发明名称 |
Honeycomb seal for abradable angel wing |
摘要 |
An abradable honeycomb is integrally formed in a turbine nozzle (11) sealing flange (16) for engagement with a bucket angel wing (14) to reduce the leakage of air into the turbine's hot gas path. The honeycomb is integrally formed in a turbine nozzle sealing flange (16) using a sinker EDM method to directly sink the honeycomb into the sealing flange (16) itself so that the honeycomb is an integral part of the flange (16). For repair, an entirely new honeycomb flange can be made and welded or brazed on to the turbine nozzle (11). |
申请公布号 |
EP2602043(B1) |
申请公布日期 |
2016.04.20 |
申请号 |
EP20120187219 |
申请日期 |
2012.10.04 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LACY, BENJAMIN PAUL;CHUPP, RAYMOND;SHENG, NUO |
分类号 |
B23H1/04;B23H9/10;F01D11/00 |
主分类号 |
B23H1/04 |
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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