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1. 发明申请

WO2013007890A1 SYSTÈME DE LEURRAGE PAR CONTRE-MESURE DESTINE A ÊTRE MONTE SUR UN AÉRONEF 审中-公开
标题翻译：预计在飞机上安装的对称系统
公开(公告)号：WO2013007890A1
公开(公告)日：2013-01-17
申请号：PCT/FR2012/000275
申请日：2012-07-09
申请人： MBDA FRANCE , LE CROLLER David , ASSOULY Jean-Luc
发明人： LE CROLLER David , ASSOULY Jean-Luc
IPC分类号： F41F3/06 , F41F5/00 , F41F7/00 , F42B12/70
CPC分类号： B64D1/02 , F41A9/72 , F41F3/06 , F41F5/00 , F41F7/00 , F42B12/70
摘要： Pour permettre le lancement de projectiles de leurrage 6 avec une qualité de vol optimale, les projectiles comprennent, respectivement, des corps cylindriques extérieurs (80) dimensionnellement identiques, reçus dans ledit tube et présentant chacun un dispositif de stabilisation aérodynamique a empennages déployables (9), prenant une position repliée dans le corps lorsque le projectile est dans le tube, et une position déployée en sortie de celui-ci. Pour cela, ledit système comprend un module d'éjection des projectiles (8), a passage axial (12), agence fixement dans le prolongement du tube, à I'opposé du mécanisme d'avance, et contenant successivement, par suite du mécanisme de commande, le projectile a éjecter (6) par un dispositif d'éjection commandable (25) lie audit module.
摘要翻译：为了以最佳的飞行质量发射诱饵射弹（6），射弹分别包括尺寸相同的外部圆柱体（80），容纳在所述管中，每个具有可展翅片（9）空气动力学稳定装置当射弹在管中时，其在体内采用折叠位置，并且在管外部展开位置。为了实现这一点，所述系统包括具有轴向通道（12）的弹射射出系统（8），其固定地布置在管的延续部中，在与推进机构相反的一端，并且在控制机构之后，由与所述模块连接的可控喷射装置（25）喷射的射弹（6）。

2. 发明申请

WO2005015116A3 AIR-BASED VERTICAL LAUNCH BALLISTIC MISSILE DEFENSE 审中-公开
公开(公告)号：WO2005015116A3
公开(公告)日：2005-02-17
申请号：PCT/US2004/014245
申请日：2004-05-06
申请人： BAE SYSTEMS APPLIED TECHNOLOGIES, INC. , MCCANTS, Thomas, H., Jr.
发明人： MCCANTS, Thomas, H., Jr.
IPC分类号： F41F3/06
摘要： An air-based vertical launch system is described by means of which ballistic missile defense can be achieved effectively from a large aircraft. A method for ensuring safe missile egress is proposed. A method for ensuring that the missile strikes the ballistic missile payload section is also proposed. Together, the air basing method employing vertical (or near-vertical) launch and semi-active laser guidance yield an affordable and operationally effective missile defense against both tactical and long-range ballistic missiles. The affordability of missile defense is enhanced by the ability of an aircraft equipped with a vertical launcher to simultaneously carry out several defensive and offensive missions and to provide other capabilities such as satellite launch at other times. Methods for employing an aircraft equipped with a vertical (or near-vertical launcher) and one or more of the proposed egress assurance mechanisms in offensive ground attack missions, mine laying, and satellite launch missions are also proposed.

3. 发明申请

WO01008975A1 AEROSPACE SYSTEM 审中-公开
标题翻译：航空系统
公开(公告)号：WO01008975A1
公开(公告)日：2001-02-08
申请号：PCT/RU1999/000261
申请日：1999-07-29
IPC分类号： B64D1/10 , B64D5/00 , B64D7/08 , B64G1/00 , B64G5/00 , F41F3/06
CPC分类号： B64D5/00 , B64D1/10 , B64D7/08 , B64G1/005 , B64G5/00
摘要： The invention relates to an aerospace system designed to put payloads into low and medium orbits. In such a system, a launcher (2) provided with a payload (3) is disposed in the fuselage (5) of the mother aircraft (1), within a transport and launching container (6). A hermetic pneumatic chamber (14) contains supply members (8) for supplying the rocket with fuel and working medium, de-fueling members (9) and makeup fuel supply members (10) as well as electrical connections (11). All such elements and connections are coupled to one end of the rocket (2) by means of connectors (15). The container (6) is equipped with an automatic dropping system (7), which comprises a high-pressure system (16), and is connected to the chamber (14) by a stop valve (17). The free end (19) of the container (6) is provided with a tear-off membrane (20) and hermetically connected to the perimeter of an opening in the fuselage (5). The invention provides for a greater degree of operation safety and is more environment-friendly; moreover, the cost of putting payloads into orbit is reduced.
摘要翻译：本发明涉及一种设计用于将有效载荷置于低和中等轨道的航空航天系统。在这种系统中，在运输和发射容器（6）内，在母机（1）的机身（5）中设置具有有效载荷（3）的发射器（2）。密封气动室（14）包含用于向火箭提供燃料和工作介质的供给构件（8），减燃构件（9）和补充燃料供应构件（10）以及电气连接（11）。所有这些元件和连接通过连接器（15）联接到火箭（2）的一端。容器（6）配备有自动落下系统（7），其包括高压系统（16），并通过截止阀（17）连接到室（14）。容器（6）的自由端（19）设置有撕裂膜（20）并与机身（5）中的开口的周边气密连接。本发明提供更大程度的操作安全性并且更环保; 此外，将有效载荷投入轨道的成本降低。

4. 发明申请

WO2021126348A1 CRUISE MISSILE WEAPON ACTIVE HAZARD MITIGATION SYSTEM 审中-公开
公开(公告)号：WO2021126348A1
公开(公告)日：2021-06-24
申请号：PCT/US2020/054515
申请日：2020-10-07
申请人： RAYTHEON COMPANY
发明人： BARENTS, Dennis D. , CHRISTIANSON, Kim L. , LATTIMORE, Aaron C. , KNIGHT, Andrew K.
IPC分类号： F42B39/20 , F42B39/14 , F42B39/16 , F42B39/18 , F41F3/06 , G08B17/06 , F42B15/34
摘要： A mitigation control system is arranged in an environment containing an energetic material and includes an abnormal temperature sensor for detecting an abnormal temperature of the environment, a power source that is mechanically actuated by the abnormal temperature sensor when the abnormal temperature exceeds a predetermined abnormal temperature threshold, a mitigation controller that is actuated by the power source, and a plurality of local temperature sensors that are communicatively coupled to the mitigation controller and are arranged for detecting critical temperatures in specific regions of the environment. The mitigation controller executes a mitigation action when one of the critical temperatures exceeds a predetermined critical temperature threshold for the corresponding specific region.

5. 发明申请

WO2021019212A1 ARMING APPARATUS 审中-公开
公开(公告)号：WO2021019212A1
公开(公告)日：2021-02-04
申请号：PCT/GB2020/051759
申请日：2020-07-23
申请人： BAE SYSTEMS PLC
发明人： MURRAY, Steven Robert
IPC分类号： F41F5/00 , B64D1/04 , B64D1/06 , F41F3/06 , F42B25/00
摘要： There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an arming connector coupled with the linking connector and a first fuze input of the store; wherein each of the first attachment system and the second attachment system comprises: an arming unit; a first frangible connector coupled with the arming unit and the linking connector; and a second frangible connector coupled with the linking connector and the store.

6. 发明申请

WO2020112199A3 MUNITIONS RACK WITH STRUCTURAL ELEMENT AND INSERTABLE EJECTORS 审中-公开
公开(公告)号：WO2020112199A3
公开(公告)日：2020-06-04
申请号：PCT/US2019/049465
申请日：2019-09-04
申请人： RAYTHEON COMPANY
发明人： BAILEY, Robert A. , ERDMANN, James T. , STREIB, Stephen A. , GUERRERO, Armando , MCMAHON, Roy P. , DEHERDT, Jessica R.
IPC分类号： B64D1/04 , B64D7/08 , F41F3/06
摘要： A munitions rack includes a munitions rack structure that houses multiple compact ejectors. The structure includes a pair of internal longitudinal ribs, inboard of a pair of external longitudinal ribs. A spine of the munitions rack structure links all the ribs, and the munitions rack structure may be formed out of a single piece of material. The ribs define a pair of side recesses on the port and starboard sides of the bomb, which each may be further subdivided into a forward pocket and an aft pocket. Removable ejectors are located in the pockets. The ejectors may receive pressurized gas from pressurized gas source(s) located outside of the ejectors. The ejectors may each have multiple forward pistons and multiple aft pistons. The ejectors may include pitch control valving to control the relative amounts of pressurized gas sent to the forward piston(s) and aft piston(s).

7. 发明申请

WO2010030843A1 COMPOSITE REINFORCED MISSILE RAIL 审中-公开
标题翻译：复合强化铁路
公开(公告)号：WO2010030843A1
公开(公告)日：2010-03-18
申请号：PCT/US2009/056606
申请日：2009-09-11
申请人： RAYTHEON COMPANY , GARRISON, Robert, A. , BAILEY, Robert, A.
发明人： GARRISON, Robert, A. , BAILEY, Robert, A.
IPC分类号： F41F3/04 , F41F3/06 , B64D7/08
CPC分类号： F41F3/0406 , B64D7/08 , F41F3/06 , Y10T29/49826
摘要： According to one embodiment, an apparatus comprises a frame portion made of metal and having a substantially elongated shape. The frame portion comprises one or more cavities situated in a longitudinal direction, and a composite material is disposed within the cavities to structurally reinforce the frame portion. The frame portion includes one or more missile guides situated in the longitudinal direction and configured to slidingly engage a weapon.
摘要翻译：根据一个实施例，一种装置包括由金属制成且具有基本细长形状的框架部分。框架部分包括位于纵向方向上的一个或多个空腔，并且复合材料设置在空腔内以在结构上加强框架部分。框架部分包括位于纵向方向上的一个或多个导弹引导件并且构造成滑动地接合武器。

8. 发明申请

WO2008121431A3 MUNITIONS CONTROL UNIT 审中-公开
标题翻译：弹药控制单元
公开(公告)号：WO2008121431A3
公开(公告)日：2008-11-27
申请号：PCT/US2008052295
申请日：2008-01-29
申请人： RAYTHEON CO , SITZMANN RICHARD L , PETERS RYAN J , HAGGH ALAN
发明人： SITZMANN RICHARD L , PETERS RYAN J , HAGGH ALAN
IPC分类号： F41F3/055 , F41F3/06 , F41G7/00
CPC分类号： F41F3/06 , F41F3/055 , F41G7/007
摘要： A munitions control unit (30) for integrating existing electronics of a vehicle (10) with at least one weapon (22), wherein said existing vehicle electronics are not equipped to interface with the at least one weapon includes a first I/O interface (32) for communicating control signals with said vehicle (10), at least one second I/O interface (34a-34d, 35a-35b, 37) different from the first I/O interface (32), said at least one second I/O interface communicating control signals with said weapon (22), a processor (57) and memory (58) operatively coupled to said first and at least one second I/O interface, and reconfigurable logic stored in memory and executable by the processor. The reconfigurable logic is operative to enable the munitions control unit to interface with a plurality of vehicles having different interfaces.
摘要翻译：一种用于将车辆（10）的现有电子装置与至少一个武器（22）集成在一起的军火控制单元（30），其中所述现有车辆电子装置未被配备为与所述至少一个武器接口，所述军火控制单元包括第一I / O接口 32），用于与所述车辆（10）通信控制信号;至少一个不同于所述第一I / O接口（32）的第二I / O接口（34a-34d，35a-35b，37），所述至少一个第二I / O接口与所述武器（22）通信控制信号，可操作地耦合到所述第一和至少一个第二I / O接口的处理器（57）和存储器（58）以及存储在存储器中并且可由处理器执行的可重新配置逻辑。可重新配置逻辑可操作以使弹药控制单元能够与具有不同接口的多个车辆接口。

9. 发明申请

WO2022196597A1 誘導飛翔体ハードキルシステム审中-公开
公开(公告)号：WO2022196597A1
公开(公告)日：2022-09-22
申请号：PCT/JP2022/011152
申请日：2022-03-12
申请人：合同会社ＩＰマネジメント
发明人：吉原　和男
IPC分类号： B64C13/18 , B64D1/04 , B64D7/08 , F41F3/06
摘要：【課題】赤外線を終末誘導に採用している誘導飛翔体に対してはフレアが妨害手段として用いられるが、同時多目標処理能力を有する赤外線センサーの場合、赤外線センサーが目標の追尾を開始する前にフレアを展開しなければ、本物の目標（航空機）が追尾される可能性がある。レーダー誘導を終末誘導に採用している誘導飛翔体に対してはチャフが妨害手段として用いられるが、誘導飛翔体を欺瞞するには、大量のチャフが必要となる。また、一度欺瞞に成功しても、再度捕捉される可能性がある。【解決手段】網や弾体を広範囲に射出するハードキルシステムを航空機に搭載し、ハードキルシステムが航空機から切り離された後の軌道と、誘導飛翔体の機動を予測し、航空機から切り離されたハードキルシステムを誘導飛翔体に衝突させるよう航空機の機動を制御する事で、誘導飛翔体を物理的に無力化する誘導飛翔体ハードキルシステムを提供する。

10. 发明申请

WO2022167779A1 JETTISON AND ARMING SYSTEM 审中-公开
公开(公告)号：WO2022167779A1
公开(公告)日：2022-08-11
申请号：PCT/GB2022/050220
申请日：2022-01-27
申请人： BAE SYSTEMS PLC
发明人： GRIMSHAW, William Henry , INGRAM, Ronald Henry James
IPC分类号： F41F3/06 , B64D1/04 , B64D7/08 , F41F5/00 , F42C15/00 , F42C15/44 , F42B25/00
摘要： There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an arming clip; wherein each of the first attachment system and the second attachment system comprises: a first frangible connector coupled with the arming unit and the linking connector; and a second frangible connector comprising a first end coupled with the linking connector and a second end comprising a clip, the second end being configured to pass through a lug of said store and then couple to the second frangible connector.

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