The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 05, 2019

Filed:

Jun. 22, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Gregory Allen Boardman, Liberty Township, OH (US);

Pradeep Naik, Bangalore, IN;

Allen Michael Danis, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F23R 3/00 (2006.01); F23R 3/14 (2006.01); F23R 3/28 (2006.01); F23D 11/38 (2006.01);
U.S. Cl.
CPC ...
F23R 3/06 (2013.01); F01D 25/24 (2013.01); F02C 3/04 (2013.01); F23D 11/383 (2013.01); F23R 3/002 (2013.01); F23R 3/007 (2013.01); F23R 3/14 (2013.01); F23R 3/286 (2013.01); F05D 2220/32 (2013.01); F23R 2900/03043 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A rich-quench-lean combustor assembly for a gas turbine engine includes a fuel nozzle and a dome, the fuel nozzle attached to the dome. The combustor assembly additionally includes a liner attached to or formed integrally with the dome, the liner and the dome together defining at least in part a combustion chamber. The liner extends between a forward end and an aft end. The liner includes a plurality of quench air jets positioned between the forward end and aft end. The quench air jets include a plurality of primary stage air jets and a plurality of secondary stage air jets. The plurality of primary stage air jets are each spaced from the plurality of secondary stage air jets along the axial direction and together provide the combustion chamber with a quench airflow.


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