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:
Mar. 23, 2021

Filed:

Jul. 25, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Zhongtao Dai, West Hartford, CT (US);

Lance L. Smith, West Hartford, CT (US);

Jeffrey M. Cohen, Hebron, CT (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F02C 3/04 (2006.01); F02C 9/26 (2006.01); F23R 3/26 (2006.01); F23R 3/28 (2006.01); F23D 11/38 (2006.01); F23R 3/34 (2006.01); F23R 3/14 (2006.01); F23C 7/00 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/222 (2013.01); F02C 3/04 (2013.01); F02C 9/26 (2013.01); F23C 7/004 (2013.01); F23D 11/383 (2013.01); F23R 3/14 (2013.01); F23R 3/26 (2013.01); F23R 3/28 (2013.01); F23R 3/286 (2013.01); F23R 3/343 (2013.01); F23R 3/346 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2220/323 (2013.01); F23D 2202/00 (2013.01); F23D 2900/00008 (2013.01); F23D 2900/00015 (2013.01); F23D 2900/11001 (2013.01); F23R 2900/03343 (2013.01);
Abstract

A combustor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a combustion chamber, and a fuel injector assembly in communication with the combustion chamber that has a swirler body situated about a nozzle to define an injector passage that converges to a throat. The throat is defined at a distance from the combustion chamber. The nozzle includes a primary fuel injector along a first fuel injector axis and at least one secondary plain jet fuel injector axially forward of the primary fuel injector.


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