Reverse rotation prevention in centrifugal compressor
11499767 ยท 2022-11-15
Assignee
Inventors
Cpc classification
F25B2500/27
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2700/195
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2600/2501
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2600/0253
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02B30/70
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F25B31/026
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B39/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0261
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0246
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/116
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2700/193
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0292
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2700/197
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F25B49/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B31/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method of operating a heat exchanger system in which a compressor, which is drivable by a motor, is fluidly interposed between an evaporator and a condenser following receipt of a shutdown command is provided. The method includes positioning inlet guide vanes (IGVs) of the compressor in a first position in the event of at least one of a first precondition being in effect and the first and a second precondition both not being in effect. The method further includes positioning the IGVs in a second position in an event the first precondition is not in effect but the second precondition is in effect, ramping a speed of the compressor down until a third precondition takes effect, removing power from the motor and positioning the IGVs in the first position once power is removed from the motor.
Claims
1. A method of operating a heat exchanger system in which a compressor, which is drivable by a motor, is fluidly interposed between an evaporator and a condenser, the method comprising following receipt of a shutdown command: determining that a first precondition is not in effect; determining whether a second precondition is in effect; in response to determining that the first and second preconditions are both not in effect: closing inlet guide vanes (IGVs) of the compressor at a maximum rate so that the IGVs occupy a first position; and in response to determining that the first precondition is not in effect and the second precondition is in effect: holding the IGVs in a second position; ramping a speed of the compressor down until a third precondition takes effect; removing power from the motor; and closing the IGVs once power is removed from the motor.
2. The method according to claim 1, further comprising opening a hot gas bypass (HGBP) valve immediately following receipt of the shutdown command.
3. The method according to claim 1, wherein: the first precondition comprises a variable frequency drive (VFD) fault being declared, the second precondition comprises an operating point being less than a VFD surge prevention line, and the third precondition comprises a pressure difference between the compressor and the condenser being less than a predefined amount.
4. The method according to claim 3, wherein the predefined amount is about 3 PSI.
5. The method according to claim 3, wherein the first position comprises a fully closed position of the IGVs.
6. The method according to claim 3, wherein the ramping of the speed of the compressor down comprises ramping the speed of the compressor down to 0 RPM within a predefined time.
7. A controller to operate a heat exchanger system following receipt of a shutdown command, the controller being configured to: close inlet guide vanes (IGVs) of a compressor at a maximum rate so that the IGVs occupy a first position in the event of first and second preconditions both not being in effect; hold the IGVs in a second position in an event the first precondition is not in effect but the second precondition is in effect; ramp a speed of the compressor down until a third precondition takes effect; remove power from a motor configured to drive the compressor; and close the IGVs once power is removed from the motor.
8. The controller according to claim 7, wherein the controller is further configured to open a hot gas bypass (HGBP) valve immediately following receipt of the shutdown command.
9. The controller according to claim 7, wherein: the first precondition comprises a variable frequency drive (VFD) fault being declared, the second precondition comprises an operating point being less than a VFD surge prevention line, and the third precondition comprises a pressure difference between the compressor and the condenser being less than a predefined amount.
10. The controller according to claim 9, wherein the predefined amount is about 3 PSI.
11. The controller according to claim 9, wherein the first position comprises a fully closed position of the IGVs.
12. The controller according to claim 9, wherein the controller is configured to ramp the speed of the compressor down to 0 RPM within a predefined time.
13. A heat exchanger system, comprising: a compressor comprising inlet guide vanes (IGVs) at an inlet thereof; a motor configured to drive the compressor; and a controller, wherein the controller is configured to control the compressor, the IGVs and the motor and, upon receipt of a shutdown command, closes the IGVs at a maximum rate so that the IGVs occupy a first position in the event of first and second preconditions both not being in effect, holds the IGVs in a second position in an event the first precondition is not in effect but the second precondition is in effect, ramps a speed of the compressor down until a third precondition takes effect, removes power from the motor and closes the IGVs once power is removed from the motor.
14. The heat exchanger system according to claim 13, further comprising an evaporator and a condenser, wherein the compressor is interposed between the evaporator and the condenser.
15. The heat exchanger system according to claim 14, further comprising a hot gas bypass (HGBP) valve downstream from the compressor, interposed between the evaporator and the condenser, wherein the controller opens the HGBP valve immediately following the receipt of the shutdown command.
16. The heat exchanger system according to claim 13, wherein: the first precondition comprises a variable frequency drive (VFD) fault being declared, the second precondition comprises an operating point being less than a VFD surge prevention line, and the third precondition comprises a pressure difference between the compressor and the condenser being less than a predefined amount.
17. The heat exchanger system according to claim 13, wherein the predefined amount is about 3 PSI.
18. The heat exchanger system according to claim 13, wherein the first position comprises a fully closed position of the IGVs.
19. The heat exchanger system according to claim 13, wherein the controller ramps the speed of the compressor down to 0 RPM within a predefined time.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The subject matter, which is regarded as the disclosure, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features and advantages of the disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
(2)
(3)
(4)
(5)
(6) These and other advantages and features will become more apparent from the following description taken in conjunction with the drawings.
DETAILED DESCRIPTION
(7) As will be described below, a control algorithm is proposed for use with water-cooled chillers, in particular, to prevent reverse rotation of the compressor following unit shutdown. The control algorithm generally opens inlet guide vanes (IGVs) of the compressor and a hot gas bypass valve (HGBP) when a shutdown command is provided and received. In addition, a monitoring unit monitors condenser and evaporator pressures so that compressor rotational speed can be held at zero until equalization.
(8) With reference to
(9) The compressor 11 may include or be provided as a centrifugal compressor that operates by compressing fluids as a result of a rotation of the compressor 11 about a longitudinal axis thereof. Such rotation can be driven in part by motor 111, which is powered by power source 112.
(10) The IGVs 110 of the compressor 11 are provided at an inlet of the compressor 11 and can assume various angular positions, which are referred to herein as IGV positions, and which include fully closed positions and multiple open positions. When the IGVs 110 assume the fully closed positions, the compressor 11 does not receive saturated vapor from the evaporator 14. By contrast, when the IGVs assume any of the open positions, the compressor 11 is receptive of the saturated vapor from the evaporator 14 in an amount which is related to how open the IGVs 110 are.
(11) When the IGVs 110 assume one of the open positions, the IGVs 110 can be closed or opened at a rate that is reflective of a need for the compressor 11 to decrease or increase the amount of saturated vapor it can receive. In addition, the IGVs 110 can be closed to the fully closed position at a maximum closure rate in some cases.
(12) As shown in
(13) With reference to
(14) With reference back to
(15) With reference to
(16) In accordance with embodiments, the shutdown command may be received in block 401 from an operator or a high level control element in response to a variable frequency drive (VFD) being in effect, for example. More particularly, the shutdown command may be generated and received from a building control system (based on a load requirement), a chiller control system (e.g., as part of operations for monitoring freeze protection, surges, motor winding temperatures, oil pressures, bearing temperatures, high compressor discharge temperatures, etc.), a VFD alarm and a bearing controller alarm.
(17) In an event the first precondition is not in effect (e.g., the VFD fault is not in effect and has not been declared), the method includes determining whether a second precondition is in effect (block 405). In accordance with embodiments, the second precondition may include or be provided as an operating point of the heat exchanger system 10 or the compressor 11 being less than or below the VPF surge prevention line 201. In an event the second precondition is determined to not be in effect (e.g., the operating point of the heat exchanger system 10 or the compressor 11 is greater than or equal to the VPF surge prevention line 201), the method further includes closing the IGVs 110 at the maximum rate (block 406). Alternatively, in an event the second precondition is determined to be in effect (e.g., the operating point of the heat exchanger system 10 or the compressor 11 is below the VPF surge prevention line 201), the method further includes holding a position of the IGVs 110 (block 407).
(18) At this point, the method also includes ramping a speed of the compressor 11 down to zero RPM within a given time (block 408), determining whether a third precondition is in effect (block 409), removing power from the motor 111 in an event the third precondition is determined to be in effect (block 410) and closing the IGVs 110 once the power is removed (block 411). In accordance with embodiments, the given time may be about five seconds and the third precondition may include or be provided as a cooler-condenser pressure difference being less than a given pressure (e.g., about 3 PSI).
(19) While the disclosure is provided in detail in connection with only a limited number of embodiments, it should be readily understood that the disclosure is not limited to such disclosed embodiments. Rather, the disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the disclosure. Additionally, while various embodiments of the disclosure have been described, it is to be understood that the exemplary embodiment(s) may include only some of the described exemplary aspects. Accordingly, the disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.