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. 05, 2019

Filed:

Mar. 11, 2014
Applicant:

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

Inventors:

Yoshiaki Arakawa, Tokyo, JP;

Kazuaki Hashiguchi, Tokyo, JP;

Keiji Takeno, Tokyo, JP;

Atsushi Yuasa, Tokyo, JP;

Takahiro Jojima, Tokyo, JP;

Hideta Ogawa, Kanagawa, JP;

Shogo Sawa, Kanagawa, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23D 14/24 (2006.01); F23D 11/24 (2006.01); F23C 7/00 (2006.01); F23D 11/38 (2006.01); F23R 3/14 (2006.01);
U.S. Cl.
CPC ...
F23D 14/24 (2013.01); F23C 7/004 (2013.01); F23D 11/24 (2013.01); F23D 11/383 (2013.01); F23R 3/14 (2013.01); F23C 2900/06041 (2013.01);
Abstract

A combustion burner for a boiler includes: an inner cylinder defining a fuel supply passage for supplying fuel; an outer cylinder surrounding the inner cylinder and defining an air supply passage between the inner cylinder and the outer cylinder; and a swirler in the air supply passage, the swirler being configured to swirl air in the air supply passage. The swirler includes a plurality of blades radially disposed between the inner cylinder and the outer cylinder, the plurality of blades extending from an air-supply side toward a combustion-space side of the air supply passage, and each of the plurality of blades having, at least on an inner cylinder side of the blade, a section with a thickness varied in a burner axial direction, the thickness being smaller at an edge portion on the combustion-space side than at a maximum-thickness section of the blade.


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