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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 ; 248/554
출원번호 US-0892647 (1997-07-15)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Desmond, Esq.
인용정보 피인용 횟수 : 30  인용 특허 : 7
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.] 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 t...

이 특허를 인용한 특허 피인용횟수: 30

  1. DeDe, Brian C.; Light, Stacey H.. APU selective cool down cycle. USP2015119188065.
  2. Thies, Robert; Buchholz, Carsten; Staudte, Andreas. Accessory mounting for a gas turbine. USP2016089416734.
  3. Brand, Joseph Horace; Dooley, Kevin; Dowhan, Michael; Youssef, Nashed; Harvey, Richard; Savage, William. Aircraft propulsion system. USP2009067540450.
  4. Addis, Mark. Aircraft propulsion systems. USP2010077752834.
  5. Buchheit, Catherine. Aircraft provided with a fuel cell system. USP2013098523105.
  6. Bonner, Brett Colin; Nager, Eric Andrew. Alignment system for exhaust installation. USP20190410246198.
  7. Kohn, Thierry; Fert, Jeremy Edmond. Arrangement for a tank between a nacelle cowling and a turbomachine. USP2017049611047.
  8. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2011118061650.
  9. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2011027891605.
  10. Nguyen,Phuong H.; Sikora,Joseph A.; Campbell,Thomas A.. Automatic control systems for aircraft auxiliary power units, and associated methods. USP2008047364116.
  11. Williams,Nicholas A.. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner. USP2008047350619.
  12. Cazals, Olivier. Beam mounted rear propulsion system for an aircraft and aircraft with such system. USP2012078220739.
  13. Stebbins, Robin William; Kauffman, Brad Alan; Kraft, Kurt Randall; Vyeson, Craig Alan. Compliance mechanism. USP2010127850122.
  14. Liston Laurence D. N. ; Schoepf Joseph L.. Detachable integral aircraft tailcone and power assembly. USP2001106308915.
  15. Campbell, Thomas A.; Chambers, David S.; Willie, Robert H.; Rust, Charles W.. Dual flow APU inlet and associated systems and methods. USP2009117611093.
  16. Campbell,Thomas A.; Chambers,David S.; Willie,Robert H.; Rust,Charles W.. Dual flow APU inlet and associated systems and methods. USP2008037344107.
  17. DeDe, Brian C.; Lau, David; Jewess, Gordon F.. Fire resistant structural mount yoke and system. USP2014118882029.
  18. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  19. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  20. Campbell,Thomas A.; Voll,William A.; Diamond,John A.. Integrated axially varying engine muffler, and associated methods and systems. USP2007097267297.
  21. Pina López, José Maria; Sanz Martinez, Pablo Timoteo. Interchangeable joint concept for an aircraft rear fuselage cone. USP2014098844874.
  22. Lemire, Jacques; Olsen, Kirk W.; DePriest, Francis J.; Law, Thomas R.; Whiteford, Gerald P.; Bachmeyer, Paul J.. Mounting assembly for an aircraft auxiliary power unit and method. USP2003066581874.
  23. Carlson, David; Madaus, Brandon; Harthcock, Matthew; Barton, Kearney; Taylor, Charles L.; Walker, Jason. Panel structure. USP2017069688050.
  24. 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.
  25. Meseguer Mata, Alejandro; Postigo Rodriguez, Angel; Villanueva Montero, Rafael; De La Sen Perez, Daniel. Tail-cone of an aircraft with movable fairing. USP2014028657233.
  26. Doleski,Robert F.; Oliver,Stephen F.; Olson,Stanley J.. Tailcone assembly for a submarine countermeasure. USP2006047026540.
  27. Lwasa, Ronald M.; Chow, Allen D.. Thermally compliant APU exhaust duct arrangements and associated systems and methods. USP2010087765784.
  28. Kush, Ivan; Henson, Larry Nolan. Turbine exhaust cylinder baffle seal and method for installing turbine exhaust cylinder baffle seal. USP2017119822664.
  29. Schiebel, Hans-Georg. Unmanned helicopter. USP2010057721988.
  30. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.