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특허 상세정보

Variable coupling arrangement for an integrated missile steering system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/003.22 ; 600/228 ; 239/265.29 ; 239/265.31 ; 244/169
출원번호 US-0935571 (1997-09-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bissell
인용정보 피인용 횟수 : 15  인용 특허 : 7
초록

An integrated system for missile steering, which uses both jet reaction control (JRC) and aerofin control systems, is provided with a variable coupling mechanism for adjusting the relative responsiveness of the two systems in accordance with the pressurization state of the JRC system pressure chamber. In one embodiment, the pivoting action of a joystick which actuates the gas flow control pintles of the JRC system is permitted only under sufficient pressurization of the pressure chamber. In a second embodiment, the extent to which the pintles protrude fr...

대표
청구항

[ What is claimed is:] [1.]1. Variable response jet reaction control apparatus for controlling the flight of a missile, said apparatus comprising:a pressure chamber;a plurality of thrust nozzles in communication with said pressure chamber, said thrust nozzles adapted for directional emission of gases generated in said pressure chamber;a movably mounted gas flow controller;a plurality of pintles each associated with a corresponding one of said plurality of thrust nozzles, said pintles adapted to vary the flow of gases through said thrust nozzles in respon...

이 특허를 인용한 특허 피인용횟수: 15

  1. Morgan, Robert W; Normoyle, James P; Wuest, Kurt J; Drake, David. Air vehicle with control surfaces and vectored thrust. USP2015099121680.
  2. Schroeder,Richard W.. Fin retention and deployment mechanism. USP2009017475846.
  3. Smith,Douglas L.; Morris,Joseph P.. Frictional roll control apparatus for a spinning projectile. USP2008087412930.
  4. Kim,Won Hoon; Bae,Joo Chan; Lim,Seong Taek; Park,Sung Han. Jet vane thrust vector control system. USP2008017313910.
  5. Lawandy, Nabil M.; Conroy, Jeffrey L.; Smuk, Andrei. Marking articles using a covert digitally watermarked image. USP2009057529385.
  6. Lawandy,Nabil M.; Conroy,Jeffrey L.; Smuk,Andrei. Marking articles using a covert digitally watermarked image. USP2007027184569.
  7. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016019242745.
  8. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  9. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  10. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016049302790.
  11. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  12. Morris,Joseph P.; Smith,Douglas L.. Projectile trajectory control system. USP2008047354017.
  13. Ericson,Charles R.; May,Michael C.. Tandem motor actuator. USP2007087255304.
  14. Kawai, Ronald Tatsuji. Thrust vectoring system and method. USP2012088240125.
  15. Fink,Lawrence E.. Two-axis thrust vectoring nozzle. USP2007057216476.