发明授权
US07959406B2 Close coupled gearbox assembly for a tip turbine engine 有权
用于尖端涡轮发动机的紧耦合齿轮箱组件

Close coupled gearbox assembly for a tip turbine engine
摘要:
A gearbox assembly (90) closely couples a fan-turbine rotor assembly (25) and an axial compressor rotor (46) to reduce the overall engine length and minimizes the number of engine bearings.
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