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:
Jul. 30, 2024

Filed:

Sep. 21, 2021
Applicant:

Hitachi Industrial Products, Ltd., Tokyo, JP;

Inventors:

Kiyotaka Hiradate, Tokyo, JP;

Kazuhiro Tsukamoto, Tokyo, JP;

Yuta Mochizuki, Tokyo, JP;

Hiromi Kobayashi, Tokyo, JP;

Takahiro Nishioka, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/28 (2006.01); F04D 17/12 (2006.01); F04D 29/44 (2006.01);
U.S. Cl.
CPC ...
F04D 29/286 (2013.01); F04D 17/12 (2013.01); F04D 29/441 (2013.01);
Abstract

A multistage centrifugal compressor capable of maintaining and improving efficiency while having a static flow path with a reduced outer diameter is provided. Each of return flow paths is provided with a plurality of return vanes disposed in a circular cascade form centered on a center line of a rotational shaft. Each of the return vanes is disposed as a leading vane (A) and a trailing vane (B). The trailing vanes are offset toward the pressure surface side of the leading vanes in a circumferential direction and provided so as to guide a flow from the pressure surface side of the leading vanes to negative pressure surfaces of the trailing vanes. At least one of (1) maximum camber positions (I) of the leading vanes (A), (2) circumferential angles γ formed by trailing edges (A) of the leading vanes and leading edges (B) of the trailing vanes in the circumferential direction centered on the center line of the rotational shaft, and (3) circumferential angles θ formed by the leading edges (B) of the trailing vanes and trailing edges (B) of the trailing vanes in the circumferential direction centered on the center line of the rotational shaft is changed in accordance with the positions of centrifugal compressor stages of the multistage centrifugal compressor.


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