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. 05, 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);

John Carl Jacobson, Melrose, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/42 (2006.01); F23R 3/06 (2006.01); F23R 3/50 (2006.01);
U.S. Cl.
CPC ...
F23R 3/007 (2013.01); F23R 3/002 (2013.01); F23R 3/06 (2013.01); F23R 3/42 (2013.01); F23R 3/50 (2013.01); F05D 2240/35 (2013.01); F05D 2300/6033 (2013.01); F23R 2900/00005 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); Y02T 50/675 (2013.01);
Abstract

A combustor assembly for a gas turbine engine includes a liner and a combustor dome. The combustor dome and liner together at least in part define a combustion chamber. The combustor dome includes a transition portion and a forward wall. The transition portion extends from the forward wall towards the liner. Additionally the transition portion may define an angle relative to the forward wall and/or may define a radius of curvature between the forward wall of the combustor dome and a flat of the transition portion of the combustor dome for increasing an aerodynamic efficiency of the combustor dome.


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