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1. 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。

2. 发明申请

WO2015008037A1 A THRUST FLOW POWERED VEHICLE 审中-公开
标题翻译：推力动力车
公开(公告)号：WO2015008037A1
公开(公告)日：2015-01-22
申请号：PCT/GB2014/052114
申请日：2014-07-10
申请人： MBDA UK LIMITED
发明人： POULTON, Ross William , LEE, Daemon , HUSSAIN, Mohammad Azad , MACHELL, Anthony
IPC分类号： F02K9/80 , F02K9/90 , F02K1/00
CPC分类号： F02K1/78 , B63H11/12 , B64G1/40 , F02K1/002 , F02K9/805 , F02K9/90
摘要： Thrust flow powered vehicle (100) comprising a first thrust flow expeller (130) for expelling a first thrust flow in a first direction, a second thrust flow expeller (131) for expelling a second thrust flow in a second direction, the second direction being a different direction to the first direction but sharing a plane with the first direction, a thrust flow deflector surface (124) at an angle to the plane of the first and second directions, and an outlet portion for providing an output thrust flow, such that, in use, the thrust flow deflector surface deflects at least a portion of both the first and second thrust flows to form the output thrust flow such that the output thrust flow has a component in the plane of the first and second directions, and a component out of that plane.
摘要翻译：推力流动动力车辆（100）包括用于排出第一方向上的第一推力流的第一推力流动推进器（130），用于沿第二方向排出第二推力流的第二推力流动推进器（131），所述第二方向为与第一方向不同的方向，但是与第一方向共享平面，与第一和第二方向的平面成一定角度的推力流动偏转器表面（124）以及用于提供输出推力流的出口部分，使得在使用中，推力流动偏转器表面使第一和第二推力流的至少一部分偏转以形成输出推力流，使得输出推力流在第一和第二方向的平面中具有分量，出了那架飞机。

3. 发明申请

WO2013144639A1 COMPOSITE MATERIAL SUITABLE FOR A MORPHING SKIN 审中-公开
标题翻译：复合材料适用于变形皮肤
公开(公告)号：WO2013144639A1
公开(公告)日：2013-10-03
申请号：PCT/GB2013/050826
申请日：2013-03-28
申请人： MBDA UK LIMITED , IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE
发明人： MACHELL, Anthony , HUSSAIN, Mohammed Azad , ROBINSON, Paul , MAPLES, Henry Alexander , BISMARCK, Alexander , TRIDECH, Charnwit
IPC分类号： B29C61/06 , B29C70/88 , B64C3/44
CPC分类号： B64C3/38 , B29C61/00 , B29C70/086 , B29C70/205 , B64C3/20 , B64C9/00 , B64C13/28 , B64C2003/445 , C08L33/26 , C08L63/00 , Y02T50/43
摘要： A morphing skin for an air vehicle structure, the skin being formed by a composite material (1) comprising: a multiplicity of fibres (3), a matrix (5) incorporating the fibres, and a thermo-sensitive material (7) such as a thermo-plastic. The thermo-sensitive material (7) is reversibly transitionable in response to a change in temperature, between (i) an ambient temperature mode in which the thermo-sensitive material is capable of transferring loads in the composite material, and (ii) a heated mode in which the ability of the thermo-sensitive material to transfer the loads is reduced. This allows the stiffness of the skin to be temporarily reduced to enable the skin to be morphed into a different shape.
摘要翻译：用于空气车辆结构的变形皮肤，所述皮肤由复合材料（1）形成，所述复合材料（1）包括：多根纤维（3），包含所述纤维的基体（5）和热敏材料（7），例如热塑性塑料。热敏材料（7）响应于温度变化而可逆地转变，（i）热敏材料能够传递复合材料中的载荷的环境温度模式，和（ii）加热的降低了热敏材料传递负载的能力的模式。这允许临时减少皮肤的刚度，以使皮肤变形成不同的形状。

4. 发明公开

EP2606307A1 MISSILE CANISTER 有权
标题翻译： LENKFLUGKÖRPERBEHÄLTER
公开(公告)号：EP2606307A1
公开(公告)日：2013-06-26
申请号：EP11745574.1
申请日：2011-08-15
申请人： MBDA UK Limited
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.

5. 发明授权

EP2830857B1 COMPOSITE MATERIAL SUITABLE FOR A MORPHING SKIN 有权
公开(公告)号：EP2830857B1
公开(公告)日：2019-02-06
申请号：EP13713485.4
申请日：2013-03-28
申请人： MBDA UK Limited , Imperial College of Science, Technology and Medicine
发明人： MACHELL, Anthony , HUSSAIN, Mohammed Azad , ROBINSON, Paul , MAPLES, Henry Alexander , BISMARCK, Alexander , TRIDECH, Charnwit
IPC分类号： B29C61/06 , B29C70/88 , B64C3/44

6. 发明公开

EP2830857A1 COMPOSITE MATERIAL SUITABLE FOR A MORPHING SKIN 审中-公开
标题翻译：可变形水面上合适的复合材料
公开(公告)号：EP2830857A1
公开(公告)日：2015-02-04
申请号：EP13713485.4
申请日：2013-03-28
申请人： MBDA UK Limited , Imperial College of Science, Technology and Medicine
发明人： MACHELL, Anthony , HUSSAIN, Mohammed Azad , ROBINSON, Paul , MAPLES, Henry Alexander , BISMARCK, Alexander , TRIDECH, Charnwit
IPC分类号： B29C61/06 , B29C70/88 , B64C3/44
CPC分类号： B64C3/48 , B29C61/00 , B29C70/086 , B29C70/205 , B64C3/20 , B64C2003/445 , C08L33/26 , C08L63/00 , Y02T50/43
摘要： A morphing skin for an air vehicle structure, the skin being formed by a composite material which includes: a multiplicity of fibres, a matrix incorporating the fibres, and a thermo-sensitive material, such as a thermo-plastic. The thermo-sensitive material can be reversibly transitionable in response to a change in temperature, between (i) an ambient temperature mode in which the thermo-sensitive material is capable of transferring loads in the composite material, and (ii) a heated mode in which the ability of the thermo-sensitive material to transfer the loads is reduced. This can allow the stiffness of the skin to be temporarily reduced to enable the skin to be morphed into a different shape.

7. 发明公开

EP3022429A1 A THRUST FLOW POWERED VEHICLE 有权
标题翻译：逆冲流动力车辆
公开(公告)号：EP3022429A1
公开(公告)日：2016-05-25
申请号：EP14739539.6
申请日：2014-07-10
申请人： MBDA UK Limited
发明人： POULTON, Ross William , LEE, Daemon , HUSSAIN, Mohammad Azad , MACHELL, Anthony
IPC分类号： F02K9/80 , F02K9/90 , F02K1/00
CPC分类号： F02K1/78 , B63H11/12 , B64G1/40 , F02K1/002 , F02K9/805 , F02K9/90
摘要： Thrust flow powered vehicle (100) comprising a first thrust flow expeller (130) for expelling a first thrust flow in a first direction, a second thrust flow expeller (131) for expelling a second thrust flow in a second direction, the second direction being a different direction to the first direction but sharing a plane with the first direction, a thrust flow deflector surface (124) at an angle to the plane of the first and second directions, and an outlet portion for providing an output thrust flow, such that, in use, the thrust flow deflector surface deflects at least a portion of both the first and second thrust flows to form the output thrust flow such that the output thrust flow has a component in the plane of the first and second directions, and a component out of that plane.

8. 发明授权

EP2606307B1 MISSILE CANISTER 有权
标题翻译：导弹TANK
公开(公告)号：EP2606307B1
公开(公告)日：2016-11-23
申请号：EP11745574.1
申请日：2011-08-15
申请人： MBDA UK Limited
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

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