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특허 상세정보

Vehicle rotation and control mechanism

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/14    F42B-010/50    F42B-015/01    B64G-001/62   
미국특허분류(USC) 244/160 ; 244/138A ; 244/139 ; 244/063 ; 244/032.8 ; 102/384 ; 102/388
출원번호 US-0719457 (1996-09-25)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Harness Dickey & Pierce P.L.C.
인용정보 피인용 횟수 : 18  인용 특허 : 6
초록

A nose assembly and method for controlling the rotation and stabilizing the orientation of a vehicle during landing maneuvers. The vehicle includes a nose assembly that is coupled to an airframe thereof and that has a frame and flap assembly. The flap assembly includes an actuating means and a flap coupled to the frame such that the actuating means moves the flap from and between a fully retracted position and a fully extended position in response to a guidance signal received from a flight control computer. In a preferred embodiment of the present inven...

대표
청구항

[ What is claimed is:] [1.] A vehicle adapted to be launched into orbit about the earth and to return to the earth without jettisoning any portions of the vehicle, said vehicle comprising:an airframe; anda nose assembly coupled to said airframe, said nose assembly including a frame and a flap assembly having a plurality of independent flaps coupled to said frame for independent movement from and between fully retracted positions and fully extended positions, said flap assembly further including an actuating assembly for moving said flaps from and between...

이 특허를 인용한 특허 피인용횟수: 18

  1. August,Henry. Aerodynamic control of a hypersonic entry vehicle. USP2007067229048.
  2. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118894016.
  3. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118878111.
  4. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118876059.
  5. Boelitz, Frederick W.. Compensating for wind prior to engaging airborne propulsion devices. USP2013048424808.
  6. Grillos, Emmanuel; Trimble, Dennis Arthur; Grose, Douglas Lewis. Composite structures for aerospace vehicles, and associated systems and methods. USP2015079079674.
  7. Grillos, Emmanuel; Trimble, Dennis Arthur; Grose, Douglas Lewis. Composite structures for aerospace vehicles, and associated systems and methods. USP2016109469418.
  8. Featherstone, Mark. Control surfaces for use with high speed vehicles, and associated systems and methods. USP2015038991767.
  9. Featherstone, Mark; Boelitz, Frederick W.; Ramsey, Roger E.; Biggs, David M.. Control surfaces for use with high speed vehicles, and associated systems and methods. USP2017029580191.
  10. Auger, Valery; Balemboy, Christophe; Laine, Robert Andre; Perkinson, Marie-Claire. Landing device for a space probe, and landing method for a probe provided with such a device. USP2015038991764.
  11. Boelitz, Frederick W.; Featherstone, Mark; Gil, Christopher M.; Ramsey, Roger E.; Biggs, David M.. Launch vehicles with fixed and deployable deceleration surfaces, and/or shaped fuel tanks, and associated systems and methods. USP2013048408497.
  12. Featherstone, Mark; Sanders, John Michael; Ramsey, Roger E.; Wetzel, Eric David. Launch vehicles with ring-shaped external elements, and associated systems and methods. USP2016119487308.
  13. Boelitz, Frederick W.; Hilstad, Mark O.. Predicting and correcting trajectories. USP2014058729442.
  14. Janeke, Charl E.. Reversible space plane. USP2012078215589.
  15. Janeke, Charl E.. Reversible space plane. USP2013088505852.
  16. Janeke, Charl E.. Reversible space plane. USP2010047690601.
  17. Janeke,Charl E.. Reversible space plane. USP2008037344111.
  18. Bezos, Jeffrey P.; Lai, Gary; Findlay, Sean R.. Sea landing of space launch vehicles and associated systems and methods. USP2014038678321.