发明申请
US20090148297A1 FAN-TURBINE ROTOR ASSEMBLY FOR A TIP TURBINE ENGINE 有权
用于提升涡轮发动机的风力涡轮机转子总成

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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