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. 15, 2020

Filed:

Oct. 08, 2013
Applicant:

Ansaldo Energia Switzerland Ag, Baden, CH;

Inventors:

Robert Marmilic, Rieden, CH;

Jaan Hellat, Baden-Rütihof, CH;

Ewald Freitag, Baden, CH;

Adnan Eroglu, Untersiggenthal, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/00 (2006.01); F02C 7/141 (2006.01); F02C 7/228 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F02C 3/00 (2013.01); F02C 7/141 (2013.01); F02C 7/228 (2013.01); F23R 3/346 (2013.01); F05D 2220/722 (2013.01); F23R 2900/03341 (2013.01); Y02E 20/16 (2013.01); Y02E 20/18 (2013.01); Y02T 50/671 (2013.01); Y02T 50/675 (2013.01);
Abstract

The invention relates to a gas turbine assembly which substantially includes at least one compressor, at least one first burner, at least one second burner that is connected downstream of the first burner, and at least one turbine that is connected downstream of the second burner. At least the first and second burner form a component of a tubular or quasi-tubular combustion chamber element in the flow direction of the combustion path of the burners. The combustion chamber element being closed or quasi-closed and extending between the compressor and the turbine. The combustion chamber elements are arranged around the rotor of the gas turbine assembly in the shape of a ring.


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