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Variable area nozzle for gas turbine engines driven by shape memory alloy actuators 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
  • F02K-003/075
  • F02K-001/12
출원번호 US-0517937 (2000-03-03)
발명자 / 주소
  • Rey Nancy M.
  • Miller Robin M.
  • Tillman Thomas G.
  • Rukus Robert M.
  • Kettle John L.
  • Dunphy James R.
  • Chaudhry Zaffir A.
  • Pearson David D.
  • Dreitlein Kenneth C.
  • Loffredo Constantino V.
  • Wyno
출원인 / 주소
  • United Technologies Corporation
인용정보 피인용 횟수 : 139  인용 특허 : 5

초록

A gas turbine engine includes a variable area nozzle having a plurality of flaps. The flaps are actuated by a plurality of actuating mechanisms driven by shape memory alloy (SMA) actuators to vary fan exist nozzle area. The SMA actuator has a deformed shape in its martensitic state and a parent shap

대표청구항

[ We claim:] [1.]1. A gas turbine engine situated about a center axis and enclosed in a nacelle, said nacelle having a trailing end in a downstream portion thereof, said trailing end defining a fan exit nozzle area, said gas turbine engine comprising:a plurality of flaps each of said flaps having an

이 특허에 인용된 특허 (5)

  1. Cincotta Manuel (Tiverton RI) Nadolink Richard H. (Portsmouth RI), Articulated control surface.
  2. Thoma Paul E. (Cedarburg WI) Kao Ming-Yuan (Fox Point WI) Schmitz Dwight M. (West Allis WI), Extended life SMA actuator.
  3. Morris Garron, Fluid moving device and associated method.
  4. Roglin Robert L. (Duluth GA) Hanagud Sathyanaraya (Atlanta GA), Variable camber control of airfoil.
  5. Giffin ; III Rollin G. (Cincinnati OH), Variable specific thrust turbofan engine.

이 특허를 인용한 특허 (139)

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