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:
Oct. 25, 2016

Filed:

Nov. 22, 2012
Applicants:

Kyky Technology Co., Ltd., Beijing, CN;

Tsinghua University, Beijing, CN;

Inventors:

Kai Zhang, Beijing, CN;

Han Wu, Beijing, CN;

Qizhi Li, Beijing, CN;

Xiaozhang Zhang, Beijing, CN;

Meng Zou, Beijing, CN;

Assignees:

KYKY TECHNOLOGY CO., LTD., Beijing, CN;

TSINGHUA UNIVERSITY, Beijing, CN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01R 31/28 (2006.01); H02K 15/16 (2006.01); F04D 29/058 (2006.01); F04D 29/66 (2006.01); F04D 19/04 (2006.01); G01M 1/20 (2006.01); H02K 7/09 (2006.01); F16C 32/04 (2006.01);
U.S. Cl.
CPC ...
H02K 15/165 (2013.01); F04D 19/042 (2013.01); F04D 29/058 (2013.01); F04D 29/662 (2013.01); F16C 32/0442 (2013.01); G01M 1/20 (2013.01); H02K 7/09 (2013.01); F16C 32/0444 (2013.01); F16C 2231/00 (2013.01); F16C 2360/45 (2013.01); Y10T 29/49004 (2015.01);
Abstract

A method of rotor dynamic balancing for magnetic levitation molecular pump, including the steps of: activating an force free control module after activating a motor of the magnetic levitation molecular pump; if the maximum radial vibration amplitude does not exceed ½ of a protective clearance during the acceleration of the rotor under the control of the force free control module, indicating that the force free control module is able to inhibit the co-frequency vibration of the rotor, so as to allow the rotational speed of said rotor to exceed its rigid critical rotational speed; performing rotor dynamic balancing operation at a high speed by an influence coefficient method. The method of rotor dynamic balancing can directly perform rotor dynamic balancing operation with respect to the rotor at a high-speed, which facilitates the rotor dynamic balancing operation so as to perform the rotor dynamic balancing operation more quickly and efficiently.


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