Abstract: A turbine engine shroud segment comprises a body including a radially outer surface having axially and circumferentially spaced apart edge surfaces. The segment includes a projection integral with and projecting generally radially outwardly from the body, and positioned at a generally midway surface portion between the axially spaced apart edge surfaces. The projection comprises a head and a transition portion with a cross section smaller than that of the head and integral with and between the head and the body. In a turbine engine shroud assembly, a plurality of such shroud segments are assembled circumferentially with a shroud hanger carrying the projection in a hanger cavity through end portions of radially inner opposed hook members that register with the projection at the transition portion.

Abstract: A turbine engine shroud segment comprises a segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, and a plurality of axially and circumferentially spaced apart edge surfaces connected with and between the inner and outer surfaces. For carrying the segment body, the segment includes a projection, in one form a single projection, integral with and projecting generally radially outwardly from the body. The projection is selected to be positioned at a generally midway surface portion of the body radially outer surface between at least one of the plurality of spaced apart edge surfaces. The projection comprises a projection head spaced apart from the body radially outer surface and a projection transition portion, having a transition surface, integral with both the projection head and the body radially outer surface.