发明名称 GAS TURBINE ENGINE AIRFOIL INTEGRATED HEAT EXCHANGER
摘要 A heat exchanger apparatus includes: (a) an airfoil having opposed pressure and suction sides, a root, a tip, and spaced-apart leading and trailing edges; and (b) a plenum integrally formed within the airfoil which is configured to receive a flow of circulating working fluid; and (c) inlet and outlet ports communicating with the plenum and an exterior of the airfoil.
申请公布号 US2011268562(A1) 申请公布日期 2011.11.03
申请号 US20100771508 申请日期 2010.04.30
申请人 GENERAL ELECTRIC COMPANY 发明人 KNIGHT, III GLENN;LUKOVIC BOJAN;LABORIE DANIEL;SCHEFFEL KENNETH S.
分类号 F04D29/58 主分类号 F04D29/58
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