Invention Grant
US07883315B2 Seal assembly for a fan rotor of a tip turbine engine 有权
尖端涡轮发动机的风扇转子的密封组件

Seal assembly for a fan rotor of a tip turbine engine
Abstract:
A seal assembly (118) mounted within a nonrotatable static inner support structure (16) for engagement with an axial seal face surface (114) and a radial seal face surface (116). The radial seal (120) engages the axial seal face surface and the axial seal (122) engages the radial seal face surface. The seal assembly provides minimal leakage of core airflow to increase the tip turbine engine operating efficiency.
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