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Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-001/09
  • F02K-001/04
  • F02K-003/04
출원번호 US-0719080 (1996-09-24)
발명자 / 주소
  • Cariola Roy E.
  • Aten Michael R.
출원인 / 주소
  • Rohr, Inc.
대리인 / 주소
    Schlesinger
인용정보 피인용 횟수 : 115  인용 특허 : 0

초록

A structure to provide a variable nozzle for the fan air flow of a turbofan aircraft gas turbine engine with the nozzle being defined by the exit throat area defined by the aft edge of a trailing edge portion of the fan cowl and the core engine housing. A trailing edge cowl portion is slidably posit

대표청구항

[ What is claimed is:] [1.] A structure to provide a variable nozzle for the fan air flow of an aircraft gas turbine engine, the nozzle being defined by the spacing between a trailing edge portion of the translating cowl and the core engine housing to provide a determinable exit throat area for such

이 특허를 인용한 특허 (115)

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