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 | 尤其用于诸如固定翼飞机的飞机的远程武器站 | CN201280046002.3 | 2012-09-18 | CN103842764A | 2014-06-04 | A·伊索拉; G·B·莱奥内西奥 |
| 远程武器站（10）包括：用于向目标开火的枪炮（12）；遥控板或面板（14），其布置在距所述枪炮（12）一距离处并且构造成由操作员启动，从而控制所述枪炮（12）；自动目标瞄准系统（32），其构造成给所述遥控板（14）提供目标瞄准信号，该目标瞄准信号指示必须被所述枪炮（12）打击的目标的位置；平台（18），所述遥控板（14）组装在该平台并且所述平台能装配在飞机上；和组装在所述平台（18）上的支撑部件（28），该支撑部件支撑所述自动目标瞄准系统（32）并且容纳所述枪炮（12），以便通过所述遥控板（14）根据所述目标瞄准信号来控制所述枪炮。 | ||||||
| 2 | 一种狙击步枪用两脚架 | CN201710346324.4 | 2017-05-17 | CN106979720A | 2017-07-25 | 艾川; 王敏祥; 谢凤; 张宁林; 范方梅; 袁安; 庞方跃; 郝雨佳 |
| 本发明公开了一种狙击步枪用两脚架，属于枪械技术领域。它包括接口座、基座，所述基座上连接有两根支撑筒，所述基座的下端面上竖向设有内孔，所述基座的内孔中由上至下依次设有上橡胶垫片、球状的铰链、下橡胶垫片、调节螺母，所述上橡胶垫片的下端面和下橡胶垫片的上端面为与所述铰链对应的圆弧面，所述调节螺母与基座的内孔螺纹配合，对下橡胶垫片提供竖向的作用力，所述铰链上设有连杆依次穿过上橡胶垫片、基座的上端面并与接口座固定连接，所述基座的上端面上设有供所述连杆转动的横向限位腰形孔。它能实现狙击步枪的支撑角度、支撑高度的调节。 | ||||||
| 3 | 用于对武器管进行热补偿的装置和方法 | CN201280027160.4 | 2012-06-04 | CN103582799A | 2014-02-12 | D·布伦纳; R·迈尔 |
| 本发明涉及一种用于对武器（10）的武器管（11）进行热补偿的装置，所述武器具有至少一个武器管（11），所述武器管支承在管摇架（3）中以及支承在作为管摇架（3）的延长部的管支承件（4）中，在管摇架（3）和管支承件（4）上设置多个温度传感器（p1-p16），所述温度传感器通过数据线路（6）与数据盒（7）连接，所述数据盒（7）与数据处理装置（9）连接，数据处理装置（9）能作用在武器（10）的致动器上。通过温度传感器（p1-p16）测量管摇架（3）和管支承件（4）的温度。然后，确定管摇架（3）和管支承件（4）的上侧与下侧之间以及右侧和左侧之间的温度差。利用所述值计算管倾斜度，通过调整武器管（11）在方位角和/或仰角上的定向来补偿所述管倾斜度。 | ||||||
| 4 | 一种全电动驱动式突击步枪枪架 | CN201610743342.1 | 2016-08-29 | CN106123676A | 2016-11-16 | 高建东; 周维智; 刘文波 |
| 本发明涉及步枪枪架结构，特别提供一种全电动驱动式突击步枪枪架。所述固定架用于固定步枪，固定架尾部通过固定销轴与三角支架顶部活动连接，固定架通过固定销轴相对于三角支架旋转，还包括用于控制步枪俯仰动作的电动推杆，和用于控制步枪水平旋转动作的旋转电机、与旋转电机配合使用的减速转盘；电动推杆的一端与步枪固定架的头部活动连接，电动推杆的另一端与减速转盘活动连接；减速转盘与三角支架底部通过螺栓连接，连接基板与减速转盘通过螺栓连接。在实现步枪动作的基础上，提高射击精度、结构相对简单，易于维护、重量较小，成本较低。通过电动推杆实现俯仰动作，通过电机及减速转盘实现旋转动作，通过避震弹簧提高了射击精度。 | ||||||
| 5 | 用于飞机的远程武器站 | CN201280046002.3 | 2012-09-18 | CN103842764B | 2016-08-17 | A·伊索拉; G·B·莱奥内西奥 |
| 远程武器站（10）包括：用于向目标开火的枪炮（12）；遥控板或面板（14），其布置在距所述枪炮（12）一距离处并且构造成由操作员启动，从而控制所述枪炮（12）；自动目标瞄准系统（32），其构造成给所述遥控板（14）提供目标瞄准信号，该目标瞄准信号指示必须被所述枪炮（12）打击的目标的位置；平台（18），所述遥控板（14）组装在该平台并且所述平台能装配在飞机上；和组装在所述平台（18）上的支撑部件（28），该支撑部件支撑所述自动目标瞄准系统（32）并且容纳所述枪炮（12），以便通过所述遥控板（14）根据所述目标瞄准信号来控制所述枪炮。 | ||||||
| 6 | 用于对武器管进行热补偿的装置和方法 | CN201280027160.4 | 2012-06-04 | CN103582799B | 2015-12-23 | D·布伦纳; R·迈尔 |
| 本发明涉及一种用于对武器（10）的武器管（11）进行热补偿的装置，所述武器具有至少一个武器管（11），所述武器管支承在管摇架（3）中以及支承在作为管摇架（3）的延长部的管支承件（4）中，在管摇架（3）和管支承件（4）上设置多个温度传感器（p1-p16），所述温度传感器通过数据线路（6）与数据盒（7）连接，所述数据盒（7）与数据处理装置（9）连接，数据处理装置（9）能作用在武器（10）的致动器上。通过温度传感器（p1-p16）测量管摇架（3）和管支承件（4）的温度。然后，确定管摇架（3）和管支承件（4）的上侧与下侧之间以及右侧和左侧之间的温度差。利用所述值计算管倾斜度，通过调整武器管（11）在方位角和/或仰角上的定向来补偿所述管倾斜度。 | ||||||
| 7 | 武器銃身の熱補償を実施するための装置および方法 | JP2014514024 | 2012-06-04 | JP6092853B2 | 2017-03-08 | ドミニク ブルンナー; ラファエル マイアー |
| 8 | Apparatus and method for performing a thermal compensation of the weapon barrel | JP2014514024 | 2012-06-04 | JP2014521910A | 2014-08-28 | ブルンナー ドミニク; マイアー ラファエル |
| 銃身クレードル（３）内および銃身クレードル（３）の延長部分としての銃身支持体（４）内に取付けられた少なくとも１つの武器銃身（１１）を有する銃（１０）の武器銃身の熱補償を実施するための装置および方法において、銃身クレードル（３）および銃身支持体（４）内に複数の温度センサ（ｐ１〜ｐ１６）が組み込まれ、データライン（６）を介してデータボックス（７）に接続されており、データボックス（７）はデータ処理装置（９）に接続されており、ここでデータ処理装置（９）は銃（１０）のアクチュエータに作用できることを特徴とする装置及び方法が提供されている。 銃身クレードル（３）および銃身支持体（４）における温度は、温度センサ（ｐ１〜ｐ１６）を用いて測定される。 銃身クレードル（３）と同様銃身支持体（４）の上側と下側の間および右側と左側の間の温度差が次に決定される。 その後、これらの値から銃身の傾斜が計算され、銃身の傾斜は次に、方位および／または仰角における武器銃身（１１）の配向を調整することによって補償される。
【選択図】図２ |
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| 9 | Cannon and military vehicle | US14119182 | 2012-05-15 | US09360266B2 | 2016-06-07 | 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. | ||||||
| 10 | DEVICE AND METHOD FOR THE THERMAL COMPENSATION OF A WEAPON BARREL | US14100963 | 2013-12-09 | US20140290471A1 | 2014-10-02 | Dominic BRUNNER; Raffael MEIER |
| A device and a method for performing thermal compensation of a weapon barrel of a gun having at least one weapon barrel which is mounted in a barrel cradle and in a barrel support as a prolongation of the barrel cradle. A plurality of temperature sensors are integrated into the barrel cradle and the barrel support and are connected via data lines to a data box. The data box is connected to a data processing device, which acts on actuators of the gun. The temperature at the barrel cradle and the barrel support is measured by temperature sensors. The temperature difference between upper and lower sides and right-hand and left-hand sides of the barrel cradle and the barrel support are determined. The barrel inclination is then calculated from these values, and the barrel inclination is then compensated by adjusting the orientation of the weapon barrel in its azimuth and/or elevation. | ||||||
| 11 | REMOTE WEAPON STATION, IN PARTICULAR FOR AIRCRAFT, SUCH AS FIXED-WING AIRCRAFT | US14346636 | 2012-09-18 | US20140230641A1 | 2014-08-21 | Andrea Isola; Gian Battista Leonesio |
| 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. | ||||||
| 12 | Jungle fighter aircraft conversion kit | US11265924 | 2005-11-03 | US20060249013A1 | 2006-11-09 | David Harding |
| 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. | ||||||
| 13 | Vehicle control unit | US60157245 | 1945-06-26 | US2448129A | 1948-08-31 | TURNBULL WILLIAM J |
| 14 | Remote weapon station, in particular for aircraft, such as fixed-wing aircraft | US14346636 | 2012-09-18 | US09151573B2 | 2015-10-06 | Andrea Isola; Gian Battista Leonesio |
| 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. | ||||||
| 15 | BELT/METALLIC LINK CHAIN LOADED AMMUNITION FEEDER IN A REMOTE CONTROLLED WEAPON STATION | US14406077 | 2013-06-03 | US20150153123A1 | 2015-06-04 | Shimon Chachamian; Ran Hamish |
| Belt/Metallic Link Chain Loaded Ammunition Feeder in a Remote Controlled Weapon Station (RCWS). The feeder includes a feeding mechanism for routing chained ammunition from ammunition reservoir means towards the weapon's bullets entrance opening. The feeding mechanism has a first chute assembly for routing chained ammunition from the ammunition reservoir means towards the region of the RCWS's elevating/lowering axis, and a second chute assembly for continuing routing the chained ammunition from the region of the elevating/lowering axis towards the entry opening of the bullets entrance of the weapon. The chained ammunition traverses over the elevating/lowering axis region by passing from the first chute assembly to the second chute assembly. The first chute assembly remains static and the second chute assembly is dynamic and propelled together with the mounting bracket assembly around the elevating/lowering axis. | ||||||
| 16 | Underwater weapon system having a rotatable gun | US10730184 | 2003-12-08 | US06848386B1 | 2005-02-01 | Thomas J. Gieseke |
| An underwater weapon system having a housing formed by first and second halves thereof sandwiched about a gun system that is rotatably mounted to and between the first and second halves. The gun system includes a gun and ammunition sealed within a waterproof housing with a muzzle of the gun protruding from the waterproof housing. The gun system is rotatable relative to the first and second halves of the housing while the housing can be maneuvered to rotate through a plane of rotation of the gun system as the housing moves through the water. | ||||||
| 17 | Aircraft support plank mounted 30 mm machine gun | US09873341 | 2001-06-04 | US06401592B1 | 2002-06-11 | Charles E. Rostocil |
| A machine gun, representatively a 30 mm machine gun, is mounted on an outer end portion of a support plank structure projecting out of the cabin area of a helicopter using a roller cradle assembly secured to the outer plank end. A variety of structural improvements are incorporated into the machine gun to (1) reduce its mechanical complexity, (2) reduce its firing recoil to make the gun more suitable for light aircraft mounting, and to improve the gun's firing controllability and accuracy, and (3) to make the gun easily and quickly field strippable, for cleaning, inspection and repair purposes, without requiring the services of a highly skilled armament mechanic or taking the gun to a specialized repair facility. | ||||||
| 18 | Aircraft support plank mounted 30 mm machine gun | US09588618 | 2000-06-06 | US06263776B1 | 2001-07-24 | Charles E. Rostocil |
| A machine gun, representatively a 30 mm machine gun, is mounted on an outer end portion of a support plank structure projecting out of the cabin area of a helicopter using a roller cradle assembly secured to the outer plank end. A variety of structural improvements are incorporated into the machine gun to (1) reduce its mechanical complexity, (2) reduce its firing recoil to make the gun more suitable for light aircraft mounting, and to improve the gun's firing controllability and accuracy, and (3) to make the gun easily and quickly field strippable, for cleaning, inspection and repair purposes, without requiring the services of a highly skilled armament mechanic or taking the gun to a specialized repair facility. | ||||||
| 19 | Aircraft support plank mounted 30 MM machine gun | US09007090 | 1998-01-14 | US06176169B1 | 2001-01-23 | Charles E. Rostocil |
| A machine gun, representatively a 30 mm machine gun, is mounted on an outer end portion of a support plank structure projecting out of the cabin area of a helicopter using a roller cradle assembly secured to the outer plank end. A variety of structural improvements are incorporated into the machine gun to (1) reduce its mechanical complexity, (2) reduce its firing recoil to make the gun more suitable for light aircraft mounting, and to improve the gun's firing controllability and accuracy, and (3) to make the gun easily and quickly field strippable, for cleaning, inspection and repair purposes, without requiring the services of a highly skilled armament mechanic or taking the gun to a specialized repair facility. | ||||||
| 20 | Belt/metallic link chain loaded ammunition feeder in a remote controlled weapon station | US14406077 | 2013-06-03 | US10132581B2 | 2018-11-20 | Shimon Chachamian; Ran Hamish |
| Belt/Metallic Link Chain Loaded Ammunition Feeder in a Remote Controlled Weapon Station (RCWS). The feeder includes a feeding mechanism for routing chained ammunition from ammunition reservoir means towards the weapon's bullets entrance opening. The feeding mechanism has a first chute assembly for routing chained ammunition from the ammunition reservoir means towards the region of the RCWS's elevating/lowering axis, and a second chute assembly for continuing routing the chained ammunition from the region of the elevating/lowering axis towards the entry opening of the bullets entrance of the weapon. The chained ammunition traverses over the elevating/lowering axis region by passing from the first chute assembly to the second chute assembly. The first chute assembly remains static and the second chute assembly is dynamic and propelled together with the mounting bracket assembly around the elevating/lowering axis. | ||||||
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