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특허 상세정보

Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-017/10    F02C-006/08   
출원번호 US-0427771 (2012-03-22)
등록번호 US-9267390 (2016-02-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz, P.C.
인용정보 피인용 횟수 : 1  인용 특허 : 33
초록

A system for selectively supplying air between separate plena of a gas turbine engine includes a gas turbine engine, a door, and a bi-metallic door actuator. The gas turbine engine comprises at least a first plenum and a second plenum, and has an opening between the first plenum and the second plenum. The is door mounted in the gas turbine engine and is movable between a closed position, in which air is prevented from flowing through the opening, and an open position, in which air may flow though the opening. The bi-metallic door actuator is coupled to t...

대표
청구항

1. A system for selectively supplying air between separate plena of a gas turbine engine, comprising: a gas turbine engine comprising at least a first plenum and a second plenum, and having an opening between the first plenum and the second plenum;a door mounted in the gas turbine engine and movable between a closed position, in which air is prevented from flowing through the opening, and an open position, in which air may flow though the opening; anda bi-metallic door actuator coupled to the door and configured to selectively move the door between the c...

이 특허에 인용된 특허 (33)

  1. Clark, Daniel; Webster, John R. Actuator. USP2011108043045.
  2. Williams Gregg G. (Milford MI). Aft fan gas turbine engine. USP1992115161369.
  3. Parikh, Pradip G.; Willie, Robert H.. Air inlet and method for a highspeed mobile platform. USP2011017861968.
  4. Andrie Michael J. (Columbus IN). Air to air heat exchanger internal bypass. USP1992105152144.
  5. Mark D. Ralston. Aircraft auxiliary air intake with ram and flush opening door. USP2002026349899.
  6. Coffinberry George A. (West Chester OH). Aircraft engine electrically powered boundary layer bleed system. USP1992055114103.
  7. Chamay Anthony J. ; Zelazny Isaac,KRX. Aircraft engine pitot plenum intake. USP1998035725180.
  8. Coffinberry George A. (West Chester OH). Aircraft gas turbine engine bleed air energy recovery apparatus. USP1992085137230.
  9. Grudich George (Rochester MI). Bi-metallic vane vent damper. USP1984044441653.
  10. Wakeman Thomas G. (West Chester OH). Compact air-to-air heat exchanger for jet engine application. USP1980024187675.
  11. Elovic Ernest (Cincinnati OH). Cooling air cooler for a gas turbofan engine. USP1981034254618.
  12. Lardellier Alain Marie Joseph (Melun FR). Device for boosting and bleeding a gas turbine engine. USP1976063964257.
  13. Hein,Jeffrey M.; Williams,Nicholas A.; Sheoran,Yogendra Y.; Lam,Cecilia S.; Cowans,Ora M.; Higuera,Benjamen K.; Peduchi,Andrew S.; Sellahewa,Ravisha P.; Brown,Daniel. Dual action inlet door and method for use thereof. USP2006037014144.
  14. Porte, Alain; Prat, Damien. Dual flow turbine engine equipped with a precooler. USP2012088250852.
  15. Patrick John P. (S. Windsor CT) Goodman Robert B. (West Hartford CT). Fluid temperature control system. USP1982034318509.
  16. Coffinberry George A. (West Chester OH). Gas turbine engine cooling system. USP1995025392614.
  17. Vermejan Alexander E. (Mason OH) Daiber Paul C. (Cincinnati OH) Morton Scott C. (Cincinnati OH) Taylor Michelle L. (Cincinnati OH). Gas turbine engine fan cooled heat exchanger. USP1993125269135.
  18. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed. USP1992095143329.
  19. Loxley Russell A. (Leicestershire GB2) Clarke Andrew (Nottingham GB2). Heat exchange apparatus for gas turbine fluids. USP1995085438823.
  20. Nikkanen John P. ; Sandahl Steven D. ; Zysman Steven H.. Heat exchanger system for a gas turbine engine. USP2000086106229.
  21. Chapman William I. (Birmingham MI). Integrated propulsion system. USP1992095150569.
  22. Herzog Claus (Mnchen DEX) Schwab Rainer R. (Karlsfeld DEX) Rd Klaus (Grbenzell DEX) Mark Harald (Karlsfeld DEX). Method and apparatus for cooling an airplane engine. USP1992125167117.
  23. DeAnna Russell. Passive bimetallic actuator for heat transfer. USP2000036039262.
  24. Pineo, Gregory Merle; Cheadle, Brian E.; Peric, Yuri. Plug bypass valves and heat exchangers. USP2010127854256.
  25. Miller Franklin E. (Cincinnati OH). Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine. USP1992065123242.
  26. Song, Gangbing; Ma, Ning. Shape memory alloy actuated adaptive exhaust nozzle for jet engine. USP2009097587899.
  27. Coffinberry George A. ; Leonard Gary L.. System and method of providing clean filtered cooling air to a hot portion of a gas turbine engine. USP1999075918458.
  28. Parikh, Pradip G; Atkey, Warren A. Tandem air inlet apparatus and method for an airborne mobile platform. USP2009127624944.
  29. Goodman Robert B. (West Hartford CT). Temperature control system. USP1991125072781.
  30. Speer Stephen R. (Spokane WA). Turbine engine having combustor air precooler. USP1991055012646.
  31. Olver, Bryan; Ciampa, Alessandro; Marrano, Roberto; Trepanier, Richard; Lamarre, Sylvain; Bernard, Martin; Germain, Patrick. Turbofan bypass duct air cooled fluid cooler installation. USP2011017861512.
  32. Porte, Alain. Turbofan provided with a pre-cooler. USP2011047926261.
  33. Diermayer Werner (1275 Panorama Dr. Lafayette CA 94549). Vent control arrangement for combustion apparatus. USP1981014245778.