Turbine engine shroud assembly including axially floating shroud segment
AssigneeGeneral Electric Company
InventorsChristopher Charles Glynn, Mary Ellen Alford, Mark Eugene Noe, Toby George Darkins, Jr.
Life of this patent
Estimating the term…
Loading patent…
AssigneeGeneral Electric Company
InventorsChristopher Charles Glynn, Mary Ellen Alford, Mark Eugene Noe, Toby George Darkins, Jr.
Estimating the term…
At least one shroud segment, floating axially independently of adjacent turbine engine shroud assembly members, includes a segment body comprising a radially outer surface and a radially outwardly projecting segment support that includes an axial support wall surface therein. The assembly includes a shroud hanger in axial juxtaposition with the segment support, and at least one axial support projection from the shroud hanger into the segment support at the support wall surface. The support projection supports the shroud segment releasably at the support wall surface sufficiently to enable relative axial movement of the shroud segment on the support projection independently of the shroud hanger and adjacent engine members.
A turbine engine shroud segment for assembly circumferentially about an axial flow engine axis, separate and spaced apart from any blading member, the shroud segment comprising a shroud segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, and at least one shroud segment support integral with the shroud segment body for carrying the shroud segment body, the segment support projecting generally radially outwardly from the shroud segment body radially outer surface, wherein:
A turbine engine shroud assembly comprising at least one shroud segment floating axially independently of other engine members disposed in adjacent juxtaposition with the shroud segment in which:
Dependencies are inferred from the claim text.