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Turbine Blade

Abstract: A turbine engine [10] comprises an airfoil [78] having one or more internal cooling circuits [120, 122, 124]. The cooling circuits [120, 122, 124] can be fed with a flow of cooling fluid from one or more cooling air inlet passages [88, 90, 92]in fluid communication with the cooling circuits [120, 122, 124]. The cooling circuits [120, 122, 124] can provide the cooling fluid flow within the airfoil [78] to cool the airfoil [78], as well as provide a cooling fluid to a plurality of film holes [200] to create a cooling film on the external surface of the airfoil [78]. 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. KRUMANAKER, Matthew Lee
1 Neumann Way, Cincinnati, OH 45215, USA
2. BRASSFIELD, Steven Robert
9025 Centre Pointe Drive, West Chester, OH 45069, USA
3. BERGHOLZ, Robert Frederick
10200 Anderson Way, Cincinnati, OH 45243, USA
4. SMITH, Aaron Ezekiel
9075 Centre Pointe Drive, West Chester, OH 45069, USA
5. DOOLEY, Weston Nolan
1 Neumann Way, Cincinnati, OH 45069, USA

Specification

SOFT COPY ATTACHED IN PDF

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