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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0821376 (1992-01-16) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 67 인용 특허 : 0 |
An aircraft engine mount includes a frame fixedly joined in a gas turbine engine and a platform fixedly joined to an aircraft wing or tail pylon. A first beam is pivotally joined to the frame and the platform at first and second joints, respectively. The first beam is additionally joined to the plat
A mount for supporting a gas turbine engine to an aircraft pylon comprising: a frame fixedly joined in said gas turbine engine; a platform fixedly joined to said pylon; a first beam pivotally joined to said frame at a first joint and pivotally joined to said platform at a second joint, and joined ad
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