Multistage centrifugal compressor

Patent metadata

Field	Value
Publication number	US-10077778-B2
Application number	US-201414916282-A
Country	US
Kind code	B2
Filing date	Sep 12, 2014
Priority date	Sep 18, 2013
Publication date	Sep 18, 2018
Grant date	Sep 18, 2018

Abstract

A multistage centrifugal compressor includes a rotating shaft; a first impeller and a second impeller fixed to the rotating shaft; and a casing configured to surround the rotating shaft and the first and second impellers, that forms a first diffuser channel allowing the flowing through of a fluid which is discharged from the first impeller, that forms a first return channel, that forms a second diffuser channel allowing the flowing through of the fluid which is discharged from the second impeller, that forms a second return channel, wherein the first impeller is disposed adjacent to the second impeller in the axial direction of the rotating shaft, in the first diffuser channel, a vaneless diffuser is disposed, and in the second diffuser channel, a vaned diffuser having multiple vanes is disposed.

First claim

The invention claimed is:

1. A multistage centrifugal compressor comprising:
a rotating shaft;
a first impeller and a second impeller fixed in an axial direction of the rotating shaft, and rotating together with the rotating shaft; and
a casing configured to surround the rotating shaft and the first and second impellers, that forms a first diffuser channel allowing the flowing through of a fluid which is discharged from the first impeller to an outward side in a radial direction, that forms a first return channel by which the fluid flowing through the first diffuser channel is guided to an inward side in the radial direction, and is introduced into the second impeller, that forms a second diffuser channel allowing the flowing through of the fluid which is discharged from the second impeller to the outward side in the radial direction, that forms a second return channel by which the fluid flowing through the second diffuser channel is guided to the inward side in the radial direction,
wherein the first impeller is disposed adjacent to the second impeller in the axial direction of the rotating shaft,
wherein in the first diffuser channel, a vaneless diffuser is disposed,
wherein in the second diffuser channel, a vaned diffuser having multiple vanes is disposed, and
wherein the sectional area of a flow path of the second impeller is smaller than the sectional area of a flow path of the first impeller.

Assignees

• Mitsubishi Heavy Ind Compressor Corp

Inventors

• Yamashita Shuichi

Classifications

• F04D29/053

  Shafts · CPC title

• F04D29/4226

  Fan casings · CPC title

• F04D29/286

  multi-stage rotors · CPC title

• F05D2250/52

  Outlet · CPC title

• F04D29/444

  Bladed diffusers · CPC title