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:
Nov. 17, 2020

Filed:

Jun. 08, 2016
Applicant:

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

Inventors:

Masaki Mitani, Kanagawa, JP;

Koshiro Fukumoto, Kanagawa, JP;

Toshihiko Saito, Tokyo, JP;

Mitsunori Isono, Tokyo, JP;

Dai Morishige, Tokyo, JP;

Nobuyuki Izutsu, Kanagawa, JP;

Hiroyuki Yamasaki, Kanagawa, JP;

Yoshiyuki Wada, Kanagawa, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F23R 3/14 (2006.01); F02C 7/232 (2006.01); F23R 3/32 (2006.01); F02C 3/04 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F23R 3/286 (2013.01); F02C 3/04 (2013.01); F02C 7/232 (2013.01); F23R 3/14 (2013.01); F23R 3/28 (2013.01); F23R 3/32 (2013.01); F23R 3/343 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F23N 2227/22 (2020.01); F23N 2241/20 (2020.01);
Abstract

Provided are a combustor nozzle, a gas turbine combustor, a gas turbine, a cover ring, and a combustor nozzle manufacturing method. The combustor nozzle includes: a nozzle body provided with a fuel flow passage; a cover ring that is disposed on an outer side of the nozzle body so as to form air flow passages that allow air to jet out toward a front side; and fuel injection nozzles that are provided in a leading end part of the nozzle body at predetermined intervals in a circumferential direction and extend through the cover ring so as to be able to inject fuel from the fuel flow passage toward the front side. The cover ring has an outer circumferential surface cover that covers an outer circumferential surface of the nozzle body, a leading end surface cover that covers a leading end surface of the nozzle body, and a plurality of inclined flow passages that extend through the leading end surface cover in a thickness direction and are inclined in a predetermined direction relative to a direction of a central axis.


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