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:
Oct. 01, 2019

Filed:

Feb. 25, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

David Andrew Hannwacker, Torrance, CA (US);

Stephen John Howell, West Newbury, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F23R 3/00 (2006.01); F23R 3/04 (2006.01); F23R 3/28 (2006.01); F23R 3/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F23R 3/02 (2013.01); F23R 3/04 (2013.01); F23R 3/283 (2013.01); F23R 2900/03044 (2013.01); Y02T 50/675 (2013.01);
Abstract

A combustor assembly for a gas turbine engine includes a combustor dome defining an opening, a cooling hole, and at least in part defining a combustion chamber. The combustor dome includes a first side and a second side, the cooling hole extending from the first side to the second side. The combustor assembly additionally includes a fuel-air injector hardware assembly positioned at least partially within the opening of the combustor dome and including a heat shield. The heat shield includes a heat deflector lip. The cooling hole in the combustor dome is oriented to direct a cooling airflow onto the heat deflector lip to maintain at least a portion of the heat shield within a desired operating temperature range.


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