Sign In to Follow Application
View All Documents & Correspondence

“Igniter Assembly For A Gas Turbine Engine”

Abstract: ABSTRACT OF THE DISCLOSURE In one aspect the present subject matter is directed to an igniter assembly for a gas turbine engine. The igniter assembly includes an outer housing and an igniter tube that extends radially through the outer housing. The igniter tube includes an ignition tip, a nut coupled to the igniter tube and disposed at least partially within the outer housing and a biasing member that extends between an inner surface of a top portion of the outer housing and the nut. A flexible seal extends radially inwardly from a bottom side of the nut and a retention collar is coupled to the igniter tube proximate to the ignition tip. The retention collar is configured to couple to a mounting ring connected to an outer liner of a combustor for the gas turbine engine.

Get Free WhatsApp Updates!
Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
03 June 2016
Publication Number
51/2016
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. HUANG, Fei
1 Neumann Way Cincinnati, OH 45215 US
2. DAY, Christophe J.
1 Neumann Way Cincinnati, OH 45215 US

Specification

SOFT COPY ATTACHED IN PDF

Documents