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. 19, 2019

Filed:

Jul. 27, 2016
Applicant:

Mitsubishi Hitachi Power Systems, Ltd., Nishi-ku, Yokohama, JP;

Inventors:

Takanori Shibata, Yokohama, JP;

Naoto Omura, Yokohama, JP;

Chihiro Myoren, Yokohama, JP;

Yasuo Takahashi, Yokohama, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/54 (2006.01); F04D 29/32 (2006.01); F04D 29/52 (2006.01); F04D 19/02 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 29/542 (2013.01); F01D 5/143 (2013.01); F01D 5/145 (2013.01); F04D 19/02 (2013.01); F04D 29/321 (2013.01); F04D 29/324 (2013.01); F04D 29/526 (2013.01); F04D 29/544 (2013.01); F04D 29/547 (2013.01); F04D 29/681 (2013.01); F04D 29/682 (2013.01); F04D 29/684 (2013.01); F01D 5/141 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/122 (2013.01); F05D 2240/304 (2013.01); F05D 2240/306 (2013.01); F05D 2240/80 (2013.01); F05D 2250/71 (2013.01); F05D 2250/713 (2013.01);
Abstract

An axial flow compressor includes multiple rotor blade rows configured to include multiple rotor blades and multiple stator blade rows configured to include multiple stator blades, the multiple rotor blades and the multiple stator blades being arranged in an annular channel through which a working fluid flows. A portion of at least one wall surface on an inner peripheral side and an outer peripheral side of the annular channel, the portion being at an arrangement portion where at least any one blade row of the rotor blade rows and the stator blade rows is located, has a protruding portion such that downstream side part of the portion is curved so as to further protrude to the annular channel than upstream side part of the portion. Each blade of the blade row located at the protruding portion of the wall surface is configured such that an increase rate in a wall surface direction of a blade outlet angle in a blade end portion on the side of the wall surface having the protruding portion is greater than an increase rate in the wall surface direction of a blade outlet angle in a blade height intermediate portion.


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