Engine Component

Abstract: An engine component (80) for a gas turbine engine includes a film-cooled substrate (82) having a hot surface (84) facing hot combustion gas flow and a cooling surface (86) facing a cooling fluid flow. A film hole (90) extends through the substrate to an outlet (94) on the hot surface (84). A flow conditioning structure (112, 142) is provided downstream of the outlet (94). FIG.l

Patent Information

Application #

Filing Date

24 February 2016

Publication Number

36/2016

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 USA

Inventors

1. BUNKER, Ronald Scott

One Neumann Way Cincinnati, OH 45215 USA

Specification

SOFT COPY ATTACHED IN PDF

Documents

Application Documents

#	Name	Date
1	201644006327-Correspondence-NOTARIZED ASSIGNMENT-PA-050716.pdf	2016-07-28
1	Power of Attorney [24-02-2016(online)].pdf	2016-02-24
2	201644006327-NOTARIZED ASSIGNMENT-050716.pdf	2016-07-28
2	Form 5 [24-02-2016(online)].pdf	2016-02-24
3	201644006327-Power of Attorney-050716.pdf	2016-07-28
3	Form 3 [24-02-2016(online)].pdf	2016-02-24
4	abstract 201644006327.jpg	2016-07-12
4	Drawing [24-02-2016(online)].pdf	2016-02-24
5	Description(Complete) [24-02-2016(online)].pdf	2016-02-24
6	abstract 201644006327.jpg	2016-07-12
6	Drawing [24-02-2016(online)].pdf	2016-02-24
7	201644006327-Power of Attorney-050716.pdf	2016-07-28
7	Form 3 [24-02-2016(online)].pdf	2016-02-24
8	201644006327-NOTARIZED ASSIGNMENT-050716.pdf	2016-07-28
8	Form 5 [24-02-2016(online)].pdf	2016-02-24
9	201644006327-Correspondence-NOTARIZED ASSIGNMENT-PA-050716.pdf	2016-07-28
9	Power of Attorney [24-02-2016(online)].pdf	2016-02-24