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. 07, 2023

Filed:

Apr. 25, 2019
Applicant:

Mitsubishi Electric Corporation, Tokyo, JP;

Inventors:

Takuya Teramoto, Tokyo, JP;

Hiroyasu Hayashi, Tokyo, JP;

Ryo Horie, Tokyo, JP;

Kazuya Michikami, Tokyo, JP;

Takahiro Yamatani, Tokyo, JP;

Hiroshi Tsutsumi, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 17/16 (2006.01); F04D 29/28 (2006.01); F04D 29/30 (2006.01); F04D 29/42 (2006.01); F04D 29/44 (2006.01); F04D 29/60 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 17/162 (2013.01); F04D 29/282 (2013.01); F04D 29/30 (2013.01); F04D 29/424 (2013.01); F04D 29/44 (2013.01); F04D 29/60 (2013.01); F04D 29/68 (2013.01);
Abstract

An impeller includes a backing plate, a rim disposed so as to face the backing plate, and a plurality of blades arranged in a circumferential direction around a virtual rotation axis of the backing plate. Each of the plurality of blades has an inner circumferential end, an outer circumferential end a sirocco blade portion being forward-swept and including the outer circumferential end and having a blade outlet angle of larger than 90 degrees, and a turbo blade portion being swept-back and including the inner circumferential end, a first region located closer to the backing plate than a middle point in an axial direction of the rotation axis, and a second region located closer to the rim than the first region. Each of the plurality of blades is formed such that a blade length in the first region is longer than a blade length in the second region. In the first region and the second region, a ratio of the turbo blade portion in the radial direction is larger than a ratio of the sirocco blade portion in the radial direction.


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