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 |