发明名称 Airfoil heat shield
摘要 Exemplary embodiments include a multi-layer, modular and replaceable heat shield for gas turbines. The heat shield apparatus can include a base layer adjacent the airfoil and a thermal layer coupled to the base layer, wherein the base layer and the thermal layer match a contour of the airfoil.
申请公布号 US9528382(B2) 申请公布日期 2016.12.27
申请号 US200912615674 申请日期 2009.11.10
申请人 General Electric Company 发明人 Morgan Victor John;Johns David Richard
分类号 F01D25/12;F01D5/28;F01D5/14 主分类号 F01D25/12
代理机构 代理人 Cusick Ernest G.;Landgraff Frank A.
主权项 1. A heat shield apparatus for an airfoil, the apparatus comprising: casing walls configured to be positioned and removable from a turbomachine casing; a wall disposed between and integrally formed with the casing walls, the wall including: a base layer adjacent the airfoil; anda thermal layer adjacent the airfoil, wherein the thermal layer matches a contour of the airfoil; the heat shield being distinct from and configured to be removably mounted to the airfoil.
地址 Schenectady NY US