发明名称 |
TURBINE COMPONENT WITH COOLING FEATURES AND METHOD FOR MANUFACTURING THE SAME |
摘要 |
<P>PROBLEM TO BE SOLVED: To provide a turbine component including cooling features and a method for manufacturing the turbine component. <P>SOLUTION: The present disclosure is directed to the use and manufacture of the cooling features within the component (54) used in a hot gas path such as within a turbine (10). In one embodiment, channels (110) are formed (56) within an external surface (102) of the component (54) and filled (60) with a removable material (120). The external surface (102) and channels (110) may then be coated with one or more layers such as a structural layer (130) and/or top coating (134). The removable material (120) may then be removed (68) to leave the channels (110) free of the removable material (120). <P>COPYRIGHT: (C)2012,JPO&INPIT |
申请公布号 |
JP2012112381(A) |
申请公布日期 |
2012.06.14 |
申请号 |
JP20110251175 |
申请日期 |
2011.11.17 |
申请人 |
GENERAL ELECTRIC CO <GE> |
发明人 |
BUNKER RONALD SCOTT;WEI BIN;RITTER ANN M;LIPKIN DON MARK;REBAK RAUL BASILIO;KOOL LAWRENCE BERNARD;GRAY DENNIS MICHAEL |
分类号 |
F02C7/00;F01D5/28;F01D25/00 |
主分类号 |
F02C7/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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