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특허 상세정보

Thruster system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/033   
미국특허분류(USC) 244/322 ; 239/26519
출원번호 US-0129419 (1987-11-25)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 20  인용 특허 : 4

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 ...


A thrust control valve operable to control the supply of gas from gas generating means to provide thrust comprising: a housing for pressurized gas; conical thrust nozzle means having the smaller end thereof attached to said housing and having an axial inlet surrounded by a valve seat; valve means in said housing including means defining a tubular valve chamber aligned with said nozzle means and having an open end and a closed end and a valve member reciprocable in and sealingly engaged with the side walls of said chamber, one end of said valve member bei...

이 특허를 인용한 특허 피인용횟수: 20

  1. Le Fur, Thierry; Debons, Bernard; LaFond, Andre; Dumortier, Andre. Compact optimal and modulatable thrust device for controlling aerospace vehicles. USP2003046543717.
  2. Kranz Walter (Taufkrichen DEX). Control propulsion unit, especially for exerting transverse forces on a missile. USP1990124979697.
  3. Hayward, David G.. Flow control valve. USP2014028656941.
  4. Abel Stephen G. ; Ryan William F. ; Pepe Michael A. ; Silk Joseph P. ; Hopper Douglas T.. Force driven hot gas proportional thruster valve. USP2001056233919.
  5. Haight, Stephen D.; Chasman, Daniel; Perez, Juan A.. Hybrid missile propulsion system with reconfigurable multinozzle grid. USP2012028117847.
  6. Chasman,Daniel B.; Leal,Michael; Haight,Stephen D.. Missile control system and method. USP2007107287725.
  7. Chasman,Daniel; Haight,Stephen D.; Facciano,Andrew B.. Missile control system and method. USP2006097108223.
  8. Joseph R. Mayersak. Precision guidance system for aircraft launched bombs. USP2002106460801.
  9. Abel, Steve; Tseng, Raymond R.. Pressure assisted direct drive proportional hot-gas thruster. USP2014048707675.
  10. Tseng Raymond R.. Pressure balanced poppet valve. USP2001086276125.
  11. Chasman, Daniel; Haight, Stephen D.. Propulsion system with canted multinozzle grid. USP2010127856806.
  12. Lane, Jeffery G.; Magarro, Richard B.. Rocket engine nacelle. USP2004076758437.
  13. Cover, Cary L.; Drendel, Albert S.. Rocket thruster assembly comprising load-balanced pintle valve. USP2012078215097.
  14. Cover, Cary L.; Drendel, Albert S.. Rocket thruster comprising load-balanced pintle valve. USP2010127849695.
  15. Rohrbaugh,Eric M.; White,Jeffrey M.. Steerable, intermittently operable rocket propulsion system. USP2007107281367.
  16. Kato,Hiroshi; Takahashi,Tatsuo; Tanaka,Hideaki; Nishikawa,Tatsuya. Thrust control valve. USP2006107117681.
  17. Hidaka, Shozo; Moriwaki, Atsushi; Futahashi, Kensuke; Hosaka, Shuhei; Nagase, Masaaki; Kojima, Kohei; Inada, Mitsuru. Thrust control valve and flying object. USP20181110138844.
  18. Starken,George M.. Thruster gas control mechanism. USP2006016986497.
  19. Voigt Allan A.. Variable coupling arrangement for an integrated missile steering system. USP2001116315239.
  20. Woessner, George T.; Abel, Stephen G.; Baker, Mark H.; Alexander, Dennis M.. Vehicle, lightweight pneumatic pilot valve and related systems therefor. USP2005106951317.