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:
Apr. 18, 2017

Filed:

Dec. 11, 2014
Applicants:

Andrew J. Olsen, Amesbury, MA (US);

Ivar Austrem, Oslo, NO;

M. Serkan Yildirim, Mjondalen, NO;

Zheji Liu, Olean, NY (US);

Inventors:

Andrew J. Olsen, Amesbury, MA (US);

Ivar Austrem, Oslo, NO;

M. Serkan Yildirim, Mjondalen, NO;

Zheji Liu, Olean, NY (US);

Assignee:

Dresser-Rand Company, Olean, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/54 (2006.01); F23R 3/60 (2006.01); F02C 7/24 (2006.01); F02C 3/14 (2006.01);
U.S. Cl.
CPC ...
F23R 3/54 (2013.01); F02C 3/145 (2013.01); F02C 7/24 (2013.01); F23R 3/06 (2013.01); F23R 3/60 (2013.01); F05D 2260/201 (2013.01); F05D 2260/96 (2013.01); F05D 2260/963 (2013.01); F05D 2270/14 (2013.01); F23R 2900/00014 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A gas turbine may include a rotatable shaft, a compressor disposed about the rotatable shaft and configured to output compressed air, and a combustor disposed about the rotatable shaft. The combustor may be configured to receive the compressed air and output high temperature compressed gas. The gas turbine may further include a power turbine disposed about the rotatable shaft and configured to receive the high temperature compressed gas, and a first liner defining a plurality of holes and disposed around the combustor. The power turbine may be configured to expand the high temperature compressed gas and rotate the rotatable shaft. The first liner may have a first end and a longitudinally opposite second end. The first end may be coupled to an inner surface of the casing at or adjacent an upstream end of the combustor and the second end may be substantially free from any connection with the casing.


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