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특허 상세정보

Detachable integral aircraft tailcone and power assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/054 ; 244/055 ; 244/120 ; 244/248 ; 244/554
출원번호 US-0455608 (1999-12-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Desmond, Esq.
인용정보 피인용 횟수 : 30  인용 특허 : 1
초록

The present invention provides a tailcone and power assembly mountable to the body of an aircraft using a height adjustable dolly. The tailcone assembly comprises a longitudinal support member, a gas turbine engine mounted to the support member; a firewall; two curved rotatable casings hingeably connected to the support member; an inlet duct extending from an aperture in one of the rotatable casings to the engine inlet; an integral exhaust casing, and interface means for making necessary engine accessory connections to the aircraft. The tailcone is insta...

대표
청구항

[ What is claimed is:] [1.]1. An aircraft tailcone assembly comprising:a longitudinal support member having forward and aft axial ends;a gas turbine engine mounted within said tailcone to said support member, said engine having an inlet and an exhaust;a firewall extending from said support member forward of said engine;at least one curved rotatable casing hingeably connected to said support member and rotatable from a closed position to an open position thereby exposing said engine;an inlet duct extending from an aperture in one of said rotatable casings...

이 특허를 인용한 특허 피인용횟수: 30

  1. Buchheit, Catherine. Aircraft provided with a fuel cell system. USP2013098523105.
  2. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2011118061650.
  3. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2011027891605.
  4. Nguyen,Phuong H.; Sikora,Joseph A.; Campbell,Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2008047364116.
  5. Williams,Nicholas A.. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner. USP2008047350619.
  6. DeDe, Brian C.; Martinez, David Eugene; Lau, David; Tate, Mark C.. Auxiliary power unit fire enclosure. USP2014018631637.
  7. DeDe, Brian C.; Lau, David; Adair, David Ronald; Schade, Christine Ingrid. Auxiliary power unit fire enclosure drain seal. USP2014098820045.
  8. Williams, Nicholas A.; Dittmar, Kevin S.. Auxiliary power unit with integral firebox. USP2009057526921.
  9. Cazals, Olivier. Beam mounted rear propulsion system for an aircraft and aircraft with such system. USP2012078220739.
  10. Mayes,Harold G. Closure panel arrangement. USP2007087255307.
  11. Campbell, Thomas A.; Chambers, David S.; Willie, Robert H.; Rust, Charles W.. Dual flow APU inlet and associated systems and methods. USP2009117611093.
  12. Campbell,Thomas A.; Chambers,David S.; Willie,Robert H.; Rust,Charles W.. Dual flow APU inlet and associated systems and methods. USP2008037344107.
  13. Brown,Daniel V.; Asplund,Kyle D.; Michalski, Jr.,Joseph W.. Eccentric exhaust muffler for use with auxiliary power units. USP2008057367424.
  14. Eleftheriou, Andreas; Denis, David; Leclair, Denis; Roussel, Yves. Gas turbine engine case and method of making. USP2010097797922.
  15. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  16. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  17. Campbell,Thomas A.; Voll,William A.; Diamond,John A.. Integrated axially varying engine muffler, and associated methods and systems. USP2007097267297.
  18. Napier, James C.; Francisco, Jay M.. Low noise exhaust ducting system. USP2013028371521.
  19. Starobinski, Rudolf; Siercke, Matthias. Silencer for an auxiliary power unit of an aircraft. USP2014078763751.
  20. Zielinski, Edward; Bernier, Alan T.; Knechtel, Kent W.; Campbell, Thomas A.; White, Jeffrey J.; Ralston, Mark D.. Systems and methods for starting aircraft engines. USP2009047513119.
  21. Meseguer Mata, Alejandro; Postigo Rodriguez, Angel; Villanueva Montero, Rafael; De La Sen Perez, Daniel. Tail-cone of an aircraft with movable fairing. USP2014028657233.
  22. Lwasa, Ronald M.; Chow, Allen D.. Thermally compliant APU exhaust duct arrangements and associated systems and methods. USP2010087765784.
  23. Vignali, Mark; Merritt, Brent J.. Three-way mount bracket for aircraft cabin air supply system. USP2015028955809.
  24. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai. Turbofan case and method of making. USP2010087770378.
  25. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai. Turbofan case and method of making. USP2010097793488.
  26. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai. Turbofan case and method of making. USP2010087765787.
  27. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai. Turbofan case and method of making. USP2010067739866.
  28. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai. Turbofan case and method of making. USP2009077565796.
  29. Eleftheriou,Andreas; Lobo,Kevin Walter; Weinberg,Maurice; Liu,Quantai. Turbofan case and method of making. USP2008057370467.
  30. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.