发明名称 COMPRESSOR BLADE WITH FLEXIBLE TIP ELEMENTS AND PROCESS THEREFOR
摘要 A compressor blade and process for inhibiting rub encounters between a blade tip of the blade and an interior surface of a case that surrounds the rotating hardware within a compressor section of a turbomachine. The compressor blade includes a cap that defines the blade tip at a radially outermost end of the blade, and a plurality of flexible elements extending from a surface of the cap that defines the blade tip. The flexible elements extend from the surface in a span-wise direction of the blade, and are operable to become rigid due to centrifugal stiffening at compressor operating speeds and, optionally, cut a groove the interior surface of the case.
申请公布号 US2012134786(A1) 申请公布日期 2012.05.31
申请号 US20100955009 申请日期 2010.11.29
申请人 GENERAL ELECTRIC COMPANY 发明人 CAIRO RONALD RALPH;NELSON WARREN ARTHUR
分类号 F01D5/20;B23P15/04 主分类号 F01D5/20
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