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Shroud Assembly And Shroud For Gas Turbine Engine

Abstract: Shrouds and shroud assemblies for gas turbine engines are provided. A shroud includes a shroud body. The shroud body 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 flange extending from the shroud body, and a bore hole defined in the flange. The bore hole extends generally circumferentially through the flange between a first opening and a second opening. Fig.1

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Patent Information

Application #
Filing Date
19 April 2016
Publication Number
44/2016
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
bpo.mail@ge.com
Parent Application

Applicants

GENERAL ELECTRIC COMPANY
1 River Road Schenectady, New York 12345 USA

Inventors

1. HEITMAN, Bryce Loring
1 Neumann Way Cincinnati, Ohio 45215 US
2. RADWANSKI, Michael Todd
1 Neumann Way Cincinnati, Ohio 45215 US
3. SENILE, Darrell Glenn
1 Neumann Way Cincinnati, Ohio 45215 US

Specification

Claims:As Attached , Description:As Attached

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