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특허 상세정보

Generator for flight vehicle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-041/00    B64D-027/20    B64D-033/00    B64D-033/02    F01D-015/10   
출원번호 US-0095613 (2013-12-03)
등록번호 US-9517843 (2016-12-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Barnes & Thornburg, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 12
초록

A flight vehicle includes a fuselage and a gas turbine engine. The gas turbine engine is coupled to the fuselage to provide thrust when air surrounding the flight vehicle is admitted to the gas turbine engine and combusted with fuel. The flight vehicle further includes a generator coupled to the gas turbine engine to provide power to equipment included in the vehicle.

대표
청구항

1. A flight vehicle comprising: a fuselage including a nose and a tail spaced apart from the nose,a gas turbine engine located in a space formed in the fuselage and located between the nose and the tail, anda generator unit coupled to the gas turbine engine via a generator shaft, at least a portion of the generator shaft located exterior to the generator unit and the gas turbine engine, to cause a portion of the generator unit to rotate therewith, the generator unit being located in spaced-apart relation to the gas turbine engine between the nose and the...

이 특허에 인용된 특허 (12)

  1. Reysa Gary D. ; Swenson Lynn A. ; Hutchison Robert A. ; Fung Kenny L.. Auxiliary power and thrust unit. USP2001066247668.
  2. Kern, John M.; Chung, KiYoung; Qu, Ronghai; Wu, Wei; Young, Craig D.; Toot, Peter D.; Glynn, Christopher; Compton, Tom. Electric power generation using power turbine aft of LPT. USP2009047514810.
  3. Jeffrey Ronald Coles GB; Marc Holme GB; James Patrick Doyle GB. Electrical generator an aero-engine including such a generator, and an aircraft including such a generator. USP2002106467725.
  4. Hardy Richard (The Boeing Company ; P.O. Box 3999 ; M/S 80-PA Seattle WA 98124-2499) Neumann Frank D. (The Boeing Company ; P.O. Box 3999 ; M/S 80-PA Seattle WA 98124-2499) Ruzicka Dennis E. (The Boe. Fighter aircraft. USP1997115683061.
  5. Kern, John M.; Qu, Ronghai; Young, Craig Douglas. Integrated boost cavity ring generator for turbofan and turboshaft engines. USP2012068198744.
  6. Kern, John Michael; Wiegman, Herman Lucas Norbert. Integrated electrical power extraction for aircraft engines. USP2009107605483.
  7. Kern,John Michael; Wiegman,Herman Lucas Norbert. Integrated electrical power extraction for aircraft engines. USP2008127468561.
  8. Ullyott, Richard; Fielding, Bruce; Trumper, Ronald. Method of operating a gas turbine engine. USP2011047926287.
  9. Russ, David Everett. Multi-speed gearbox for low spool driven auxiliary component. USP2011057942079.
  10. Finch Thomas E. (Spring Branch TX) Cavatorta Enrico (San Antonio TX) Paschal William (Schertz TX). S-duct for a turbo-jet aircraft engine. USP1994045299760.
  11. Cote, Richard A.; Nozari, Farhad. Systems and methods for providing AC power from multiple turbine engine spools. USP2011108039983.
  12. Welch, Richard C.; Bueche, Gerard H.; DeGroff, William T.; Albero, Jose; Makuszewski, Jerzy. Turbofan emergency generator. USP2010117841163.