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