发明名称 |
Method of manufacturing a turbomachine element and device obtained in this way |
摘要 |
Use of the stator blade platforms for the deposition of a track of adjacent abradable material inside an external turbomachine shell is disclosed. The stator blades are attached to the shell so as to define an annular edge that is substantially continuous and the abradable material is deposited using this edge to delimit a boundary of the track of abradable material.
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申请公布号 |
US8192150(B2) |
申请公布日期 |
2012.06.05 |
申请号 |
US20080343675 |
申请日期 |
2008.12.24 |
申请人 |
DERCLAYE ALAIN;LEBRUN RODOLPHE;TECHSPACE AERO |
发明人 |
DERCLAYE ALAIN;LEBRUN RODOLPHE |
分类号 |
F01D11/00 |
主分类号 |
F01D11/00 |
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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