发明名称 TURBINE ENGINE COMPONENT, PROCESS FOR COATING AND MODIFIED BLADE TIP
摘要 A modified blade tip (14) with abrasive coating (16) comprises a blade having a tip (14) with a center (36) between corners (22) proximate a leading edge (24) and a trailing edge (26). The blade (10) having a top surface, the top surface being modified proximate said corners (22). The abrasive coating (16) is bonded to the tip (14) at the top surface. The abrasive coating (16) is thicker proximate the corners (22) than at the center (36) of the blade tip (14).
申请公布号 EP3056676(A1) 申请公布日期 2016.08.17
申请号 EP20160155325 申请日期 2016.02.11
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 STROCK, CHRISTOPHER W.
分类号 F01D5/20;F01D11/12 主分类号 F01D5/20
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