Shroud segment and assembly for a turbine engine
First Claim
1. A turbine engine shroud segment comprising a shroud segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, a first plurality of spaced apart axial edge surfaces connected with and between each of the inner and outer surfaces, and a second plurality of spaced apart circumferential edge surfaces connected with and between each of the inner and outer surfaces, wherein:
- the shroud segment includes a shroud segment projection, for carrying the shroud segment body, integral with and projecting generally radially outwardly from the shroud segment body radially outer surface;
the projection being positioned on the shroud segment body radially outer surface at a generally midway surface portion between at least one of the first and second plurality of edge surfaces;
the projection comprising a projection head spaced apart from the shroud body radially outer surface, and a projection transition portion having a transition surface, the projection transition portion being integral with both the projection head and the shroud body radially outer surface, the transition portion being smaller in cross section than the projection head in at least one of the axial and circumferential directions.
2 Assignments
0 Petitions
Accused Products
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. The transition portion has a cross section smaller than the cross section of the projection head, at least in one of the axial and circumferential directions. In a turbine engine shroud assembly, a plurality of such shroud segments are assembled circumferentially with a shroud hanger that carries the segments in a hanger cavity. The cavity is defined at least in part by radially inner opposed hook members each including an end portion that registers with and carries the shroud segment at the projection transition surface.
49 Citations
19 Claims
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1. A turbine engine shroud segment comprising a shroud segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, a first plurality of spaced apart axial edge surfaces connected with and between each of the inner and outer surfaces, and a second plurality of spaced apart circumferential edge surfaces connected with and between each of the inner and outer surfaces, wherein:
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the shroud segment includes a shroud segment projection, for carrying the shroud segment body, integral with and projecting generally radially outwardly from the shroud segment body radially outer surface;
the projection being positioned on the shroud segment body radially outer surface at a generally midway surface portion between at least one of the first and second plurality of edge surfaces;
the projection comprising a projection head spaced apart from the shroud body radially outer surface, and a projection transition portion having a transition surface, the projection transition portion being integral with both the projection head and the shroud body radially outer surface, the transition portion being smaller in cross section than the projection head in at least one of the axial and circumferential directions. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 14, 15, 16, 17, 18, 19)
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9. A method for making a turbine engine shroud segment comprising a shroud segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, a first plurality of spaced apart axial edge surfaces connected with and between each of the inner and outer surfaces, and a second plurality of spaced apart circumferential edge surfaces connected with and between each of the inner and outer surfaces,
the shroud segment including a shroud segment projection, for carrying the shroud segment body, integral with and projecting generally radially outwardly from the shroud segment body radially outer surface; -
the projection being positioned on the shroud segment body radially outer surface at a generally midway surface portion between at least one of the first and second plurality of edge surfaces;
the projection comprising a projection head spaced apart from the shroud body radially outer surface, and a projection transition portion having a transition surface, the projection transition portion being integral with both the projection head and the shroud body radially outer surface, the transition portion being smaller in cross section than the projection head in at least one of the axial and circumferential directions comprising the steps of;
determining operating forces acting during engine operation on the shroud segment body as a result of a combination of temperature differential and pressure differential between an air cooled radially outer surface and the radially inner surface exposed to a flowstream of the turbine engine; and
,selecting the position of the projection on the midway surface portion substantially to reduce the operating forces acting on the projection carrying the shroud segment body. - View Dependent Claims (10, 11, 12, 13)
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Specification