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Detachable integral aircraft tailcone and power assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-027/00
출원번호 US-0892647 (1997-07-15)
발명자 / 주소
  • Liston Laurence D. N.
  • Schoepf Joseph L.
  • Royalty Charles Michael
출원인 / 주소
  • AlliedSignal Inc.
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 con

대표청구항

[ 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 forw

이 특허에 인용된 특허 (7)

  1. Bacon Richard J. (1268 Northridge Ct. Golden CO 80401), 3x multi-engine jet configuration.
  2. Sherry Philip David,GBX ; Welsh Robert,GBX ; Johnson Kenneth Henry,GBX, Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel.
  3. O'Boyle Brian J. ; Adamson Eric E. ; Schramm Michael R., Aircraft support pylon.
  4. O\Quinn Russell P. (Long Beach CA) Culver Irven H. (Playa Del Rey CA), Aircraft with interchangeable fuselage.
  5. Moorehead James R. (Bellevue WA), Nacelle assembly and mounting structures for a turbofan jet propulsion engine.
  6. Hapke Donald W. (Issaquah WA), Retractable nozzle fairing system for aeroplane center boost engine.
  7. Finch Thomas E. (Spring Branch TX) Cavatorta Enrico (San Antonio TX) Paschal William (Schertz TX), S-duct for a turbo-jet aircraft engine.

이 특허를 인용한 특허 (30)

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