Method for controlling a compressor

Patent metadata

Field	Value
Publication number	US-10087944-B2
Application number	US-201113640602-A
Country	US
Kind code	B2
Filing date	Apr 8, 2011
Priority date	Apr 20, 2010
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

A method for controlling a compressor that includes a compressor element, whereby during a transition from full load or partial load to zero load, a process A is followed that involves: (1) reducing the inlet pressure; and (2) reducing the speed and/or the drive torque. During a transition from zero load to part load or full load, a process B is followed that involves: (3) increasing of the speed or drive; and (4) increasing the inlet pressure.

First claim

The invention claimed is:

1. A method for controlling a compressor that includes one or more compressor elements, each element having an inlet on an inlet side and an outlet on an outlet side, comprising:
during a transition from full load or partial load to zero load, at least a first of said compressor elements carries out a process A that comprises the steps:
at least temporarily reducing an inlet pressure of the first compressor element;
subsequently or simultaneously, reducing a drive torque of the first compressor element to a zero torque while a speed of the first compressor element is decreased to a minimum speed; and
increasing the drive torque from zero torque to a minimum torque to maintain the rotation of the first compressor element at the minimum speed at which the first compressor element is rotating, and
during a transition from zero load to partial load or full load, at least the first of said compressor elements carries out a process B that comprises the steps:
increasing the drive torque of the first compressor element from the minimum torque to a maximum torque in which the first compressor element is rotating from the minimum speed to a nominal speed or to within a nominal speed range; and
subsequently or simultaneously increasing the inlet pressure of the first compressor element.

2. The method according to claim 1 , wherein the process A comprises the step of, at least before reducing the inlet pressure of the first compressor element, reducing an outlet pressure of the first compressor element.

3. The method according to claim 2 , wherein the outlet pressure of the first compressor element is reduced by opening a blow-off valve on the outlet side of the first compressor element or on the outlet side of another compressor element located downstream from the first compressor element.

4. The method according to claim 1 , wherein the process B comprises the step of, at least after increasing the inlet pressure of the first compressor element, increasing an outlet pressure of the first compressor element.

5. The method according to claim 4 , wherein the outlet pressure of the first compressor element is raised by closing a blow-off valve on the outlet of the first compressor element or on an outlet side of another compressor element located downstream from the first compressor element.

6. The method according to claim 5 , wherein the another compressor element located downstream from the first compressor element is a screw compressor element.

7. The method according to claim 1 , wherein the process B comprises the step of increasing the inlet pressure of the first compressor element to an operating value.

8. The method according to claim 1 , wherein the inlet pressure of the first compressor element is changed by opening or closing an inlet valve on the inlet side of the first compressor element or on an inlet side of another compressor element located upstream from the first compressor element.

9. The method according to claim 1 , wherein the inlet pressure of the first compressor element is changed by opening or closing a blow-off valve located upstream from the first compressor element.

10. The method according to claim 1 , wherein the inlet pressure of the first compressor element is changed by adjusting an operating mode of another compressor element located upstream from the first compressor element.

11. The method according to claim 1 , wherein the inlet pressure of the first compressor element is changed by controlling another compressor element located upstream from the first compressor element, said another compressor element being constructed in the form of a screw compressor element.

12. The method according to claim 2 , wherein the outlet pressure of the first compressor element is changed by adjusting an operating mode of another compressor element, located downstream from the first compressor element.

13. The method according to claim 12 , wherein the another compressor element located downstream from the first compressor element is a screw compressor element.

14. The method according to claim 1 , wherein the one or more compressor elements comprises a directly driven compressor element or a compressor with at least one directly driven compressor element.

15. The method according to claim 7 , wherein an outlet pressure of the first compressor element is reduced by opening a blow-off valve on the outlet side of the first compressor element or on the outlet side of another compressor element located downstream from the first compressor.

16. The method according to claim 14 , wherein the inlet pressure of the first compressor element is changed by opening or closing an inlet valve on the inlet side of the first compressor element or on an inlet side of another compressor element located upstream from the first compressor element, wherein an outlet pressure of the first compressor element is reduced by opening a blow-off valve on the outlet side of the first compressor element or on the outlet side of another compressor element located downstream from the first compressor element, wherein said inlet valve and said blow-off valve are controlled together.

17. The method according to claim 1 , wherein the compressor comprises at least one compressor element that is constructed in the form of a directly driven turbo compressor element, and
at least another compressor element that is constructed in the form of a speed-controlled screw compressor element.

18. The method according to claim 17 , wherein all said compressor elements are incorporated in one housing.

19. The method according to claim 1 , wherein in process A the step of reducing the drive torque of the first compressor element to the zero torque takes place subsequently to the reduction of the inlet pressure of the first compressor element.

20. The method according to claim 1 , wherein the minimum speed is increased to the nominal speed or to within a nominal speed range with a minimal amount of torque.

Assignees

• Huberland Filip Gustaaf M
• Pahner Uwe
• Beyens Filip Petrus I
• Janssens Stijn Jozef Rita Johanna
• Atlas Copco Airpower Nv

Inventors

• Huberland Filip Gustaaf M
• Pahner Uwe
• Beyens Filip Petrus I
• Janssens Stijn Jozef Rita Johanna

Classifications

• F04D27/0284

  Conjoint control of two or more different functions · CPC title

• F04D27/0261 Primary

  by varying driving speed · CPC title

• F04D17/12

  Multi-stage pumps · CPC title

• F04D27/0215

  Arrangements therefor, e.g. bleed or by-pass valves · CPC title

• Y10S415/00

  Rotary kinetic fluid motors or pumps · CPC title