Invention Grant
US08313293B2 Turbofan mounting system 有权
Turbofan安装系统

Turbofan mounting system
Abstract:
A gas turbine engine has a rear mounting assembly incorporating a mounting apparatus attached to a bypass duct wall with a link device for transferring core portion related inertia-induced loads, from an MTF of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.
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