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:
Sep. 01, 2015

Filed:

Dec. 29, 2011
Applicants:

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

Christian Lee Vandervort, Voorheesville, NY (US);

Narendra Joshi, Schenectady, NY (US);

Sherif Mohamed, Niskayuna, NY (US);

Inventors:

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

Christian Lee Vandervort, Voorheesville, NY (US);

Narendra Joshi, Schenectady, NY (US);

Sherif Mohamed, Niskayuna, NY (US);

Assignee:

General Electric Company, Niskayuna, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/16 (2006.01); F23N 5/00 (2006.01); F02C 3/14 (2006.01); F02C 9/16 (2006.01); F23R 3/34 (2006.01); F02C 3/20 (2006.01);
U.S. Cl.
CPC ...
F23N 5/003 (2013.01); F02C 3/14 (2013.01); F02C 3/16 (2013.01); F02C 9/16 (2013.01); F23R 3/34 (2013.01); F02C 3/20 (2013.01); F23N 2041/20 (2013.01); F23R 2900/03341 (2013.01);
Abstract

A combustor system for use in a turbine engine is provided. The turbine engine includes turbine assembly that includes a fluid inlet, a fluid outlet, and a combustion gas path defined therebetween. The combustor system includes a first combustor assembly and a second combustor assembly. The first combustor assembly is coupled to the turbine assembly for channeling a first flow of combustion gases through the turbine assembly. The first combustor assembly is oriented adjacent to the turbine assembly inlet to channel the first flow of combustion gases to the turbine assembly through the turbine assembly inlet. The second combustor assembly is coupled to the turbine assembly along the combustion gas path for channeling a second flow of combustion gases through the turbine assembly.


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