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:
May. 01, 2018

Filed:

Oct. 10, 2014
Applicant:

Mitsubishi Hitachi Power Systems, Ltd., Yokohama, Kanagawa, JP;

Inventors:

Shohei Numata, Yokohama, JP;

Osami Yokota, Yokohama, JP;

Tetsuma Tatsumi, Yokohama, JP;

Akinori Hayashi, Yokohama, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/16 (2006.01); F23R 3/44 (2006.01); F23R 3/00 (2006.01); F23R 3/54 (2006.01);
U.S. Cl.
CPC ...
F23R 3/44 (2013.01); F23R 3/005 (2013.01); F23R 3/16 (2013.01); F23R 3/54 (2013.01); F23R 2900/03045 (2013.01);
Abstract

A gas turbine combustor is provided in which product reliability and heat transfer promotion are compatible while suppressing an increase in pressure loss. In a gas turbine combustor comprising a combustor liner, an outer tube provided around an outer periphery of the combustor liner, and an annular flow passage in which a cooling medium (cooling air) flows and which is formed between an outer surface of the combustor liner and an inner surface of the outer tube, the outer tube includes an inner diameter reduced portion and a taper portion smoothly connecting the inner diameter reduced portion and an inner peripheral portion on an upstream side, and is provided at an inner surface of the taper portion with longitudinal vortex generating means generating a vortex that has a central rotation axis in a flowing direction of the cooling medium (cooling air).


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