发明名称 GAS TURBINE ENGINE ROTOR DRAIN FEATURE
摘要 An assembly for a gas turbine engine includes a rotor formed by a drum and a hub. The drum has a generally conically shaped inner surface that defines a flow path along a first cavity. The hub is connected to the drum and has a conically shaped inner surface that defines a flow path along a second cavity.
申请公布号 EP2912269(A1) 申请公布日期 2015.09.02
申请号 EP20130849562 申请日期 2013.10.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LITTLE, JONATHAN D.;WALKER, HERBERT L.;JAYASINGH, ARUN
分类号 F01D5/06;F01D5/02;F02C7/00 主分类号 F01D5/06
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