Invention Grant
US08128021B2 Engine mount system for a turbofan gas turbine engine 有权
用于涡轮风扇燃气涡轮发动机的发动机支架系统

Engine mount system for a turbofan gas turbine engine
Abstract:
A mount system for a gas turbine engine includes an aft mount which reacts at least a portion of a thrust load at an engine case generally parallel to an engine axis.
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