초록 ▼

A stability control algorithm is provided for a centrifugal compressor. The stability control algorithm is used to control a variable geometry diffuser and a hot gas bypass valve (when provided) in response to the detection of compressor instabilities. The stability control algorithm can adjust the

A stability control algorithm is provided for a centrifugal compressor. The stability control algorithm is used to control a variable geometry diffuser and a hot gas bypass valve (when provided) in response to the detection of compressor instabilities. The stability control algorithm can adjust the position of a diffuser ring in the variable geometry diffuser in response to the detection of a surge condition or a stall condition. In addition, the diffuser ring in the variable geometry diffuser can be adjusted to determine an optimal position of the diffuser ring. The stability control algorithm can also be used to open a hot gas bypass valve in response to the detection of continued surge conditions.

대표청구항 ▼

What is claimed is: 1. A chiller system comprising: a compressor, a condenser, and an evaporator connected in a closed refrigerant circuit; the compressor comprising: a compressor inlet to receive uncompressed refrigerant vapor from the chiller system; a compressor outlet to discharge compressed re

What is claimed is: 1. A chiller system comprising: a compressor, a condenser, and an evaporator connected in a closed refrigerant circuit; the compressor comprising: a compressor inlet to receive uncompressed refrigerant vapor from the chiller system; a compressor outlet to discharge compressed refrigerant vapor to the chiller system; and a diffuser being disposed adjacent to the compressor outlet, the diffuser comprising a diffuser space configured to permit passage of compressed refrigerant vapor to the compressor outlet and a diffuser ring adjustably positioned in the diffuser space to vary a size of the diffuser space to control flow of compressed refrigerant vapor through the diffuser space; and a stability control system to control the position of the diffuser ring in the diffuser space in response to the detection of stall conditions or surge conditions in the compressor to maintain stable operation of the compressor. 2. The chiller system of claim 1 wherein the stability control system extends the diffuser ring into the diffuser space in response to the detection of a surge condition. 3. The chiller system of claim 2 wherein the stability control system continuously extends the diffuser ring into the diffuser space for a predetermined surge reaction time period in response to the detection of a surge condition. 4. The chiller system of claim 3 wherein the predetermined surge reaction time period is between about 1 and about 30 seconds. 5. The chiller system of claim 1 wherein the stability control system extends the diffuser ring into the diffuser space in response to the detection of a stall condition. 6. The chiller system of claim 5 wherein the stability control system continuously extends the diffuser ring into the diffuser space in response to the detection of a stall condition until the detected stall condition is corrected or a surge condition is detected. 7. The chiller system of claim 1 wherein the stability control system holds the diffuser ring in position in the diffuser space in response to a predetermined condition. 8. The chiller system of claim 1 wherein the stability control system retracts the diffuser ring from the diffuser space in response to a predetermined condition. 9. The chiller system of claim 8 wherein the stability control system incrementally retracts the diffuser ring from the diffuser space in response to pulses having a predetermined pulse interval until a stall condition is detected or a surge condition is detected. 10. The chiller system of claim 9 wherein the predetermined pulse interval is between about 0.5 seconds and about 5 seconds. 11. The chiller system of claim 1 further comprising a hot gas bypass valve connected between the compressor outlet and the compressor inlet, the hot gas bypass valve being configured to permit a portion of the compressed refrigerant vapor to flow from the compressor outlet to the compressor inlet. 12. The chiller system of claim 11 wherein the stability control system holds the diffuser ring in position in the diffuser space in response to the hot gas bypass valve being opened. 13. A stability control system for maintaining stable operation of a centrifugal compressor having a compressor inlet, a compressor outlet and a variable geometry diffuser with an adjustable flow passage, the stability control system comprising: a stall reacting state to adjust a flow passage of a variable geometry diffuser in response to detecting a stall condition in a centrifugal compressor; and a surge reacting state to adjust a flow passage of a variable geometry diffuser in response to detecting a surge condition in a centrifugal compressor. 14. The stability control system of claim 13 wherein the surge reacting state is configured to continuously close a flow passage of a variable geometry diffuser for a predetermined surge reaction time period. 15. The stability control system of claim 14 wherein the predetermined surge reaction time period is between about 1 second and about 30 seconds. 16. The stability control system of claim 13 wherein the stall reacting state is configured to continuously close a flow passage of a variable geometry diffuser until the detected stall condition is corrected or a surge condition is detected. 17. The stability control system of claim 13 further comprising a probing state to adjust a flow passage of a variable geometry diffuser to obtain an optimal position for a diffuser ring. 18. The stability control system of claim 17 wherein the probing state is configured to incrementally open a flow passage of a variable geometry diffuser until a stall condition is detected or a surge condition is detected. 19. The stability control system of claim 13 further comprising a surge waiting state to hold a position of a flow passage of a variable geometry diffuser in response to a surge condition being corrected in the surge reacting state. 20. The stability control system of claim 19 wherein the surge waiting state is configured to hold a position of a flow passage of a variable geometry diffuser until a predetermined surge waiting period expires or a second surge condition occurs. 21. The stability control system of claim 20 wherein the predetermined surge waiting time period is between about 30 seconds and about 15 minutes. 22. The stability control system of claim 20 further comprising a hot gas override state to hold a position of a flow passage of a variable geometry diffuser in response to the occurrence of a second surge condition in the surge waiting state. 23. The stability control system of claim 13 further comprising a stall waiting state to hold a position of a flow passage of a variable geometry diffuser in response to one of correction of a stall condition in the stall reacting state and starting of a compressor. 24. The stability control system of claim 23 wherein the stall waiting state is configured to hold a position of a flow passage of a variable geometry diffuser until one of a predetermined stall waiting period expires, pre-rotation vanes are moved more than a predetermined threshold amount, a stall condition occurs and a surge condition occurs. 25. The stability control system of claim 24 wherein the predetermined stall waiting period is between about 5 minutes and about 15 minutes. 26. The stability control system of claim 24 wherein the predetermined threshold amount is greater than 0% and less than or equal to about 5% of a range of pre-rotation vane motion. 27. The stability control system of claim 13 wherein the surge reacting state has priority over the stall reacting state. 28. The stability control system of claim 13 further comprising a startup state to fully open a flow passage of a variable geometry diffuser prior to staffing a compressor. 29. A method of providing stability control in a centrifugal compressor having a variable geometry diffuser with an adjustable flow passage, the method comprising the steps of: repeatedly detecting for a surge condition in a centrifugal compressor during operation of a centrifugal compressor; repeatedly detecting for a stall condition in a centrifugal compressor during operation of a centrifugal compressor; continuously closing a flow passage of a variable geometry diffuser in response to the detection of a surge condition in a centrifugal compressor for a predetermined surge reaction time period; and continuously closing a flow passage of a variable geometry diffuser in response to the detection of a stall condition in a centrifugal compressor until the detected stall condition is corrected or a surge condition is detected. 30. The method of claim 29 wherein the predetermined surge reaction time period is between about 1 second and about 30 seconds. 31. The method of claim 29 further comprising the step of incrementally opening a flow passage of a variable geometry diffuser in response to a predetermined condition until one of a stall condition is detected and a surge condition is detected. 32. The method of claim 29 further comprising the step of holding a position of a flow passage of a variable geometry diffuser in response to a surge condition being corrected in the surge reacting state until a predetermined surge waiting period expires or a second surge condition occurs. 33. The method of claim 32 wherein the predetermined surge waiting time period is between about 30 seconds and about 15 minutes. 34. The method of claim 29 further comprising the step of fully opening a flow passage of a variable geometry diffuser in response to stopping a centrifugal compressor. 35. The method of claim 29 further comprising the step of holding a position of a flow passage of a variable geometry diffuser in response to one of correction of a stall condition and starting of a centrifugal compressor until one of a predetermined stall waiting period expires, pre-rotation vanes are moved more than a predetermined threshold amount, a stall condition occurs and a surge condition occurs. 36. The method of claim 35 wherein the predetermined stall waiting period is between about 5 minutes and about 15 minutes. 37. The method of claim 35 wherein the predetermined threshold amount is greater than 0% and less than or equal to about 5% of a range of pre-rotation vane motion.