发明名称 FLOW DIVERTER TO REDIRECT SECONDARY FLOW
摘要 An assembly for a gas turbine engine includes a seal and a flow diverter. The flow diverter is disposed adjacent the seal to direct a secondary gas flow that passes across the seal away from a rotor cavity such that the secondary gas flow travels back toward a main gas flow path of the gas turbine engine.
申请公布号 EP2938867(A4) 申请公布日期 2016.04.20
申请号 EP20130867393 申请日期 2013.12.17
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CHUONG, CONWAY;CARELLA, JOHN, A.
分类号 F02C7/28;F01D5/08;F01D9/06;F01D11/00;F02K1/42 主分类号 F02C7/28
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