发明名称 Gas turbine engine component with cooling holes having a multi-lobe configuration
摘要 An engine component includes a body; and a plurality of cooling holes formed in the body, at least one of the cooling holes having a multi-lobed shape with at least a first lobe, a second lobe, and a third lobe.
申请公布号 EP2662528(A3) 申请公布日期 2015.08.12
申请号 EP20130157092 申请日期 2013.02.27
申请人 HONEYWELL INTERNATIONAL INC. 发明人 MALAK, MALAK FOUAD;RANA, RAJIV;TAPIA, LUIS;CHOU, DAVID;LIU, JONG
分类号 F01D5/18 主分类号 F01D5/18
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