US20080053300A1 - Gun Mount - Google Patents
Gun Mount Download PDFInfo
- Publication number
- US20080053300A1 US20080053300A1 US11/569,967 US56996705A US2008053300A1 US 20080053300 A1 US20080053300 A1 US 20080053300A1 US 56996705 A US56996705 A US 56996705A US 2008053300 A1 US2008053300 A1 US 2008053300A1
- Authority
- US
- United States
- Prior art keywords
- weapon
- mount
- folding
- vehicle
- threaded shaft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000010304 firing Methods 0.000 claims description 15
- 238000000034 method Methods 0.000 claims 1
- 230000007246 mechanism Effects 0.000 description 5
- 239000000969 carrier Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
- F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns
Definitions
- the present invention is in the field of mounts for weapons. More specifically the invention relates to vehicle mounting of guns, light cannons and missiles.
- Typical combat vehicles are personnel carriers and armoured personnel carriers.
- weapons mounted on combat vehicles such weapons are rocket launchers machine guns of various types, light cannons, grenade launchers etc.
- Crew carriers such as armoured crew carriers are often required to be transported to sites of action. Actual transport may be effected by boarding the vehicle on a carrier boat or a pane. In such case it may be beneficial to lower the profile of the vehicle and external mount.
- U.S. Pat. No. 5,056,409 a turret for mounting weapons an a carrier vehicle deck is disclosed, in which the mount is easily convertible from a prostrate to upright position, in which the weapon mounted is easily controlled by crewmen.
- FIG. 1A is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in a prostrate position;
- FIG. 1B is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in an upright position;
- FIG. 1C is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in an upright position, with gun pointing upwards;
- FIG. 2A is a schematic isometric view of gun mounted in a mount of the invention.
- FIG. 2B is a schematic isometric view of gun as in FIG. 2A , with legs separated by the action of threaded shaft.
- FIG. 3 is a schematic isometric view of a gun mounted in a receptacle integrated in the upper axis of the mount in a prostrate configuration;
- FIG. 4 is a schematic isometric view of a gun mounted in a mount of the invention with two guide bars and two threaded shafts;
- FIG. 5 is a schematic isometric view of a gun mounted in a mount of the invention demonstrating the rotation mechanisms of aim control.
- FIG. 6 is a schematic description of the sources of geometric variability defining the position of the weapon in a mount of the invention.
- a weapon such as a machine gun, a missile launcher, a light cannon, a medium cannon or a combination thereof, is installed in a configurable mount.
- the folding weapon mount of the invention is capable of changing configuration.
- the folding weapon mount (FWM) 20 supported by turret 22 forms a part of the payload of armoured vehicle 24 . It is set to a full prostrate configuration, in which gun 26 is at its lowest available position.
- FIG. 1B mount has been contracted in order to raise the gun 26 well above the surface of the armoured vehicle's deck on which it is installed.
- FIG. 1A the folding weapon mount (FWM) 20 , supported by turret 22 forms a part of the payload of armoured vehicle 24 . It is set to a full prostrate configuration, in which gun 26 is at its lowest available position.
- FIG. 1B mount has been contracted in order to raise the gun 26 well above the surface of the armoured vehicle's deck on which it is installed.
- the gun 26 is tilted pointing upwards to a very high elevation angle around a pivot 28 .
- This high elevation angle allows for large super-elevation angles or for firing at high angle targets to be achieved.
- the FWM of the invention uses a screw thread as the driving mechanism of contracting the legs as is described schematically in FIGS. 2A-2B to which reference is now made.
- gun 40 is supported by a support 41 mounted on the weapon bearing cross bar (WBCB) 42 .
- Leg 44 is set at an angle with leg 46 , such that the legs are separated at a distance 48 at the bottom. The distance is kept by virtue of thread shaft 50 .
- Shaft 50 is rotatable by virtue of the coupling to electric motor 52 .
- FIG. 2B the shaft 50 has rotated such that the distance 48 has increased.
- Legs 44 and 46 sustaining the WBCB have separated by rotating around pivot 52 being coaxial with WBCB 42 .
- the contraction mechanism is explained further with reference to FIG.
- Gun 70 is installed in receptacle 72 , typically referred to as a cradle.
- Threaded shaft 74 has a journal at one end inserted in cylindrical bearing 76 whereas at the other end, the threaded shaft 74 is inserted in threaded cylinder 78 .
- the rotation of threaded shaft 74 causes legs 80 and 82 either to spread apart or contract, changing angle a correspondingly. In this prostrate position, the gun and mount installed on an armoured carrier vehicle is more easily loaded in a carrier platform, such as an air carrier or a ferryboat.
- gun 92 is shown, installed in a receptacle 94 on a mount manufactured in accordance with a preferred embodiment of the invention.
- Two aligning beams 96 are disposed connecting between the front lower axis 98 and rear lower axis 100 .
- Threaded shafts 102 are inserted as journals in to respective cylindrical bearings 104 .
- An upper axis of the mount (the WBCB) has a pivot extension 106 for coupling to an electric actuator (not shown).
- the entire construction and mounted gun are installed on a turret 108 .
- the front lower axis 98 is fixed to the turret or to the deck of the carrying vehicle, for example by a bolt 110 .
- the threaded shafts can be rotated by electric or mechanical actuators or manually, for example, by the use of a wrench.
- the actuator is connected permanently to the threaded shafts, in such a case, the folding state of the mount can be changed at any time, unless a specific configuration becomes fixed.
- provisions are made to install more than one weapon on the same mount, for example rocket launchers and a heavy machine gun.
- the FWM and weapons installed therein are completely controllable from inside the carrying vehicle.
- the crew may be concealed inside the vehicle and yet completely control the activity of the weapon and FWM by remote control mechanism.
- the actuators governing the horizontal angle and vertical angle of the weapon are fully controlled from inside the carrier.
- target acquisition and firing control is also provided through an electronic control system.
- FIG. 6 a scheme shows the sources of information fed into and integrated by firing control system 128 .
- the configurational and positioning data of the FWM utilized is typically inclination angle 130 , horizontal angle 132 and folding state 136 .
- the firing control system is able to calculate at any state the required parameter associated with the acquisition of a target.
- Another input apparatus advantageously applied to such a mount is a range finder 138 , the output of which can be fed automatically to the firing control system.
- the elevation angle required could be different for different folding states.
- Information related to the state of the FWM can be obtained from sensors attached or associated with the FWM, for example a north finding device can serve as a horizontal angle source, an inclinometer can serve as inclination data source.
- a relative position of the FWM with respect to the carrying vehicle is obtained by using angular sensors of the resolver type.
- the data of such sensors is accurate and reliable.
- the firing control system is digital, requiring that all position data obtained from the sensors is digitized prior to sending to the firing control system.
- the firing control system can be programmed to include information regarding safety zones, in which firing of the mounted weapons is prohibited.
- the firing control system feeds positioning control signals to the set of actuators 140 regulating the configuration of the FWM and the weapon, in order to bring the whole system to a position such that the target is aimed at properly, taking in consideration proper elevation angle and prohibited zones.
- the use of a mount of the invention adds an additional degree of freedom to the firing control system.
- the elevation angle computed for a specific target relates to not only to the static positioning of the weapon relative to a deck of the carrier vehicle, but also of the instantaneous folding state o the FWM.
- the benefit is especially noticeable in built up areas in which the buildings and other artifacts aimed at or obstructing the line of sight to a target may be very close to the carrying vehicle, such that the folding state affect the actual capability of sighing a specific target or otherwise have an appreciable effect on the firing angle by changing the distance of the weapon from the deck of the carrier vehicle vertically.
- the FWM may be folded down to reduce the profile of the crew carrier harboring the FWM, thus decreasing the chances of exposure.
- the folding mechanism of the instant invention based on a threaded shaft is very robust and can be used to raise or lower light to relatively heavy weapons either manually or mechanically by the use of an actuator. If the actuator as in some embodiment is an electric motor, actuation can be controlled remotely and even during travel or even battle.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
A folding weapon mount installed on the deck of a carrier vehicle. In one folding configuration the profile of the vehicle, mount and mounted weapon is lowest with respect to the profile obtained in an upright configuration. The folding is achieved by the rotation of a threaded shaft which changes the distance between two parallel lower axes. Appropriate legs pivotally respectively connect each lower axis to one parallel upper axis serving also as a weapon bearing cross bar.
Description
- The present invention is in the field of mounts for weapons. More specifically the invention relates to vehicle mounting of guns, light cannons and missiles.
- Mounting of weapons on vehicles is implemented in cases in which the vehicle is to take part in combat or defensive activity. Typical combat vehicles are personnel carriers and armoured personnel carriers. In the art there are several types of weapons mounted on combat vehicles, such weapons are rocket launchers machine guns of various types, light cannons, grenade launchers etc. Crew carriers such as armoured crew carriers are often required to be transported to sites of action. Actual transport may be effected by boarding the vehicle on a carrier boat or a pane. In such case it may be beneficial to lower the profile of the vehicle and external mount. In U.S. Pat. No. 5,056,409 a turret for mounting weapons an a carrier vehicle deck is disclosed, in which the mount is easily convertible from a prostrate to upright position, in which the weapon mounted is easily controlled by crewmen.
-
FIG. 1A is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in a prostrate position; -
FIG. 1B is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in an upright position; -
FIG. 1C is a schematic side view of an armoured carrier on which a mounted gun is installed in accordance with the present invention, configured in an upright position, with gun pointing upwards; -
FIG. 2A is a schematic isometric view of gun mounted in a mount of the invention; -
FIG. 2B is a schematic isometric view of gun as inFIG. 2A , with legs separated by the action of threaded shaft. -
FIG. 3 is a schematic isometric view of a gun mounted in a receptacle integrated in the upper axis of the mount in a prostrate configuration; -
FIG. 4 is a schematic isometric view of a gun mounted in a mount of the invention with two guide bars and two threaded shafts; -
FIG. 5 is a schematic isometric view of a gun mounted in a mount of the invention demonstrating the rotation mechanisms of aim control. -
FIG. 6 is a schematic description of the sources of geometric variability defining the position of the weapon in a mount of the invention. - In accordance with the present invention, a weapon such as a machine gun, a missile launcher, a light cannon, a medium cannon or a combination thereof, is installed in a configurable mount. As described schematically in FIGS. 1A-C to which reference is now made, the folding weapon mount of the invention is capable of changing configuration. In
FIG. 1A , the folding weapon mount (FWM) 20, supported byturret 22 forms a part of the payload ofarmoured vehicle 24. It is set to a full prostrate configuration, in whichgun 26 is at its lowest available position. InFIG. 1B mount has been contracted in order to raise thegun 26 well above the surface of the armoured vehicle's deck on which it is installed. InFIG. 1C , a particular aspect of the invention is demonstrated schematically. According to this aspect, thegun 26 is tilted pointing upwards to a very high elevation angle around apivot 28. This high elevation angle, allows for large super-elevation angles or for firing at high angle targets to be achieved. - The FWM of the invention uses a screw thread as the driving mechanism of contracting the legs as is described schematically in
FIGS. 2A-2B to which reference is now made. As can be seen inFIG. 2A ,gun 40 is supported by asupport 41 mounted on the weapon bearing cross bar (WBCB) 42.Leg 44 is set at an angle withleg 46, such that the legs are separated at adistance 48 at the bottom. The distance is kept by virtue ofthread shaft 50. Shaft 50 is rotatable by virtue of the coupling toelectric motor 52. InFIG. 2B theshaft 50 has rotated such that thedistance 48 has increased.Legs pivot 52 being coaxial withWBCB 42. The contraction mechanism is explained further with reference toFIG. 3 . Gun 70 is installed inreceptacle 72, typically referred to as a cradle. Threadedshaft 74 has a journal at one end inserted incylindrical bearing 76 whereas at the other end, the threadedshaft 74 is inserted in threadedcylinder 78. The rotation of threadedshaft 74 causeslegs - In
FIG. 4 to which reference is now made,gun 92 is shown, installed in areceptacle 94 on a mount manufactured in accordance with a preferred embodiment of the invention. Two aligningbeams 96 are disposed connecting between the frontlower axis 98 and rearlower axis 100. Threadedshafts 102 are inserted as journals in to respectivecylindrical bearings 104. An upper axis of the mount (the WBCB) has apivot extension 106 for coupling to an electric actuator (not shown). The entire construction and mounted gun are installed on aturret 108. In some embodiment of the invention the frontlower axis 98 is fixed to the turret or to the deck of the carrying vehicle, for example by abolt 110. The threaded shafts can be rotated by electric or mechanical actuators or manually, for example, by the use of a wrench. In some embodiments the actuator is connected permanently to the threaded shafts, in such a case, the folding state of the mount can be changed at any time, unless a specific configuration becomes fixed. In some embodiments provisions are made to install more than one weapon on the same mount, for example rocket launchers and a heavy machine gun. - In
FIG. 5 to which reference is now made, the vertical angle of rotation provided by the turret is described by double headedarrow 120. Rotating of the weapon around thehorizontal axis 122 is carried out preferably by the action of an actuator (not shown) linked to pivotextension 124 of theWBCB 122. - Firing Control and Crew Safety
- In a preferred embodiment of the invention the FWM and weapons installed therein are completely controllable from inside the carrying vehicle. The crew may be concealed inside the vehicle and yet completely control the activity of the weapon and FWM by remote control mechanism. Thus, the actuators governing the horizontal angle and vertical angle of the weapon are fully controlled from inside the carrier. In another aspect of the invention, target acquisition and firing control is also provided through an electronic control system.
- In
FIG. 6 to which reference is now made, a scheme shows the sources of information fed into and integrated by firingcontrol system 128. The configurational and positioning data of the FWM utilized is typicallyinclination angle 130,horizontal angle 132 andfolding state 136. As a consequence, the firing control system is able to calculate at any state the required parameter associated with the acquisition of a target. Another input apparatus advantageously applied to such a mount is arange finder 138, the output of which can be fed automatically to the firing control system. Thus for a specific folding state, the elevation angle required could be different for different folding states. Information related to the state of the FWM can be obtained from sensors attached or associated with the FWM, for example a north finding device can serve as a horizontal angle source, an inclinometer can serve as inclination data source. In a preferred embodiment of the present invention, a relative position of the FWM with respect to the carrying vehicle is obtained by using angular sensors of the resolver type. The data of such sensors is accurate and reliable. Advantageously, the firing control system is digital, requiring that all position data obtained from the sensors is digitized prior to sending to the firing control system. The firing control system can be programmed to include information regarding safety zones, in which firing of the mounted weapons is prohibited. The firing control system feeds positioning control signals to the set ofactuators 140 regulating the configuration of the FWM and the weapon, in order to bring the whole system to a position such that the target is aimed at properly, taking in consideration proper elevation angle and prohibited zones. - Benefits of a Mount Embodying the Invention
- As described above, the use of a mount of the invention adds an additional degree of freedom to the firing control system. Thus the elevation angle computed for a specific target relates to not only to the static positioning of the weapon relative to a deck of the carrier vehicle, but also of the instantaneous folding state o the FWM. The benefit is especially noticeable in built up areas in which the buildings and other artifacts aimed at or obstructing the line of sight to a target may be very close to the carrying vehicle, such that the folding state affect the actual capability of sighing a specific target or otherwise have an appreciable effect on the firing angle by changing the distance of the weapon from the deck of the carrier vehicle vertically. In open areas, the FWM may be folded down to reduce the profile of the crew carrier harboring the FWM, thus decreasing the chances of exposure.
- The folding mechanism of the instant invention based on a threaded shaft is very robust and can be used to raise or lower light to relatively heavy weapons either manually or mechanically by the use of an actuator. If the actuator as in some embodiment is an electric motor, actuation can be controlled remotely and even during travel or even battle.
Claims (5)
1. A folding weapon mount for bearing at least one weapon, wherein said mount is installed on the deck of a carrier vehicle such that in one configuration the profile of the vehicle and mount and mounted weapon is low with respect to the profile obtained in an upright configuration of said mount, said mount comprising:
parallel front and a rear lower axes;
an upper axis serving as a weapon bearing cross-bar;
a weapon support connected with said upper axis,
at least one threaded shaft for changing the distance between said lower axes, and
legs connected to said lower axes for sustaining said weapon bearing cross-bar.
2. A folding weapon mount as in claim 1 and wherein said at least one threaded shaft is connected to a mechanical actuator.
3. A folding weapon mount as in claim 2 and wherein said actuator is an electric motor.
4. A method for changing the distance of at least one weapon from the deck of the carrier vehicle vertically, wherein a folding weapon mount supports said at least one weapon, and wherein a weapon bearing cross-bar of said mount is lowered and raised by the rotation of at least one threaded shaft.
5. A folding weapon mount for bearing at least one weapon on a carrier vehicle, wherein a firing control system thereof collects information related to at least one of the group containing distance from target, weapon inclination, horizontal weapon angle and folding state of said folding mount, and wherein said firing control system calculates angular parameters which are fed to a set of actuators to regulate the configuration of the folding weapon mount and the weapon.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL16233604A IL162336A0 (en) | 2004-06-03 | 2004-06-03 | Gun mount |
IL162336 | 2004-06-03 | ||
PCT/IL2005/000583 WO2005118295A2 (en) | 2004-06-03 | 2005-06-02 | Gun mount |
Publications (1)
Publication Number | Publication Date |
---|---|
US20080053300A1 true US20080053300A1 (en) | 2008-03-06 |
Family
ID=35463405
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/569,967 Abandoned US20080053300A1 (en) | 2004-06-03 | 2005-06-02 | Gun Mount |
Country Status (3)
Country | Link |
---|---|
US (1) | US20080053300A1 (en) |
IL (1) | IL162336A0 (en) |
WO (1) | WO2005118295A2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080105481A1 (en) * | 2006-11-02 | 2008-05-08 | Hutcheson Timothy L | Reconfigurable balancing robot and method for dynamically transitioning between statically stable mode and dynamically balanced mode |
US20080121097A1 (en) * | 2001-12-14 | 2008-05-29 | Irobot Corporation | Remote digital firing system |
US8109191B1 (en) | 2001-12-14 | 2012-02-07 | Irobot Corporation | Remote digital firing system |
US20130306814A1 (en) * | 2010-09-29 | 2013-11-21 | Jeffrey T. Shimmel | Portable equipment system mount |
RU2527595C1 (en) * | 2013-04-26 | 2014-09-10 | Открытое акционерное общество "Завод им. В.А. Дегтярева" | Combat employment of remote-control weapon mobile complex |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITTO20080371A1 (en) | 2008-05-19 | 2009-11-20 | Alenia Aeronautica Spa | TOWER, PARTICULARLY FOR PROTECTED MILITARY VEHICLE, WITH SUPPORT STRUCTURE FOR FIRE WEAPON. |
IL200036A (en) | 2009-07-23 | 2015-02-26 | Rafael Advanced Defense Sys | System and method for protected reloading of a remote controlled weapon station |
IL209195A (en) | 2010-11-08 | 2014-09-30 | Rafael Advanced Defense Sys | Turret assembly |
SA115360300B1 (en) | 2014-02-14 | 2017-08-29 | ميريل افياشين، انك. | Modular weapon station system |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2366642A (en) * | 1940-03-19 | 1945-01-02 | Motley Lewis | Gun mounting |
US4141277A (en) * | 1977-02-11 | 1979-02-27 | Creusot-Loire | Installation for launching missiles |
US4282794A (en) * | 1979-04-30 | 1981-08-11 | Miller Avy L | Self-propelled off-road vehicle |
US4667565A (en) * | 1984-12-14 | 1987-05-26 | Tetradyne Corporation | Rapid response patrol and antiterrorist vehicle |
US4721026A (en) * | 1986-03-17 | 1988-01-26 | Esperanza Y Cia, S.A. | Mortar |
US5617666A (en) * | 1995-08-15 | 1997-04-08 | Scott; Dewey L. | Firearm rest |
US5937561A (en) * | 1998-03-25 | 1999-08-17 | Abernethy; Steve T. | Firearm bench rest |
US6907812B1 (en) * | 2003-01-21 | 2005-06-21 | United Defense Lp | Pop-up weapon system |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1939699A (en) * | 1931-11-30 | 1933-12-19 | Clarence F Hofstetter | Gun mount |
US5347910A (en) * | 1985-10-15 | 1994-09-20 | The Boeing Company | Target acquisition system |
US5129308A (en) * | 1989-03-21 | 1992-07-14 | Fuereder Georg F | Combat vehicle with extendible combat platform |
US6237462B1 (en) * | 1998-05-21 | 2001-05-29 | Tactical Telepresent Technolgies, Inc. | Portable telepresent aiming system |
US6584881B1 (en) * | 2001-03-26 | 2003-07-01 | United Defense Lp | Multi-purpose missile launcher system for a military land vehicle |
-
2004
- 2004-06-03 IL IL16233604A patent/IL162336A0/en unknown
-
2005
- 2005-06-02 US US11/569,967 patent/US20080053300A1/en not_active Abandoned
- 2005-06-02 WO PCT/IL2005/000583 patent/WO2005118295A2/en active Application Filing
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2366642A (en) * | 1940-03-19 | 1945-01-02 | Motley Lewis | Gun mounting |
US4141277A (en) * | 1977-02-11 | 1979-02-27 | Creusot-Loire | Installation for launching missiles |
US4282794A (en) * | 1979-04-30 | 1981-08-11 | Miller Avy L | Self-propelled off-road vehicle |
US4667565A (en) * | 1984-12-14 | 1987-05-26 | Tetradyne Corporation | Rapid response patrol and antiterrorist vehicle |
US4721026A (en) * | 1986-03-17 | 1988-01-26 | Esperanza Y Cia, S.A. | Mortar |
US5617666A (en) * | 1995-08-15 | 1997-04-08 | Scott; Dewey L. | Firearm rest |
US5937561A (en) * | 1998-03-25 | 1999-08-17 | Abernethy; Steve T. | Firearm bench rest |
US6907812B1 (en) * | 2003-01-21 | 2005-06-21 | United Defense Lp | Pop-up weapon system |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080121097A1 (en) * | 2001-12-14 | 2008-05-29 | Irobot Corporation | Remote digital firing system |
US8109191B1 (en) | 2001-12-14 | 2012-02-07 | Irobot Corporation | Remote digital firing system |
US8375838B2 (en) * | 2001-12-14 | 2013-02-19 | Irobot Corporation | Remote digital firing system |
US20080105481A1 (en) * | 2006-11-02 | 2008-05-08 | Hutcheson Timothy L | Reconfigurable balancing robot and method for dynamically transitioning between statically stable mode and dynamically balanced mode |
US7798264B2 (en) * | 2006-11-02 | 2010-09-21 | Hutcheson Timothy L | Reconfigurable balancing robot and method for dynamically transitioning between statically stable mode and dynamically balanced mode |
US20120016520A1 (en) * | 2006-11-02 | 2012-01-19 | Hutcheson Timothy L | Reconfigurable balancing robot and method for dynamically transitioning between statically stable mode and dynamically balanced mode |
US20130306814A1 (en) * | 2010-09-29 | 2013-11-21 | Jeffrey T. Shimmel | Portable equipment system mount |
US9423069B2 (en) * | 2010-09-29 | 2016-08-23 | The United States Of America As Represented By The Secretary Of The Navy | Portable equipment system mount |
US9752721B2 (en) | 2010-09-29 | 2017-09-05 | The United States Of America As Represented By The Secretary Of The Navy | Portable equipment system mount |
RU2527595C1 (en) * | 2013-04-26 | 2014-09-10 | Открытое акционерное общество "Завод им. В.А. Дегтярева" | Combat employment of remote-control weapon mobile complex |
Also Published As
Publication number | Publication date |
---|---|
WO2005118295A2 (en) | 2005-12-15 |
IL162336A0 (en) | 2005-11-20 |
WO2005118295A3 (en) | 2007-07-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7669513B2 (en) | Multiple weapon system for armored vehicle | |
US8393258B2 (en) | Retractable turret | |
US9523548B2 (en) | Operational control logic for harmonized turret with gimbaled sub-systems | |
US6584881B1 (en) | Multi-purpose missile launcher system for a military land vehicle | |
US10371479B2 (en) | Stabilized integrated commander's weapon station for combat armored vehicle | |
EP1923657B1 (en) | A compact, fully stabilised, four axes, remote weapon station with independent line of sight | |
US8794120B2 (en) | Mortar | |
US10309745B2 (en) | Mobile turret weapon delivery system | |
NO318664B1 (en) | Weapon control system that has weapon stabilization | |
CN103842764A (en) | Remote weapon station, in particular for aircraft, such as fixed-wing aircraft | |
US5992292A (en) | Fire control device for, in particular, transportable air defense systems | |
US11719500B2 (en) | Ammunition launching device | |
US20080053300A1 (en) | Gun Mount | |
ITMI20060668A1 (en) | AUXILIARY STORAGE DEVICE | |
RU142907U1 (en) | ARMOR TRANSPORT DIVISION | |
US4353283A (en) | Firing turret for a vehicle, and vehicle including such a turret | |
EP1671075B1 (en) | Multiple weapon system for an armored vehicle | |
US4346644A (en) | Foldout cradle apparatus for mounting an automatic cannon to a turret exterior | |
DE1800330A1 (en) | Armored vehicle with anti-aircraft armament | |
RU2027974C1 (en) | Tank | |
RU2280225C2 (en) | Gun barrel bore direction monitor | |
CN110887405A (en) | Rocket projectile vehicle-mounted and ground integrated launching vehicle | |
RU2222759C2 (en) | Rocket launcher | |
KR20240173635A (en) | Weapon Aiming System | |
GB2140539A (en) | Sighting means for fighting vehicles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |