发明名称 COOLING A MULTI-WALLED STRUCTURE OF A TURBINE ENGINE
摘要 An assembly is provided for a turbine engine. This turbine engine assembly includes a body, a shell and a heat shield panel. The panel is attached to the shell with a tapered cooling cavity between the shell and the panel. The panel defines a cooling aperture configured to direct air out of the cooling cavity to impinge against the body.
申请公布号 WO2015077600(A1) 申请公布日期 2015.05.28
申请号 WO2014US66880 申请日期 2014.11.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CUNHA, FRANK J.;KOSTKA, JR., STANISLAV
分类号 F02C7/12;F01D25/12;F02C3/14;F02C7/18;F02C7/24 主分类号 F02C7/12
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