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특허 상세정보

System for steering a missile by means of lateral gas jets

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66   
미국특허분류(USC) 244/322
출원번호 US-0665899 (1991-03-07)
우선권정보 FR-0003253 (1990-03-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 17  인용 특허 : 0
초록

A system is disclosed for steering a missile by means of gas jets, comprising a gas generator connectable to at least a pair of lateral nozzles via rotary valving means, movable under the action of drive means and controlling the passage of the gases through said nozzles wherein with each nozzle is associated an individual rotary valving member; each valving member is controlled in rotation by the piston of a jack, one chamber of which receives a part of the gas generated by said gas generator, the position of said piston being controlled by controlling ...

대표
청구항

A system for steering a missile by means of gas jets, comprising a gas generator connectable to at least a pair of lateral nozzles via rotary valving means, movable under the action of drive means and controlling the passage of the gases through said nozzles: wherein with each nozzle is associated an individual rotary valving member; each valving member is controlled in rotation by the piston of a jack, one chamber of which receives a part of the gas generated by said gas generator, the position of said piston being controlled by controlling the flowrate...

이 특허를 인용한 특허 피인용횟수: 17

  1. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  2. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  3. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  4. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP200108RE37331.
  5. Bergmann, Edward; London, Brian; Dineen, Andrew. Guidance control system for projectiles. USP2012098269156.
  6. Strassman, Doron; Elkanick, Mark E.. Integrated propulsion and attitude control system from a common pressure vessel for an interceptor. USP2015038975565.
  7. Zeglar, Frank C.. Integrated vehicle fluids. USP2014118884202.
  8. Zegler, Frank C.. Integrated vehicle fluids. USP2017129850008.
  9. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  10. Voigt Che-Ram S. (Geyserville CA). Mechanism for thrust vector control using multiple nozzles. USP1997095662290.
  11. Schroeder Wayne K.. Method and apparatus for rapidly turning a vehicle in a fluid medium. USP2001106308911.
  12. Blackburn, Thomas R.. Methods and apparatus for guiding a projectile. USP2011017872215.
  13. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  14. Carlson, Robert J.. Steerable projectile charging system. USP2013018362408.
  15. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  16. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  17. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.