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 |
|---|---|---|---|---|---|---|
| 1 | 一种高炮降雨弹发射架 | CN201611240657.0 | 2016-12-29 | CN106767154A | 2017-05-31 | 孙军锋; 党小军 |
| 本发明提供了一种高炮降雨弹发射架，包括发射台、固定脚和炮筒；所述炮筒一端设置在发射台中心，炮筒能绕发射台中心转动，仰角采用先用技术进行自由调整，固定脚分别通过连接架连接在发射台上，且固定脚为四组均布在发射台四周；所述发射台上还均布设置四个台面孔，所述台面孔内插设有斜支撑架，所述斜支撑架用于辅助支撑发射台，斜支撑架可通过螺纹固定方式设置在台面孔内；所述固定脚内部通过弹簧组件结构起到支撑和缓冲；本发明结构简单，缓冲效果好，能有效吸收炮弹发射瞬间的反作用力，延长发射架的使用寿命，同时能够保证发射时设备的安全可靠。 | ||||||
| 2 | 用于车辆上的火器的定位结构 | CN201280014032.6 | 2012-03-13 | CN103459970B | 2015-07-22 | C·A·亚尔代拉; P·阿里吉 |
| 本发明涉及一种定位结构，其用于车辆上的武器，该车辆装备有装甲座舱(A)，并且其中该武器被约束到车辆的顶部。这样的定位结构直接接合到车辆的框架，并且具体地接合到界定了装甲座舱的加强杆(B)，该加强杆通常称为翻滚保护杆。 | ||||||
| 3 | 用于车辆上的火器的定位结构 | CN201280014032.6 | 2012-03-13 | CN103459970A | 2013-12-18 | C·A·亚尔代拉; P·阿里吉 |
| 本发明涉及一种定位结构，其用于车辆上的武器，该车辆装备有装甲座舱（A），并且其中该武器被约束到车辆的顶部。这样的定位结构直接接合到车辆的框架，并且具体地接合到界定了装甲座舱的加强杆（B），该加强杆通常称为防滚保护杆。 | ||||||
| 4 | Vehicle firearm positioning structure | JP2013558521 | 2012-03-13 | JP2014511987A | 2014-05-19 | イアルデッラ，カルロ，アルベルト; アリギ，パオロ |
| 【解決手段】本発明の車両銃火器位置決め構造は、装甲操縦席を備えた車両のルーフ又は最上部に兵器（銃火器）が固定されている。 当該構造は、車のフレーム、特に、ロール・バーと称され、装甲操縦席との境界を区画する補強バーに直接固定されている。
【選択図】図１ｄ |
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| 5 | Missile launcher | JP24332691 | 1991-09-24 | JPH0579796A | 1993-03-30 | MURAOKA NOBUYUKI |
| PURPOSE:To stably fix a launcher firing base by providing a firing base supporter having a coupler including pins provided at the firing base, a pair of legs rotatably mounted at the ends of the pins of the coupler, and a foundation fixing bracket mounted by other pins at the other ends of the legs. CONSTITUTION:The missile launcher comprises a coupler 1a having pins so provided at a launcher firing base 9 as to perpendicularly cross a firing base propulsion force henerated by the deflection of a jet stream in the case of launching a missile, a pair of legs 1b rotatably mounted at the ends of the pins of the coupler, and a foundation fixing bracket 1c mounted by other pins at the other ends of the legs. A firing base supporter is mounted in response to a size between the firing base and a foundation after the firing base 9 is horizontally set by four jacks 2. Thus, fire base propulsion force generated at the time of launching the missile is supported by the four jacks to prevent the firing base from moving forward. Since the legs are obliquely provided, it can resist strongly against the propulsion force even by a small-sized apparatus. | ||||||
| 6 | Weapon Maintenance Stand | US15662133 | 2017-07-27 | US20190033031A1 | 2019-01-31 | Hernán Luis y Prado |
| In one aspect the invention features a weapon maintenance stand that includes a base plate, a support flange, and a wall structure. The support flange is spaced from the base plate and defines a first plurality holes extending through the support flange. A subset of the first plurality of holes are configured to match a pattern of bolt holes of a deck-mounted weapon system and at least one of the first plurality of holes is configured to receive an alignment structure of the deck-mounted weapon system. The wall structure is attached to the base plate at a first end and attached to the support flange at a second end. The wall structure defines at least one tunnel extending through the wall, with the at least one tunnel being sized to accept umbilical components of the deck-mounted weapons system. | ||||||
| 7 | VEHICLE ATTACHED GUN MOUNT | US13012520 | 2011-01-24 | US20120186438A1 | 2012-07-26 | David C. Frey; Richard J. Nowicki |
| A gun mount for mounting a weapon to a vehicle includes a weapon mount plate defining a planar surface. First and second side plates are oriented at an angle to the weapon mount plate planar surface. Front and rear plates are perpendicular to the weapon mount plate and the first and second side plates supporting the weapon mount plate and fixed to the first and second side plates. A male tab extends from both the first and second side plates. A female slot is created in individual ones of both the front and rear plates. The female slot is aligned to slidably receive the male tab with a male tab freely extending portion extending beyond the female slot. A tab weld joint created at the freely extending portion of the male tab fixes the first and second side plates to the front and rear plates. | ||||||
| 8 | Interface pallet assembly for a helicopter-based weapon system | US10216467 | 2002-08-12 | US06564690B1 | 2003-05-20 | David R. Long |
| Disclosed herein is an interface pallet assembly for use between the cabin deck of a helicopter and a large, heavy weapon system. The assembly incorporates a self-contained truss assembly designed to support a cantilevered platform, external to the helicopter's cabin, to which the weapon system's turret is attached. Existing deck connection points are utilized to secure the interface pallet assembly to the cabin deck. The interface pallet assembly adds 20E to the downward angle of fire of the weapon system and provides for azimuth rotation of 180E. The present assembly possesses the rotational stiffness required by the turret stabilization system in order to maintain firing accuracy during burst mode sequences. The interface pallet assembly is fabricated of a variety of strong, lightweight materials so as to not unduly add to the overall weight of the helicopter and its payload, and provides storage or mounting locations for accessories associated with the turret and weapon system. | ||||||
| 9 | Apparatus and methods for mounting a weaponry support plank on the cabin area floor of a helicopter | US417922 | 1995-04-06 | US5517895A | 1996-05-21 | Paul H. Sanderson |
| A longitudinally central portion of a weaponry support plank is secured to the cabin area floor of a McDonnell Douglas 500/530 helicopter using a support and reinforcing system associated with forwardly and rearwardly disposed pairs of stiffening ribs anchored to the top side of the floor. Opposite end portions of the front and rear rib pairs are removed and are laterally enclosed in and anchored to elongated reinforcing structures each having opposite ends generally aligned with the opposite ends of its associated shortened rib. End members are anchored to the floor at the opposite ends of each pair of shortened ribs and are also anchored to the opposite ends of their associated reinforcing structure. Two front support strut members have upper sides fixedly secured in a spaced relationship to a front side edge of the central plank portion, and two rear support strut members have sides fixedly secured in a spaced relationship to the rear side edge of the central plank portion. The undersides of the support strut members are removably and pivotally secured to the end members by expansion pins extending along axes transverse to the stiffening ribs. In an alternate embodiment of the support and reinforcing system the front support strut members are provided with rearwardly projecting extension portions that are anchored to reinforced opposite end portions of the central floor stiffening rib. | ||||||
| 10 | System for anchoring a projectile launcher to the ground | US090175 | 1993-07-19 | US5345853A | 1994-09-13 | Roger Crepin; Thierry Bredy |
| An anchoring system for anchoring a projectile launcher to the ground. The launcher includes a tubular body accommodating at least a projectile to be fired and a propellant charge. The system further includes least one anchoring element that penetrates the ground when the projectile is fired. The anchoring element can be moved between a first position in which it is at a distance from the ground and held by a body of the launcher by means of a temporary attachment device, and a second position in which it penetrates the ground. A control system causes the anchoring spike to move automatically from its first to its second position and is constituted by the pressure of the gases resulting from ignition of propellant charge. | ||||||
| 11 | Accessory mounting apparatus for a vehicle | US14183784 | 2014-02-19 | US09079544B2 | 2015-07-14 | Jason E. Miller; Brent Terry; Garric Henry |
| An accessory mounting apparatus is provided for coupling to a vehicle roll bar. The accessory mounting apparatus illustratively includes a driver side clamping device configured to be secured to a driver side upright of the roll bar, and a passenger side clamping device configured to be secured to the passenger side upright of the roll bar. Protective sleeves cooperate with the clamping devices to protect the roll bar from damaging contact therewith. A laterally extending cross member extends between the driver side clamping device and the passenger side clamping device. | ||||||
| 12 | Mountable Fixture for Absorbing Recoil | US13802880 | 2013-03-14 | US20140260941A1 | 2014-09-18 | Jorge David De Leon; James F. Cahill; Ishankumar Patel; Reginald Heggie |
| A fixture is provided for supporting load from weapons recoil, being mountable on a flat bed of a road vehicle disposed on ground. The flat bed can receive a weapons mount. The vehicle has longitudinal, lateral and vertical orientations. The fixture includes a box brace, a recoil platform, first and second brackets, first and second beams, first and second posts and a deck. The box brace extends in the lateral direction. The recoil platform is parallel to the brace. The first and second brackets extend from the platform in the longitudinal direction. The beams are disposable parallel to the brace. The beams are translatable in the lateral direction. The first and second posts extend in the vertical direction downward from respective the first and second beams. The deck can receive the weapons mount, and is disposable on the platform and the brackets. The posts are retractable for stowage and extendible for raising the flat bed above the ground. | ||||||
| 13 | Vehicle attached gun mount | US13012520 | 2011-01-24 | US08347776B2 | 2013-01-08 | David C. Frey; Richard J. Nowicki |
| A gun mount for mounting a weapon to a vehicle includes a weapon mount plate defining a planar surface. First and second side plates are oriented at an angle to the weapon mount plate planar surface. Front and rear plates are perpendicular to the weapon mount plate and the first and second side plates supporting the weapon mount plate and fixed to the first and second side plates. A male tab extends from both the first and second side plates. A female slot is created in individual ones of both the front and rear plates. The female slot is aligned to slidably receive the male tab with a male tab freely extending portion extending beyond the female slot. A tab weld joint created at the freely extending portion of the male tab fixes the first and second side plates to the front and rear plates. | ||||||
| 14 | ACCESSORY MOUNTING APPARATUS FOR A VEHICLE | US13180906 | 2011-07-12 | US20120180281A1 | 2012-07-19 | Jason E. Miller; Brent Terry; Garric Henry |
| An accessory mounting apparatus is provided for coupling to a vehicle roll bar. The accessory mounting apparatus illustratively includes a driver side clamping device configured to be secured to a driver side upright of the roll bar, and a passenger side clamping device configured to be secured to the passenger side upright of the roll bar. Protective sleeves cooperate with the clamping devices to protect the roll bar from damaging contact therewith. A laterally extending cross member extends between the driver side clamping device and the passenger side clamping device. | ||||||
| 15 | ISO pallet concept for a gun | US12221025 | 2008-07-30 | US20090031890A1 | 2009-02-05 | Marcos Trigo; Michael Gerber |
| A lower gun mount, which can be mounted in a standardized way on a ship or a permanent ground foundation, is used so that a gun can be mounted with minimal effort quickly, reproducibly and without slip, and later dismounted. This standardized lower gun mount is mounted geometrically correctly on a foundation or ship by so-called standardized ISO corners, which can be fixed in place on supports specially provided for this purpose and a mounting frame that assists the mounting. This makes it possible for the gun to be mounted rigidly and without play. | ||||||
| 16 | Plank-mounted aircraft armanent apparatus | US060867 | 1993-05-12 | US5390582A | 1995-02-21 | Paul H. Sanderson |
| An aircraft armament mounting system includes an elongated support plank member which is insertable transversely through the aircraft cabin area so that a central portion of the plank is disposed within the cabin area and its opposite end portions project outwardly from the aircraft. The central plank portion is anchored to the air craft, and removable outer tip portions of the plank are vertically pivotable, about horizontal hinge lines, between extended and inwardly folded positions. When the outer plank tip portions are removed, specially designed mounting structures may be used to mount armament devices, such as machine guns, at the hinge lines at the outer ends of the remaining longitudinal plank portion. Representatively, these armament devices are .50 caliber machine guns housed in open framed pod structures having enclosed front end portions through which the jacketed barrels of the guns extend. Secured to these front end portions, and communicating with their interiors, are slotted blast suppressor tubes that receive the gun barrels and serve to shield the sides of the aircraft from the firing blasts of the guns, and to reduce the firing blast light transmitted into the aircraft cabin area. | ||||||
| 17 | ISO-Palettierung für ein Geschütz | EP08011975.3 | 2008-07-03 | EP2020376A3 | 2012-02-29 | Trigo, Marcos; Gerber, Michael |
Vorgeschlagen wird, eine Unterlafette zu nutzen, die normiert auf einem Schiff oder einem festen Bodenfundament montiert werden kann, so dass ein Geschütz (1) mit minimalem Aufwand schnell, reproduzierbar und rutschfest montiert und später wieder demontiert werden kann. Diese normierte Unterlafette wird mittels so genannter normierter ISO- Ecken (2), die auf speziell dafür vorgesehene Supports (3.1- 3.4) fixierbar sind, sowie einen die Montage unterstützenden Montagerahmen (10) geometrisch korrekt an ein Fundament oder Schiff montiert. Erreicht werden dadurch eine steife Lagerung und spielfreie Fixierung des Geschützes (1).
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| 18 | SYSTEME D'ANCRAGE AU SOL D'UN LANCEUR DE PROJECTILES | EP93902292.0 | 1992-12-03 | EP0572642A1 | 1993-12-08 | CREPIN, Roger; BREDY, Thierry |
| Le système d'ancrage au sol d'un lanceur de projectiles, le lanceur étant constitué d'un corps tubulaire (2) où sont au moins logés un projectile (18) à tirer et une charge propulsive (12), comprend au moins un élément d'ancrage (8) enfoncé dans le sol au moment du tir du projectile. L'élément d'ancrage (8) est mobile entre une première position où il est éloigné du sol et maintenu par le corps (2) du lanceur (1) au moyen d'un dispositif de fixation temporaire (10), et une secodne position où il est enfoncé dans le sol. Le moyen de commande pour faire passer le piton d'ancrage (8) automatiquement de sa première à sa seconde position, est constitué par la pression des gaz résultant de l'inflammation de la charge propulsive (12). | ||||||
| 19 | ISO-Palettierung für ein Geschütz | EP08011975.3 | 2008-07-03 | EP2020376A2 | 2009-02-04 | Trigo, Marcos; Gerber, Michael |
Vorgeschlagen wird, eine Unterlafette zu nutzen, die normiert auf einem Schiff oder einem festen Bodenfundament montiert werden kann, so dass ein Geschütz (1) mit minimalem Aufwand schnell, reproduzierbar und rutschfest montiert und später wieder demontiert werden kann. Diese normierte Unterlafette wird mittels so genannter normierter ISO- Ecken (2), die auf speziell dafür vorgesehene Supports (3.1- 3.4) fixierbar sind, sowie einen die Montage unterstützenden Montagerahmen (10) geometrisch korrekt an ein Fundament oder Schiff montiert. Erreicht werden dadurch eine steife Lagerung und spielfreie Fixierung des Geschützes (1).
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| 20 | SYSTEME D'ANCRAGE AU SOL D'UN LANCEUR DE PROJECTILES | EP93902292.7 | 1992-12-03 | EP0572642B1 | 1997-01-08 | CREPIN, Roger; BREDY, Thierry |
| A system for ground-anchoring a missile launcher consisting of a tubular body (2) housing at least the missile (18) to be fired and a propellant charge (12). The system includes at least one anchoring element (8) which is driven into the ground when the missile is fired. The anchoring element (8) is movable between a first position in which it is at a certain distance from the ground and supported by the body (2) of the launcher (1) via a releasable fastening device (10), and a second position in which it is driven into the ground. The control means for automatically moving the anchoring peg (8) between the first and second positions is provided by the gas pressure resulting from the lighting of the propellant charge (12). | ||||||
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