发明名称 GAS TURBINE ENGINE COMPONENT WITH INTEGRATED HEAT PIPE
摘要 A heat transfer apparatus for a gas turbine engine includes: a component (40) having a wall structure defining a flow bounding surface; a chamber (60) formed in the component (40), the chamber (60) including a wicking structure (64), a vapor channel (66), and a working fluid.
申请公布号 EP3081755(A1) 申请公布日期 2016.10.19
申请号 EP20160165250 申请日期 2016.04.14
申请人 GENERAL ELECTRIC COMPANY 发明人 GERSTLER, WILLIAM DWIGHT;KOSTKA, JAMES MICHAEL;RAMBO, JEFFREY DOUGLAS;MOORES, JOHN WILLIAM
分类号 F01D5/18;F01D9/04;F02C7/14 主分类号 F01D5/18
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