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:
Jun. 01, 2021

Filed:

Apr. 01, 2016
Applicant:

Mitsubishi Heavy Industries Aero Engines, Ltd., Aichi, JP;

Inventors:

Yoshiyuki Okabe, Tokyo, JP;

Shigenari Horie, Tokyo, JP;

Tadayuki Hanada, Aichi, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F01D 25/24 (2006.01); F02C 7/20 (2006.01); F23R 3/42 (2006.01);
U.S. Cl.
CPC ...
F01D 25/243 (2013.01); F02C 7/20 (2013.01); F23R 3/002 (2013.01); F23R 3/42 (2013.01); F23R 2900/00005 (2013.01);
Abstract

A gas turbine includes a compressor, a combustor, and a turbine. The compressor, the combustor, and the turbine are arranged along an extending direction of a rotating shaft. The gas turbine also includes a combustor casing housing the combustor and a turbine casing housing the turbine. The combustor casing and the turbine casing are joined to each other via respective flanges thereof projecting toward the outside. The gas turbine further includes a projection part on an inner face of the combustor casing. The projection part projects toward the inside in a radial direction in at least part of a range in the extending direction of the rotating shaft between the flanges and an end of a combustion chamber on the compressor side in the combustor.


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