<p>A turbine blade sealing structure for a ceramic matrix composite component is provided. The turbine sealing structure includes at least one top ply (210) abutting a top portion of a shank (106). The at least one top ply extends out over the top portion of the shank. The turbine sealing structure includes at least one side ply (220) abutting a side portion of the shank (106). The at least one side ply extends along a side portion of the shank. The at least one top ply and at least one side ply form an angel wing (108) and a skirt (106) with on the shank (106) of the ceramic matrix composite component.</p>
申请公布号
CA2877337(A1)
申请公布日期
2014.01.03
申请号
CA20132877337
申请日期
2013.06.13
申请人
GENERAL ELECTRIC COMPANY
发明人
PAIGE, ANTHONY REID;IZON, PAUL;VERRILLI, MICHAEL;MARUSKO, MARK WILLARD;NOE, MARK EUGENE;JAMISON, JOSHUA BRIAN;BRESLIN, ANDREW JOHN