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1. 发明授权

US08430361B2 Method and device enabling a rocket engine pump to be driven by an internal combustion engine 有权
标题翻译：能够使内燃机驱动火箭发动机泵的方法和装置
公开(公告)号：US08430361B2
公开(公告)日：2013-04-30
申请号：US12680608
申请日：2008-10-07
申请人： Gerald Raymond , Paul Caye , Frederic Richard
发明人： Gerald Raymond , Paul Caye , Frederic Richard
IPC分类号： B64G1/40
CPC分类号： F02K9/46 , F02K9/563
摘要： The subject of the invention is a device for driving a pump of a rocket engine of a space vehicle that comprises an air-breathing internal combustion engine running on an oxidizer/fuel mixture of the air/hydrocarbon type, wherein the supply of oxidant and fuel is provided by tanks and a circuit that are separate from the propellant tanks of the rocket engine. The invention applies to a device for fueling a rocket engine that includes at least two pumps, each driven by the device of the invention, and means for controlling the internal combustion engines for driving the pumps, adapted for independently varying the operating parameters of these engines so as to independently adjust the rotation speeds of the pumps.
摘要翻译：本发明的主题是用于驱动太空车辆的火箭发动机的泵的装置，其包括在空气/烃类型的氧化剂/燃料混合物上运行的空气呼吸内燃机，其中氧化剂和燃料的供应由坦克和与火箭发动机的推进剂罐分开的回路提供。本发明适用于一种用于加油火箭发动机的装置，该装置包括至少两个由本发明的装置驱动的泵，以及用于控制用于驱动泵的内燃机的装置，适于独立地改变这些发动机的运行参数以便独立地调节泵的转速。

2. 发明申请

US20100252686A1 METHOD AND DEVICE ENABLING A ROCKET ENGINE PUMP TO BE DRIVEN BY AN INTERNAL COMBUSTION ENGINE 有权
标题翻译：使用内燃机驱动的发动机泵的方法和装置
公开(公告)号：US20100252686A1
公开(公告)日：2010-10-07
申请号：US12680608
申请日：2008-10-07
申请人： Gerald Raymond , Paul Caye , Frederic Richard
发明人： Gerald Raymond , Paul Caye , Frederic Richard
IPC分类号： F02K9/46
CPC分类号： F02K9/46 , F02K9/563
摘要： The subject of the invention is a device for driving a pump of a rocket engine of a space vehicle that comprises an air-breathing internal combustion engine running on an oxidizer/fuel mixture of the air/hydrocarbon type, wherein the supply of oxidant and fuel is provided by tanks and a circuit that are separate from the propellant tanks of the rocket engine. The invention applies to a device for fueling a rocket engine that includes at least two pumps, each driven by the device of the invention, and means for controlling the internal combustion engines for driving the pumps, adapted for independently varying the operating parameters of these engines so as to independently adjust the rotation speeds of the pumps.
摘要翻译：本发明的主题是用于驱动太空车辆的火箭发动机的泵的装置，其包括在空气/烃类型的氧化剂/燃料混合物上运行的空气呼吸内燃机，其中氧化剂和燃料的供应由坦克和与火箭发动机的推进剂罐分开的回路提供。本发明适用于一种用于加油火箭发动机的装置，该装置包括至少两个由本发明的装置驱动的泵，以及用于控制用于驱动泵的内燃机的装置，适于独立地改变这些发动机的运行参数以便独立地调节泵的转速。

3. 发明授权

US08226044B2 Device for reducing aerodynamic drag of a vehicale 有权
标题翻译：减少车辆气动阻力的装置
公开(公告)号：US08226044B2
公开(公告)日：2012-07-24
申请号：US12745022
申请日：2008-11-21
申请人： Gerald Raymond , Philippe Bourdieu
发明人： Gerald Raymond , Philippe Bourdieu
IPC分类号： B64G1/40
CPC分类号： B64G1/14 , B64D27/023 , B64D29/04 , B64G1/002 , F42B10/40 , F42B15/00 , Y02T50/44
摘要： A device for reducing the aerodynamic drag of a vehicle includes at least one masking element for at least one part of a nozzle of the vehicle's engine, the masking element having a resorbable material designed to be eliminated in the nozzle's flow once the engine is ignited. A space craft includes the nozzle attached to the fuselage of the space craft.
摘要翻译：用于减小车辆空气动力阻力的装置包括用于车辆发动机喷嘴的至少一部分的至少一个掩蔽元件，该掩蔽元件具有设计为一旦发动机被点燃就被消除在喷嘴流中的可再吸收材料。航天飞船包括附在飞船机身上的喷嘴。

4. 发明申请

US20110017873A1 DEVICE FOR POWERING THE PUMP OF A ROCKET ENGINE USING AN INERTIA WHEEL 有权
标题翻译：用于为动力轮驱动的发动机泵的装置
公开(公告)号：US20110017873A1
公开(公告)日：2011-01-27
申请号：US12681978
申请日：2008-10-03
申请人： Gerald Raymond
发明人： Gerald Raymond
IPC分类号： F02K9/46
CPC分类号： F02K9/563
摘要： An apparatus for driving a pump for fueling a rocket engine of a space vehicle. The apparatus comprises an inertia wheel and a transmitting device to transmit a rotation of the inertia wheel to the pump. The apparatus further comprises a measuring device to measure the rotation speed of the inertia wheel a clutching device to decouple the wheel and the pump for a speed lower than a pre-determined speed lower, which is lower than the nominal rotation speed of the wheel. The invention is particularly applicable to a space vehicle comprising a rocket engine wherein the fuel supply system comprises at least one pump driven by the apparatus of the invention and a starting device to start the apparatus while the space vehicle is in flight.
摘要翻译：一种用于驱动用于对空间车辆的火箭发动机进行加油的泵的装置。该装置包括惯性轮和传递装置，以将惯性轮的旋转传递到泵。该装置还包括测量装置，用于测量惯性轮的离合器的旋转速度，该离合器用于使车轮和泵的转速低于预定速度低于低于车轮的标称转速的预定速度。本发明特别适用于包括火箭发动机的空间飞行器，其中燃料供给系统包括由本发明的装置驱动的至少一个泵和用于在空中飞行器飞行时起动该装置的起动装置。

5. 发明授权

US08632319B2 Device for powering the pump of a rocket engine using an inertia wheel 有权
标题翻译：使用惯性轮为火箭发动机的泵供电的装置
公开(公告)号：US08632319B2
公开(公告)日：2014-01-21
申请号：US12681978
申请日：2008-10-03
申请人： Gerald Raymond
发明人： Gerald Raymond
IPC分类号： F04B49/00 , F04B23/08 , F04B9/14
CPC分类号： F02K9/563
摘要： An apparatus for driving a pump for fueling a rocket engine of a space vehicle. The apparatus comprises an inertia wheel and a transmitting device to transmit a rotation of the inertia wheel to the pump. The apparatus further comprises a measuring device to measure the rotation speed of the inertia wheel a clutching device to decouple the wheel and the pump for a speed lower than a pre-determined speed lower, which is lower than the nominal rotation speed of the wheel. The invention is particularly applicable to a space vehicle comprising a rocket engine wherein the fuel supply system comprises at least one pump driven by the apparatus of the invention and a starting device to start the apparatus while the space vehicle is in flight.
摘要翻译：一种用于驱动用于对空间车辆的火箭发动机进行加油的泵的装置。该装置包括惯性轮和传递装置，以将惯性轮的旋转传递到泵。该装置还包括测量装置，用于测量惯性轮的离合器的旋转速度，该离合器用于使车轮和泵的转速低于预定速度低于低于车轮的标称转速的预定速度。本发明特别适用于包括火箭发动机的空间飞行器，其中燃料供给系统包括由本发明的装置驱动的至少一个泵和用于在空中飞行器飞行时起动该装置的起动装置。

6. 发明申请

US20110024572A1 DEVICE FOR REDUCING AERODYNAMIC DRAG 有权
标题翻译：减少航空障碍物的装置
公开(公告)号：US20110024572A1
公开(公告)日：2011-02-03
申请号：US12745022
申请日：2008-11-21
申请人： Gerald Raymond , Philippe Bourdieu
发明人： Gerald Raymond , Philippe Bourdieu
IPC分类号： B64G1/40 , B64C1/38
CPC分类号： B64G1/14 , B64D27/023 , B64D29/04 , B64G1/002 , F42B10/40 , F42B15/00 , Y02T50/44
摘要： A device for reducing the aerodynamic drag of a vehicle includes at least one masking element for at least one part of a nozzle of the vehicle's engine, the masking element having a resorbable material designed to be eliminated in the nozzle's flow once the engine is ignited. A space craft includes the nozzle attached to the fuselage of the space craft.
摘要翻译：用于减小车辆空气动力阻力的装置包括用于车辆发动机喷嘴的至少一部分的至少一个掩蔽元件，该掩蔽元件具有设计为一旦发动机被点燃就被消除在喷嘴流中的可再吸收材料。航天飞船包括附在飞船机身上的喷嘴。

7. 发明授权

US4969211A Transceiver interference cancellation system 失效
标题翻译：收发干扰消除系统
公开(公告)号：US4969211A
公开(公告)日：1990-11-06
申请号：US150409
申请日：1988-03-15
申请人： Gerald Raymond
发明人： Gerald Raymond
IPC分类号： H01Q3/26 , H04B1/12
CPC分类号： H04B1/126 , H01Q3/2611
摘要： A transceiver interference cancellation system having an adaptive processor for receiving signals from a number of antennas and for suppressing particular signals from the antennas. The system includes a code generator which controls a switch to provide transmitted signals with a predetermined pulse code. Means including a code correlator are provided for detecting the pulse code in received signals and for controlling the operation of the adaptive processor such that wanted signals when identified are not suppressed.
摘要翻译： PCT No.PCT / GB86 / 00273 Sec。 371日期：1988年3月15日 102（e）1988年3月15日PCT提交1986年5月15日PCT公布。公开号WO87 / 07102 日期：1987年11月19日。一种收发信机干扰消除系统，具有用于从多个天线接收信号并抑制来自天线的特定信号的自适应处理器。该系统包括代码发生器，其控制开关以提供具有预定脉冲代码的发送信号。提供了包括码相关器的装置，用于检测接收信号中的脉冲码，并用于控制自适应处理器的操作，使得所识别的有用信号不被抑制。

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