkage of the bomb rack to be alternately secured and released and a solenoid body coupled to and operable to support the plunger. The plunger and the solenoid body can be movable relative to each other and the bomb rack linkage, and the solenoid body can be movable between a first position and a second position. The bomb rack lock can also include a sensor to determine whether the solenoid body is in the first position. The plunger can be movable to engage and disengage the bomb rack linkage with the solenoid body in the first position. In the second position, the solenoid body can prevent engagement between the plunger and the bomb rack linkage.
A bomb rack lock system is further disclosed. The bomb rack lock system can include a bomb rack linkage selectively movable between at least first and second positions. The system can also include a piston in fluid communication with a fluid source via a fluid conduit, the fluid source being configured to provide a pressurized fluid to actuate the piston to apply a force to the bomb rack linkage to cause the bomb rack linkage to move. Furthermore, the system can include a bomb rack lock operable with the bomb rack linkage to alternately secure and release the bomb rack linkage. The bomb rack lock can include a solenoid body and a plunger coupled to the solenoid body, the plunger being movable relative to the solenoid body to engage and disengage the bomb rack linkage. Additionally, the system can include a redundancy system to prevent unwanted movement of the bomb rack linkage. The redundancy system can include a vent in fluid communication with the fluid source and having an open position and a closed position. The redundancy system can also include a coupling between the plunger and the vent, the coupling being configured to activate and open the vent when the plunger is engaged with the bomb rack linkage, and to deactivate and close the vent when the plunger is disengaged from the bomb rack linkage. When open, the vent can cause the pressurized fluid to escape the fluid conduit to prevent actuation of the piston and movement of the bomb rack linkage. When closed, the vent can prevent pressurized fluid from escaping the fluid conduit via the vent to facilitate movement of the bomb rack linkage.
One embodiment of a bomb rack lock 10 is illustrated in
To provide for both in-flight and ground operation of the bomb rack lock 10, the plunger 11 and the solenoid body 12 can be movable relative to each other and the bomb rack linkage 20. To engage and disengage the bomb rack linkage 20, the plunger 11 can be movable generally in direction 4. Additionally, the solenoid body 12 can be movable generally in direction 5. For example, as shown in
With the solenoid body 12 in the first position 1, the plunger 11 can be movable to engage and disengage the bomb rack linkage 20, as shown in
In one aspect, the solenoid body 12 can be coupled to a lever arm 16 configured to facilitate movement of the solenoid body 12 between the first position 1 and the second position 2, such as for ground operation of the bomb rack lock 10. The lever arm 16 can be rotatably coupled to a base 17 and can be machine or manually actuatable to move the solenoid body 12 between the first position 1 and the second position 2. In a particular aspect, the lever arm 16 can interface with a channel 18. The channel 18 can include a retaining feature, such as a detent 19a, 19b or a lock, to inhibit movement of the lever arm 16 from the first position 1 and/or the second position 2. In other words, the solenoid body 12 can be prevented from unintentionally moving out of the first position 1 and/or the second position 2 by use of the retaining feature, thereby preventing unintentionally releasing or securing of the bomb rack linkage 20 through movement of the solenoid body 12.
In another aspect, the bomb rack lock 10 can be configured to automatically lock the bomb rack linkage 20 for in-flight operation in the event that the solenoid body 12 is out of the first position 1 when aircraft power is first applied to the bomb rack in its normal operating sequence. For example, following ground operations of the bomb rack lock 10, the solenoid body 12 may be left out of the first position 1 by mistake or oversight, thus preventing the plunger from engaging the bomb rack linkage 20. To provide for this automatic in-flight locking feature, the bomb rack lock 10 can include a plunger extension 14 configured to apply a force to the solenoid body 12 to move the solenoid body 12 to the first position 1. For example, the bomb rack lock 10 can include or otherwise be associated with a stationary push plate 15 that supports the plunger extension 14 as the plunger extension 14 applies force to the solenoid body 12 to move the solenoid body 12 to the first position 1. Upon movement of the solenoid body 12 to the first position 1, as shown in
In a particular aspect, the plunger 11 can be biased to engage the bomb rack linkage 20, such that actuation of the plunger 11 causes the plunger 11 to disengage the bomb rack linkage 20 and deactivation allows the plunger 11 to move, via its bias, into engagement with the bomb rack linkage 20. For example, the plunger 11 and the plunger extension 14 can comprise a single unitary structure disposed within an electrical coil to form a solenoid. The entire unitary structure can be biased to engage the plunger 11 portion with the bomb rack linkage 20. The solenoid can be actuated to act against the bias and disengage the plunger portion 11 from the bomb rack linkage 20. Simultaneously, the plunger extension portion 14 of the unitary structure can extend from an end of the solenoid body 12. If the plunger extension portion 14 contacts the push plate 15, the plunger extension portion 14 can cause the solenoid body 12 to move toward the first position 1.
The bomb rack lock 10 can also include a sensor to determine whether the solenoid body 12 is in the first position 1 (or the second position 2). For example, to automatically lock the bomb rack linkage 20, upon the sensor determining that the solenoid body 12 is not in the first position 1, the plunger extension 14 can cause the solenoid body 12 to move to the first position 1. In a particular exemplary embodiment illustrated schematically in
In a particular aspect, the detent 19a can assist the solenoid body 12 in moving to, and maintaining the first position 1. For example, as the solenoid body 12 moves toward the first position 1, the lever arm 16 interfaces with the channel 18 until the lever arm encounters the detent 19a. Initially, the detent 19a can resist movement of the lever arm 16, but as the lever arm 16 continues along the channel 18 past the detent 19a, the detent 19a can urge the lever arm 16 forward in the direction of travel, forcing the solenoid body 12 into the first position 1. Thus, the detent 19a can help ensure that the member 9 is able to open the switch 13 by providing a force to act against the spring 8 that biases the switch in the closed position.
In one aspect, the switch 13 can be electrically coupled to a power supply 90, such that when power is supplied to the switch 13 and the solenoid body 12 is not in the first position 1, power can be supplied to a solenoid or motor via the switch 13 to actuate the plunger extension 14 and cause the solenoid body 12 to move to the first position 1. In this way, the solenoid body 12 can be automatically moved to the first position 1 to lock the bomb rack linkage 20 upon powering up the power supply. Alternatively, when the solenoid body 12 is in the first position 1 and the switch 13 is open, the solenoid or motor can receive an actuation signal or power from a command module 92, such as for in-flight operation of the bomb rack lock 10. In this way, the plunger 11 can be actuated to disengage from the bomb rack linkage 20 as described herein. In one aspect, the command module 92 can receive power from the power supply 90 in order to actuate the plunger 11.
As used herein, the term “sensor” is not to be limited to traditional sensors only, and may include a device that can be used to function as a sensor, such as a switch. A sensor can include a position sensor, a Hall effect sensor, a capacitive sensor, a laser rangefinder, a linear encoder, a rotary encoder, a switch, or any other type of sensor or device that can be used to determine the position of the solenoid body 12.
It should be recognized that a solenoid body as disclosed herein need not be oriented such that the plunger moves perpendicular to the bomb rack movement. For example, a solenoid body can be disposed such that the plunger moves parallel to the bomb rack movement, such as to actuate a lever that engages/disengages the bomb rack or to operate a crank that causes engagement/disengagement with the bomb rack.
In use, such as for ground operation,
In one embodiment, the bomb rack linkage 20 can include a linkage mechanism that interfaces with the bomb rack lock 10 in order to release a bomb prior to discharging the bomb from the bomb rack. A member of a ground crew can manually unlock the rack by moving the lever arm 16 and displacing the solenoid body 12. In this case the manual unlock function is advantageous because it does not require power from the aircraft in order to release the lock. The ground crew member can also manually lock the rack prior to flight. If the bomb rack inadvertently remains unlocked following ground maintenance, the bomb rack lock 10 can be configured to automatically lock the rack to remedy such an oversight. For example, when the aircraft is powered up, the switch 13 can be in the closed position, with the solenoid body 12 out of the first position 1, to cause power to be supplied to a solenoid to cause the plunger extension 14 to push against the push plate 15 until the solenoid body 12 is displaced to the first position 1. At this point, the switch 13 can open to deactivate the solenoid. Upon deactivation of the solenoid, the plunger 11 can be biased to move into engagement with the bomb rack linkage 20, thus automatically locking the bomb rack when the aircraft is powered up. In the locked position, an in-flight crew member can unlock the bomb rack by sending a signal to move the plunger 11 out of engagement with the bomb rack linkage 20. For example, the signal can provide power to activate the solenoid, thereby causing the plunger 11 to move against the bias and out of engagement with the bomb rack linkage 20. With the bomb rack linkage 20 unlocked, the linkage can be moved to release the bomb so that the bomb can be ejected from the rack as intended.
As illustrated in
When open, the vent 51 can cause pressurized fluid to escape the fluid conduit 42 to prevent actuation of the bomb rack linkage 20. When closed, the vent 51 can prevent pressurized fluid from escaping the fluid conduit 42 via the vent to pressurize and facilitate movement of the bomb rack linkage 20. Thus, the vent can be controlled by the plunger 11 to prevent actuation the bomb rack linkage 20. This configuration can prevent over-pressurizing the fluid system when movement of the bomb rack linkage 20 would be prevented by the plunger 11.
The redundancy system 50 can further include a second vent 52. Like the first vent 51, the second vent 52 can have an open position (shown in
The redundancy system 150 can also have a second coupling 58 between the solenoid body 12 and the second vent 52. The solenoid body 12 can be movable relative to the bomb rack linkage 20 between the first position 1 (shown in
It should be recognized that a vent can be digital in nature, being only either fully open or fully closed. On the other hand, a vent can be analog in nature, with a transition between fully open and fully closed. As such, an “open” vent can be less than fully open and a “closed” vent can be less than fully closed. An “open” analog vent can therefore result in some fluid pressure acting on a piston, which can cause some negligible amount of movement of a bomb rack. This is within the scope of the present disclosure and is acceptable for an “open” vent, since a negligible amount of movement of the bomb rack is not likely to pose a safety concern and over-pressurization of the fluid system is not likely, given the open vent, even if not fully open.
In one embodiment, the valves 51, 52 can be substituted with electrical switches and the fluid conduit 42 can be substituted with a control circuit. Thus, the positions of the solenoid body 12 and the plunger 11 can be used to control switches coupled to a control circuit that allows or prevents actuation of the bomb rack linkage 20. For example, the control circuit can control firing of a cartridge that generates a gas propellant for actuating the bomb rack linkage 20. Such control circuits and cartridges are commonly found in traditional bomb rack actuation designs.
Shown in
The system 100 can further comprise a redundancy system 150 to prevent unwanted movement of the bomb rack linkage 120. The redundancy system 150 can have a vent 151 in fluid communication with the fluid source 140. The vent 151 can have an open position (shown in
When open, the vent 151 can cause the pressurized fluid to escape the fluid conduit 142 to prevent actuation of the piston 130 and movement of the bomb rack linkage 120. When closed, the vent 151 can prevent pressurized fluid from escaping the fluid conduit 142 via the vent to pressurize and actuate the piston 130, and to facilitate movement of the bomb rack linkage 120. Thus, the vent 151 can be controlled by the plunger 111 to prevent actuation of the piston 130 when the plunger 111 is engaged with the bomb rack linkage 120. This configuration can prevent over-pressurizing the fluid system when movement of the piston 130 would be prevented by the plunger 111.
The redundancy system 150 can further include a second vent 152 in fluid communication with the fluid source 140. Like the first vent 151, the second vent 152 can have an open position (shown in
The redundancy system 150 can also have a second coupling 158 between the solenoid body 112 and the second vent 152. The solenoid body 112 can be movable relative to the bomb rack linkage 120 between a first position (shown in
It should be recognized that a vent can be digital in nature, being only either fully open or fully closed. On the other hand, a vent can be analog in nature, with a transition between fully open and fully closed. As such, an “open” vent can be less than fully open and a “closed” vent can be less than fully closed. An “open” analog vent can therefore result in some fluid pressure acting on a piston, which can cause some negligible amount of movement of a bomb rack. This is within the scope of the present disclosure and is acceptable for an “open” vent, since a negligible amount of movement of the bomb rack is not likely to pose a safety concern and over-pressurization of the fluid system is not likely, given the open vent, even if not fully open.
The bomb rack linkage 120 can include a first catch 121 and a second catch 122. Each of the first catch 121 and the second catch 122 can be engageable and disengageable with the plunger 111 to alternately secure and release the bomb rack linkage 120. In one aspect, the plunger 111 can engage the first catch 121 to secure the bomb rack linkage 120 in a first position and the plunger 111 can engage the second catch 122 to secure the bomb rack linkage 120 in a second position. For example, the second catch 122 can be engaged by the plunger 111 following release of the plunger 111 from the first catch 121 and movement of the bomb rack linkage 120. In a particular aspect, the engagement with the second catch 122 can be used to control the first vent 151. For example, the engagement with the second catch 122 can cause the coupling 156 to open the vent 151 to cause the pressurized fluid to escape the fluid conduit 142 to prevent further movement of the bomb rack linkage 120 by the piston 130. Thus, the second catch 122 can provide the dual functions of securing the bomb rack linkage 120 in a given position and controlling the vent 151. In one aspect, a spring 132 can be included that provides a force on the bomb rack linkage 120. In a particular aspect, the spring 132 can act against movement of the bomb rack linkage 120 from an engagement position with the first catch 121 to an engagement position with the second catch 122. Thus, for example, the spring 132 can apply a force on the bomb rack linkage 120 to return the bomb rack linkage 120 to engage the first catch 121 upon release from the second catch 122.
The bomb rack lock system 100 can further comprise a second piston 160 in fluid communication with the fluid source 140 via the fluid conduit 142. As with the first piston 130, the fluid source 140 can be configured to provide pressurized fluid to actuate the second piston 160. The second piston 160 can be configured to apply a force to ejection feet 170 to cause the ejection feet 170 to move. In this case, engagement of the plunger 111 with the second catch 122 can cause the coupling 156 to open the vent 151 and the pressurized fluid to escape the fluid conduit 142 to prevent further movement of the ejection feet 170 by the second piston 160. In one aspect, a spring 162 can be included that acts against movement of the ejection feet 170 caused by the second piston 160. Thus, for example, the spring 162 can apply a force on the ejection feet 170 to retract the ejection feet 170 upon venting of the pressurized fluid.
In one aspect, the bomb rack linkage 120 can include a mechanism configured to alternately secure and release a payload 180 upon movement of the bomb rack linkage 120, such as a linkage member. Such movement can be between a first position with the plunger 111 engaging the first catch 121 and a second position with the plunger 111 engaging the second catch 122. The securing and releasing mechanism can include a coupling feature, such as a hook 126 to couple with the payload 180. The hook 126 can be moved to secure or release the payload 180 by a coupling 124, such as a mechanical linkage, with the bomb rack linkage 120. In a particular aspect, the bomb rack linkage 120 can form a part of a mechanical linkage coupled to the hook 126. In another aspect, the ejection feet 170 can be configured to transfer force from the second piston 160 to the payload 180 to discharge the payload 180 from a stored position. Actuation of the second piston 160 can be coordinated with actuation of the hook 126 to apply a force to the payload 180 following release from the hook 126.
With continued reference to
Facilitating opening and closing of the vent can comprise providing a coupling between the plunger of the bomb rack lock and the vent, the coupling being configured to activate and open the vent when the plunger is engaged with the bomb rack linkage, and to deactivate and close the vent when the plunger is disengaged from the bomb rack linkage.
Facilitating opening and closing of the vent can further comprise providing a second vent in fluid communication with the fluid source. The second vent can have an open position and a closed position. A second coupling between the solenoid body and the second vent can be provided, the solenoid body being movable relative to the bomb rack linkage between a first position and a second position. The plunger can be movable to engage and disengage the bomb rack linkage with the solenoid body in the first position, wherein the solenoid body, in the second position, prevents engagement between the plunger and the bomb rack linkage. The second coupling can be configured to activate and open the second vent when the solenoid body is out of the first position, and to deactivate and close the second vent when the solenoid body is in the first position. The second vent, when open, can cause the pressurized fluid to escape the fluid conduit to prevent actuation of the piston and movement of the bomb rack linkage. The second vent, when closed, can prevent pressurized fluid from escaping the fluid conduit via the second vent, wherein the pressurized fluid actuates the piston and causes the bomb rack linkage to move when the first vent and the second vent are each in the closed positions.
One skilled in the art will recognize that the various components and elements of the invention described herein may be used according to their disclosed relative functions in other applications. For example, the structure describing the bomb rack lock can be used to alternately engage and disengage an object other than a bomb rack linkage. Likewise, the automatic locking features and redundancy system can be used in applications other than those described herein relating to a bomb rack. As such, the terms used herein are not to be limited only to bomb rack applications and terminology and may be viewed generically for use in other applications.
It is to be understood that the embodiments of the invention disclosed are not limited to the particular structures, process steps, or materials disclosed herein, but are extended to equivalents thereof as would be recognized by those ordinarily skilled in the relevant arts. It should also be understood that terminology employed herein is used for the purpose of describing particular embodiments only and is not intended to be limiting.
Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present invention. Thus, appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment.
As used herein, a plurality of items, structural elements, compositional elements, and/or materials may be presented in a common list for convenience. However, these lists should be construed as though each member of the list is individually identified as a separate and unique member. Thus, no individual member of such list should be construed as a de facto equivalent of any other member of the same list solely based on their presentation in a common group without indications to the contrary. In addition, various embodiments and example of the present invention may be referred to herein along with alternatives for the various components thereof. It is understood that such embodiments, examples, and alternatives are not to be construed as de facto equivalents of one another, but are to be considered as separate and autonomous representations of the present invention.
Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided, such as examples of lengths, widths, shapes, etc., to provide a thorough understanding of embodiments of the invention. One skilled in the relevant art will recognize, however, that the invention can be practiced without one or more of the specific details, or with other methods, components, materials, etc. In other instances, well-known structures, materials, or operations are not shown or described in detail to avoid obscuring aspects of the invention.
While the foregoing examples are illustrative of the principles of the present invention in one or more particular applications, it will be apparent to those of ordinary skill in the art that numerous modifications in form, usage and details of implementation can be made without the exercise of inventive faculty, and without departing from the principles and concepts of the invention. Accordingly, it is not intended that the invention be limited, except as by the claims set forth below.
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