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특허 상세정보

Reaction control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66   
미국특허분류(USC) 244/322
출원번호 US-0308460 (1989-02-10)
우선권정보 GB-0003164 (1988-02-11)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 11  인용 특허 : 3
초록

A projectile reaction control system includes a nozzle assembly in which the efflux exhausted thereby may be controlled in a continuously variable fashion. In one example control is by means of a slidable piston so that the thrust developed by the nozzle assembly is substantially linearly dependent on the displacement of the piston, whereby the reaction control system may be controlled by an autopilot with little or no modification.

대표
청구항

A projectile including a reaction control system, said system including at least one nozzle assembly, said at least one nozzle assembly comprising a housing defining a nozzle outlet means and a bore adjacent said outlet, a piston means located in said bore and movable to open or to close said nozzle outlet means, drive means for moving said piston means and passage means extending through said piston means whereby the pressure at one end of said piston and means is transmitted to the other end thereof.

이 특허를 인용한 특허 피인용횟수: 11

  1. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  2. Hibma Richard A. ; Hilscher Richard W. ; Miralles Carlos T. ; Ward Jerry D. ; Wright Blaine G.. Apparatus for defending a vehicle against an approaching threat. USP2001056231003.
  3. Blake, Jesse H.; Murphy, Matthew G.. Bang-bang control using tangentially mounted surfaces. USP2014088816261.
  4. Fago, Frank M.; Knipfer, James E.; Neer, Charles S.. Hydraulic remote for a medical fluid injector. USP2016069375557.
  5. Fago, Frank M.; Knipfer, James E.; Neer, Charles S.. Hydraulic remote for a medical fluid injector. USP2012028118780.
  6. Hallum, Charles E.. Integrated valve assembly. USP199209H001098.
  7. Arkhangelsky Ivan Ivanovitch,RUX ; Bolotov Eugene Gueorguevitch,RUX ; Philippov Vladimir Sergueevitch,RUX ; Mizrokhi Vladimir Yakovlevitch,RUX ; Svetlov Vladimir Grigorievitch,RUX ; Stanevsky Gregory. Missile launching and orientation system. USP1998105823469.
  8. Joseph R. Mayersak. Precision guidance system for aircraft launched bombs. USP2002106460801.
  9. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  10. 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.
  11. Voigt Allan A.. Variable coupling arrangement for an integrated missile steering system. USP2001116315239.