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1. 发明授权

US06969025B1 Servo actuation systems 失效
标题翻译：伺服驱动系统
公开(公告)号：US06969025B1
公开(公告)日：2005-11-29
申请号：US07421629
申请日：1989-10-06
申请人： John F. Bugge , Kenneth C. Goulding , Anthony Machell
发明人： John F. Bugge , Kenneth C. Goulding , Anthony Machell
IPC分类号： G05D3/12 , F41G7/00
CPC分类号： G05D3/12 , G05B2219/34013 , G05B2219/34027 , G05B2219/42097
摘要： A dual servo system for a seeker actuator comprises a seeker head gimballed on a platform and driven in the pitch and yaw senses by respective fast, i.e. high bandwidth low ambit, servo sub-systems, the platform being pivotally mounted with respect to a base and driven in the pitch and yaw senses by respective slow, i.e. low bandwidth high ambit, servo systems. The pivotal mounting between the platform and the base is configured to provide a spherical bearing of relatively large area (typically about 85° solid angle) to provide good resistance to high acceleration loads.
摘要翻译：一种用于探测器致动器的双伺服系统包括一个探针头，该探测器头部平台放置在平台上，并以相应的快速，即高带宽低范围的伺服子系统以俯仰和偏航感驱动，平台相对于基座枢转地安装，通过相应的慢速，即低带宽高动量的伺服系统在俯仰和偏航感测中驱动。平台和底座之间的枢轴安装被配置成提供一个相对较大面积（通常约为85°立体角）的球面轴承，以提供良好的抵抗高加速度载荷。

2. 发明授权

US08973480B2 Missile canister 有权
标题翻译：导弹罐
公开(公告)号：US08973480B2
公开(公告)日：2015-03-10
申请号：US13816850
申请日：2011-08-15
申请人： Bryan Bowen , Anthony Machell , Terence Edward Kavanagh , Dennis George Turner
发明人： Bryan Bowen , Anthony Machell , Terence Edward Kavanagh , Dennis George Turner
IPC分类号： F41F3/04 , 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. 发明授权

US4955558A Reaction control system 失效
标题翻译：反应控制系统
公开(公告)号：US4955558A
公开(公告)日：1990-09-11
申请号：US308460
申请日：1989-02-10
申请人： Anthony Machell , Peter G. Foulsham
发明人： Anthony Machell , Peter G. Foulsham
IPC分类号： F02K9/88 , F42B10/66
CPC分类号： F02K9/88 , F42B10/663
摘要： A projectile reaction control system includes a nozzle assembly in which the efflux exhausted thereby may be controlled in a continuously variable fashion. In one example control is by means of a slidable piston so that the thrust developed by the nozzle assembly is substantially linearly dependent on the displacement of the piston, whereby the reaction control system may be controlled by an autopilot with little or no modification.

4. 发明申请

US20150136910A1 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：US20150136910A1
公开(公告)日：2015-05-21
申请号：US13989453
申请日：2013-03-28
申请人： Mohammed Azad Hussain , Anthony Machell , Paul Robinson , Henry Alexander Maples , Chamwit Tridech , Alexander Bismarck
发明人： Mohammed Azad Hussain , Anthony Machell , Paul Robinson , Henry Alexander Maples , Chamwit Tridech , Alexander Bismarck
IPC分类号： B64C3/38 , C08L33/26 , C08L63/00 , B64C9/00 , B64C13/28
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.
摘要翻译：用于空气车辆结构的变形皮肤，皮肤由复合材料形成，所述复合材料包括：多根纤维，包含纤维的基体，以及热敏材料，例如热塑性塑料。热敏材料可以响应于温度变化而可逆地转换，（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）加热模式热敏材料传递负载的能力降低。这可以使皮肤的刚度暂时降低，以使皮肤变形成不同的形状。

5. 发明申请

US20130139676A1 MISSILE CANISTER 有权
公开(公告)号：US20130139676A1
公开(公告)日：2013-06-06
申请号：US13816850
申请日：2011-08-15
申请人： Bryan Bowen , Anthony Machell , Terence Edward Kavanagh , Dennis George Turner
发明人： Bryan Bowen , Anthony Machell , Terence Edward Kavanagh , Dennis George Turner
IPC分类号： F41F3/042
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。

6. 发明授权

US07207254B2 Launching of missiles 有权
标题翻译：发射导弹
公开(公告)号：US07207254B2
公开(公告)日：2007-04-24
申请号：US10106530
申请日：2002-03-20
申请人： Alan J. Veitch , Anthony Machell , John W. M. Winter , Roger T. Harriss
发明人： Alan J. Veitch , Anthony Machell , John W. M. Winter , Roger T. Harriss
IPC分类号： F41F3/042 , F41F3/077
CPC分类号： F41F3/04 , F41F3/042 , F41F3/073 , F41F3/077
摘要： A missile launcher comprising a canister for housing a missile and piston based launcher, the piston being arrested in the tube after launch of the missile.
摘要翻译：一种导弹发射器，包括用于容纳基于导弹和活塞的发射器的罐，活塞在发射导弹之后被阻塞在管中。

7. 发明申请

US20060107828A1 Launching of missiles 有权
标题翻译：发射导弹
公开(公告)号：US20060107828A1
公开(公告)日：2006-05-25
申请号：US10106530
申请日：2002-03-20
申请人： Alan Veitch , Anthony Machell , John Winter , Roger Harriss
发明人： Alan Veitch , Anthony Machell , John Winter , Roger Harriss
IPC分类号： F41F3/00
CPC分类号： F41F3/04 , F41F3/042 , F41F3/073 , F41F3/077
摘要： A missile launcher comprising a canister for housing a missile and piston based launcher, the piston being arrested in the tube after launch of the missile.
摘要翻译：一种导弹发射器，包括用于容纳基于导弹和活塞的发射器的罐，活塞在发射导弹之后被阻塞在管中。

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