子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | QUICK-DETACHABLE MULTI-PURPOSE ACCESSORY MOUNTING PLATFORM | US15995446 | 2018-06-01 | US20180299237A1 | 2018-10-18 | Darrel R. Barnette |
| Accessories may be mounted using a quick-detachable multi-purpose accessory mounting platform. The platform may include one or more clamps to receive an object, such as a firearm. The platform also may include at least one recessed mounting pad, at least one rear shelf, and other surfaces to provide different mounting points for accessories. | ||||||
| 22 | AIR-CONDITIONING AIR DISTRIBUTION DEVICE FOR A VEHICLE TURRET AND VEHICLE COMPRISING SUCH A DEVICE | US15101627 | 2014-11-26 | US20170028809A1 | 2017-02-02 | Jean Luc DUINAT; Patrick VENAILLE; Xavier DESCATOIRE; Marc CLAMAGIRAND |
| A vehicle and its air-conditioning air distribution device for a vehicle turret rotatably mounted with respect to a body of the vehicle. This device includes at least one annular chute coaxial to the axis of rotation of the turret and including at least one first flow orifice, the chute having an annular opening which is concentric thereto, the chute receiving a closing ring which matches with the opening of the chute, the closing ring being rotatable with respect to the chute, and including at least one second air flow orifice, the chute being intended to be made integral with the body, respectively with the turret, while the closing ring is intended to be made integral with the turret, respectively with the body. | ||||||
| 23 | Cannon and Military Vehicle | US14119182 | 2012-05-15 | US20150075358A1 | 2015-03-19 | Matthias Raczek; Jens Koester; Matthias Czok |
| A cannon and a military vehicle having such a cannon, which includes a support, a turret that is rotatable relative to the support and is provided with an opening, and a closure element disposed on the support and configured for the closing off of the opening of the turret. | ||||||
| 24 | Positive locking mechanism for rotating helicopter mount | US13687469 | 2012-11-28 | US08800421B1 | 2014-08-12 | Michael Colonnello |
| An apparatus for rotating and locking a first longitudinal member with respect to a second longitudinal member. One end of the first longitudinal member includes a locking mechanism having a generally arcuate outer surface with a plurality of deep and shallow notches formed therein. The notches correspond to different positions of rotation of the first and second members. One end of the second longitudinal member includes a yoke rotatably connected to the locking mechanism with a pivot pin. A locking plunger in the second longitudinal member engages the notches in the locking mechanism and is translatable between fully locked and fully unlocked positions. In the fully locked position, the first and second members are not rotatable with respect to each other. | ||||||
| 25 | Field gun aim | US13708605 | 2012-12-07 | US08726784B2 | 2014-05-20 | Keith Dawson; Frederick Herbert; John Michael Webb |
| A howitzer suitable for deployment on a ground plane, the howitzer having an ordnance for firing a projectile. The ordnance can include a barrel defining a barrel axis and having a muzzle towards the front end of the howitzer and a breech assembly at the back end of the barrel; a cradle for holding the ordnance at a traverse and an elevation; two trunnion pins located on the cradle, which co-locate with receiving trunnion bearings on a saddle, wherein in a first position said breech is located forward of the trunnion, in a second position, at the end of the recoil stroke, the breech is retracted substantially behind the trunnion, wherein a recoil stroke is variable depending on the selection of the elevation. | ||||||
| 26 | FIELD GUN AIM | US13708605 | 2012-12-07 | US20140102286A1 | 2014-04-17 | Keith DAWSON; Frederick Herbert; John Michael Webb |
| A howitzer suitable for deployment on a ground plane, the howitzer having an ordnance for firing a projectile. The ordnance can include a barrel defining a barrel axis and having a muzzle towards the front end of the howitzer and a breech assembly at the back end of the barrel; a cradle for holding the ordnance at a traverse and an elevation; two trunnion pins located on the cradle, which co-locate with receiving trunnion bearings on a saddle, wherein in a first position said breech is located forward of the trunnion, in a second position, at the end of the recoil stroke, the breech is retracted substantially behind the trunnion, wherein a recoil stroke is variable depending on the selection of the elevation. | ||||||
| 27 | System and method for retrofit mechanism for motorizing a manual turret | US11151190 | 2005-05-31 | US07030579B1 | 2006-04-18 | John J. Schmitz; Paul A. Petrovich; A. David Stormer; Robert G. Washburn |
| A mechanism for retrofitting a turret that has a manual rotation system with a motorized turret rotation system includes a gear box mechanically coupled to the turret, an electrically powered prime mover unit mechanically coupled to the gear box, a user operated control device electrically coupled to the prime mover unit, and an electrical power supply electrically coupled to the prime mover unit. The turret rotates relative to a body structure. The gear box and the prime mover unit are mounted to the body structure. The control device and the electrical power supply are positioned on the turret. The power supply provides electrical power to the prime mover. The control device presents a control signal to the prime mover when the user actuates the control device, and the turret rotates in response to the control signal. | ||||||
| 28 | Aircraft support plank mounting of 30 mm machine guns | US812756 | 1997-03-06 | US5767436A | 1998-06-16 | Paul H. Sanderson; Charles E. Rostocil |
| An elongated support plank structure longitudinally extends transversely through the cabin area of a helicopter and has outer end portions projecting outwardly beyond opposite sides of the helicopter. A pair of 30 mm machine guns are mounted on the plank end portions and are supplied with belted ammunition from magazine boxes mounted on the plank within the cabin area via flexible feed chutes interconnected between the magazine boxes and interiorly rollered feed adapters interconnected between the outer ends of the feed chutes and the inlets of the machine gun feeder mechanisms. The 30 mm machine guns are secured to the outer plank end portions by specially designed mounting structures each having a cradle portion with axis-adjustable roller assemblies that engage the gun and essentially preclude lateral movement thereof relative to the cradle, but permit roller-guided longitudinal gun recoil movement, during firing of the gun. During firing of the gun, the gun moves longitudinally relative to fixed position recoil pin portions of the mounting structure and resiliently transfers its longitudinal recoil and counter recoil forces to such pin portions. Each cradle is gimbal-supported within a mounting structure securable to one of the plank ends, and a bore sight adjustment subassembly is interconnected between the mounting structure and the cradle and is used to pivotally adjust the cradle relative to the mounting structure about two mutually perpendicular axes to thereby adjust the elevation and azimuth bore sight settings of the gun. | ||||||
| 29 | 화기 거치 장치 및 이를 구비한 경계 로봇 | KR1020110024342 | 2011-03-18 | KR1020120106306A | 2012-09-26 | 박인규 |
| PURPOSE: An apparatus for mounting firearm and sentry robot comprising the same are provided to increase the probability of hit by compensating the error caused by wind or the rotation of a bullet in advance. CONSTITUTION: An apparatus for mounting firearm is composed of a frame(100), a picturing unit(200), a tilting base(300), a firearm mount(400), and a driving unit(500). The picturing units are arranged to pictures to be moved vertically in vertical direction. The tilting base is arranged to be rotated vertically. The firearm mount is located to be rotated horizontally and a firearm is mounted on the firearm mount. The driving unit is rotate in the tilting base. | ||||||
| 30 | DISPOSITIF DE DISTRIBUTION D'AIR DE CLIMATISATION POUR UNE TOURELLE D'UN VÉHICULE ET VÉHICULE COMPORTANT UN TEL DISPOSITIF | EP14825396.6 | 2014-11-26 | EP3077235B1 | 2018-01-03 | DUINAT, Jean Luc; VENAILLE, Patrick; DESCATOIRE, Xavier; CLAMAGIRAND, Marc |
| 31 | DISPOSITIF DE DISTRIBUTION D'AIR DE CLIMATISATION POUR UNE TOURELLE D'UN VÉHICULE ET VÉHICULE COMPORTANT UN TEL DISPOSITIF | EP14825396.6 | 2014-11-26 | EP3077235A1 | 2016-10-12 | DUINAT, Jean Luc; VENAILLE, Patrick; DESCATOIRE, Xavier; CLAMAGIRAND, Marc |
| The invention relates to a vehicle and to the air-conditioning air distribution device (10) thereof for a vehicle turret (1) that is rotatably mounted in relation to a vehicle body (80). Said device is characterized in that it comprises at least one annular channel (11) which is coaxial to the rotational axis of the turret and which comprises at least one first flow opening (12a). Said channel (11) comprises an annular opening (14) that is concentric therewith, and said channel (11) receives a sealing ring (13) that corresponds to the opening (14) of the channel. Said ring (13) is capable of turning in relation to the channel (11) and comprises at least one second airflow opening (15). The channel (11) is to be rigidly connected to the body (80) with respect to the turret, while the sealing ring (13) is to be rigidly connected to the turret (1) with respect to the body. | ||||||
| 32 | BELT/METALLIC LINK CHAIN LOADED AMMUNITION FEEDER IN A REMOTE CONTROLLED WEAPON STATION | EP13800475 | 2013-06-03 | EP2856065A4 | 2016-02-10 | CHACHAMIAN SHIMON; HAMISH RAN |
| 33 | BELT/METALLIC LINK CHAIN LOADED AMMUNITION FEEDER IN A REMOTE CONTROLLED WEAPON STATION | EP13800475.9 | 2013-06-03 | EP2856065A1 | 2015-04-08 | CHACHAMIAN, Shimon; HAMISH, Ran |
| Belt/Metallic Link Chain Loaded Ammunition Feeder in a Remote Controlled Weapon Station (RCWS) that comprises feeding mechanism for routing chained ammunition from ammunition reservoir means towards the weapon's bullets entrance opening wherein said feeding mechanism comprises - a first chute assembly for routing chained ammunition from said ammunition reservoir means towards the region of the RCWS's elevating/lowering axis, wherein said first chute assembly is mounted on the RCWS's rotatable turret assembly; and a second chute assembly for continuing routing said chained ammunition from the region of said elevating/lowering axis towards the entry opening of the bullets entrance of the weapon, wherein the second chute is mounted the RCWS's mounting bracket; and wherein the chained ammunition traversing over said elevating/lowering axis region in its passing from the first chute assembly to the second chute assembly happens when said ammunition is directed in an orientation that is at least substantially suited to the direction of said elevating/lowering axis; and at the time that said mounting bracket assembly is propelled to elevating/lowering motion around said elevating/lowering axis, the first chute assembly remains static and the second chute assembly is dynamic and propelled together with said mounting bracket assembly around said elevating/lowering axis. | ||||||
| 34 | VORRICHTUNG UND VERFAHREN ZUR THERMALKOMPENSATION EINES WAFFENROHRES | EP12725763.2 | 2012-06-04 | EP2718657B1 | 2016-05-18 | BRUNNER, Dominic; MEIER, Raffael |
| 35 | GESCHÜTZ UND MILITÄRISCHES FAHRZEUG | EP12769882.7 | 2012-05-15 | EP2710323B1 | 2015-07-29 | RACZEK, Matthias; KÖSTER, Jens; CZOK, Matthias |
| 36 | REMOTE WEAPON STATION, IN PARTICULAR FOR AIRCRAFT, SUCH AS FIXED-WING AIRCRAFT | EP12780803.8 | 2012-09-18 | EP2758740A1 | 2014-07-30 | ISOLA, Andrea; LEONESIO, Gian Battista |
| A remote weapon station (10) includes a firearm (12), which is able to fire ammunitions against a target. A remote control board or panel (14) is arranged at a distance from the firearm (12) and is configured to be activated by an operator, so as to control the firearm (12). An automatic target aiming system (32) is configured to provide the remote control board (14) with target aiming signals, which indicate the position of a target that has to be hit by the firearm (12). The remote control board (14) is assembled on a platform (18) which is adapted to be fitted to an aircraft. A support element (28) mounts on the platform (18) and supports the automatic target aiming system (32) and houses the adjustable firearm (12) in a controlled way by the remote control board (14) as a function of the target aiming signals. | ||||||
| 37 | VORRICHTUNG UND VERFAHREN ZUR THERMALKOMPENSATION EINES WAFFENROHRES | EP12725763.2 | 2012-06-04 | EP2718657A1 | 2014-04-16 | BRUNNER, Dominic; MEIER, Raffael |
| The invention relates to a device and a method for the thermal compensation of a weapon barrel of a gun (10) comprising at least one weapon barrel (11) that is mounted in a cradle (3) and in a barrel support (4) as an extension of the cradle (3). Multiple temperature sensors (p1-p16) are integrated in the cradle (3) and the barrel support (4). The sensors are connected to a data box (7) via data lines (6), and the data box (7) is connected to a data processing device (9). The data processing device (9) can act on actuators of the gun (10). The temperature of the cradle (3) and the barrel support (4) is measured by means of the temperature sensors (p1-p16). Then, the temperature differences between the upper and lower sides and the right and left sides of the cradle (3) and of the barrel support (4) are ascertained. The barrel inclination is calculated from said values, and then a compensation for the barrel inclination is carried out by adjusting the alignment of the weapon barrel (11) in azimuth and/or elevation. | ||||||
| 38 | GESCHÜTZ UND MILITÄRISCHES FAHRZEUG | EP12769882.7 | 2012-05-15 | EP2710323A1 | 2014-03-26 | RACZEK, Matthias; KÖSTER, Jens; CZOK, Matthias |
| The invention relates to an ordnance with a chassis (30) and a tower (10) that is mounted such as to be rotatable with respect to the chassis (30) and that has a closable opening (12), wherein the opening (12) can be closed by a closing element (20) arranged on the chassis (30). The invention also relates to a military vehicle having an ordnance (4), which comprises a chassis (30) and a tower (10) that is mounted such as to be rotatable with respect to the chassis (30) and that has a closable opening (12), wherein the opening (12) can be closed by a closing element (20) arranged on the chassis (30). | ||||||
| 39 | JUNGLE FIGHTER AIRCRAFT CONVERSION KIT | PCT/US2006017973 | 2006-05-09 | WO2007114831A2 | 2007-10-11 | HARDING DAVID K |
| A jungle fighter aircraft conversion kit comprised of a gattling gun works (1) that is mounted at the nose cone (3) under portion of an aircraft (2), avionics grayboxes (8), vibration trays (5), a hood (9) for enclosure and a machine gun (10). The gattling gun works (1) is designed for repeat fire power in intermittent operations while the air vents (4) in the gattling machine gun works (1) are designed for cooling the weapon. The grayboxes (8) are located within the gattling works weapon (1) and are designed for control within the cockpit (7) of the aircraft. Both the weapon and the grayboxes (8) have vibration trays (5) mounted at each equipment base. The machine gun (10) is preferably compact and lightweight and similar in design to those used by United States secret service agents. | ||||||
| 40 | BELT/METALLIC LINK CHAIN LOADED AMMUNITION FEEDER IN A REMOTE CONTROLLED WEAPON STATION | PCT/IL2013050474 | 2013-06-03 | WO2013183046A8 | 2015-01-15 | CHACHAMIAN SHIMON; HAMISH RAN |
| Belt/Metallic Link Chain Loaded Ammunition Feeder in a Remote Controlled Weapon Station (RCWS) that comprises feeding mechanism for routing chained ammunition from ammunition reservoir means towards the weapon's bullets entrance opening wherein said feeding mechanism comprises - a first chute assembly for routing chained ammunition from said ammunition reservoir means towards the region of the RCWS's elevating/lowering axis, wherein said first chute assembly is mounted on the RCWS's rotatable turret assembly; and a second chute assembly for continuing routing said chained ammunition from the region of said elevating/lowering axis towards the entry opening of the bullets entrance of the weapon, wherein the second chute is mounted the RCWS's mounting bracket; and wherein the chained ammunition traversing over said elevating/lowering axis region in its passing from the first chute assembly to the second chute assembly happens when said ammunition is directed in an orientation that is at least substantially suited to the direction of said elevating/lowering axis; and at the time that said mounting bracket assembly is propelled to elevating/lowering motion around said elevating/lowering axis, the first chute assembly remains static and the second chute assembly is dynamic and propelled together with said mounting bracket assembly around said elevating/lowering axis. | ||||||
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