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Engine Component

Abstract: An engine component (68) includes a hot surface (90) in thermal communication with a hot combustion gas flow, and a cooling surface (104), opposite the hot surface (90), along which a cooling fluid flows. At least one vortex generator (102) is provided on the cooling surface (104), and can induce a vortex in the cooling fluid in response to contact with the flowing cooling fluid.

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Patent Information

Application #
Filing Date
23 December 2015
Publication Number
35/2016
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

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

Inventors

1. BERGHOLZ, Robert Frederick
GE Aviation 9025 Centre Pointe Drive West Chester, OH 45069 USA
2. SMITH, Aaron Ezekiel
GE Aviation 9025 Centre Pointe Drive West Chester, OH 45069 USA

Specification

SOFT COPY ATTACHED IN PDF

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