| 发明名称 |
METHOD FOR MANUFACTURING HOT GAS PATH COMPONENT AND HOT GAS PATH TURBINE COMPONENT |
| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a method for manufacturing a hot gas path component and a hot gas path turbine component. <P>SOLUTION: A method for manufacturing the hot gas path component of a turbine is provided, and the method includes a step of forming cooling channels in a surface of a member. The method also includes steps of: disposing a layer on the surface of the member to enclose the cooling channels, the layer being disposed on a portion of the member to be cooled; and bonding the layer to the surface. The bonding step includes a step of heating the member and the layer. <P>COPYRIGHT: (C)2012,JPO&INPIT |
| 申请公布号 |
JP2012184763(A) |
申请公布日期 |
2012.09.27 |
| 申请号 |
JP20120044910 |
申请日期 |
2012.03.01 |
| 申请人 |
GENERAL ELECTRIC CO <GE> |
发明人 |
KOTTILINGAM SRIKANTH CHANDRUDU;BUCCI DAVID VINCENT;LACY BENJAMIN PAUL;MOREY KATHLEEN BLANCHE;TOLLISON BRIAN LEE;WALSH PATRICK THOMAS |
| 分类号 |
F02C7/00;B23K1/00;B23K3/06;C23C28/00;F01D5/18;F01D5/28;F01D9/02;F01D25/00;F01D25/12;F02C7/18 |
主分类号 |
F02C7/00 |
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