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Shrouds And Methods For Forming Turbine Components

Abstract: Shrouds and methods for forming turbine components 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 cooling passage defined in the shroud, the cooling passage extending generally circumferentially through the shroud. FIG.1

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Patent Information

Application #
Filing Date
06 October 2016
Publication Number
16/2017
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, United States of America

Inventors

1. STAPLETON, David Scott
1000 Western Avenue, Lynn, Massachusetts 01905, USA
2. GROVES II, Robert Charles
1 Neumann Way, Cincinnati, Ohio 45215, USA

Specification

SOFT COPY ATTACHED IN PDF

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