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Aircraft gas turbine engine sideways mount 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-027/00
  • F02C-007/20
출원번호 US-0165627 (1993-12-13)
발명자 / 주소
  • O\Brien Michael T. (Cincinnati OH) Bobo
  • deceased Melvin (late of Cincinnati OH by Beatrice L. Bobo
  • executor)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 66  인용 특허 : 0

초록 ▼

An aircraft engine sideways mount assembly includes a thrust mount and an engine suspension for suspending the engine structure sideways from the aircraft such that the thrust mount is operable to react substantially all the thrust load forces from the engine to the aircraft. The thrust mount has a

대표청구항 ▼

A mount assembly for mounting an aircraft gas turbine engine sideways to an aircraft by the engine\s structure which rotatably supports the engine rotor assembly about an engine centerline, said mount assembly comprising; a pivotable engine suspension including a pivotable support mount for mounting

이 특허를 인용한 특허 (66)

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  31. Williams,Nicholas A., Integrated mount duct for use with airborne auxiliary power units and other turbomachines.
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  64. Heyerman, Jeffrey Bernard; Olver, Bryan W.; Fielding, Bruce; Smythe, Carl, Turbofan mounting system.
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  65. Beutin,Bruno; Yvon,Didier; Mazeaud,Georges; Burdin,Fabien, Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position.
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