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. 17, 2020

Filed:

Mar. 06, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nayan Vinodbhai Patel, Liberty Township, OH (US);

Chad Holden Sutton, Nashville, TN (US);

Duane Douglas Thomsen, Lebanon, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F23R 3/10 (2006.01); F23R 3/00 (2006.01); F23R 3/14 (2006.01);
U.S. Cl.
CPC ...
F23R 3/283 (2013.01); F23R 3/002 (2013.01); F23R 3/10 (2013.01); F05D 2230/642 (2013.01); F05D 2240/15 (2013.01); F23R 3/14 (2013.01); F23R 3/286 (2013.01);
Abstract

A combustion section for gas turbine engine includes an inner liner, an outer liner, and a dome attached to the inner liner and to the outer liner. A heat shield is attached to the dome, with the dome, the heat shield, or both define an opening. The combustion section also includes a fuel nozzle extending at least partially into the opening, the fuel nozzle defining a fuel nozzle axis and a radial direction relative to the fuel nozzle axis. The fuel nozzle defines an aft end, the aft end of the fuel nozzle positioned forward of the aft surface of the heat shield along the fuel nozzle axis such that the aft end of the fuel nozzle defines a minimum separation from the aft surface of the heat shield along the fuel nozzle axis of at least about 0.15 inches.


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