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:
Oct. 06, 2015

Filed:

Jun. 15, 2011
Applicant:

Dimitrie Negulescu, Berlin, DE;

Inventor:

Dimitrie Negulescu, Berlin, DE;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 3/06 (2006.01); F02C 3/14 (2006.01); F23R 3/16 (2006.01); F23R 3/50 (2006.01); F23R 3/58 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F02C 3/06 (2013.01); F01D 9/041 (2013.01); F02C 3/14 (2013.01); F23R 3/16 (2013.01); F23R 3/50 (2013.01); F23R 3/58 (2013.01); F05D 2240/129 (2013.01); F05D 2250/314 (2013.01); Y02T 50/671 (2013.01);
Abstract

A gas-turbine combustion chamber arrangement includes a flame tube, a diffuser element arranged upstream of the flame tube in the flow direction, the diffuser element including an annular duct, and an axial compressor arranged upstream of the diffuser element. The diffuser element features an annular guide vane area in which guide vanes are arranged, which for redirecting an incoming flow are provided at an angle (α) in a range between 28° and 32° relative to a central axis of the gas turbine. Downstream of the guide vane area, a diffuser area is arranged, the diffuser area not being provided with flow-guiding elements affecting the flow, where burners arranged in the annular combustion chamber are provided with their burner axes at an angle (β) between 40° and 50° relative to the central axis.


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