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특허 상세정보

Detachable thrust vector mechanism for an aeronautical vehicle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/027    F42B-015/033   
미국특허분류(USC) 244/322 ; 244/324 ; 244/58 ; 244/63
출원번호 US-0005714 (1987-01-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 5
초록

A relatively inexpensive, high efficiency, detachable thrust vector mechanism is provided for addressing the current shortcomings in the art. In the illustrative embodiment, the invention is used in conjunction with a nautical or aeronautical vehicle having primary propulsion means and at least one fin movable, to provide maneuverability, in response to a conventional control system. The invention is a detachable thrust vector mechanism comprising auxiliary propulsion means pivotally attached to the missile through connecting means. Contact means are pro...

대표
청구항

A detachable thrust vector mechanism for a missile having a primary propulsion means and at least one control fin movable in response to a control system, said detachable thrust vector mechanism comprising: a ring member shaped and adapted for slidable engagement with the aft end of said missile; auxiliary propulsion means pivotally attached to said ring member; and contact means affixed to said auxiliary propulsion means and configured for contacting said at least one control fin whereby bidirectional motion of said fin produces corresponding bidirectio...

이 특허를 인용한 특허 피인용횟수: 19

  1. Facciano, Andrew B.; Lehner, Paul; Anderson, Wayne N.. Dissolvable thrust vector control vane. USP2003046548794.
  2. Fu, Jyun-Horng; Paulic, Antonio. Drag-stabilized water-entry projectile and cartridge assembly. USP2012078222583.
  3. Strayer, James David. Drone launch systems and methods. USP2018059969491.
  4. Axford, Richard Desmond Joseph; Beggs, Kevin William. Guidance device. USP2014038674277.
  5. Haight, Stephen D.; Chasman, Daniel; Perez, Juan A.. Hybrid missile propulsion system with reconfigurable multinozzle grid. USP2012028117847.
  6. Ruszkowski, Jr.,Robert A.. Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea. USP2006087097136.
  7. Black,William L.; Marian,Steven J.. Method and apparatus for determining a position of a location dependent device. USP2008097422440.
  8. Black,William L.; Marian,Steven J.. Method and apparatus for determining a position of an attitude control motor on a guided missile. USP2008107442073.
  9. Caye, Paul; Caillaud, James; Laporte, Guillaume. Method and system for piloting a flying craft with rear propulsion unit. USP2014098825231.
  10. Chasman,Daniel B.; Leal,Michael; Haight,Stephen D.. Missile control system and method. USP2007107287725.
  11. Roland Gauggel DE; Michael Arnold DE; Reinhard Kruger DE; Norbert Tranapp DE. Missile for combating stationary and/or moving targets. USP2002106462322.
  12. Teetzel, James W.; Celona, Marc J.; Lemire, Gary M.. Modular rocket system. USP2015119194678.
  13. Zasadny Philip J. ; Moore William A. ; Marrin Alf. Multiposition folding control surface for improved launch stability in missiles. USP1998105816532.
  14. Chasman, Daniel; Haight, Stephen D.. Propulsion system with canted multinozzle grid. USP2010127856806.
  15. Mueller George E. ; Pohl Henry O.. Recoverable booster stage and recovery method. USP2000126158693.
  16. Hoover, Randall L.. Releasable forward section of an underwater vehicle. USP20181010112691.
  17. Niemi, Pekka; Kautto, Jussi; Hakari, Seppo. Support member for supporting shell, and method. USP2013038387508.
  18. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.
  19. Page, Mark A.; McLarty, Doug; Fazio, Adrian; Durand, Christian; Emerick, Bob. Unmanned aerial vehicle and launch assembly. USP2009077556219.