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Nacelle and mounting arrangement for an aircraft engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/20
  • B64D-027/18
  • B64D-027/26
출원번호 US-0117464 (1993-09-07)
발명자 / 주소
  • Brodell Robert F. (Marlborough CT) Hovan Edward J. (Manchester CT) Selfors Steven T. (Somerville MA) Loffredo Constantino V. (Newington CT) Duesler Paul W. (Manchester CT)
출원인 / 주소
  • United Technologies Corporation (East Hartford CT 02)
인용정보 피인용 횟수 : 160  인용 특허 : 0

초록 ▼

A nacelle and mounting arrangement for a high bypass ratio ducted fan aircraft engine mounted external to the aircraft main structure is disclosed. The nacelle and mounting arrangement isolate the engine from the adverse effects of certain aerodynamic forces acting on the nacelle by transferring sub

대표청구항 ▼

For an aircraft ducted fan engine with a core section bounded by a core case and enclosed within a core cowl, a fan section of larger diameter than said core section secured to and concentric with said core section and bounded by a fan case having a fan duct outer wall downstream thereof, said fan d

이 특허를 인용한 특허 (160)

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