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특허 상세정보

Spoiler torque controlled supersonic missile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/62   
미국특허분류(USC) 244/321 ; 244/327
출원번호 US-0626510 (1990-12-12)
우선권정보 FR-0016406 (1989-12-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 18  인용 특허 : 0
초록

A supersonic guided missile has a fuselage terminating at the front in a nose and at the rear in a base and is provided externally with fixed rear planes. At a longitudinal distance from the center of gravity is at least one spoiler mobile transversely between a configuration retracted inside the fuselage and an active configuration in which the spoiler projects laterally from the fuselage.

대표
청구항

Supersonic guided missile comprising a fuselage terminating in a front nose and in a rear base and provided externally with fixed aft planes and a torque inducing device comprising at a longitudinal distance from the center of gravity of said missile, at least one spoiler transversely mobile between a configuration retracted inside said fuselage and an active deployed configuration in which said spoiler projects laterally from said fuselage.

이 특허를 인용한 특허 피인용횟수: 18

  1. Alban, III, William H.; Johnston, Karl A.; Eiswirth, Edward A.; Morgan, David E.. Aerodynamic re-entry vehicle control with active and passive yaw flaps. USP2009117611095.
  2. Zachrisson, Björn. Arrangement and method for launching counter-measures. USP2013078490924.
  3. Clancy,John A.; Bybee,Thomas D.; Friedrich,William A.. Fixed canard 2-D guidance of artillery projectiles. USP2006016981672.
  4. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  5. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  6. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  7. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  8. Grau, John C.; Fiorellini, Arthur J.; Carr, Raymond E.. Jump correcting projectile system. USP2003106629668.
  9. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  10. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  11. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  12. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  13. Finn Kevin P. (Tucson AZ) Schwartz ; II Homer H. (Oro Valley AZ) Connel Tim S. (Tucson AZ) Snyder Richard J. (Tucson AZ) Oh Youn H. (Oro Valley AZ). Missile having non-cylindrical propulsion section. USP1997105677508.
  14. Cahayla, Jason R.. Pneumatically actuated control surface for airframe body. USP2013098525090.
  15. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  16. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  17. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  18. Tyree, Anthony K.. System and method for navigating an object. USP2013088502126.