Magnetic bearing centrifugal compressor and controlling method thereof

Patent metadata

Field	Value
Publication number	US-10920784-B2
Application number	US-201916293839-A
Country	US
Kind code	B2
Filing date	Mar 6, 2019
Priority date	Nov 14, 2018
Publication date	Feb 16, 2021
Grant date	Feb 16, 2021

Abstract

A magnetic bearing centrifugal compressor includes a magnetic bearing spindle having a thrust disk, front and rear axial bearings, an impeller and at least one labyrinth seal. The front and the rear axial bearings are disposed individually to opposing sides of the thrust disk. First and second clearances exist axially between the rear and front axial bearings, respectively, and the thrust disk. The impeller connects a front end of the magnetic bearing spindle. The labyrinth seal pairs the magnetic bearing spindle into an oblique arrangement with respect to the axial direction, and each the labyrinth seal is spaced from the magnetic bearing spindle or the impeller by a labyrinth-seal clearance. By controlling the thrust disk axially, a clearance ratio of the first clearance to the second clearance can be varied to adjust the labyrinth-seal clearance. In addition, a magnetic bearing centrifugal compressor controlling method is also provided.

First claim

What is claimed is:

1. A magnetic bearing centrifugal compressor, comprising:
a magnetic bearing spindle, movable in an axial direction, including an axial thrust-reducing ring;
a thrust disk, sleeving fixedly the magnetic bearing spindle in a radial direction;
a front axial bearing and a rear axial bearing, disposed individually at two opposing sides of the thrust disk, wherein a first clearance exists between the rear axial bearing and the thrust disk in the axial direction, wherein a second clearance exists between the front axial bearing and the thrust disk in the axial direction;
an impeller, connected to a front end of the magnetic bearing spindle;
at least one labyrinth seal, pairing with the magnetic bearing spindle into an oblique arrangement with respect to the axial direction, each of the at least one labyrinth seal being spaced from the magnetic bearing spindle or the impeller by a labyrinth-seal clearance;
at least one touchdown bearing disposed by sleeving the magnetic bearing spindle without direct contact in the axial direction, wherein a first touchdown-bearing clearance and a second touchdown-bearing clearance exist at opposing sides of the at least one touchdown bearing in the axial direction, and a third touchdown-bearing clearance and a fourth touchdown-bearing clearance exist between the at least one touchdown bearing and the magnetic bearing spindle in the radial direction; and
at least one radial bearing disposed by sleeving the magnetic bearing spindle without direct contact in the axial direction, wherein the at least one radial bearing is located between the at least one touchdown bearing and the thrust disk in the axial direction, and a first radial-bearing clearance and a second radial-bearing clearance exist between the at least one radial bearing and the magnetic bearing spindle in the radial direction;
wherein, by controlling a position of the thrust disk in the axial direction, a clearance ratio of the first clearance to the second clearance is varied to adjust the labyrinth-seal clearance;
wherein the first clearance is larger than the first touchdown-bearing clearance, the first clearance is larger than the second touchdown-bearing clearance, the second clearance is larger than the first touchdown-bearing clearance, and the second clearance is larger than the second touchdown-bearing clearance, such that a displacement of the magnetic bearing spindle in the axial direction is limited; and
wherein the first clearance is larger than the first touchdown-bearing clearance, the first radial-bearing clearance is larger than the third touchdown-bearing clearance, the first radial-bearing clearance is larger than the fourth touchdown-bearing clearance, the second radial-bearing clearance is larger than the third touchdown-bearing clearance, and the second radial-bearing clearance is larger than the fourth touchdown-bearing clearance, such that another displacement of the magnetic bearing spindle in the radial direction is limited.

2. The magnetic bearing centrifugal compressor of claim 1 , wherein, when the at least one labyrinth seal sleeves the impeller, the impeller has an oblique surface pairing with the at least one labyrinth seal into a corresponding oblique arrangement, the labyrinth-seal clearance exists between the oblique surface and the at least one labyrinth seal, and an angle between the oblique surface and the axial direction is smaller than or equal to 90 degrees.

3. The magnetic bearing centrifugal compressor of claim 1 , wherein, when the at least one labyrinth seal sleeves the axial thrust-reducing ring, the axial thrust-reducing ring has an oblique surface pairing with the at least one labyrinth seal into a corresponding oblique arrangement, the labyrinth-seal clearance exists between the oblique surface and the at least one labyrinth seal, and an angle between the oblique surface and the axial direction is smaller than or equal to 90 degrees.

4. The magnetic bearing centrifugal compressor of claim 1 , wherein the at least one labyrinth seal is formed as a diverging structure while viewed from the thrust disk.

5. The magnetic bearing centrifugal compressor of claim 1 , further including a driving device for driving the magnetic bearing spindle.

6. The magnetic bearing centrifugal compressor of claim 5 , wherein the driving device includes a motor rotor and a motor stator pairing, without contacting, the motor rotor, and both the motor rotor and the motor stator are arranged to circle the magnetic bearing spindle with the motor rotor being mounted at the magnetic bearing spindle.

7. A method for controlling a magnetic bearing centrifugal compressor, comprising the steps of:
(a) providing the magnetic bearing centrifugal compressor of claim 1 ;
(b) determining whether or not an axial thrust of the magnetic bearing spindle is within an allowable range; and
(c) controlling a position of the thrust disk in the axial direction to adjust the labyrinth-seal clearance.

8. The method for controlling a magnetic bearing centrifugal compressor of claim 7 , after the step (a), further including a step of setting parameters, including an allowable axial thrust, a minimal value of the first touchdown-bearing clearance, a minimal value of the second touchdown-bearing clearance, a maximal displacement allowance of clearance, an upper dead band, a lower dead band, a unit displacement of clearance control, and a cyclic control time.

9. The method for controlling a magnetic bearing centrifugal compressor of claim 8 , wherein the step (b) includes a step (b1) of monitoring the axial thrust of the magnetic bearing spindle, measuring a first touchdown-bearing clearance and a second touchdown-bearing clearance, and waiting for the cyclic control time.

10. The method for controlling a magnetic bearing centrifugal compressor of claim 9 , after the step (b1), further including the steps of:
(b11) determining whether or not the axial thrust is larger than a sum of the allowable axial thrust and the upper dead band; and
(b12) if positive, further determining whether or not the first touchdown-bearing clearance is larger than the minimal value of the first touchdown-bearing clearance.

11. The method for controlling a magnetic bearing centrifugal compressor of claim 10 , wherein the step (c) includes the steps of:
(c1) if a judgment in the step (b12) is positive, further determining whether or not the unit displacement of clearance control is larger than or equal to the maximal displacement allowance of clearance; and
(c2) if positive, controlling a center of the magnetic bearing spindle to displace simultaneously the thrust disk in the axial direction toward the rear axial bearing by a distance equal to the maximal displacement allowance of clearance, so that the first touchdown-bearing clearance is reduced.

12. The method for controlling a magnetic bearing centrifugal compressor of claim 11 , if a judgment in the step (c1) is negative, further including a step of controlling the center of the magnetic bearing spindle to displace simultaneously the thrust disk in the axial direction toward the rear axial bearing by a distance equal to the unit displacement of clearance control, so that the first touchdown-bearing clearance is reduced.

13. The method for controlling a magnetic bearing centrifugal compressor of claim 10 , wherein, if a judgment in the step (b11) is negative, then perform the steps of:
(b13) determining whether or not the axial thrust is less than a sum of the allowable axial thrust and the lower dead band; and
(b14) if positive, determining whether or not the second touchdown-bearing clearance is larger than the minim

Assignees

• Ind Tech Res Inst

Inventors

• Lin Jun-Jie
• Chung Jenn-Chyi
• Liu Chung-Che
• Hung Kuo-Shu

Classifications

• F04D29/162

  of a centrifugal flow wheel · CPC title

• F04D29/058

  magnetic; electromagnetic · CPC title

• F04D29/052

  Axially shiftable rotors (F04D29/051 takes precedence {; control by creating a by-pass F04D27/0246}) · CPC title

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F04D29/051 Primary

  Axial thrust balancing · CPC title