Invention Grant
- Patent Title: Shroud assembly and shroud for gas turbine engine
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Application No.: US14686800Application Date: 2015-04-15
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Publication No.: US09863265B2Publication Date: 2018-01-09
- Inventor: David Scott Stapleton
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric Company
- Agent William Scott Andes
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F01D11/08 ; F01D9/04 ; F01D25/24 ; F01D5/02 ; F01D25/00 ; F02C3/04 ; F04D29/32

Abstract:
Shroud assemblies and shrouds for gas turbine engines are provided. A shroud includes a shroud body which includes a forward surface, a rear surface axially spaced from the forward surface, an inner surface extending between the forward surface and the rear surface, and an outer surface extending between the forward surface and the rear surface and radially spaced from the inner surface. The shroud further includes a forward flange extending from the outer surface of the shroud body, and a rear flange extending from the outer surface of the shroud body, the rear flange axially spaced from the forward flange. The shroud further includes a rib disposed between and in contact with the forward flange and the rear flange.
Public/Granted literature
- US20160305265A1 SHROUD ASSEMBLY AND SHROUD FOR GAS TURBINE ENGINE Public/Granted day:2016-10-20
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