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:
Oct. 06, 2020

Filed:

Apr. 03, 2015
Applicant:

Mitsubishi Heavy Industries, Ltd., Tokyo, JP;

Inventors:

Yasuro Sakamoto, Tokyo, JP;

Hiroyuki Hamana, Yokohama, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/54 (2006.01); F01D 9/04 (2006.01); F04D 29/32 (2006.01); F04D 29/66 (2006.01);
U.S. Cl.
CPC ...
F04D 29/547 (2013.01); F01D 9/041 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F04D 29/667 (2013.01);
Abstract

A rotor blade () provided in an axial flow compressor () including a rotating shaft, a casing (), a diffuser portion () provided on a downstream side of the casing to communicate with a flow path (C) of the casing and form an annular shape and configured to define a diffuser flow path (DC) in which a cross-sectional area of the flow path expands toward the downstream side, a plurality of stator vane rows (), and rotor blade rows () performing compression of a gas. A plurality of rotor blades are spaced apart from each other in a circumferential direction, and constitute a final rotor blade row (A) positioned on a most downstream side among the rotor blade rows, and include a blade portion () having a larger deflection angle on a hub side and a chip side than at a central portion in a blade height direction.


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