This invention relates to systems and methods for actively countering forces experienced by an object or person and more particularly, although not exclusively, to systems and methods for actively countering forces experienced by a manned (or unmanned) vehicle upon encountering blast waves of a mine or other explosive device or other undesired forces.
U.S. Patent Application Publication No. 2012/0239247 of Eridon, whose contents also are incorporated herein by this reference, purports to disclose “systems and methods for mitigating the effects of sudden accelerative forces on vehicles due to, for example, land mines and improvised explosive devices (IEDs).” See Eridon Application, p. 1, ¶0002. Described generally in the Eridon Application is such a system having sensors, a control system, countermeasures, and a human interface. According to the Eridon Application, the control system,
Absent from the skeletal Eridon Application is, among other things, any discussion of numerous components of a satisfactory countermeasures system. No comprehensive trigger and activation system (TAS) is described, for example, and the sole identifications of a “human interface” in the Eridon Application are a block in the diagram of its
The present invention seeks to supply multiple novel components and techniques for creating active countermeasures systems deployable under a wide variety of hostile and other conditions. An exemplary TAS may, for example, comprise any or all of a first responder unit (FRU), a control display assembly (CDA), processors, sensors, and an electronic safe and arm device (ESAD). Each component assembly may be incorporated into a line replaceable unit (LRU) if desired, although such incorporation is not necessary.
Together with appropriate countermeasures, the TAS may be used to protect crew members of a vehicle from injury or death caused by, for example, IED or mine blasts or vehicle collisions or rollovers. Systems of the invention additionally may record event or damage information (for maintenance, evaluation, or otherwise) or transmit it remotely to alert other vehicles or headquarters operations of impending danger. The Global Positioning System (GPS) or any other suitable locator system may be used in connection with the invention.
The FRU is configured to allow personnel outside a vehicle to disable the countermeasures of the vehicle when appropriate to do so. Should personnel within the vehicle be injured or trapped, for example, first responders may need to breach the vehicle hull or otherwise attempt to enter the vehicle for rescue purposes. Because in some cases these actions could risk activation of any undeployed countermeasures, to avoid further risk to life and property first responders desirably may disable the countermeasures before acting. Preferably (although not necessarily) at least one FRU is mounted near the front or rear of the vehicle so as to be accessed externally thereof; a locking cover or other structure may be provided to reduce the possibility of inadvertent or improper disabling of the countermeasures.
The CDA is intended to allow crew of a vehicle to monitor and control status of the countermeasures systems. It preferably provides visual indication of system status, although aural, tactile, or other status indications may be provided alternatively or additionally. Equally preferably, the CDA comprises multiple switches necessarily operated in certain sequences and at certain time intervals to reduce risk of unintended arming or disarming of the countermeasures by the vehicle crew. The switches, further, beneficially may have differing actuating mechanisms, although such differing mechanisms are not required.
One or more processors may be utilized as part of each countermeasures system of the present invention. Preferably the processors are dual-core, allowing for parallel processing to occur. Data buses may transfer signals to and from the processors, which also may communicate electrically with a system interface chip (integrated circuit). Processors may control, provide information to, or receive information from, any or all of the FRU, CDA, and ESAD, vehicle sensors, and vehicle safety equipment such as airbags, active seat controls, intelligent clothing, seatbelt pretensioners, etc.
Sensors associated with the present invention may sense any or all of pressure, angular movement rate, acceleration, strain (deformation), force, displacement, velocity, or electric or magnetic field strength. Because the sensors may be deployed in electrically-noisy environments, signals from the sensors may be encoded using, for example, Manchester coding principles. Preferably, multiple sensors are used on each vehicle, with at least some not co-located with others. If desired, countermeasures deployment may be conditioned on certain signal types and durations being received from multiple non-co-located sensors.
The ESAD functions to arm and initiate countermeasures upon command of a processor. Like various other aspects of the inventive systems, the ESAD preferably “fails safe”—i.e. if it is non-functional, it enters or reverts to a mode in which countermeasures cannot activate. Fuze cord or any other suitable material may connect the ESAD to the countermeasures.
Countermeasures themselves may be of varying types yet remain consistent with the present invention. Advantageously, however, countermeasures may include cartridges into which ejectable masses and charges are loaded. Currently preferred ejectable masses are predominantly solids (as opposed to liquids or gases), with preferred solids either being disintegrable or comprising multiplicities of disintegrated particles. If so, the likelihood of serious injury to a bystander impacted by a portion of the ejected mass may be reduced.
Cartridge countermeasures may be placed in barrels mounted to or otherwise connected or attached to vehicles. The barrels may be constructed in sets or individually as desired and configured to receive cartridges in any manner allowing initiation of the propellant. In some versions of the invention, banks of barrels are mounted at the four corners of the roof of a vehicle. Alternatively or additionally, barrels may be mounted on vehicle sides, fronts, or rears. Presently preferred in some versions is that barrels not be placed on the vehicle undercarriage, although such placement could occur in other versions. Because the cartridges are separate from the barrels, the cartridges may be transported apart from the barrels and loaded only when needed, further reducing risk of undesired countermeasure deployment.
It thus is an optional, non-exclusive object of the present invention to provide systems and methods for countering at least certain undesired forces acting on a vehicle.
It is another optional, non-exclusive object of the present invention to provide systems and methods for devising countermeasures systems deployable under a wide variety of conditions.
It is also an optional, non-exclusive object of the present invention to provide systems and methods incorporating some or all of an FRU, a CDA, processors, sensors, and an ESAD, any of which may be incorporated into an LRU.
Numerous other objects, feature, and advantages of the present invention will be apparent to those skilled in relevant fields with reference to the remaining text and the drawings of this application.
Depicted in
As illustrated in
FRU 14 beneficially may include a box housing switch 38 and be either attached to or integrated into a hull of a vehicle so as to be accessible externally thereof. Alternatively, FRU 14 may comprise a cover for switch 38 or any other object or assembly configured to restrict access to the switch 38. In at least some embodiments of the invention, FRU 14 will be locked, limiting access to switch 38 to those possessing an appropriate unlocking key or tool or knowing a suitable combination of symbols.
In particular, first responders to an accident or catastrophe involving the vehicle may need to breach its hull or otherwise enter its interior so as to rescue personnel or equipment contained therein. Entry activities of these first responders, or other actions impacting the vehicle, could risk activation of as-yet undeployed countermeasures 34. Accordingly, the first responders may desire to access and open switch 38 upon arrival at the vehicle so as to reduce the possibility of countermeasures 34 deployed undesirably. Of course, persons skilled in appropriate fields of endeavor will recognize that FRU 14 is optional and in certain circumstances either may be omitted from TAS 10 or configured otherwise as described herein.
CDA 18 appears in
CDA 18 functions to, among other things, allow crew of a vehicle to control and monitor status of TAS 10. CDA 18 preferably is positioned in a dashboard of a vehicle with its face 54 visible to the crew and may, for example, include power switch 58 and an associated visual indicator 62. Also depicted in
In at least some versions of the invention, and assuming switch 38 is closed, TAS 10 may be initialized by closing power switch 58 (shown in
During the POST, bit status indicators 82 preferably flash in an orange hue. Successful completion of the POST causes bit status indicators 82 to remain illuminated for a brief period (e.g. one second) and then darken if all LRUs are deemed to be operating normally. By contrast, if an LRU fails the POST, its corresponding bit status indicator 82 will remain illuminated. Further, if any failure constitutes a safety-critical system fault, TAS 10 will enter a “fail safe” mode, and any attempt to recover from such a mode will, at minimum, require power switch 58 to be toggled off and then back on.
Following successful completion of the POST, respective arm power and arm enable switches 58 and 74 may become active. Arm power switch 58 preferably is a momentary switch; to initiate arming of countermeasures 34, an operator toggles the switch 58 and releases it. Under normal operation and proper sequencing, indicator 70 illuminates in a yellow hue.
One proper sequencing technique requires crew manipulation of arm enable switch 74 to occur within a defined time period following toggling and release of arm power switch 58. Such a defined time period may, for example, be between approximately 0.5-6.0 seconds. If switch 74 is not manipulated within the period, indicator 70 will de-illuminate and arm power switch 58 will deactivate, necessitating re-toggling and release of switch 58 to re-start the sequence. By contrast, if cover 86 is moved and switch 74 is manipulated within the period, indicator 78 illuminates and TAS 10 enters an “arm enable” mode.
With TAS 10 in this “arm enable” mode, processor 22 controls deployment of countermeasures 34 (unless switch 38 or 58 is opened). Processor 22 directly or indirectly receives signals from sensors 26 and determines if deployment of any countermeasure 34 is appropriate. If deployment is appropriate, processor 22 signals ESAD 30. In some versions of the invention, processor 22 may be housed in an enclosure having deformable brackets so as to allow dampening of shocks otherwise likely experienced by the processor 22.
Presently-preferred masses 94 are predominantly solids (rather than liquids or gases). Such preferred solids either are disintegrable upon ejection from the vehicle or comprise multiplicities of disintegrated particles. Disintegration of mass 94 upon deployment of countermeasures 34 is preferred so as to reduce likelihood of serious injury to at least some bystanders possibly impacted by mass 94.
Charge 98 may be or include any propellant or other substance capable of causing a countermeasure 34 to eject from a vehicle. Upon receipt of a suitable signal from processor 22, ESAD 30 activates initiator 102, which in turn ignites detonation cord 106 connected to a countermeasure 34. Detonation of cord 106 causes deflagration (if pyrotechnic) or other activation of charge 98 so as to eject mass 94 from the vehicle. A single initiator 102 may be employed to launch any number of countermeasures 34; alternatively, each countermeasure 34 may be associated with a separate initiator 102. To expedite initiation, capacitors associated with initiator 102 may be pre-charged under certain conditions.
Depending on the locations and types of forces encountered by sensors 26, any one or more banks 110 may launch countermeasures 34. Moreover, if a bank 110 includes more than one barrel 114, less than all countermeasures 34 loaded in the barrels 114 may be launched at any particular time. Launching of countermeasures 34 further may be staggered or sequenced in time (either within a particular bank 110 or between particular banks 110).
Presently preferred is that barrels 114 be vertical (or substantially so) with their openings 118 positioned upward when mounted to a vehicle. In this manner, a countermeasure 34 will be ejected upward from the vehicle upon deployment, producing a downward force vector upon ejection. Such downward force vector is intended to counteract (in whole or in part) an upward force impacting a vehicle because of, e.g., explosion of a mine or IED, collision of the vehicle with an object, or departure of the vehicle from a roadway or other normal travel surface.
Alternatively, one or more barrels 114 could be tilted or otherwise repositionable relative to a (nominal) vertical orientation. If so, deployment of materials loaded therein could be used to establish different force vectors acting on a vehicle, or the barrels 114 (regardless of orientation) could be used to deploy flares, missiles, projectiles, or other objects for various purposes. Because banks 110 themselves may have substantial mass, they may function as armor for a vehicle. Reactive armor plates or tiles may be deployed, as may any mass associated with a vehicle (e.g. engine, engine cover, battery, water supply, passive armor, etc.).
TAS 10 may be modular, scalable, and configured to be adapted for use with a variety of vehicles or other objects. Sensors 26 may sense such things as changes in acceleration, pressure, strain (deformation), force, displacement, infrared (IR) signals, radio frequency (RF) signals, acoustic signals, electric or magnetic field strength, or RADAR or LIDAR signals. Those skilled in the art will recognize that other signals, events, or changes may be sensed alternatively or additionally. However, presently preferred as sensors 26 are accelerometers augmented by either or both of strain and force sensors. At least some sensors 26 preferably are housed in enclosures mounted to or integrated into areas of a vehicle such as its A/B/C/D pillars or drivetrain tunnel or in other stiff (rigid) structural locations.
Data from sensors 26 may be filtered or encoded (or both) to reduce noise or other incorrect information being received by processor 22. Some versions of TAS 10 further contemplate comparing information from at least two non-co-located sensors 26 as part of an assessment of the validity and location of a blast or other event.
The foregoing is provided for purposes of illustrating, explaining, and describing embodiments of the present invention. Modifications and adaptations to these embodiments will be apparent to those skilled in the art and may be made without departing from the scope or spirit of the invention.
This application claims the benefit of (1) U.S. Provisional Patent Application Ser. No. 61/689,468, filed Jun. 6, 2012, and entitled “Physical Design Criteria for Active Blast Countermeasure System” and (2) U.S. Provisional Patent Application Ser. No. 61/689,471, filed Jun. 6, 2012, and entitled “Active Blast Countermeasure System,” the entire contents of both of which applications are incorporated herein by this reference.
Number | Name | Date | Kind |
---|---|---|---|
3580354 | Hewitt | May 1971 | A |
3995656 | Mills, Jr. | Dec 1976 | A |
4573396 | Streetman et al. | Mar 1986 | A |
5012721 | Medin et al. | May 1991 | A |
5401055 | Pham | Mar 1995 | A |
5765783 | Albion | Jun 1998 | A |
5931499 | Sutherland | Aug 1999 | A |
6065558 | Wielenga | May 2000 | A |
6095459 | Codina | Aug 2000 | A |
6170847 | Pham | Jan 2001 | B1 |
6394738 | Springer | May 2002 | B1 |
6556908 | Lu et al. | Apr 2003 | B1 |
6588799 | Sanchez | Jul 2003 | B1 |
6938924 | Feldman et al. | Sep 2005 | B2 |
7494153 | Wang | Feb 2009 | B2 |
20040200347 | Grosch | Oct 2004 | A1 |
20050230176 | Wang | Oct 2005 | A1 |
20060027419 | Ponomarev et al. | Feb 2006 | A1 |
20060086243 | Seo et al. | Apr 2006 | A1 |
20070144337 | Zhang et al. | Jun 2007 | A1 |
20080216699 | McAleer et al. | Sep 2008 | A1 |
20110245994 | Sloman | Oct 2011 | A1 |
20120239247 | Eridon | Sep 2012 | A1 |
20130204496 | Sloman | Aug 2013 | A1 |
Number | Date | Country |
---|---|---|
2031658 | Jul 1979 | DE |
3118377 | Jun 1982 | DE |
2822106 | Aug 1996 | DE |
19631715 | Jan 2000 | DE |
19832662 | Feb 2000 | DE |
19913845 | Jun 2002 | DE |
10259918 | Jul 2004 | DE |
10317314 | Jul 2004 | DE |
10259918 | Jun 2005 | DE |
202005006655 | Aug 2005 | DE |
19909905 | Jul 2009 | DE |
1382932 | Jan 2004 | EP |
1467171 | Oct 2004 | EP |
1605225 | Dec 2005 | EP |
1698850 | Sep 2006 | EP |
1746379 | Jan 2007 | EP |
1790938 | May 2007 | EP |
2003418 | Dec 2008 | EP |
2362177 | Aug 2011 | EP |
2907206 | Apr 2008 | FR |
2003127462 | Mar 2005 | RU |
0239048 | May 2002 | WO |
2004106840 | Dec 2004 | WO |
2005113330 | Dec 2005 | WO |
2006034528 | Apr 2006 | WO |
2008063205 | May 2008 | WO |
2009114172 | Sep 2009 | WO |
2009117648 | Sep 2009 | WO |
2010067093 | Jun 2010 | WO |
2011148118 | Dec 2011 | WO |
2011148118 | Dec 2011 | WO |
2012035282 | Mar 2012 | WO |
2012052768 | Apr 2012 | WO |
2012085138 | Jun 2012 | WO |
2014039126 | Mar 2014 | WO |
Entry |
---|
International Preliminary Report on Patentability dated Dec. 18, 2014 in Application No. PCT/US2013/044024. |
PCT/US2013/044024, International Search Report and Written Opinion dated Apr. 2, 2014, 10 pages. |
DARPA: “Persistent Stare Exploitation and Analysis System (PerSEAS),” Federal Business Opportunities, Sep. 18, 2009 (3 pages). |
Number | Date | Country | |
---|---|---|---|
20150251616 A1 | Sep 2015 | US |
Number | Date | Country | |
---|---|---|---|
61689468 | Jun 2012 | US | |
61689471 | Jun 2012 | US |