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특허 상세정보

Aircraft having an aft engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00    B64C-001/16    B64D-027/14    B64D-029/00   
출원번호 US-0859549 (2015-09-21)
등록번호 US-9637217 (2017-05-02)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    GE Global Patent Operation
인용정보 피인용 횟수 : 1  인용 특허 : 37
초록

An aircraft is provided including a fuselage and an aft engine. The fuselage defines a top side, a bottom side, and a frustum located proximate an aft end of the aircraft. The frustum defines a top reference line extending along the frustum at a top side of the fuselage, and a bottom reference line extending along the frustum at a bottom side of the fuselage. The top and bottom reference lines meet at a reference point aft of the frustum. The fuselage further defines a recessed portion located aft of the frustum and indented inwardly from the bottom refe...

대표
청구항

1. An aircraft extending between a forward end and an aft end, the aircraft comprising: a fuselage defining a top side and a bottom side, the fuselage additionally defining a frustum located proximate the aft end of the aircraft, the frustum defining a top reference line extending along the frustum at the top side of the fuselage and a bottom reference line extending along the frustum at the bottom side of the fuselage, the top and bottom reference lines meeting at a reference point located aft of the frustum, the fuselage further defining a recessed por...

이 특허에 인용된 특허 (37)

  1. Chene, Gilles; Gantie, Fabrice; Porte, Alain. Acoustic coating for an aircraft incorporating a frost treatment system by joule effect. USP2012058181900.
  2. Shammoh, Ali A. A. J.. Adjustable angle inlet for turbojet engines. USP2013108544793.
  3. Roche, Frederic. Aircraft engine assembly comprising a junction aerodynamic fairing mounted on two separate elements. USP2012048162254.
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  8. Reyes Daniel (233 Broadway ; Rm 3615 New York NY 10007). Airplane powered by vehicular motor. USP1986084605185.
  9. Cazals, Olivier. Beam mounted rear propulsion system for an aircraft and aircraft with such system. USP2012078220739.
  10. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian. Cantilevered tip turbine engine. USP2011108033094.
  11. Neto, Rubens Domecildes. Continuous fuel management system for automatic control of aircraft center of gravity. USP2012078226040.
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  14. Bulin, Guillaume; Perret, Severine; Rogero, Jean-Michel. Electric generator disposed on a rotating turboprop part. USP2014118890343.
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  18. Moniz,Thomas Ory; Orlando,Robert Joseph. Gas turbine engine assembly and methods of assembling same. USP2009027493754.
  19. Suciu, Gabriel L.; Alvanos, Ioannis. Gas turbine engine buffer cooling system. USP2015059038398.
  20. Wynosky Thomas A. (Madison CT). Gas turbine engine nacelle. USP1988024722357.
  21. Hoffjann, Claus; Schuldzig, Hansgeorg; Westenberger, Andreas. Hybrid drive for an aircraft. USP2014028640439.
  22. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas A.; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor rotor. USP2013128596036.
  23. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor stator. USP2012028109073.
  24. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas A.; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable compressor stator. USP2013108549833.
  25. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable propeller/fan. USP2012018099944.
  26. Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable propeller/fan. USP2014108857191.
  27. Foster, Glenn B.; Hyde, Roderick A.; Ishikawa, Muriel Y.; Jung, Edward K. Y.; Kare, Jordin T.; Myhrvold, Nathan P.; Tegreene, Clarence T.; Weaver, Thomas Allan; Wood, Jr., Lowell L.; Wood, Victoria Y. H.. Hybrid propulsive engine including at least one independently rotatable turbine stator. USP2012108291716.
  28. Quiroz-Hernandez, Esteban. Method for balancing a propulsive system having non-hull contra-rotating propellers. USP2015048998580.
  29. Gruensfelder Cynthia Ann ; Wille Robert Henry. Mission adaptive inlet. USP2000076089505.
  30. Thompson, Ewan F. Mounting arrangement. USP2005126976655.
  31. Cazals, Olivier; Genty de la Sagne, Jaime; Rittinghaus, Denis. Multi-engine aircraft. USP2011037905449.
  32. Parente Charles A.. Noise suppression system for a jet engine. USP1998025721402.
  33. Stolte, Ralf-Henning. Power distribution system. USP2014038672263.
  34. Kuhn, Jr., Ira F.. Purebred and hybrid electric VTOL tilt rotor aircraft. USP2013068469306.
  35. Kouros, Areian; Aubert, Roger; Madej, Paul. System and method of augmenting power in a rotorcraft. USP2015018939399.
  36. Suciu, Gabriel L.; Merry, Brian. Tip turbine engine support structure. USP2011077976273.
  37. McComb, James G.. Unconventional integrated propulsion systems and methods for blended wing body aircraft. USP2010027665689.