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1. 发明申请

WO2015193399A1 LAUNCHING AERIAL DEVICES 审中-公开
标题翻译：发射空中装置
公开(公告)号：WO2015193399A1
公开(公告)日：2015-12-23
申请号：PCT/EP2015/063646
申请日：2015-06-17
申请人： LOCKHEED MARTIN CORPORATION , SMOKER, Thomas William
发明人： SMOKER, Thomas William
IPC分类号： F41F3/07 , F41F3/042
CPC分类号： F41F3/07 , F41F3/042
摘要： A launch container apparatus for ejection from a submerged launch platform and a method for ejecting a launch container apparatus are disclosed. The apparatus comprises an enclosure for carrying an unmanned aerial device and a surfacing sensor configured to generate a control signal in response to detection of surfacing of the launch container apparatus. Petals are configured to provide buoyancy and stabilization for the launch container apparatus are also provided. A petal drive mechanism moves, in response to the control signal, the petals from a folded position to an expanded position.
摘要翻译：公开了一种用于从淹没式发射平台喷射的发射容器装置和用于喷射发射容器装置的方法。该装置包括用于承载无人驾驶空中装置的外壳和配置成响应于发射容器装置的表面的检测而产生控制信号的表面传感器。还提供花瓣配置为提供浮力和稳定发射容器设备。花瓣驱动机构响应于控制信号而将瓣从折叠位置移动到展开位置。

2. 发明申请

WO2012022964A1 MISSILE CANISTER 审中-公开
公开(公告)号：WO2012022964A1
公开(公告)日：2012-02-23
申请号：PCT/GB2011/051536
申请日：2011-08-15
申请人： MBDA UK LIMITED , BOWEN, Bryan , MACHELL, Anthony , KAVANAGH, Terence, Edward , TURNER, Dennis, George
发明人： BOWEN, Bryan , MACHELL, Anthony , KAVANAGH, Terence, Edward , TURNER, Dennis, George
IPC分类号： F41F3/042 , F42B39/14
CPC分类号： F41F3/042 , F42B39/14
摘要： The invention covers a missile canister (10) for accommodating a missile (20) along a longitudinal axis (L) of the canister. The canister comprises a plurality of generally planar longitudinal wall portions (14) connected together to form a tubular vessel having a polygonal cross - section. The interconnecting portions (16) between wall sections (14) are generally flexible so that when a missile (20) is launched the bending moment at the interconnecting portions (16) generated by the increase of pressure in the vessel is substantially less than the bending moment (10) generated at the wall portions (14). The interconnecting portions (16) allow relative angular deflection between adjacent wall portions (14) at respective interconnecting portions (16) when said missile (20) is launched.
摘要翻译：本发明涉及一种用于沿着罐的纵向轴线（L）容纳导弹（20）的导弹筒（10）。所述罐包括连接在一起的多个大致平面的纵向壁部分（14），以形成具有多边形横截面的管状容器。壁部分（14）之间的互连部分（16）通常是柔性的，使得当发射导弹（20）时，通过容器中的压力增加产生的互连部分（16）处的弯曲力矩大大小于弯曲在壁部（14）处产生的力矩（10）。当所述导弹（20）被启动时，互连部分（16）允许相应的互连部分（16）处的相邻壁部分（14）之间的相对角度偏转。

3. 发明申请

WO2005001372A3 MULTIPLE TUBE PNEUMATIC LAUNCHER 审中-公开
标题翻译：多管气动推杆
公开(公告)号：WO2005001372A3
公开(公告)日：2005-08-11
申请号：PCT/US2004009427
申请日：2004-03-29
申请人： AAI CORP , MILLER STEPHEN W , FOX STEVEN J , FEILD DAVID M , BAUERNSCHUB RICHARD A , METTEE JUSTIN A
发明人： MILLER STEPHEN W , FOX STEVEN J , FEILD DAVID M , BAUERNSCHUB RICHARD A , METTEE JUSTIN A
IPC分类号： F41F20060101 , F41F3/042
CPC分类号： F41A23/42 , F41B11/00 , F41B11/62 , F41F3/042
摘要： A launcher includes a plurality of launch tubes (110) for stowing and launching a plurality of air vehicles. A central air manifold (310) is operatively connected to an air storage tank (150); a first launch tube air manifold (320) is operatively connected to a first group of the launch tubes (110) and operatively connected to the central air manifold (310). The first launch air manifold (320) has a separate port corresponding to each launch tube (110) of the first group of launch tubes. A release valve mechanism (360) is removably mounted in one of the ports (355) of the first launch tube air manifold (320), the release valve mechanism (360) controlling the passage of launch air between the first launch tube air manifold (320) and the launch tube corresponding to the port (355) in which the release valve mechanism (360) is mounted. A plug (350) is removably mounted in each of the ports (355) not occupied by the release valve mechanism (360).
摘要翻译：发射器包括多个用于收起和发射多个空中飞行器的发射管（110）。中央空气歧管（310）可操作地连接到空气存储罐（150）; 第一发射管空气歧管（320）可操作地连接到第一组发射管（110）并可操作地连接到中央空气歧管（310）。第一发射空气歧管（320）具有对应于第一组发射管的每个发射管（110）的单独端口。释放阀机构（360）可移除地安装在第一发射管空气歧管（320）的一个端口（355）中，释放阀机构（360）控制发射空气在第一发射管空气歧管（ 320）和对应于其中安装有释放阀机构（360）的端口（355）的发射管。插塞（350）可移除地安装在不被释放阀机构（360）占据的每个端口（355）中。

4. 发明申请

WO2015121093A1 CASING WITH LIQUID DISPENSER 审中-公开
标题翻译：带液体分配器
公开(公告)号：WO2015121093A1
公开(公告)日：2015-08-20
申请号：PCT/EP2015/051993
申请日：2015-01-30
申请人： INNOVANTIX GMBH
发明人： ROCCA, Tiziano , KAPRANOV, Andrey
IPC分类号： F41H9/10 , H04M1/04
CPC分类号： B05B11/3059 , A45C11/00 , A45C15/00 , A45C2011/002 , A45D34/02 , A45D2034/007 , A45D2200/057 , B05B11/00 , B05B15/62 , F41F3/042 , F41F3/045 , F41F3/0455 , F41H9/10 , H04B1/3888 , H04M1/21
摘要： The present invention relates to a casing (1) for a mobile electronic device (17), the casing comprising a dispenser (2), which comprises a spraying unit (3) and a reservoir, wherein the dispenser can be moved from a secure position to at least one dispensing position.
摘要翻译：本发明涉及一种用于移动电子设备（17）的壳体（1），该壳体包括一个分配器（2），该分配器包括一个喷射单元（3）和一个储存器，其中分配器可以从安全位置移动至少一个分配位置。

5. 发明申请

WO2010006724A3 SOLID-PROPELLANT ROCKET MOTOR 审中-公开
标题翻译： SOLID电厂
公开(公告)号：WO2010006724A3
公开(公告)日：2011-01-13
申请号：PCT/EP2009004917
申请日：2009-07-08
申请人： DIEHL BGT DEFENCE GMBH & CO KG , FISCH PETER GERD , ELSNER GERD
发明人： FISCH PETER GERD , ELSNER GERD
IPC分类号： F02K9/34 , F02K9/36 , F41F3/042 , F41F3/06
CPC分类号： F02K9/34 , F02K9/36 , F05D2260/20 , F05D2300/603 , F41F3/042
摘要： The invention relates to a solid-propellant rocket motor (10) comprising an outer cladding (13) and a combustion chamber (20) arranged in the outer cladding (13). In order to simplify the fixing of fittings (14a, 14b, 14c, 5, 6), the combustion chamber (20) is embodied as a single component separate from the outer cladding (13).
摘要翻译：本发明涉及具有外护套（13）和外壳（13）的内部的固体发动机（10），其布置在所述燃烧室（20）。为了简化接头的紧固（14A，14B，14C，5，6）的燃烧室（20）的建议来进行作为一个单独的，从外封套（13）的单独部件。

6. 发明申请

WO2008134108A2 APPARATUS AND METHOD FOR SELECTIVELY AFFECTING A LAUNCH TRAJECTORY OF A PROJECTILE 审中-公开
标题翻译：用于选择性地影响项目的发射轨迹的装置和方法
公开(公告)号：WO2008134108A2
公开(公告)日：2008-11-06
申请号：PCT/US2008054150
申请日：2008-02-15
申请人： LOCKHEED CORP , PATEL UMANG R , SCHROEDER WAYNE K , BANKS JOHNNY E
发明人： PATEL UMANG R , SCHROEDER WAYNE K , BANKS JOHNNY E
IPC分类号： F42B5/067
CPC分类号： F42B5/067 , F41F3/042 , F41F3/052 , F41F3/077 , F42B5/073
摘要： An apparatus for selectively affecting a launch trajectory of a projectile from a canister includes means for selectively positioning the projectile with respect to the canister and a sabot operably associated with the projectile and the means for selectively positioning the projectile. A projectile launch system includes a canister, a projectile disposed in the canister, and means for selectively positioning the projectile with respect to the canister. A method for affecting a launch trajectory of a projectile includes providing a canister and a projectile disposed in the canister and adjusting a position of the projectile with respect to the canister.
摘要翻译：一种用于选择性地影响炮弹从炮弹的发射轨道的装置包括用于选择性地将射弹相对于碳罐定位的装置和与炮弹可操作地相关联的弹壳以及用于选择性定位炮弹的装置。射弹发射系统包括罐，置于罐中的射弹，以及用于选择性地将射弹相对于罐定位的装置。用于影响抛射物的发射轨迹的方法包括提供设置在罐中的罐和抛射物并且调整射弹相对于罐的位置。

7. 发明申请

WO2008127441A2 HERMETIC COVERING SYSTEM AND METHOD FOR A PROJECTILE 审中-公开
标题翻译：流程覆盖系统及方法
公开(公告)号：WO2008127441A2
公开(公告)日：2008-10-23
申请号：PCT/US2007085895
申请日：2007-11-29
申请人： RAYTHEON CO , MASON JAMES S , WILSON JAMES S
发明人： MASON JAMES S , WILSON JAMES S
IPC分类号： F41A35/02 , F42B39/00
CPC分类号： F42B39/00 , F41F3/042 , F41F3/073
摘要： In one embodiment, a hermetic covering system includes a projectile and at least one bag. The projectile has a body and a component that houses moisture-sensitive equipment. The at least one bag may be coupled to the body such that the projectile protrudes through the opening and the component is disposed in the inner cavity to protect the component during storage of the projectile.
摘要翻译：在一个实施例中，气密性覆盖系统包括射弹和至少一个袋。抛射体具有容纳湿气敏感设备的身体和部件。所述至少一个袋可以联接到所述主体，使得所述弹丸突出穿过所述开口，并且所述部件设置在所述内腔中，以在所述弹丸储存期间保护所述部件。

8. 发明申请

WO2005001372A2 MULTIPLE TUBE PNEUMATIC LAUNCHER 审中-公开
标题翻译：多管气动推杆
公开(公告)号：WO2005001372A2
公开(公告)日：2005-01-06
申请号：PCT/US2004/009427
申请日：2004-03-29
申请人： AAI CORPORATION , MILLER, Stephen, W. , FOX, Steven, J. , FEILD, David, M. , BAUERNSCHUB, Richard, A. , METTEE, Justin, A.
发明人： MILLER, Stephen, W. , FOX, Steven, J. , FEILD, David, M. , BAUERNSCHUB, Richard, A. , METTEE, Justin, A.
IPC分类号： F41F
CPC分类号： F41A23/42 , F41B11/00 , F41B11/62 , F41F3/042
摘要： A launcher includes a plurality of launch tubes for stowing and launching a plurality of air vehicles. A central air manifold is operatively connected to an air storage tank; a first launch tube air manifold is operatively connected to a first group of the launch tubes and operatively connected to the central air manifold. The first launch tube air manifold has a separate port corresponding to each launch tube of the first group of launch tubes. A release valve mechanism is removably mounted in one of the ports of the first launch tube air manifold, the release valve mechanism controlling the passage of launch air between the first launch tube air manifold and the launch tube corresponding to the port in which the release valve mechanism is mounted. A plug is removably mounted in each of the ports not occupied by the release valve mechanism.
摘要翻译：发射器包括用于收起和发射多个空中车辆的多个发射管。中央空气歧管可操作地连接到储气罐; 第一发射管空气歧管可操作地连接到第一组发射管并可操作地连接到中央空气歧管。第一发射管空气歧管具有对应于第一组发射管的每个发射管的单独端口。释放阀机构可移除地安装在第一发射管空气歧管的一个端口中，释放阀机构控制在第一发射管空气歧管和发射管之间的发射空气通过，其中释放阀机构安装。塞子可移除地安装在未被释放阀机构占据的每个端口中。

9. 发明申请

WO2015127178A1 PAYLOAD LAUNCHER AND AUTONOMOUS UNDERWATER VEHICLE 审中-公开
标题翻译：负载起重机和自主的水下车辆
公开(公告)号：WO2015127178A1
公开(公告)日：2015-08-27
申请号：PCT/US2015/016778
申请日：2015-02-20
申请人： LOCKHEED MARTIN CORPORATION
发明人： SYLVIA, Russell, M. , LEWIS, Martin, C. , WHALEN, Mark, E. , GORDON, Robert, P.
IPC分类号： B63G8/00 , B64F5/00
CPC分类号： F41F3/042 , B63G8/001 , B63G8/30 , B63G2008/004 , B64C39/024 , B64C2201/08 , B64F1/04 , F41B11/72 , F41B11/80 , F41F3/07 , F42B14/06 , F42B15/105
摘要： A payload launch system is described that provides one launch solution suitable for multiple applications. A payload, such as a UAV, is launched from a sealed launch tube using compressed gas or other energy source. The launch tube can be used to transport and protect the payload from harsh environments for extended periods prior to launch.
摘要翻译：描述了有效载荷发射系统，其提供适用于多个应用的一个发射解决方案。有效载荷，如无人机，使用压缩气体或其他能源从密封发射管发射。发射管可用于在发射前长时间运输和保护有效负载免受恶劣环境的影响。

10. 发明申请

WO2013122514A1 A COUNTERMASS CONTAINER FOR USE IN A RECOILLESS WEAPON AND A RECOILLESS WEAPON COMPRISING SUCH A COUNTERMASS CONTAINER 审中-公开
标题翻译：用于复原武器的计数器容器和包含这样的计数器容器的恢复武器
公开(公告)号：WO2013122514A1
公开(公告)日：2013-08-22
申请号：PCT/SE2012/000017
申请日：2012-02-13
申请人： SAAB AB , NILSSON, Mats
发明人： NILSSON, Mats
IPC分类号： F41A1/10
CPC分类号： F41A1/10 , F41F3/042
摘要： The present invention relates to a countermass container (13) for use in a recoilless weapon (1) comprising an envelope (16) enclosing a countermass (4). The invention also refers to a recoilless weapon (1) comprising a barrel (2) accommodating an ammunition unit (3) such as a projectile or shell, a propellant charge (12) and a countermass container (13) comprising an envelope (16) enclosing a countermass (4), the barrel (2) comprising a front end opening for firing the ammunition unit (3) out of the barrel (2) and a rear end opening (15) for ejecting the comprised envelope (16) and countermass (4) of the counter mass container (13). The invention proposes a solution to symmetry problems and increases the hit rate. According to the proposed solution the envelope (16) is divided into a front section (17) and a rear section (18), the rear section ( 18) of the envelope ( 16) having a weaker construction than the front section (17) of the envelope (16) to more easily crack than the front section (17) of the envelope.
摘要翻译：本发明涉及一种用于无后坐力武器（1）的反质量容器（13），其包括封闭反质量（4）的外壳（16）。本发明还涉及一种无后坐力武器（1），其包括容纳诸如射弹或壳体的弹药单元（3）的枪管（2），推进剂装料（12）和包括外壳（16）的反质量容器（13）封闭反质量（4），所述筒体（2）包括用于将所述弹药单元（3）从所述筒体（2）中射出的前端开口和用于喷射所述包络（16）和反质量的后端开口（15）（13）的内部（4）。本发明提出了解决对称问题并提高命中率的方法。根据所提出的解决方案，外壳16被分成前部17和后部18，外壳16的后部18具有比前部17更弱的构造。的信封（16）比信封的前部（17）更容易裂开。

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