Centrifugal compressor

US11885347B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11885347-B2
Application numberUS-202117485988-A
CountryUS
Kind codeB2
Filing dateSep 27, 2021
Priority dateMar 28, 2019
Publication dateJan 30, 2024
Grant dateJan 30, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A centrifugal compressor includes a shaft member and an impeller. The shaft member extends in an axial direction and is rotatable. The impeller includes a hub that is disposed on an end portion of the shaft member, and a plurality of blades disposed on an outer peripheral surface of the hub. The impeller has a shape that tapers outward in the axial direction. A cover member is disposed at least at an end portion of the impeller outside in the axial direction. The cover member is joined to outer peripheries of the plurality of blades in a radial direction and covers at least a part of the plurality of blades from outside in the radial direction. A first bearing is disposed outside in the radial direction of the cover member, the first rotatably supporting the impeller.

First claim

Opening claim text (preview).

The invention claimed is: 1. A centrifugal compressor comprising: a shaft member that extends in an axial direction and that is rotatable; a motor that drives rotation of the shaft member; and an impeller configured to include: a hub that is disposed on an end portion of the shaft member and a plurality of blades disposed on an outer peripheral surface of the hub, the impeller having a shape that tapers outward in the axial direction, a cover member being disposed at least at an end portion of the impeller outside in the axial direction, the cover member being joined to outer peripheries of the plurality of blades in a radial direction and covering at least a part of the plurality of blades from outside in the radial direction, a first bearing disposed outside in the radial direction of the cover member, the first bearing rotatably supporting the impeller, a second bearing disposed outside in the radial direction of the shaft member in a part located opposite to the impeller as viewed from the motor, the second bearing rotatably supporting the shaft member, and a third bearing rotatably supporting the shaft member is not provided outside in the radial direction of the shaft member in a part located between the motor and the impeller. 2. The centrifugal compressor according to claim 1 , wherein the cover member is a shroud that covers an entirety of the plurality of blades. 3. The centrifugal compressor according to claim 1 , wherein the first bearing is gas bearing. 4. The centrifugal compressor according to claim 2 , wherein the first bearing is a gas bearing. 5. The centrifugal compressor according to claim 1 , wherein the impeller is a first impeller, the centrifugal compressor further comprises a second impeller configured the same as the first impeller, the first and second impellers are disposed at each of two end portions of the shaft member, the first bearing is provided for the cover member of the first impeller, and a fourth bearing that rotatably supports the second impeller is not provided outside in a radial direction of the second impeller. 6. The centrifugal compressor according to claim 2 , wherein the impeller is a first impeller, the centrifugal compressor further comprises a second impeller configured the same as the first impeller, the first and second impellers are disposed at each of two end portions of the shaft member, the first bearing is provided for the cover member of the first impeller, and a fourth bearing that rotatably supports the second impeller is not provided outside in a radial direction of the second impeller. 7. The centrifugal compressor according to claim 3 , wherein the impeller is a first impeller, the centrifugal compressor further comprises a second impeller configured the same as the first impeller, the first and second impellers are disposed at each of two end portions of the shaft member, the first bearing is provided for the cover member of the first impeller, and a fourth bearing that rotatably supports the second impeller is not provided outside in a radial direction of the second impeller.

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What does patent US11885347B2 cover?
A centrifugal compressor includes a shaft member and an impeller. The shaft member extends in an axial direction and is rotatable. The impeller includes a hub that is disposed on an end portion of the shaft member, and a plurality of blades disposed on an outer peripheral surface of the hub. The impeller has a shape that tapers outward in the axial direction. A cover member is disposed at least…
Who is the assignee on this patent?
Daikin Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F04D29/056. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 30 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).