发明名称 GAS TURBINE ENGINE AIRFOIL INTEGRATED HEAT EXCHANGER
摘要 A heat exchanger apparatus includes: (a) an airfoil (42) having opposed pressure and suction sides (54, 52), a root (50), a tip (48), and spaced-apart leading and trailing edges (44, 46); and (b) a plenum (62, 162, 262) integrally formed within the airfoil (42) which is configured to receive a flow of circulating working fluid; and (c) inlet and outlet ports (72, 74) communicating with the plenum (62, 162, 262) and an exterior of the airfoil (42).
申请公布号 CA2737338(A1) 申请公布日期 2011.10.30
申请号 CA20112737338 申请日期 2011.04.14
申请人 GENERAL ELECTRIC COMPANY 发明人 KNIGHT, GLENN, III;LUKOVIC, BOJAN;LABORIE, DANIEL;SCHEFFEL, KENNETH S.
分类号 F02C7/14;F01D9/02;F01D25/12;F16N39/02;F28D1/02 主分类号 F02C7/14
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