发明名称 |
METHOD FOR COATING A BLADE AND BLADE OF A GAS TURBINE |
摘要 |
Process for coating hollow internally cooled gas turbine blades (1) where the blade base material (3) on the outer blade side has an external coating (5) consisting of an adhesive layer (6) based on MCrAlY and a heat insulating Zr oxide ceramic layer (9), and a Cr diffusion layer (7) on the inner side of the blades. An independent claim is included for a gas turbine blade as described above. |
申请公布号 |
EP1969156(B1) |
申请公布日期 |
2012.09.05 |
申请号 |
EP20060849387 |
申请日期 |
2006.12.12 |
申请人 |
MAN DIESEL & TURBO SE |
发明人 |
CHANDRA, SHARAD;CZECH, NORBERT |
分类号 |
C23C28/00;C23C4/06;C23C16/06;C23C30/00 |
主分类号 |
C23C28/00 |
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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