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1. 发明授权

US4826104A Thruster system 失效
标题翻译：推力系统
公开(公告)号：US4826104A
公开(公告)日：1989-05-02
申请号：US129419
申请日：1987-11-25
申请人： James Bennett , Martin R. Heath , Peter G. Foulsham
发明人： James Bennett , Martin R. Heath , Peter G. Foulsham
IPC分类号： F02K9/80 , F42B15/033
CPC分类号： F02K9/805 , F42B10/663
摘要： A thrust control valve which is operable to direct a gas supply to provide thrust is disclosed. The gas supply to obtained from a hot gas generator eg a rocket motor combustion chamber, and is directed through a nozzle by the operation of a plunger mounted within a pressure chamber. The pressure in the pressure chamber is controlled by the operation of a solenoid-operated poppet valve which moves between two positions to either pressurize the chamber ie sealing the nozzle with the plunger to provide no thrust, or to de-pressurize the chamber ie allowing gas from the gas supply to exit via the nozzle thereby providing thrust.
摘要翻译：公开了可操作以引导气体供应以提供推力的推力控制阀。从热气发生器例如火箭发动机燃烧室获得的气体供应，并且通过安装在压力室内的柱塞的操作而被引导通过喷嘴。压力室中的压力通过电磁操作的提升阀的操作来控制，该提升阀在两个位置之间移动以对腔室进行加压，即，用柱塞密封喷嘴以提供推力，或者对腔室进行减压，即允许气体从气体供应通过喷嘴出口，从而提供推力。

2. 发明授权

US5720448A Shock absorbers 失效
标题翻译：减震器
公开(公告)号：US5720448A
公开(公告)日：1998-02-24
申请号：US666121
申请日：1991-03-01
申请人： Peter G. Foulsham , Stewart E. Woolsey
发明人： Peter G. Foulsham , Stewart E. Woolsey
IPC分类号： F16F1/12 , F16F7/08 , F42B15/04 , F41G7/32
CPC分类号： F16F1/12 , F16F7/08 , F42B15/04
摘要： This invention relates to a shock absorber for use with a command link controlled missile system. The shock absorber being designed to absorb the shocks produced by launch and missile movements and being particularly applicable to fibre optic command link systems.
摘要翻译：本发明涉及一种与指挥链控制导弹系统一起使用的减震器。减震器设计用于吸收由发射和导弹运动产生的冲击，特别适用于光纤命令链路系统。

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.

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