Engine Component

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Engine Component

Abstract: An engine component for a gas turbine engine includes a film-cooled substrate having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. The substrate includes one or more film holes that have a metering section defining a metering diameter and a diffusing section that defines a hooded length.

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Notices, Deadlines & Correspondence

Patent Information

Application #

Filing Date

15 March 2016

Publication Number

41/2016

Publication Type

INA

Invention Field

MECHANICAL ENGINEERING

Status

bpo.mail@ge.com

Parent Application

Applicants

GENERAL ELECTRIC COMPANY

1 River Road Schenectady, New York 12345 USA

Inventors

1. BUNKER, Ronald Scott

GE Aviation 9075 Centre Pointe Drive West Chester, OH 45069 USA

2. BUCK, Frederick Alan

GE Aviation Centre Pointe 3 MD S172 1 Neumann Way West Chester, OH 45069 USA

3. BRIGGS, Robert David

GE Aviation Centre Pointe 3 MD S172 1 Neumann Way Cincinnati, OH 45215 USA

4. BRAINCH, Gulcharan Singh

9075 Centre Pointe Drive CPT III 4th Floor M/D S174 West Chester, OH 45069 USA

5. FELDMANN, Kevin Robert

1 Neumann Way, MD S136 Cincinnati, OH 45215 USA

Specification

SOFT COPY ATTACHED IN PDF