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특허 상세정보

Aircraft with active center of gravity control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-037/00   
미국특허분류(USC) 244/135.C; 244/093; 701/001; 701/003; 073/065.05
출원번호 US-0656501 (2003-09-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Koestner Bertani LLP
인용정보 피인용 횟수 : 25  인용 특허 : 9
초록

A supersonic aircraft comprises a wing, a fuselage, a plurality of fuel tanks contained within the wing and/or fuselage, and a fuel transfer system communicatively coupled to the plurality of fuel tanks and capable of transferring fuel among the plurality of fuel tanks. The aircraft further comprises at least one sensor capable of indicating a flight parameter and a controller. The controller is coupled to the one or more sensors and to the fuel transfer system. The controller can transfer fuel among the plurality of fuel tanks and adjust the aircraft ce...

대표
청구항

1. A supersonic aircraft comprising:an aerodynamic body; a plurality of fuel tanks contained within the aerodynamic body; a fuel transfer system communicatively coupled to the plurality of fuel tanks and capable of transferring fuel among the plurality of fuel tanks; at least one sensor capable of indicating a flight parameter; and a controller coupled to the at least one sensor and the fuel transfer system, the controller configured to transfer fuel among the plurality of fuel tanks to position the aircraft center-of-gravity in a relatively aft position...

이 특허를 인용한 특허 피인용횟수: 25

  1. Cutler, Theron L.; Shelly, Mark A.. Aerial refueling system. USP2010027665479.
  2. Cutler,Theron L.; Shelly,Mark A.. Aerial refueling system. USP2008127458543.
  3. Burris, Curt B.. Aerodynamic wing load distribution control. USP2015048998132.
  4. Tanner, Richard Bruce. Aircraft spillover fuel tank. USP2012058172182.
  5. Neto, Rubens Domecildes. Continuous fuel management system for automatic control of aircraft center of gravity. USP2012078226040.
  6. Moser, Matthew A.; Finn, Michael R.; Thoreen, Adam. Control interface for leading and trailing edge devices. USP2017059656741.
  7. McDonough, Terry L.; Kernast, Magnus; Padilla, Carlos E.; Tillotson, Shane C.. Determining a profile for an aircraft prior to flight using a fuel vector and uncertainty bands. USP2016069361486.
  8. Helppi, Benjamin M.; McCormick, Douglas M.; Ayala, Marc. Event depiction on center of gravity curve. USP20180910082439.
  9. Johnson, Richard A.; Penty, Michael J.; Striefel, Michael A.; Duranti, Thomas R.; Duranti, legal representative, Diane. Fuel balancing system. USP2009097591277.
  10. Moser, Matthew A.; Liu, Benjamin M.; Finn, Michael R.. Leading and trailing edge device deflections during descent of an aircraft. USP2016059327827.
  11. Moser, Matthew A.; Gardner, Mark J.; Finn, Michael R.; Good, Mark S.; Malachowski, Adam P.; Thommen, Monica E.; Amorosi, Stephen R.; Onu, Dan. Leading edge variable camber system and method. USP2015119180962.
  12. Heaven, Jr., George H.; Walden, Michael K.. Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments. USP2011027878449.
  13. Almalki, Mohammad F.; Elshafei, Moustafa. Method and apparatus for tracking center of gravity of air vehicle. USP2012098260477.
  14. Delporte, Martin; Essadouni, Malika. Method and device for correcting the lateral dissymmetry of an aircraft. USP2012078231082.
  15. Paillard, Pierre; Larcher, David. Method and system for maneuvering an aircraft by shifting its center of gravity. USP2013108548721.
  16. Klooster, Joel Kenneth. Method for flying an aircraft along a flight path. USP2014028645009.
  17. Spottiswoode, Michael; Burckhart, Antoine; Sjungargard, Petter. Method of controlling the centre of gravity of an aircraft. USP2014088814096.
  18. Moser, Matthew A.; Finn, Michael R.; Liu, Benjamin M.. Optimized flap positioning for go-around operations. USP2016029254909.
  19. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Murphy, Robert M.; Thoreen, Adam. System and method for optimizing performance of an aircraft. USP2016069359065.
  20. Preus, Robert W.. System for providing dynamic pitch control in a wind turbine. USP2013118573937.
  21. Freund, Donald. Systems and methods for controlling a magnitude of a sonic boom. USP20181010093410.
  22. Freund, Donald. Systems and methods for controlling a magnitude of a sonic boom. USP2016099446839.
  23. Freund, Donald. Systems and methods for controlling a magnitude of a sonic boom. USP2017029561847.
  24. Freund, Donald. Systems and methods for controlling a magnitude of a sonic boom. USP2017029580169.
  25. Alber, Mark R.. Vehicle with asymmetric nacelle configuration. USP2018069988148.