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
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