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:
Nov. 03, 2020

Filed:

Oct. 17, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Arthur Wesley Johnson, Cincinnati, OH (US);

Joseph Zelina, Waynesville, OH (US);

Eric John Stevens, Mason, OH (US);

Clayton Stuart Cooper, Loveland, OH (US);

Beverly Stephenson Duncan, West Chester, OH (US);

Juntao Zhang, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/58 (2006.01); F23R 3/14 (2006.01); F23R 3/12 (2006.01); F23R 3/18 (2006.01); F23R 3/04 (2006.01); F23R 3/50 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F23R 3/58 (2013.01); F01D 25/00 (2013.01); F23R 3/04 (2013.01); F23R 3/12 (2013.01); F23R 3/14 (2013.01); F23R 3/18 (2013.01); F23R 3/50 (2013.01); F05D 2240/35 (2013.01); F05D 2240/36 (2013.01); F23R 2900/00015 (2013.01);
Abstract

A trapped vortex combustor for use in a gas turbine engine defines a radial direction, an axial direction, and a circumferential direction. The trapped vortex combustor includes an outer vortex chamber wall defining a forward end, and a dome attached to, or formed integrally with, the outer vortex chamber wall at the forward end of the outer vortex chamber wall. The dome and outer vortex chamber wall define at least in part a combustion chamber having an outer trapped vortex chamber. The dome includes an air chute defining an airflow direction. The radial direction and axial direction of the trapped vortex combustor define a reference plane extending through the air chute, the airflow direction of the air chute defining an angle greater than zero with the reference plane.


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