Hot gas bypass control for centrifugal chillers

Information

  • Patent Grant
  • 6691525
  • Patent Number
    6,691,525
  • Date Filed
    Tuesday, May 21, 2002
    22 years ago
  • Date Issued
    Tuesday, February 17, 2004
    20 years ago
Abstract
Methods and systems consistent with this invention control a hot gas bypass valve in a refrigeration system including a centrifugal compressor, a condenser, an evaporator, and a hot gas bypass line between the compressor and the evaporator. Such methods and systems continuously sense for a surge condition during operation of the refrigeration system, indicate a surge condition when the refrigeration system is operating under surge conditions, and open at least partially the hot gas bypass valve in response to the sensed surge condition to return the refrigeration system to operating under non-surge conditions. Methods and systems consistent with this invention also sense a present head parameter representative of the present head of the compressor, sense a present load parameter representative of the present load, and control the hot gas bypass valve so as to avoid surging in the compressor in response to the present head parameter, the present load parameter, and stored head and load parameters.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates generally to the control of a centrifugal liquid chiller, and more specifically to the use of a hot gas bypass valve or another orifice in a centrifugal liquid chiller to minimize surge.




2. Description of the Related Art




As generally known, surge is an unstable condition that may occur when compressors, such as centrifugal compressors, are operated at light loads and high-pressure ratios. It is a transient phenomenon characterized by high frequency oscillations in fluid pressure and flow, and, in some cases, a complete flow reversal through the compressor. Surge, if uncontrolled, causes excessive vibrations that may result in permanent damage to the compressor. Further, surge may cause excessive electrical power consumption if the drive device is an electric motor.




It is generally known that a hot gas bypass (HGBP) flow helps avoid surge during low-load or partial-load conditions. As the cooling load decreases, the requirement for hot gas bypass flow increases. The amount of hot gas bypass flow at a certain load condition is dependent on a number of parameters and is controlled by a HGBP valve.




A HGBP valve control in the prior art provides for an analog electronic circuit that outputs a DC voltage signal that is proportional to the required opening of the valve. The prior art system, however, requires manual calibration at two different chiller operating points at which the compressor just begins to surge. As a consequence, a good deal of time is spent performing the calibration with the assistance of a service technician. Further, variation of coolant flow, which is necessary for many applications, requires repeated calibration.




Another disadvantage of the prior art is that it makes the false assumption that the “surge boundary,” which defines the conditions under which the compressor would surge as a function of certain parameters, is a straight line. Instead, it is often characterized by a curve that may deviate significantly from a straight line at various parameters. This inaccuracy of the prior art may cause the HGBP valve to open prematurely, or it may allow the unit to surge unnecessarily at the operating conditions.




Thus, it is desirable to provide an automatic control system for the HGBP valve or other flow control devices to provide optimal control that is responsive to the characteristic of a given centrifugal chiller system.




SUMMARY OF THE INVENTION




This summary and the following detailed description should not restrict the scope of the claimed invention. Both provide examples and explanations to enable others to practice the invention. The accompanying drawings, which form part of the detailed description, show several embodiments of the invention and, together with the description, explain the principles of the invention.




Methods and systems consistent with this invention control a hot gas bypass valve in a refrigeration system including a centrifugal compressor, a condenser, an evaporator, and a hot gas bypass line between the compressor and the evaporator. Such methods and systems continuously sense for a surge condition during operation of the refrigeration system, indicate a surge condition when the refrigeration system is operating under surge conditions, and open at least partially the hot gas bypass valve in response to the sensed surge condition to return the refrigeration system to operating under non-surge conditions.




Methods and systems consistent with this invention control a hot gas bypass valve in a refrigeration system including a centrifugal compressor, a condenser, an evaporator, and a hot gas bypass line between the compressor and the evaporator. Such methods and systems sense a present head parameter representative of the present head of the compressor, sense a present load parameter representative of the present load, and control the hot gas bypass valve so as to avoid surging in the compressor in response to the present head parameter, the present load parameter, and stored head and load parameters.











BRIEF DESCRIPTION OF THE DRAWINGS




The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate several embodiments of the invention and together with the description, serve to explain the principles of the invention. In the drawings,





FIG. 1

is a diagram of a refrigeration system consistent with this invention;





FIG. 2

is a plot of a surge boundary curve and a table that stores data points that define the surge boundary curve, all consistent with this invention;





FIGS. 3A

,


3


B, and


3


C are flow charts of a control process, consistent with this invention, using the surge boundary curve of

FIG. 2

; and





FIGS. 4A

,


4


B, and


4


C are flow charts of a control process, consistent with this invention, that may operate without the surge boundary curve of FIG.


2


.











DESCRIPTION OF THE PREFERRED EMBODIMENT




The following description of embodiments of this invention refers to the accompanying drawings. Where appropriate, the same reference numbers in different drawings refer to the same or similar elements.





FIG. 1

is a diagram of a refrigeration system


100


consistent with this invention. Refrigeration system


100


also includes a centrifugal compressor


110


that compresses refrigerant vapor and delivers it to a condenser


112


via a line


114


. Condenser


112


includes a heat-exchange coil


116


having an inlet


118


and an outlet


120


connected to a cooling tower


122


or other cooling system. Condensed liquid refrigerant from condenser


112


flows via a line


124


to an evaporator


126


. A variable orifice


172


located in line


124


causes a pressure drop that regulates the flow of liquid refrigerant to evaporator


126


. In another embodiment, variable orifice


172


may be replaced by a conventional fixed orifice plate. Evaporator


126


includes a heat-exchanger coil


128


having a supply line


128


S and a return line


128


R connected to a cooling load


130


. Vapor refrigerant in the evaporator


126


returns to compressor


110


via a suction line


132


containing pre-rotational vanes (PRV)


133


. A hot gas bypass (HGBP) valve


134


is interconnected between a line


136


from the outlet of compressor


110


and a line


138


connected to an inlet of PRV


133


.




A control panel


140


includes an interface module


146


for opening and closing HGBP valve


134


. A valve controller


174


opens and closes variable orifice


172


(relative to its previous position) based on signals received from microprocessor


150


delivered through interface module


146


. Control panel


140


also includes an analog to digital (A/ID) converter


148


, a microprocessor


150


, and a memory


144


, preferably a non-volatile memory. Refrigeration system


100


includes many other features which are not shown in FIG.


1


and are not needed to describe or explain the present invention. These features have been purposely omitted to simplify the drawing for ease of illustration.




A pressure sensor


154


generates a DC voltage signal


152


proportional to the pressure in condenser


110


. Pressure sensor


154


preferably directly senses the pressure in compressor


110


, but it can also sense a pressure at other positions, as long as the sensed pressure is directly or indirectly representative of the pressure in condenser


110


. A pressure sensor


160


generates a DC voltage signal


162


proportional to the pressure in evaporator


126


. Again, pressure sensor


160


preferably senses the pressure in evaporator


126


directly, but it also may sense a related pressure representative of the pressure in evaporator


126


. Typically, these signals


152


,


162


are between 0.5 and 4.5V (DC). A PRV position sensor


156


senses the relative position of the PRV vane. For example, the sensor may be a potentiometer that provides a DC voltage signal


158


that is proportional to the position of PRV


133


. A temperature sensor


170


on supply line


128


S generates a DC voltage signal


168


proportional to the chilled water temperature leaving evaporator


126


(LCHWT). Again, temperature sensor


170


preferably senses the temperature of the chilled water (or other fluid) as it leaves the evaporator, but it can also sense a temperature that is related and representative of the temperature of the chilled water leaving evaporator


126


.




The four analog DC voltage signals


158


,


152


,


162


, and


168


are inputs to control panel


140


and are converted to digital signals


176


by A/D converter


148


. Digital signals


176


are inputs to microprocessor


150


. Software that runs microprocessor


150


performs all necessary calculations and decides what the HGBP valve


134


position and variable orifice


172


position should be, as described below, as well as other functions. One of these functions is to electronically detect surge in compressor


110


and then move HGBP valve


134


and/or variable orifice


172


to more open or more closed positions according to sensed parameters and preselected criteria stored in memory


144


. Microprocessor


150


controls HGBP valve


134


and valve controller


174


through interface module


146


. Microprocessor


150


may run an application that resides in memory


144


to control elements of system


100


.




Methods and systems consistent with this invention adaptively determine the position of HGBP valve


134


as system


100


operates by using a surge boundary curve. An adaptive hot gas bypass (adaptive HGBP or AHGBP) process may create a surge boundary curve, which represents the conditions under which surge occurs as a function of system parameters. Two system parameters that may be used to define the surge boundary curve are (1) the chiller cooling load, and (2) the compressor head.

FIG. 2

is a plot


206


of a surge boundary curve


204


and a table


202


that stores data points that define the surge boundary curve


204


, all consistent with this invention. Table


202


may be stored in memory


144


. Curve


204


defines two regions: (1) surge region A and (2) non-surge region B.




In the preferred embodiment, the chiller cooling load is represented by PRV position


158


and the compressor head is represented by the control pressure ratio. The control pressure ratio is described in more detail below. Table


202


stores the PRV index, which corresponds to PRV position


158


, and the control pressure ratio. The values stored in table


202


correspond to curve


204


. Thus, the PRV index is on the abscissa (x-axis) and the control pressure ratio is on the ordinate (y-axis) of plot


206


.




Surge boundary curve


204


is useful while refrigeration system


100


is operating under non-surge conditions in non-surge region B, where HGBP valve


134


is closed, to identify the conditions that would drive compressor


110


into surge, i.e., into surge region A. Once refrigeration system


100


is operating under surge conditions, however, surge boundary curve


204


may not indicate the parameters defining the surge and non-surge regions. This characteristic is true because while HGBP valve


134


is open, either alone or in combination with variable orifice


174


, the PRV position becomes uncorrelated to the actual surge boundary. When HGBP valve


134


is fully or partially open, system


100


is said to be operating in the “HGBP region.” Therefore, while system


100


operates under non-surge conditions (in non-surge region B), surge boundary curve


204


indicates the conditions under which system


100


would surge (i.e., enter surge region A). Curve


204


may also be useful for other information as to the surge characteristics of the compressor.




In the preferred embodiment, methods and systems consistent with this invention may determine surge boundary curve


204


during operation of system


100


. Also, surge boundary curve


204


may be updated and changed during operation of system


100


. For instance, initially table


202


may have no control pressure values. Surge boundary curve


204


and the values in table


202


may be determined by detecting compressor


110


surge as it begins to take place (while system


100


was previously operating under non-surge conditions), and storing values that represent the compressor head and chiller load, i.e., the surge point, in table


202


. The surge point may not be stored in all circumstances, however. The surge point may not be stored if system


100


conditions are unstable. System


100


conditions may be unstable, for instance, if the rate of change of the leaving chilled water temperature is greater than approximately 0.3° F. per second. The leaving chilled water temperature (LCHWT)


128


S is obtained via sensor


170


, and its rate of change may be calculated. The control pressure ratio in table


202


may be periodically cleared to reconstruct surge boundary curve


204


and the values in table


202


.




Control pressure ratios in table


202


may be organized relative to a PRV index value that corresponds to PRV position


158


. For example, a given PRV position may be converted into a percentage from zero to 100%. Zero percent may represent closed vanes, and 100% may represent wide open vanes. A present PRV index value of 1 could represent a PRV percentage of zero to 5%. A present PRV index value of 2 could represent a PRV percentage of 5% to 10%, etc. The PRV index in table


202


ranges from 1 to 20, and the corresponding stored control pressure ratios for each PRV index are represented by the letters “a” through “t,” respectively. Alternatively, table


202


can store other information such as evaporator pressure


162


, condenser pressure


152


, PRV position


158


, among other data that may be useful for determining the conditions under which surge would occur. Another, preferred method for determining the PRV index is described below with respect to FIG.


3


C.




In the preferred embodiment, the method and system disclosed in U.S. Pat. No. 5,764,062, hereby incorporated by reference, is used to detect a surge condition. Thus, if a surge event begins to occur when system


100


was previously operating under non-surge conditions, the process of the invention determines the control pressure ratio and PRV position


158


and may create a new point on surge boundary curve


204


.




As mentioned above, in the preferred embodiment, PRV position


158


represents the chiller load. Use of the PRV position may minimize variations due to flow. Various other parameters, however, may represent the chiller load. For instance, U.S. Pat. No. 4,248,055, hereby incorporated by reference, represents the chiller cooling load as the difference between evaporator returning chilled water


128


R temperature (RCHWT) and leaving chilled water


128


S temperature (LCHWT).




Various parameters may be used to represent the compressor head. For example, U.S. Pat. No. 4,248,055, hereby incorporated by reference, represents compressor head by the condenser water liquid temperature (CLT). As mentioned above, in the preferred embodiment the pressure ratio represents the compressor head. This is similar to the method and system in U.S. Pat. No. 4,282,719, hereby incorporated by reference, which also represents compressor head by a pressure ratio. The pressure ratio is defined as condenser pressure


152


minus evaporator pressure


162


, that quantity divided by evaporator pressure


162


. An “average pressure ratio” is defined as the average value of the present calculated pressure ratio and a number of past calculated pressure ratios. In the preferred embodiment, methods and systems consistent with this invention use the average pressure ratio. When the average pressure ratio is entered into table


202


it is referred to as the “control” pressure ratio because system


100


operates based upon table


202


entries. Averaging may limit erroneous values as a result of fluctuations in the pressure ratio due to surges.





FIG. 3A

is a flow chart of a process


300


A, consistent with this invention, for determining the average pressure ratio. When control process


300


A starts, the present pressure ratio (dp_p) is assigned the value of




(condenser pressure


152


/evaporator pressure


162


)−


1


,




which is equal to




((condenser pressure


152


−evaporator pressure


162


)/evaporator pressure


162


)




(step


1


). The pressure ratio should only have positive numbers. Therefore, if the present pressure ratio (dp_p) is negative (step


2


), it is set equal to zero (step


3


). Next, the average present pressure ratio (dp_pa), is assigned the average value of the past N number of pressure ratios, including the present pressure ratio (step


4


). In the preferred embodiment, N is equal to ten.





FIG. 3B

is a flow chart of a process


300


B, consistent with this invention, for controlling HGBP valve


134


. Process


300


B determines the present average pressure ratio and PRV index (step


302


). A more detailed method for determining the PRV index is described below with respect to FIG.


3


C. If the present average pressure ratio at the present PRV index is within a programmable surge margin below the control pressure ratio (step


304


) and system


100


is in the non-surge region B, methods and systems consistent with this invention partially or fully open HGBP valve


134


alone or in combination with variable orifice


172


(step


306


). In the preferred embodiment, the programmable surge margin is 0.1. If surge is detected below the programmable surge margin (step


310


), then the control pressure ratio stored in table


200


is overwritten with the present average pressure ratio at the present PRV index determined in step


302


(step


312


) and process


300


B proceeds to step


306


. After HGBP valve


134


is opened, however, the position of HGBP valve


134


is controlled by surge detection as described below with respect to

FIGS. 4B-4C

(step


306


). System


100


operates under surge conditions until conditions warrant the closing of HGBP valve


134


completely (step


308


), at which time system


100


operates under non-surge conditions in non-surge region B as defined by surge boundary curve


204


.





FIG. 3C

is a flow chart of a process


300


C for determining the PRV index (prv_index) for the stored control pressure ratios. Pre-rotational vanes


133


may be wide open, which corresponds to a value of 100%, they may be closed, which corresponds a value of 0%, or they may be anywhere in between. If the PRV value (prv_value) is less than 40% (step


53


), then the index value returned (step


58


) is the PRV value divided by four (step


54


). If the PRV value is not less than 40% (step


53


), but is less than 100%, then the index returned (step


58


) is the PRV value divided by ten, plus six. If the PRV value is not less than 100% (step


55


) then the index returned (step


58


) is the maximum value allowed (max_prv_index) in step


57


. In the preferred embodiment, the maximum value allowed is 15, and the PRV value ranges between zero and 100%. Alternatively, other PRV index algorithms are possible.




Methods and systems consistent with this invention may also vary the position of HGBP valve


134


alone or with variable orifice


172


through surge detection without the use of surge boundary curve


204


.

FIGS. 4A-4C

are flow charts of control process


400


, consistent with this invention, for controlling HGBP valve


134


alone or in combination with variable orifice


172


. Microprocessor


150


periodically executes AHGBP control process


400


. For instance, microprocessor


150


may execute control process


400


once per second or once every few minutes.




Before process


400


executes for the first time certain flag variables and timer variables are reset. For instance, flags used during process


400


are SURGE, HGBP_MODE and WOV_HALF_HGBP. These flags are set to FALSE. Timers used during process


400


are FORCE_CLOSE_TIMER, SURGE_TIMEOUT, HGBP_HOLD_PERIOD, and HGBP_CLOSE_TIMER. These timers are set to zero. Then process


400


may start its first execution loop.




If the LCHWT 128S is greater than or equal to a temperature margin, preferably 5° F., and PRV position


158


is greater than 95% (step


5


), then process


400


proceeds to steps


6


and


8


-


13


. The purpose of steps


6


and


8


-


13


is to drive the LCHWT to setpoint because a PRV opening greater than 95%, which corresponds to nearly wide open vanes (WOV), does not provide enough control range to drive the LCHWT to set point adequately. By closing HGBP valve


134


, less gas is bypassed and this produces more capacity to bring the LCHWT back to setpoint. Percentages smaller than 95% could also be used to indicate nearly wide open vanes, such as 90% or 85%.




If HGBP valve


134


is not closed (step


6


), then chiller


100


is still operating in the HGBP region, and a timer FORCE_CLOSE is checked to see if it has expired (step


8


). The FORCE_CLOSED timer measures an amount of time to lapse between incrementally closing HGBP valve


134


. If the timer FORCE_CLOSE_TIMER expired, a flag WOV_HALF_HGBP is checked to see if it is TRUE (step


9


). If WOV_HALF_HGBP is FALSE, HGBP valve


134


is closed to half of its present position (step


10


), the WOV_HALF_HGBP flag is set TRUE (step


12


), and the FORCE_CLOSE_TIMER is set for ten min (step


13


). The WOV_HALF_HGBP flag allows process


400


to close HGBP valve


134


half way the first increment of closure, and all the way for the second increment of closure. If the conditions of step


5


are TRUE, if HGBP valve


134


is not closed (step


6


), if the FORCE_CLOSE_TIMER expired (step


8


), and the WOV_HALF_HGBP flag is TRUE (step


9


), HGBP valve


134


is closed completely (step


11


).




While AHGBP process


400


is executed, a separate surge detection process continuously detects whether surge conditions are present in compressor


110


. The surge detection process may detect whether surge conditions are present at a sufficient rate such that a surge condition does not go undetected. For example, the surge detection process may detect whether surge conditions are present every second or once every few minutes. As stated above, the preferred method of detecting surge conditions is discussed in U.S. Pat. No. 5,764,062. When the surge detection process detects a valid surge, it flags it by setting a flag SURGE to TRUE. Thus, process


400


detects surge when the surge flag is TRUE. Additional steps employed as a result of step


5


being TRUE are (1) checking to see if surge is detected (step


14


), (2) incrementing the number of surges (step


15


), and (3) clearing the flag SURGE flag (step


16


). At this point, process


400


ends and may be restarted. Closing HGBP valve


134


, as a remedy to step


5


being TRUE, may result in excessive surging. Thus, it is important that steps


14


-


16


keep track of the number of surges. The chiller may be shut down if a programmable number of surges occur within a given programmable period of time. Preferably, the chiller shuts down when the number of surges reaches


20


surges in 5 minutes, but other values are possible. When step


5


becomes FALSE, the WOV_HALF_OPEN flag is set to FALSE (step


7


) and process


400


proceeds to the main HGBP control of

FIGS. 4B-4C

.




The interaction of the control features described in

FIGS. 4B-4C

position HGBP valve


134


in an optimum position based on surge detection. If surge is detected (step


17


), process


400


determines whether system


100


is operating in the HGBP region by checking the HGBP_MODE flag, i.e. HGBP valve


134


is not closed (step


19


). If it is not in the HGBP region, HGBP valve


134


is opened partially (step


20


). The value of 50% shown in step


20


is a preferred value for the initial HGBP valve


134


opening. In other embodiments, values may be used other than 50% such as 30% or 40%, for example. Opening HGBP valve


134


results in the control transitioning from the normal region to the HGBP region of operation. Thus, the HGBP_MODE flag is set TRUE to indicate that system


100


is now operating in the HGBP region (step


21


).




Next, a timer HGBP_HOLD_PERIOD is set to a programmable value (step


22


). In the preferred embodiment, HGBP_HOLD_PERIOD may range from 30 to 120 minutes but other ranges are possible (step


22


). This time period is the time in which HGBP valve


134


is held open in this position before it is incrementally closed, assuming no more surges occur in this time period. Another timer SURGE_TIMEOUT is set to a value (step


23


). In the preferred embodiment, SURGE_TIMEOUT is set to five minutes (step


23


). In other embodiments, other values may be used. This interval of time is required to allow system


100


to adjust HGBP valve


134


to opening conditions before permitting further action to be taken in opening HGBP valve


134


due to another surge event.




Methods and systems consistent with this invention incrementally open the hot gas bypass valve further surge conditions continues to exist. If step


19


is TRUE, i.e. system


100


is in the HGBP region, no further action will be taken on the movement of HGBP valve


134


until SURGE_TIMEOUT has expired (step


25


). Either way, steps


24


and


34


count the surge and clear the flag SURGE in preparation for the next possible surge. If SURGE_TIMEOUT has expired (step


25


), system


100


checks if the present position of HGBP valve


134


is greater than or equal to a value, for example 50% (step


26


). In other embodiments, values other than 50% may be used. If step


26


is TRUE, HGBP valve


134


is opened another 10% if its present position is not greater than 90%, otherwise it is opened to 100% (step


28


). Timer SURGE_TIMEOUT is reset to two minutes (step


29


), i.e. additional surges during this timer interval do not cause additional HGBP valve


134


movement.




If HGBP valve


134


is not open greater than or equal to 50% (step


26


), process


400


determines if it is open less than a value, for example 35% (step


27


). Again, values other than 35% are possible. If it is not, SURGE_TIMEOUT is reset for two minutes (step


31


), otherwise SURGE_TIMEOUT is reset to 3.5 minutes (step


33


). Other timer values are possible. Either way, HGBP valve


134


is opened to its 50% opening point (step


32


) and timer HGBP_HOLD_PERIOD is reset to a programmable value (step


30


), which may range from 30 to 120 minutes. In other embodiments, values other than this range are possible. Because the execution of steps


26


through


33


are in response to a detected surge event, the surge count is incremented (step


24


) and flag SURGE is cleared (step


34


).




Methods and systems consistent with this invention incrementally close the hot gas bypass valve if surge conditions no longer exists. For example, after the conditions stabilize and surge stops, step


17


is FALSE and process


400


checks if the timer HGBP_HOLD_PERIOD has expired (step


18


). If it has expired (step


18


), process


400


ends and may be restarted. If it has not expired (step


18


), HGBP valve


134


is held in its present position until it expires or surge occurs. As described above, HGBP_HOLD _PERIOD is the time in which HGBP valve


134


is held open before it is incrementally closed, assuming no more surges occur in this time period. If surge occurs (step


17


), then HGBP valve


134


position is increased in accordance with steps


26


through


33


.




When the timer HGBP_HOLD_PERIOD expires (step


18


), timer HGBP_CLOSE_TIMER is checked (step


35


) and if it is not expired, process


400


ends and is restarted, thus holding HGBP valve


134


in its present position until timer HGBP CLOSE_TIMER does expire. The HGBP_CLOSE_TIMER provides the delay required to slowly move HGBP valve


134


back to its closed position. As discussed above, when system


100


is powered-up, all timers are initialized to zero. The timer HGBP_CLOSE_TIMER is expired either (1) when first checked or (2) when enough time has elapsed to cause it to expire. After timer HGBP_CLOSE_TIMER is expired (step


35


), process


400


checks to see if HGBP valve


134


is closed (step


36


). If it is closed, conditions have changed to the point where the non-HGBP region of operation has been re-entered. Thus, the HGBP_MODE flag is set to FALSE (step


37


), and process


400


ends and may be restarted. Otherwise, if HGBP valve


134


is not closed (step


36


), process


400


checks to see if HGBP valve


134


is less than a programmable value Y (step


38


). Programmable value Y may range from 5 to 15%, but other values are possible. If it is, HGBP valve


134


is closed all the way (step


39


) and timer HGBP_CLOSE_TIMER is set for two minutes (step


41


). Otherwise, if step


38


is FALSE, HGBP valve


134


is closed an additional amount, and the timer HGBP_CLOSE_TIMER is set for ten minutes (step


42


).




Additionally, variable orifice


172


may be controlled in conjunction with logic statements to the control HGBP valve


134


. For instance, if surge is detected (step


17


) then the variable orifice


172


and HGBP valve


134


may be opened in combination until surge stops. Timers mentioned in

FIGS. 4C-4D

may time for both variable orifice


172


and HGBP valve


134


. Therefore, because variable orifice


172


may function similar to an additional HGBP valve, not only may surge be prevented earlier, but non-surge operation can be re-established sooner. Additionally, variable orifice


172


may be controlled with fuzzy logic as disclosed in U.S. Pat. No. 5,809,795, hereby incorporate by reference, to maintain the condenser liquid refrigerant level at a value that minimizes or prevents gas bypass to the evaporator.




As mentioned above, it is possible to combine the surge boundary curve


204


with the operation of process


400


shown in

FIGS. 4A-4C

. For instance, in order to avoid the initial surge occurrence when operating conditions approach surge boundary curve


204


from non-surge region B of operation, additional logic statements could be included in conditional step


17


. If the actual pressure ratio is within the stored control average pressure ratio minus the programmable surge margin, i.e., that the surge region A is being approached, then steps


20


through


23


of

FIG. 4B

may then be executed and the control may operate as described above.




Also, because surge boundary curve


204


may be derived or updated when surge is detected while system


100


operates in non-surge region B, an additional step may be inserted between steps


19


and


20


of

FIG. 4B

to record the surge point.




In an alternative embodiment, the system parameters that may define the surge boundary curve are the compressor head and the suction volumetric flow rate for various speeds of the compressor. This surge boundary curve may be compared with the values of the compressor head and suction volumetric flow during the operation of the chiller to determine when to open HGBP valve


134


to prevent entering the surge region.




Those skilled in the art recognize that various modifications and variations can be made in the preceeding examples without departing from the scope or spirit of the invention. For instance, surge curve


204


is determined during a calibration process.




The description of the invention does not limit the invention. Instead, it provides examples and explanations to allow persons of ordinary skill to appreciate different ways to practice the invention. The following claims define the true scope and spirit of the invention.



Claims
  • 1. A method for automatically calibrating a surge control of a refrigeration system including a centrifugal compressor having pre-rotational vanes, a condenser, an evaporator, and a hot gas bypass line between the compressor and the evaporator, said method comprising the steps of:continuously sensing for a surge condition during operation of the refrigeration system; and sensing a head parameter representative of the head of the compressor; sensing a load parameter representative of a load; and storing the head parameter and the load parameter when the surge condition is sensed as control data to be used by the control of the refrigeration system.
  • 2. The method of claim 1, wherein sensing the head parameter includessensing a pressure representative of the pressure of the liquid refrigerant in the condenser; sensing a pressure representative of the pressure of the liquid refrigerant in the evaporator; calculating a differential pressure equal to the difference between the condenser pressure and the evaporator pressure; and calculating a pressure ratio equal to the ratio of the calculated differential pressure and the evaporator pressure.
  • 3. The method of claim 2, wherein sensing the load parameter includessensing a position representative of the position of the pre-rotational vanes.
  • 4. The method of claim 1, further comprising:sensing a present head parameter representative of the present head of the compressor; sensing a present load parameter representative of the load; and controlling the hot gas bypass valve so as to avoid surging in the compressor in response to the present head parameter, the present load parameter, and the stored head and load parameters.
  • 5. The method of claim 4, wherein sensing the present head parameter includessensing a present pressure representative of the present pressure of the liquid refrigerant in the condenser; sensing a present pressure representative of the present pressure of the liquid refrigerant in the evaporator; calculating a present differential pressure equal to the difference between the present condenser pressure and the present evaporator pressure; calculating a present pressure ratio equal to the ratio between the present calculated differential pressure and the present evaporator pressure; and wherein sensing the present load parameter includes sensing a present position representative of the present position of the pre-rotational vanes.
  • 6. The method of claim 5, further including the step ofopening the hot gas bypass valve, if the present pressure ratio is within a margin of the stored control pressure ratio corresponding to the stored control vane position equal to the present vane position.
  • 7. The method of claim 6, wherein the margin is 0.1.
Parent Case Info

This is a division of application Ser. No. 09/559,726, filed Apr. 28, 2000, U.S. Pat. No. 6,427,464 which is a Continuation in Part of application Ser. No. 09/232,558 filed on Jan. 15, 1999, U.S. Pat. No. 6,202,431, both of which are incorporated herein by reference.

US Referenced Citations (42)
Number Name Date Kind
2739451 Breck Mar 1956 A
2888809 Rachfal Jun 1959 A
3174298 Kleiss Mar 1965 A
3250084 Anderson May 1966 A
3355906 Newton Dec 1967 A
3522711 Shaughnessy Aug 1970 A
3555844 Fleckenstein et al. Jan 1971 A
3780532 Norbeck et al. Dec 1973 A
4151725 Kountz et al. May 1979 A
4156578 Agar et al. May 1979 A
4164034 Glennon et al. Aug 1979 A
4177649 Venema Dec 1979 A
4183225 Politte et al. Jan 1980 A
4248055 Day, III et al. Feb 1981 A
4259845 Norbeck Apr 1981 A
4275987 Kountz et al. Jun 1981 A
4282718 Kountz et al. Aug 1981 A
4282719 Kountz et al. Aug 1981 A
4355948 Kountz et al. Oct 1982 A
4522037 Ares et al. Jun 1985 A
4546618 Kountz et al. Oct 1985 A
4581900 Lowe et al. Apr 1986 A
4608833 Kountz Sep 1986 A
4686834 Haley et al. Aug 1987 A
4726738 Nakamura et al. Feb 1988 A
4947653 Day et al. Aug 1990 A
RE33620 Persem Jun 1991 E
5065590 Powell et al. Nov 1991 A
5158024 Tanaka et al. Oct 1992 A
5259210 Ohya et al. Nov 1993 A
5272428 Spiegel et al. Dec 1993 A
5284026 Powell Feb 1994 A
5355691 Sullivan et al. Oct 1994 A
5537830 Goshaw et al. Jul 1996 A
5553997 Goshaw et al. Sep 1996 A
5669225 Beaverson et al. Sep 1997 A
5746062 Beaverson et al. May 1998 A
5794736 Millard Aug 1998 A
5873257 Peterson Feb 1999 A
5894736 Beaverson et al. Apr 1999 A
5947680 Harada et al. Sep 1999 A
6202431 Beaverson et al. Mar 2001 B1
Foreign Referenced Citations (5)
Number Date Country
1281353 Nov 1989 JP
4260755 Sep 1992 JP
4297761 Oct 1992 JP
05052433 Mar 1993 JP
6185786 Jul 1994 JP
Continuation in Parts (1)
Number Date Country
Parent 09/232558 Jan 1999 US
Child 09/559726 US