发明名称 |
Gas turbine engine component with discontinuous coated areas and corresponding coating method |
摘要 |
<p>A turbine component has an airfoil (100) extending between a leading edge (56) and a trailing edge (60), and has an outer surface. A coating includes at least two discontinuous areas (54, 62) that are spaced from each other such that there is an area of uncoated surface between the discontinuous areas of coating.
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申请公布号 |
EP2325441(A3) |
申请公布日期 |
2013.01.23 |
申请号 |
EP20100251918 |
申请日期 |
2010.11.11 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MCCALL, THOMAS;HISKES, DAVID J.;MILLER, MICHAEL L.;LILE, SCOTT C. |
分类号 |
F01D5/18;C23C4/00;F01D5/28;F01D9/04 |
主分类号 |
F01D5/18 |
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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