A composite ceramic coating 26 having abrasive properties for application to a metallic substrate such as an airfoil tip is provided which includes a ceramic matrix 34 and a plurality of ceramic abrasive particles 36 disposed within said ceramic matrix 34. The abrasive particles 36 have a shear strength substantially greater than that of the ceramic matrix 34 and possess an angular geometry. The coating is preferably plasma sprayed onto the substrate. <IMAGE>
申请公布号
EP0796929(A1)
申请公布日期
1997.09.24
申请号
EP19970301863
申请日期
1997.03.19
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SILEO, GERARD A.;WOODARD, WILLIAM J.;WALDEN, FREDERICK C.;PETTIT, HAROLD W. JR.;TWIGG, TIMOTHY A.