Invention Grant
US07883314B2 Seal assembly for a fan-turbine rotor of a tip turbine engine 有权
尖端涡轮发动机的风机 - 涡轮转子的密封组件

Seal assembly for a fan-turbine rotor of a tip turbine engine
Abstract:
A seal assembly (116) mounted within a rotationally fixed static outer support structure (14) for engagement with an annular seal face surface (172) located upon a fan-turbine rotor assembly. The seal assembly provides minimal leakage of core airflow when the airflow is turned and diffused by the diffuser section (74) to increase the engine operating efficiency.
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