Patent ID: 7052235

Claim:
A turbine engine shroud segment comprising a shroud segment body including a segment body inner surface and a segment body outer surface spaced apart from the segment body inner surface, the shroud segment body extending between spaced apart segment body first and second axial edge portions and spaced apart segment body first and second circumferential edge portions, the shroud segment including a segment projection, for carrying the shroud segment body, integral with and projecting away from the segment body outer surface, wherein: the segment projection extends axially along at least a portion of the segment body outer surface between the segment body first and second axial edge portions, spaced apart from the segment body first and second circumferential edge portions; and, the segment projection comprises at least a segment first support surface and a segment second support surface circumferentially spaced apart from the segment first support surface, each segment support surface being of selected support surface shape, the segment first support surface facing toward the segment body first circumferential edge portion and the segment second support surface facing toward the segment body second circumferential edge portion in opposition to the segment first support surface.