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:
Feb. 25, 2020

Filed:

Sep. 16, 2016
Applicant:

Hangzhou Stellar Mechanical & Electrical Technology, Inc., Zhejiang, CN;

Inventors:

Fahua Gu, San Diego, CA (US);

Peng Yuan, Zhejiang, CN;

Jiejie Song, Zhejiang, CN;

Weixing Ji, Zhejiang, CN;

Assignee:

Other;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 25/06 (2006.01); F16C 32/06 (2006.01); F04D 29/057 (2006.01); F04D 29/051 (2006.01); F04D 29/056 (2006.01); F04D 29/58 (2006.01); F04D 17/12 (2006.01); F04D 29/063 (2006.01); F04D 29/28 (2006.01); F04D 29/42 (2006.01);
U.S. Cl.
CPC ...
F04D 25/06 (2013.01); F04D 17/122 (2013.01); F04D 29/051 (2013.01); F04D 29/056 (2013.01); F04D 29/057 (2013.01); F04D 29/0513 (2013.01); F04D 29/063 (2013.01); F04D 29/286 (2013.01); F04D 29/4206 (2013.01); F04D 29/5806 (2013.01); F16C 32/064 (2013.01); F16C 32/0618 (2013.01); F16C 32/0662 (2013.01); F16C 32/0696 (2013.01); F16C 2360/44 (2013.01);
Abstract

A centrifugal compressor assembly and method of operation provides a motor that drives a first stage compressor. The motor comprises a rotor. The motor uses radial aerostatic bearings to stabilize rotation and axial displacement of the rotor. The motor also uses a thrust aerostatic bearing to balance an axial force of the rotor. The radial aerostatic bearings and the thrust aerostatic bearing use a low-viscous vapor-liquid two-phase fluid as a lubricating medium. The radial aerostatic bearings supports the rotor. The thrust aerostatic bearing uses porous aerostatic bearings that use a low-viscous vapor-liquid two-phase fluid, so as to reduce radial and axial oscillation of the rotor. This enables clearance between a blade tip of an impeller and a volute. This causes a seal clearance to be reduced by a half; thereby increasing efficiency of the centrifugal compressor by at least 10 percent.


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