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:
Feb. 15, 2022

Filed:

May. 29, 2020
Applicant:

Doosan Heavy Industries & Construction Co., Ltd., Changwon-si, KR;

Inventors:

Borys Shershnyov, Changwon-si, KR;

Alexander Myatlev, Gimhae-si, KR;

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/10 (2006.01); F01D 9/02 (2006.01); F23R 3/00 (2006.01); F23R 3/28 (2006.01); F02C 3/04 (2006.01); F02C 3/22 (2006.01); F02C 7/04 (2006.01); F02C 7/22 (2006.01); F23R 3/08 (2006.01);
U.S. Cl.
CPC ...
F23R 3/06 (2013.01); F23R 3/002 (2013.01); F23R 3/10 (2013.01); F23R 3/286 (2013.01); F01D 9/023 (2013.01); F02C 3/04 (2013.01); F02C 3/22 (2013.01); F02C 7/04 (2013.01); F02C 7/222 (2013.01); F23R 3/08 (2013.01); F23R 2900/03043 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A combustor and a gas turbine including the same which can reduce a loss of pressure and enhance a cooling efficiency of a liner and transition piece are provided. The combustor may include a liner configured to define a combustion chamber, a transition piece coupled to a rear end of the liner, a flow sleeve configured to surround the liner and the transition piece, a plurality of impingement holes formed in the flow sleeve, and a plurality of inserts inserted into at least some of the impingement holes, wherein each of the inserts may include a first channel configured to guide combustion air, introduced into an associated one of the impingement holes, in a direction parallel to a direction of extension of an annular passage between the flow sleeve and the liner or an annular passage between the flow sleeve and the transition piece, and a second channel configured to guide the combustion air, introduced into the associated one of the impingement holes, in a direction transverse to the annular passage between the flow sleeve and the liner or the annular passage between the flow sleeve and the transition piece.


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