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Turbine Blade

Abstract: TURBINE BLADE ABSTRACT A turbine blade includes an airfoil having an internal cooling circuit. The cooling circuit includes a body cooling passage with at least one turn, and a tip cooling channel that forms a cooling barrier to thermally isolate the turn from at least a portion of the exterior surface of the airfoil. FIG.1 20

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Patent Information

Application #
Filing Date
30 June 2016
Publication Number
01/2017
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. MCKENZIE, Christopher Lloyd
1000 Western Avenue, Mail Drop: 37402, Lynn, Massachusetts 01905, USA
2. MANNING, Robert Francis
1000 Western Avenue, Mail Drop: 37402, Lynn, Massachusetts 01905, USA
3. REDDY, Bhanu Mahasamudram
1000 Western Avenue, Mail Drop: 37402, Lynn, Massachusetts 01905, USA

Specification

SOFT COPY ATTACHED IN PDF FILE

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