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. 05, 2019

Filed:

Sep. 09, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nan Zong, West Chester, OH (US);

Ahmed Mostafa ELKady, West Chester, OH (US);

Mark Anthony Mueller, Cincinnati, OH (US);

Pradeep Naik, Bangalore, IN;

Gerardo Antonio Salazar Lois, West Chester, OH (US);

Rishikesh Prakash Karande, Bangalore, IN;

Jeffrey Michael Martini, West Chester, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/04 (2006.01); F23R 3/00 (2006.01); F23R 3/10 (2006.01); F23R 3/28 (2006.01); F23R 3/44 (2006.01); F23R 3/46 (2006.01); F04D 29/54 (2006.01); F23R 3/50 (2006.01); F23R 3/54 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F04D 29/542 (2013.01); F23R 3/04 (2013.01); F23R 3/10 (2013.01); F23R 3/28 (2013.01); F23R 3/44 (2013.01); F23R 3/46 (2013.01); F23R 3/50 (2013.01); F23R 3/54 (2013.01); Y02T 50/675 (2013.01);
Abstract

A system including an annular combustor having a first liner wall disposed circumferentially about an axis, a combustion chamber disposed circumferentially about the first liner wall, and a second liner wall disposed circumferentially about the combustion chamber. The annular combustor is configured to direct a combustion gas flow in a downstream direction through the combustion chamber away from a head end toward a turbine. The system also includes a supply passage configured to supply a fluid flow from a compressor to the combustion chamber. The supply passage has a flow path architecture having a turning portion that turns the fluid flow from a compressor discharge direction to an upstream direction generally opposite the downstream direction of combustion gas flow.


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