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US07927075B2 Fan-turbine rotor assembly for a tip turbine engine 有权
用于尖端涡轮发动机的风机 - 涡轮机转子组件

Fan-turbine rotor assembly for a tip turbine engine
摘要:
A fan-turbine rotor assembly (24) for a tip turbine engine (10 )includes a fan hub (64) with an outer periphery (112) scalloped by a multitude of elongated openings (114) which extend into a fan hub web (115). Each elongated opening defines an inducer receipt section (117) to receive an inducer section (66)and a hollow fan blade section (72). An inducer exhaust from each inducer section is located adjacent a core airflow passage (80) within each fan blade section to provide communication therebetween.
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