“Nozzle And Nozzle Assembly For Gas Turbine Engine”

Abstract: A nozzle (102) for a gas turbine engine (10), including an airfoil (110) having an exterior surface (112, 114, 116, 118), flange (120, 122) and radially compressive contact face (126). Also included is an airfoil support frame (108) having a mating face (126) positioned in engagement with the contact face (124). A non-orthogonal engagement angle (θ) is provided in order to transmit a compressive force (30) to the airfoil (110). FIG. 3

Patent Information

Application #

Filing Date

20 September 2016

Publication Number

12/2017

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.

Inventors

1. RUTHEMEYER, Michael Anthony

1 Neumann Way, Cincinnati, OH 45215-1988.

2. ALBRECHT, JR., Richard WILLIAM

1 Neumann Way, Evendale, OH 45215, USA

3. SENILE, Darrell Glenn

1 Neumann Way, Cincinnati, OH 45215, USA

Specification

SOFT COPY ATTACHED IN PDF

Documents

Application Documents

#	Name	Date
1	Power of Attorney [20-09-2016(online)].pdf	2016-09-20
2	Form 5 [20-09-2016(online)].pdf	2016-09-20
3	Form 3 [20-09-2016(online)].pdf	2016-09-20
4	Drawing [20-09-2016(online)].pdf	2016-09-20
5	Description(Complete) [20-09-2016(online)].pdf	2016-09-20
6	abstract-201644032094-jpeg.jpg	2016-11-01
7	Other Patent Document [21-02-2017(online)].pdf	2017-02-21
8	Correspondence by Agent_Notarized Inventor Assignment_22-02-2017.pdf	2017-02-22