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GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS
专利权人:
United Technologies Corporation
发明人:
ZHENG, Zhijun,SANDY, David F.
申请号:
EP20130746229
公开号:
EP2812247(B1)
申请日:
2013.02.05
申请国别(地区):
欧洲专利局
年份:
2016
代理人:
摘要:
A connection for mounting an aircraft engine to an aircraft pylon includes a plate to be connected to a portion of an engine, and a body that extends rearward from the plate. A back-up connection, including a pin positioned within a slotted hole, is provided between the portion of the engine and the body. When there is a normal connection between the plate and the body, there is clearance between the pin and the slotted hole.
来源网站:
中国工程科技知识中心
来源网址:
http://www.ckcest.cn/home/

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