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특허 상세정보

Variable cycle gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/16    F02C-001/00    F02C-007/32    F02C-003/107    F02C-003/13    F02C-009/18    F02K-003/02    F02K-003/075   
출원번호 US-0337924 (2011-12-27)
등록번호 US-9261019 (2016-02-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Barnes & Thornburg LLP
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

One embodiment of the present invention is a unique variable cycle gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for variable cycle gas turbine engines. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.

대표
청구항

1. A variable cycle gas turbine engine, comprising: a compressor configured to compress a core gas flow;a combustor in fluid communication with the compressor and configured to combust the core gas flow;a primary turbine drivingly coupled to the compressor and configured to receive the core gas flow, wherein the primary turbine is configured to drive the compressor;an auxiliary turbine drivingly coupled to the compressor;a valve configured to selectively direct a portion of the core gas flow to the auxiliary turbine; anda controller structured to selecti...

이 특허에 인용된 특허 (13)

  1. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  2. Moulebhar, Djamal. Aircraft with disengageable engine and auxiliary power unit components. USP2010107805947.
  3. Mahoney,Timothy D.; Laidlaw,Mitchell J.; Libera,Anthony C.. Gas turbine engine bleed air power assist system and method. USP2007077246482.
  4. Hines William R. ; Niskode Padmakar M. ; Horner Michael W.. Gas turbine engine with exhaust expander and compressor. USP2000106134876.
  5. Klingels, Hermann. Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine. USP2009097584600.
  6. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  7. Lui Clarence. Integrated bleed air and engine starting system. USP2001106305156.
  8. Epstein,Stanley W.. Onboard supplemental power system at varying high altitudes. USP2007067231770.
  9. Epstein,Stanley W.. Onboard supplemental power system at varying high altitudes. USP2006087089744.
  10. Epstein,Stanley W.. Onboard supplemental power system at varying high altitudes. USP2006097111462.
  11. Simmons John Robert (Cincinnati OH). Split fan work gas turbine engine. USP1977034010608.
  12. Iya,Sridhar K.; Roe,George M.. System and method for controlling the temperature and infrared signature of an engine. USP2009017478525.
  13. Zeiner, Peter Kenneth; Libera, Tony; Langston, Todd. Turbine drive system with lock-up clutch and method. USP2012048146370.