Methods and systems for detecting and recovering from control instability caused by impeller stall
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F25B-001/00
F25B-049/00
F25B-049/02
F04D-027/02
출원번호
US-0763436
(2014-01-24)
등록번호
US-9823005
(2017-11-21)
국제출원번호
PCT/US2014/013030
(2014-01-24)
국제공개번호
WO2014/117006
(2014-07-31)
발명자
/ 주소
Clanin, Thomas J.
Sibik, Lee L.
출원인 / 주소
TRANE INTERNATIONAL INC.
대리인 / 주소
Hamre, Schumann, Mueller & Larson, P.C.
인용정보
피인용 횟수 :
0인용 특허 :
7
초록▼
Methods and systems for detecting and recovering from control instability caused by impeller stall in a chiller system are provided. In one embodiment, an impeller stall detection and recovery component of a chiller control unit calculates a control error signal frequency spectrum for an evaporator
Methods and systems for detecting and recovering from control instability caused by impeller stall in a chiller system are provided. In one embodiment, an impeller stall detection and recovery component of a chiller control unit calculates a control error signal frequency spectrum for an evaporator leaving water temperature, determines whether a high frequency signal content of the control error signal frequency spectrum exceeds acceptable limits, and adjusts a surge boundary control curve downward by a predetermined incremental value in order to resolve instability caused by impeller stall.
대표청구항▼
1. A method for detecting and recovering from control instability caused by impeller stall in a chiller system that includes a centrifugal compressor, a chiller control unit and one or more inlet guide vanes, the method comprising: calculating a chiller control error signal based on a chilled water
1. A method for detecting and recovering from control instability caused by impeller stall in a chiller system that includes a centrifugal compressor, a chiller control unit and one or more inlet guide vanes, the method comprising: calculating a chiller control error signal based on a chilled water set point temperature signal, an evaporator leaving water temperature signal, a design delta temperature signal that is indicative of a design delta temperature across an evaporator of the chiller system and a lift compensation signal, wherein calculating the chiller control error signal includes using a leaving water temperature control algorithm;determining a frequency spectrum of the chiller control error signal to obtain a controller error signal frequency spectrum signal, wherein the frequency spectrum of the chiller control error signal is determined using a fast Fourier transform algorithm;detecting, via the chiller control unit, whether an impeller stall event has occurred based on the controller error signal frequency spectrum signal;restoring stable operation of the centrifugal compressor when an impeller stall event is detected. 2. The method of claim 1, wherein the fast Fourier transform algorithm is a 64 point fast Fourier transform algorithm. 3. The method of claim 1, wherein detecting whether the impeller stall event has occurred based on the controller error signal frequency spectrum signal includes at least one of: a high frequency signal content of the controller error signal frequency spectrum signal exceeding a low frequency signal content of the controller error signal frequency spectrum signal; orthe high frequency signal content of the controller error signal frequency spectrum signal exceeding a set point threshold level. 4. The method of claim 1, wherein detecting whether the impeller stall event has occurred based on the controller error signal frequency spectrum signal includes both of: a high frequency signal content of the controller error signal frequency spectrum signal exceeding a low frequency signal content of the controller error signal frequency spectrum signal; andthe high frequency signal content of the controller error signal frequency spectrum signal exceeding a set point threshold level. 5. The method of claim 1, wherein restoring stable operation of the centrifugal compressor includes: operating the chiller system under a surge boundary characteristic that is incrementally smaller than a previously operated at surge boundary characteristic. 6. The method of claim 1, wherein restoring stable operation of the centrifugal compressor includes at least one of increasing a compressor speed of the centrifugal compressor or decreasing an opening position of the one or more inlet guide vanes. 7. A chiller system comprising: a centrifugal compressor;one or more inlet guide vanes; anda chiller control unit that includes an impeller stall detection and recovery component, the impeller stall detection and recovery component includes: a control error signal module configured to calculate a chiller control error signal based on a chilled water set point temperature signal, an evaporator leaving water temperature signal, a design delta temperature signal and a lift compensation signal,a control error signal frequency spectrum module configured to determine a frequency spectrum of the chiller control error signal to obtain a controller error signal frequency spectrum signal, wherein the control error signal frequency spectrum module is configured to determine the frequency spectrum of the chiller control error signal using a fast Fourier transform algorithm,an impeller stall detection module configured to detect whether an impeller stall event has occurred based on the controller error signal frequency spectrum signal, andan impeller stall recovery module configured to restore stable operation of the centrifugal compressor when an impeller stall event is detected. 8. The chiller system of claim 7, wherein the control error signal module is configured to calculate the chiller control error signal using a leaving water temperature control algorithm. 9. The chiller system of claim 7, wherein the fast Fourier transform algorithm is a 64 point fast Fourier transform algorithm. 10. The chiller system of claim 7, wherein the impeller stall detection module is configured to detect whether the impeller stall event has occurred when at least one of: a high frequency signal content of the controller error signal frequency spectrum signal exceeds a low frequency signal content of the controller error signal frequency spectrum signal, orthe high frequency signal content of the controller error signal frequency spectrum signal exceeds a set point threshold level. 11. The chiller system of any of claim 7, wherein the impeller stall detection module is configured to detect whether the impeller stall event has occurred when both of: a high frequency signal content of the controller error signal frequency spectrum signal exceeds a low frequency signal content of the controller error signal frequency spectrum signal, andthe high frequency signal content of the controller error signal frequency spectrum signal exceeds a set point threshold level. 12. The chiller system of claim 7, wherein the impeller stall recover module is configured to restore stable operation of the centrifugal compressor by operating the chiller system under a surge boundary characteristic this is incrementally smaller than a previously operated at surge boundary characteristic. 13. The chiller system of claim 7, the impeller stall recover module is configured to restore stable operation of the centrifugal compressor by at least one of: increasing a compressor speed of the centrifugal compressor, ordecreasing an opening position of the one or more inlet guide vanes. 14. The chiller system of claim 7, wherein the design delta temperature signal is indicative of a design delta temperature across an evaporator of the chiller system.
Goshaw Craig M. (La Crosse WI) Sullivan Brian T. (La Crosse WI) Rentmeester Paul C. (La Crosse WI), Control method and apparatus for a centrifugal chiller using a variable speed impeller motor drive.
Watson Thomas E. (Staunton VA) Smallwood ; Jr. Paul R. (Grottoes VA), Method and apparatus for surge detection and control in centrifugal gas compressors.
Haugen Ronald L. ; Kann Meng Jeng, Method for detecting the occurrence of surge in a centrifugal compressor by detecting the change in the mass flow rate.
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