发明名称 Abrasive airfoil tip
摘要 <p>An airfoil (32) comprises a substrate (54), a residual abrasive coating (58) and a supplemental abrasive coating (62). The substrate extends along a tip section (51) of the airfoil, from a leading edge (48) to a trailing edge (50). The residual abrasive coating (58) comprises a two-phase abrasive and metal matrix material bonded to the substrate, on the tip section of the airfoil. The supplemental abrasive coating (62) comprises a two-phase abrasive and metal matrix material bonded to the residual abrasive coating and to the substrate adjacent the residual abrasive coating, on the tip section (51) of the airfoil. The supplemental abrasive coating restores the airfoil to a nominal tip height (57) in the tip section.</p>
申请公布号 EP2540961(A2) 申请公布日期 2013.01.02
申请号 EP20120169876 申请日期 2012.05.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WRABEL, PETER;DRAGHI, PETER J.;GREGG, SHAWN J.
分类号 F01D5/00;F01D5/20;F01D5/28;F01D11/12 主分类号 F01D5/00
代理机构 代理人
主权项
地址