发明名称 GEBLÄSE-TURBINEN-ROTORANORDNUNG FÜR EINEN SPITZENTURBINENMOTOR
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.
申请公布号 DE602004031986(D1) 申请公布日期 2011.05.05
申请号 DE20046031986T 申请日期 2004.12.01
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SUCIU, GABRIEL L.;NORRIS, JAMES W.;NORDEEN, CRAIG A.;MERRY, BRIAN
分类号 F02C3/073;F02K3/068 主分类号 F02C3/073
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