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특허 상세정보

Fluidic thruster control and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/02   
미국특허분류(USC) 244/322 ; 137/809 ; 137/819
출원번호 US-0184604 (1980-09-05)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 1
초록

A fluidic thruster control system and method for guided missiles and the like, which utilizes a fluidic jet interaction device for controlling a downstream fluidic vortex amplifier to modulate exhaust flow through thrust nozzles.

대표
청구항

A fluidic system for porportionally controlling warm gas flow through a pair of thrust nozzles, comprising: passage means for delivering gas flow from a source to said first and second thrust nozzles in parallel flow arrangement; a pair of fluidic vortex valves each having control ports for receiving proportional fluid signals and being operable to proportionally vary the rates of flow of warm gas through each of said thrust nozzles in relation to said fluid signals whereby the total flow through both of said nozzles remains substantially constant; a flo...

이 특허를 인용한 특허 피인용횟수: 22

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  3. Bchele-Buecher Sigfrid (Meerbusch-Strmp DEX). Device for the limitation of gas pressure in a combustion chamber provided inside a projectile. USP1989024803925.
  4. Tseng,Raymond R.; Larsen,Bruce. Diverter valve with multiple valve seat rings. USP2006027000638.
  5. Gölling, Burkhard; Bauer, Matthias. Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith. USP2014098844571.
  6. Facciano, Andrew B; Alkema, Michael S; Leal, Michael A; Chasman, Daniel; Moore, Robert T. Integral injection thrust vector control with booster attitude control system. USP2015089115964.
  7. Strassman, Doron; Elkanick, Mark E.. Integrated propulsion and attitude control system from a common pressure vessel for an interceptor. USP2015038975565.
  8. Zeglar, Frank C.. Integrated vehicle fluids. USP2014118884202.
  9. Zegler, Frank C.. Integrated vehicle fluids. USP2017129850008.
  10. Asada, Haruhiko Harry; Mazumdar, Anirban. Multi-axis water jet propulsion using Coanda effect valves. USP2015129205904.
  11. Pinson George T. (Huntsville AL). Pressure gas supply for a missile and the like. USP1987084684080.
  12. Wilmot Donald W. (Decatur GA) Taylor Robert T. (Hampton VA). Projectile having nonelectric infrared heat tracking device. USP1990104964591.
  13. Dunn Michael J. (Auburn WA). Projectile with integrated propulsion system. USP1987124711414.
  14. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  15. Davies Guy E. (Hampshire GB2). Reaction jet control system. USP1989084856734.
  16. Christensen Donald Jeffrey. Spherical chamber fluidic ball diverter valve. USP1999075927335.
  17. Dunne Brian B. (La Jolla CA). Spin-stabilized projectile with pulse receiver and method of use. USP1990084951901.
  18. 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.
  19. 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.
  20. Fujita,Toshiharu; Hidaka,Shozo. Three-axis attitude control propulsion device and flying object comprising the same. USP2006097102113.
  21. Kirschner ; Jr. Thomas J.. Thrusting apparatus. USP2001116315238.
  22. Moll, Manfred. Wing-stabilized projectile. USP1985094541592.