Engine Component And Methods For An 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 multifaceted diffusing section configured to improve the adhesion of a coating on the substrate.

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. BUNKER, Ronald Scott

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

Specification

SOFT COPY ATTACHED IN PDF

Documents

Application Documents

#	Name	Date
1	6856-CHE-2015-Correspondence-PA-NOTARIAL CERTIFICATE-020616.pdf	2016-07-21
1	Power of Attorney [23-12-2015(online)].pdf	2015-12-23
2	6856-CHE-2015-NOTARIAL CERTIFICATE-020616.pdf	2016-07-21
2	Form 5 [23-12-2015(online)].pdf	2015-12-23
3	6856-CHE-2015-Power of Attorney-020616.pdf	2016-07-21
3	Form 3 [23-12-2015(online)].pdf	2015-12-23
4	Description(Complete) [23-12-2015(online)].pdf	2015-12-23
4	Drawing [23-12-2015(online)].pdf	2015-12-23
5	Description(Complete) [23-12-2015(online)].pdf	2015-12-23
5	Drawing [23-12-2015(online)].pdf	2015-12-23
6	6856-CHE-2015-Power of Attorney-020616.pdf	2016-07-21
6	Form 3 [23-12-2015(online)].pdf	2015-12-23
7	6856-CHE-2015-NOTARIAL CERTIFICATE-020616.pdf	2016-07-21
7	Form 5 [23-12-2015(online)].pdf	2015-12-23
8	6856-CHE-2015-Correspondence-PA-NOTARIAL CERTIFICATE-020616.pdf	2016-07-21
8	Power of Attorney [23-12-2015(online)].pdf	2015-12-23