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:
Dec. 08, 2020

Filed:

Apr. 09, 2014
Applicant:

Mitsubishi Heavy Industries Thermal Systems, Ltd., Tokyo, JP;

Inventors:

Yasushi Hasegawa, Tokyo, JP;

Kenji Ueda, Tokyo, JP;

Akimasa Yokoyama, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/20 (2006.01); F04D 29/058 (2006.01); F04D 29/051 (2006.01); F04D 29/46 (2006.01); F04D 29/048 (2006.01); F04D 29/041 (2006.01); F04D 29/042 (2006.01); F04D 29/052 (2006.01);
U.S. Cl.
CPC ...
F01D 11/20 (2013.01); F04D 29/041 (2013.01); F04D 29/042 (2013.01); F04D 29/048 (2013.01); F04D 29/051 (2013.01); F04D 29/052 (2013.01); F04D 29/058 (2013.01); F04D 29/462 (2013.01);
Abstract

The purpose of the present invention is to provide: a turbo compressor which is provided with an open impeller and has the minimal gap between the shroud and the impeller such that efficiency is improved and the safe operating region is enlarged; and a turbo chiller using the same. The turbo compressor is provided with an open impeller with a shroud provided on the side of a casing, and the rotary shaft is supported by a radial magnetic bearing and a magnetic thrust bearing. The turbo compressor is provided with a control unit that comprises: a load calculating means that calculates the axial thrust load generated by the pressure distribution of the compressor; and an axial support position control means that controls a gap between the impeller and the shroud to be a target gap by varying, on the basis of the axial thrust load, the axial support position of the rotary shaft due to the magnetic thrust bearing.


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