发明名称 FAN-TURBINE ROTOR ASSEMBLY WITH INTEGRAL INDUCER SECTION FOR A TIP TURBINE ENGINE
摘要 <p>A fan-turbine rotor assembly for a tip turbine engine includes a fan hub with an outer periphery scalloped by a multitude of elongated openings which extend into a fan hub web. Each elongated opening defines an inducer section and a blade receipt section to retain a hollow fan blade section. The blade receipt section retains each of the hollow fan blade sections adjacent each inducer section. The inducer sections are cast directly into the fan hub which minimizes leakage between each fan blade section and each of the respective inducer sections to minimize airflow leakage and increase engine efficiency.</p>
申请公布号 WO2006060005(A1) 申请公布日期 2006.06.08
申请号 WO2004US40174 申请日期 2004.12.01
申请人 UNITED TECHNOLOGIES CORPORATION;SUCIU, GABRIEL L.;NORRIS, JAMES W.;NORDEEN, CRAIG A.;MERRY, BRIAN 发明人 SUCIU, GABRIEL L.;NORRIS, JAMES W.;NORDEEN, CRAIG A.;MERRY, BRIAN
分类号 F02C3/073;F02C3/08;F02K3/068 主分类号 F02C3/073
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