US3441200A - Gas compression system having inlet gas control - Google Patents

Gas compression system having inlet gas control Download PDF

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US3441200A
US3441200A US622513A US3441200DA US3441200A US 3441200 A US3441200 A US 3441200A US 622513 A US622513 A US 622513A US 3441200D A US3441200D A US 3441200DA US 3441200 A US3441200 A US 3441200A
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gas
compressor
inlet
pressure
temperature
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Eugene L Huesgen
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Carrier Corp
Elliott Turbomachinery Co Inc
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Carrier Corp
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0284—Conjoint control of two or more different functions

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  • This invention relates to gas compression systems and more particularly to gas compression systems of the type employing a multistage axial or centrifugal compressor driven by a prime mover.
  • a main control system may be provided which senses the discharge gas pressure and controls various system functions such as a discharge valve so as to maintain the discharge pressure of the system constant.
  • a gas compression system which employs a multistage air compressor having a suitable main control system to maintain a uniform discharge pressure.
  • An inlet air throttling valve controls the pressure of air admitted to the first stage of the compressor.
  • the temperature and pressure of inlet air as well as the interstage air temperature are sensed and compared against a reference signal to provide a control signal for varying the inlet air pressure by modulating the inlet throttling valve.
  • a control system in accordance with this invention provides improved operating efficiency and capacity, while at the same time it reduces the occurrences of overloads on the prime mover and surging of the compressor by taking into account the interstage gas temperature in controlling the operation of the system. Consequently, by employing the type of control system described herein, a gas compression system can be operated at more nearly optimum conditions over a wide range of ambient inlet air and interstage cooling conditions than previous systerns.
  • FIG. 1 The figure schematically illustrates a gas compression system having a control system in accordance with this invention.
  • FIGURE 1 there is shown a gas compression system embodying a multisage centrifugal or axial compressor 10 having a first stage 11 in series with a second stage 12 and a third stage 13.
  • Inlet gas line 15 is provided to admit ambient inlet air through a throttling valve 16 to first stage 11 of compressor 10.
  • Interstage gas coolers 22 and 23 having suitable cooling medium heat exchange passages 29, 30 therein are provided to cool gas passing between the stages of compressor 10.
  • Compressed air is discharged from compressor 10 through a check valve 17 in gas discharge gas line 18 into receiver 19.
  • a suitable compressed gas discharge line 20 distributes air from receiver '19 to the desired locations at which it is employed.
  • a dump valve 21 is employed to discharge compressed air from compressor when the pressure demands of receiver 19 are satisfied.
  • Dump valve 21 may be operated either as a fully opened or fully closed valve or it may be modulated according to the desired characteristics of the gas compression system.
  • a main control system is provided to control the operation of dump valve 21.
  • the main control system employs a discharge pressure sensor 25 at a suitable location 26 in line 18 or receiver 19.
  • a main control system 27 is actuated in response to a pressure signal generated by discharge pressure sensor 25 and sense a valve opening or closing signal to valve actuator 28. Control system 27 maintains the discharge pressure at substantially predetermined value irrespective of the load imposed on the. gas compression system.
  • an additional control system is provided for controlling the inlet air pressure to first stage 11 of compressor 10 by modulating inlet gas valve 16 in accordance with the condition of operation of the system.
  • an inlet air temperature sensor 34 is provided at a suitable location 35 between inlet valve 16 and first stage 11 for sensing the temperature of air admitted to the first stage of the compressor.
  • An interstage temperature sensor 36 is also provided at a suitable location 37 between first stage 11 and second stage 12.
  • Interstage temperature sensor 36 is located to sense interstage gas temperature between the inlet of scond stage 12 and the outlet of interstage gas cooler 22. Consequently, interstage temperature sensor 36 is able to compensate for variations in the flow rate and temperature of the cooling medium in the interstage cooler, as well as for unknown factors like scaling of the heat exchanger which may eifect the actual interstage gas temperature.
  • An inlet air pressure sensor 38 is provided at a suitable location 39 between inlet gas valve. 16 and first stage 11 for sensing the pressure of the air admitted to compressor 10.
  • Inlet air temperature sensor 34 generates an inlet air temperature signal which is a known function of the inlet air temperature.
  • sensor 34 may comprise a temperature responsive resistance element such as a thermistor. Because the actual characteristic of the desired inlet air temperature functions may not be linear or because the sensor may be nonlinear over the desired range of operating temperatures, a preferred embodiment of this invention employs a pair of thermistors in a suitable resistance network to provide a desired continuous, nonlinear temperature function signal.
  • interstage temperature sensor 36 may also comprise a thermistor in a resistance network which generates the desired interstage temperature function signal.
  • Inlet pressure sensor 38 may comprise a pressure transducer in the form of a potentiometer having a wiping element movable in response to pressure variations and having the desired resistance characteristic to generate the required pressure function signal by dividing current flow in a differential amplifier.
  • a reference signal generator 40 which may also comprise a potentiometer for dividing current flow in a differential amplifier, is employed to generate a reference signal corresponding to a predetermined desired condition of operation of the gas compression system, whereby the load on the compressor prime mover will not be excessive and the compressor will not be subject to surge.
  • the inlet temperature function signal, the interstage temperature function signal, the inlet pressure function signal and the reference signal are all summed in a summing circuit 45 to provide a control signal.
  • the summing circuit serves to compare the sensed function signals with the reference signal to provide a difference or error control signal which indicates the need for adjustment of the inlet air pressure condition to maintain the desired condition of operation determined by the reference signal.
  • the control signal is passed to amplifier 46 which provides either an inlet valve opening signal or an inlet valve closing signal depending on the direction of error indicated by the control signal.
  • the valve opening signal is passed, when present, to a valve opening circuit 47, which in turn causes valve actuator 49 to open inlet gas valve 16, thereby increasing the absolute pressure of air admitted to first stage 11 of compressor 10.
  • the valve closing signal when present, is passed to valve closing circuit 48 which in turn causes valve actuator 49 to close inlet gas valve 16 thereby reducing the absolute pressure of air supplied to first stage 11 of compressor 10.
  • amplifier 46 may comprise a differential amplifier and summing circuit 45 may comprise a terminal or other network arrangement for summing current signals generated by sensors 34, 36 and 38 and reference signal generator 40.
  • summing circuit 45 may comprise a terminal or other network arrangement for summing current signals generated by sensors 34, 36 and 38 and reference signal generator 40.
  • the output from differential amplifier 46 is a voltage signal from one or the other of a pair of transistors depending on the direction of the unbalance indicated by the control signal.
  • the voltage output fro-m one of the transistors is employed to switch a Triac or other switching device to its conducting state in the valve opening circuit and the voltage output from the other transistor is employed to switch a Triac to its conducting state in the valve closing state.
  • the Triacs in turn control the passage of current through the windings of a motor which rotates to open or close the inlet gas valve in a direction to reduce the unbalance in the differential amplifier by changing the sensed inlet air pressure.
  • compressor 10 is driven by a suitable prime mover (not shown) such as an electric motor.
  • a suitable prime mover such as an electric motor.
  • Compressed air is discharged from the compressor into receiver 19 until discharge pressure sensor 25 indicates that the set point pressure has been reached.
  • control 27 causes dump valve actuator 28 to move toward an open position thereby preventing passage of excess air into receiver 19 until the pressure in the receiver is reduced below the set point pressure of the main control.
  • Inlet gas temperature sensor 34 and interstage gas temperature sensor 35 sense the temperature of the gas admitted to the first and second stages respectively of compressor 10 and provide suitable temperature function current signals to summing circuit 45. Likewise, inlet pressure sensor 35 provides a pressure function current signal to summing circuit 45 as does reference signal generator 40. If the sum of the currents generated by the sensors is substantially equal to that generated by reference signal generator 40, no control signal will be supplied to amplifier 46. Preferably, a dead band is provided which will span a sufficient range of control signal magnitude to prevent hunting in the control characteristic.
  • a control signal will be passed to amplifier 46 having a direction and magnitude corresponding to the necessary change in inlet pressure that is required to again balance the operation of the system.
  • the valve opening or closing signal required for rebalancing the system will be passed to the appropriate valve opening or closing circuit to move the inlet valve actuator 49 in the proper direction to reduce the deviation from the desired operating condition.
  • the interstage temperature should suddenly rise as might happen if the interstage cooling water temperature rose or its flow rate decreased, an unbalance between the reference signal and the sensed function signals would be reflected in a control signal from summing circuit 45 causing a valve opening signal to be passed to valve actuator 49 thereby preventing the compressor from surging by increasing the inlet pressure to first stage 11 and thus decrease the overall compressor pressure ratio.
  • the summing circuit will provide a control signal to amplifier 46 to unbalance it in a direction to open inlet gas valve 16 thereby reducing the pressure lift across compressor and preventing a surge condition from occurring.
  • differential amplifier 46 will provide a valve closing signal to actuator 49 to prevent overloading of the prime mover by reducing the mass flow through the compressor.
  • a gas compression sytem having a control over inlet air admitted to the compressor which serves to compensate for both variations in inlet air temperature and pressure and also for variations in interstage conditions.
  • the point of maximum prime mover load can be closely approached without damage of an accidental overload due to changing gas conditions at any point in the system.
  • the so-called surge line of the gas compression system may be closely approached without causing the compressor to go into a surge condition due to unexpected changes in ambient or interstage gas conditions. Therefore, the gas compression system of this invention can be operated at optimum conditions over a wider range of gas conditions than could be tolerated by prior systems. Consequently, a gas compression system embodying this invention can be operated at high capacity and with great operating efficiency.
  • a gas compression system including a multistage gas compressor having a first gas compression stage and at least one following gas compression stage connected in series relation with said first stage, a prime mover connected to drive said compressor, an inlet passage for admitting inlet gas to the first stage of said gas compressor, a throttling valve for controlling flow of inlet gas to said first stage of said compressor, an outlet passage for discharging compressed discharge gas from said system, and a main control system for sensing discharge gas pressure and adjusting the conditions of operation of said system in accordance with the sensed discharge gas pressure to maintain a substantially predetermined discharge gas pressure, wherein the improvement comprises the combination of:
  • inlet gas temperature sensing means disposed for sensing the temperature of inlet gas admitted to the first stage of said compressor, and for providing an inlet gas temperature signal functionally related thereto;
  • interstage gas temperature sensing means for sensing the temperature of gas admitted to a following stage of said compressor, and for providing an interstage gas temperature signal functionally related thereto;
  • inlet gas pressure sensing means disposed for sensing the pressure of inlet gas admitted to the first stage of said compressor, and for providing an inlet gas pressure signal functionally related thereto;
  • reference signal means for providing a reference signal functionally related to a predetermined combination of each of said sensed conditions which results in a desired condition of operation of said gas compressor;
  • (g) means for adjusting said throttling valve in response to said control signal to reduce said deviation by varying the inlet gas pressure in a manner so as to shift the condition of operation of said gas compressor toward said desired condition, thereby tending to prevent overloading of said prime mover and surging of said compressor.
  • a method of operating a gas compression system having a multiple stage gas compressor driven by a prime mover to reduce overloading of said prime mover and surging of said compressor which includes the steps of sensing the discharge gas pressure of said system and adjusting the condition of operation of said system in response to sensed discharge gas pressure to maintain a substantially constant predetermined discharge pressure, wherein the improvement comprises:
  • a method of operating a gas compression system as defined in claim 4 including the step of cooling the compressed gas discharged from said first stage of said compressor prior to entry thereof into said following stage of said compressor, and sensing the temperature of the gas 7 8 admitted to said following stage subsequent to cooling 2,929,547 3/1960 Koffel 230-115 thereof so that the efiect of cooling of said gas is sensed 2,938,536 1960 Ehrenberg 10311 X and compensated for in controlling the rate of flow of gas 2,955,745 10/1960 Hunter 2301 to the inlet of said first stage. 3,007,414 11/1961 Long et a1.

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  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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Description

A ril 29, 1969 E. HUESGIIEN Filed March 13, 1967 Q 2 8 g a Q m. g 2 T i E E 1 E 5 mm 3 fifix ||lI| ll Pfizn E25 225 $232 n 2.85 25% ma 82 h =23 n u n 9. V on u mm W 3 5:25 z 5P 55 2E A $525 A 52 52 g v 525 V s\ $523 22% 85%? INVENTOR. EUGENE L. HUESGEN.
ATTORNEY.
United States Patent U.S. Cl. 230-5 5 Claims ABSTRACT OF THE DISCLOSURE A gas compression system for supplying compressed air at a uniform pressure which employs a multistage compressor. A main control is provided to maintain the discharge pressure constant. The temperature and ressure of gas admitted to the first stage of the compressor and the temperature of gas admitted to the second stage of the compressor are sensed and functions thereof are summed to provide a control signal. An inlet gas throttling valve is modulated in response to the control signal to reduce overloading of the compressor and/or to keep the compressor from surging by varying the inlet a1r pressure.
BACKGROUND OF THE INVENTION This invention relates to gas compression systems and more particularly to gas compression systems of the type employing a multistage axial or centrifugal compressor driven by a prime mover. A main control system may be provided which senses the discharge gas pressure and controls various system functions such as a discharge valve so as to maintain the discharge pressure of the system constant.
Two .problems, however, are often experienced in attempting to maintain high operating efficiency with such systems, due to changing air temperatures and pressures. First, decreases in ambient air temperature or increases in ambient air pressure may increase the flow of air through the compressor, which tends to overload the prime mover employed to drive the gas compressor. The overloading of the prime mover may result in injury or destruction of it, and attempting to avoid an overload at all conditions at which may be encountered tends to establish an artificial limit on the range of conditions of operation of the gas compression system which results in reduced efficiency. Second, reductions in density of the ambient air admitted to the compressor, such as may occur with increasing ambient air temperature, may result in a reduction in mass flow through the compressor to the point that surge is encountered. Surge is a highly undesirable, unstable condition of the compressor which results in a loss of capacity and may cause serious damage to the compressor.
It has been proposed to employ a throttling valve in the line supplying inlet air to the compressor and to modulate the throttling valve in accordance with the density of the inlet air. This type of control provides greatly improved operation of the gas compression system over a range of inlet air conditions. However, such a control still does not provide optimum efliciency of operation because the operating characteristics of the system must be a compromise which is selected so that neither surge nor prime mover overload occurs at any anticipated condition. Furthermore, where an interstage gas cooler is employed in the operation of the system, this type of control must normally operate sufficiently away from the overload and surge regions so that changes in cooling fluid flow rate or temperature as well as variations in latent heat of the gas do not result in overloads or surging. Consequently, the optimum compressor operating efficiency and pressure lift cannot always be safely achieved due to the required compromise in operating characteristics.
SUMMARY OF THE INVENTION In accordance with a preferred embodiment of this invention, a gas compression system is provided which employs a multistage air compressor having a suitable main control system to maintain a uniform discharge pressure. An inlet air throttling valve controls the pressure of air admitted to the first stage of the compressor. The temperature and pressure of inlet air as well as the interstage air temperature are sensed and compared against a reference signal to provide a control signal for varying the inlet air pressure by modulating the inlet throttling valve.
A control system in accordance with this invention provides improved operating efficiency and capacity, while at the same time it reduces the occurrences of overloads on the prime mover and surging of the compressor by taking into account the interstage gas temperature in controlling the operation of the system. Consequently, by employing the type of control system described herein, a gas compression system can be operated at more nearly optimum conditions over a wide range of ambient inlet air and interstage cooling conditions than previous systerns.
BRIEF DESCRIPTION OF THE DRAWING The figure schematically illustrates a gas compression system having a control system in accordance with this invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT This invention will be described with respect to a preferred embodiment thereof wherein the gas compression system is employed to supply compressed air to desired locations for operations of pneumatic equipment.
Referring particularly to FIGURE 1 there is shown a gas compression system embodying a multisage centrifugal or axial compressor 10 having a first stage 11 in series with a second stage 12 and a third stage 13. Inlet gas line 15 is provided to admit ambient inlet air through a throttling valve 16 to first stage 11 of compressor 10. Interstage gas coolers 22 and 23 having suitable cooling medium heat exchange passages 29, 30 therein are provided to cool gas passing between the stages of compressor 10.
Compressed air is discharged from compressor 10 through a check valve 17 in gas discharge gas line 18 into receiver 19. A suitable compressed gas discharge line 20 distributes air from receiver '19 to the desired locations at which it is employed.
In order to maintain the pressure of discharge air in receiver 19 in line 20 relatively constant at a predetermined pressure, a dump valve 21 is employed to discharge compressed air from compressor when the pressure demands of receiver 19 are satisfied. Dump valve 21 may be operated either as a fully opened or fully closed valve or it may be modulated according to the desired characteristics of the gas compression system.
A main control system is provided to control the operation of dump valve 21. The main control system employs a discharge pressure sensor 25 at a suitable location 26 in line 18 or receiver 19. A main control system 27 is actuated in response to a pressure signal generated by discharge pressure sensor 25 and sense a valve opening or closing signal to valve actuator 28. Control system 27 maintains the discharge pressure at substantially predetermined value irrespective of the load imposed on the. gas compression system.
In accordance with this invention, an additional control system is provided for controlling the inlet air pressure to first stage 11 of compressor 10 by modulating inlet gas valve 16 in accordance with the condition of operation of the system.
For this purpose, an inlet air temperature sensor 34 is provided at a suitable location 35 between inlet valve 16 and first stage 11 for sensing the temperature of air admitted to the first stage of the compressor.
An interstage temperature sensor 36 is also provided at a suitable location 37 between first stage 11 and second stage 12. Interstage temperature sensor 36 is located to sense interstage gas temperature between the inlet of scond stage 12 and the outlet of interstage gas cooler 22. Consequently, interstage temperature sensor 36 is able to compensate for variations in the flow rate and temperature of the cooling medium in the interstage cooler, as well as for unknown factors like scaling of the heat exchanger which may eifect the actual interstage gas temperature.
An inlet air pressure sensor 38 is provided at a suitable location 39 between inlet gas valve. 16 and first stage 11 for sensing the pressure of the air admitted to compressor 10.
Inlet air temperature sensor 34 generates an inlet air temperature signal which is a known function of the inlet air temperature. For this purpose, sensor 34 may comprise a temperature responsive resistance element such as a thermistor. Because the actual characteristic of the desired inlet air temperature functions may not be linear or because the sensor may be nonlinear over the desired range of operating temperatures, a preferred embodiment of this invention employs a pair of thermistors in a suitable resistance network to provide a desired continuous, nonlinear temperature function signal. interstage temperature sensor 36 may also comprise a thermistor in a resistance network which generates the desired interstage temperature function signal. Inlet pressure sensor 38 may comprise a pressure transducer in the form of a potentiometer having a wiping element movable in response to pressure variations and having the desired resistance characteristic to generate the required pressure function signal by dividing current flow in a differential amplifier.
A reference signal generator 40, which may also comprise a potentiometer for dividing current flow in a differential amplifier, is employed to generate a reference signal corresponding to a predetermined desired condition of operation of the gas compression system, whereby the load on the compressor prime mover will not be excessive and the compressor will not be subject to surge.
The inlet temperature function signal, the interstage temperature function signal, the inlet pressure function signal and the reference signal are all summed in a summing circuit 45 to provide a control signal. The summing circuit serves to compare the sensed function signals with the reference signal to provide a difference or error control signal which indicates the need for adjustment of the inlet air pressure condition to maintain the desired condition of operation determined by the reference signal.
The control signal is passed to amplifier 46 which provides either an inlet valve opening signal or an inlet valve closing signal depending on the direction of error indicated by the control signal. The valve opening signal is passed, when present, to a valve opening circuit 47, which in turn causes valve actuator 49 to open inlet gas valve 16, thereby increasing the absolute pressure of air admitted to first stage 11 of compressor 10. The valve closing signal, when present, is passed to valve closing circuit 48 which in turn causes valve actuator 49 to close inlet gas valve 16 thereby reducing the absolute pressure of air supplied to first stage 11 of compressor 10.
In the preferred embodiment of the invention, amplifier 46 may comprise a differential amplifier and summing circuit 45 may comprise a terminal or other network arrangement for summing current signals generated by sensors 34, 36 and 38 and reference signal generator 40. Thus, the summation of the net current injected into the differential amplifier circuit from the current reference and the sensors has a magnitude and a direction which unbalances the differential amplifier in a direction to provide a suitable inlet valve opening signal or closing signal, depending on the direction of the unbalance.
vIn the preferred embodiment of this invention, the output from differential amplifier 46 is a voltage signal from one or the other of a pair of transistors depending on the direction of the unbalance indicated by the control signal. The voltage output fro-m one of the transistors is employed to switch a Triac or other switching device to its conducting state in the valve opening circuit and the voltage output from the other transistor is employed to switch a Triac to its conducting state in the valve closing state. The Triacs in turn control the passage of current through the windings of a motor which rotates to open or close the inlet gas valve in a direction to reduce the unbalance in the differential amplifier by changing the sensed inlet air pressure.
In operation, compressor 10 is driven by a suitable prime mover (not shown) such as an electric motor. Compressed air is discharged from the compressor into receiver 19 until discharge pressure sensor 25 indicates that the set point pressure has been reached. When the set point pressure is reached, control 27 causes dump valve actuator 28 to move toward an open position thereby preventing passage of excess air into receiver 19 until the pressure in the receiver is reduced below the set point pressure of the main control.
Inlet gas temperature sensor 34 and interstage gas temperature sensor 35 sense the temperature of the gas admitted to the first and second stages respectively of compressor 10 and provide suitable temperature function current signals to summing circuit 45. Likewise, inlet pressure sensor 35 provides a pressure function current signal to summing circuit 45 as does reference signal generator 40. If the sum of the currents generated by the sensors is substantially equal to that generated by reference signal generator 40, no control signal will be supplied to amplifier 46. Preferably, a dead band is provided which will span a sufficient range of control signal magnitude to prevent hunting in the control characteristic. If, however, the deviation of the summed sensed function signals from the reference signal is greater than the predetermined dead band, a control signal will be passed to amplifier 46 having a direction and magnitude corresponding to the necessary change in inlet pressure that is required to again balance the operation of the system. From amplifier 46, the valve opening or closing signal required for rebalancing the system will be passed to the appropriate valve opening or closing circuit to move the inlet valve actuator 49 in the proper direction to reduce the deviation from the desired operating condition.
For example, if for some reason, the interstage temperature should suddenly rise as might happen if the interstage cooling water temperature rose or its flow rate decreased, an unbalance between the reference signal and the sensed function signals would be reflected in a control signal from summing circuit 45 causing a valve opening signal to be passed to valve actuator 49 thereby preventing the compressor from surging by increasing the inlet pressure to first stage 11 and thus decrease the overall compressor pressure ratio. If the temperature of the inlet air to first stage 11 rises, as for example due to increase in ambient temperature, or if the inlet pressure should drop, the summing circuit will provide a control signal to amplifier 46 to unbalance it in a direction to open inlet gas valve 16 thereby reducing the pressure lift across compressor and preventing a surge condition from occurring. Similarly, if the interstage temperature or inlet temperature drop, or the inlet pressure rises, differential amplifier 46 will provide a valve closing signal to actuator 49 to prevent overloading of the prime mover by reducing the mass flow through the compressor.
In accordance with this invention, there is provided a gas compression sytem having a control over inlet air admitted to the compressor which serves to compensate for both variations in inlet air temperature and pressure and also for variations in interstage conditions. The point of maximum prime mover load can be closely approached without damage of an accidental overload due to changing gas conditions at any point in the system. Likewise, the so-called surge line of the gas compression system may be closely approached without causing the compressor to go into a surge condition due to unexpected changes in ambient or interstage gas conditions. Therefore, the gas compression system of this invention can be operated at optimum conditions over a wider range of gas conditions than could be tolerated by prior systems. Consequently, a gas compression system embodying this invention can be operated at high capacity and with great operating efficiency.
While the invention has been described with reference to a preferred embodiment thereof wherein the gas compression system supplies compressed air, it will be understood that the principles of this invention are applicable to other systems embodying other gases and for other purposes, if desired.
I claim:
1. A gas compression system including a multistage gas compressor having a first gas compression stage and at least one following gas compression stage connected in series relation with said first stage, a prime mover connected to drive said compressor, an inlet passage for admitting inlet gas to the first stage of said gas compressor, a throttling valve for controlling flow of inlet gas to said first stage of said compressor, an outlet passage for discharging compressed discharge gas from said system, and a main control system for sensing discharge gas pressure and adjusting the conditions of operation of said system in accordance with the sensed discharge gas pressure to maintain a substantially predetermined discharge gas pressure, wherein the improvement comprises the combination of:
(a) inlet gas temperature sensing means disposed for sensing the temperature of inlet gas admitted to the first stage of said compressor, and for providing an inlet gas temperature signal functionally related thereto;
(b) interstage gas temperature sensing means for sensing the temperature of gas admitted to a following stage of said compressor, and for providing an interstage gas temperature signal functionally related thereto;
(c) inlet gas pressure sensing means disposed for sensing the pressure of inlet gas admitted to the first stage of said compressor, and for providing an inlet gas pressure signal functionally related thereto;
(d) means for summing said inlet and interstage temperature signals and said pressure signal to provide a summed function signal which is functionally related to each of the combined sensed conditions of operation of said gas compressor;
(e) reference signal means for providing a reference signal functionally related to a predetermined combination of each of said sensed conditions which results in a desired condition of operation of said gas compressor;
(f) means for detecting deviation of said summed function signal from said reference signal and for providing a control signal which is a function of said deviation; and
(g) means for adjusting said throttling valve in response to said control signal to reduce said deviation by varying the inlet gas pressure in a manner so as to shift the condition of operation of said gas compressor toward said desired condition, thereby tending to prevent overloading of said prime mover and surging of said compressor.
2. A gas compression system as defined in claim 1 wherein said compressor includes an interstage cooler between the first stage thereof and said following stage thereof; means to pass a cooling medium in through said interstage cooler in heat exchange relation with gas compressed from the first stage of said compressor to cool said compressed gas prior to entry into said following stage; and said interstage temperature sensor being located to sense the tempertaure of gas admitted to said following stage of said compressor after being cooled in said interstage cooler.
3. A gas compression system as defined in claim 1 wherein said inlet gas temperature signal generated by said inlet gas temperature sensing means is a nonlinear function corresponding to a predetermined nonlinear condition of operation of said gas compression system.
4. A method of operating a gas compression system having a multiple stage gas compressor driven by a prime mover to reduce overloading of said prime mover and surging of said compressor, which includes the steps of sensing the discharge gas pressure of said system and adjusting the condition of operation of said system in response to sensed discharge gas pressure to maintain a substantially constant predetermined discharge pressure, wherein the improvement comprises:
(a) sensing the temperature of gas admitted to a first stage of said compressor and generating an inlet gas temperature signal functionally related thereto;
(b) sensing the temperature of gas admitted to a stage of said compressor following said first stage thereof, and generating an interstage temperature signal functionally related thereto;
(c) sensing the pressure of gas admitted to the first stage of said compressor and generating a pressure signal functionally related thereto;
(d) generating a reference signal having a magnitude related to a desired condition of operation of said gas compression system;
(e) summing said inlet tempertaure signal, said interstage temperature signal, said inlet pressure signal and said reference signal to provide a control signal which is functionally related to the difference between the condition of operation of said gas compression system and the desired condition of operation thereof; and
(f) controlling the rate of fiow of gas to the inlet of said first stage of said compressor in response to said control signal to change inlet gas pressure to said compressor in a manner to approach the desired condition of operation of said system, thereby reducing overloading of said prime mover and surging of said compressor.
5. A method of operating a gas compression system as defined in claim 4 including the step of cooling the compressed gas discharged from said first stage of said compressor prior to entry thereof into said following stage of said compressor, and sensing the temperature of the gas 7 8 admitted to said following stage subsequent to cooling 2,929,547 3/1960 Koffel 230-115 thereof so that the efiect of cooling of said gas is sensed 2,938,536 1960 Ehrenberg 10311 X and compensated for in controlling the rate of flow of gas 2,955,745 10/1960 Hunter 2301 to the inlet of said first stage. 3,007,414 11/1961 Long et a1. 230-415 X 5 3,027,904 4/1962 Silver 230115 X References Cited 3,232,519 2/ 1966 Long 230 114 X UNITED STATIES PATENTS WILLIAM L. FREEH, Primary Examiner. 1,977,559 10/1934 Lewis et a1 266- 2,632,307 3/1953 Massey et a1 230-114 X U S C1, X R
2,696,345 12/1954 Hopper 230-115 10 230 23 PC4050 UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3, 1,2OO Dated April 29. 1969 Inventofls) Eugene Huesgen It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column 2, line #6 for "operations" read o t line +8, for "multisage" read multistage pera lon Column 3, line 28, for "soond" read second Column 6, line 33, after "predetermined" insert desired SIGNED AND SEALED MAR101970 (SEAL) Attest:
Edward M. Fletcher Jr.
WILLIAM E- SOHUYLER, JR. Mtestmg Offlccr 0n8r of Patents
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3574474A (en) * 1969-07-31 1971-04-13 Carrier Corp Method of and apparatus for controlling the operation of gas compression apparatus
US3594093A (en) * 1969-07-31 1971-07-20 Carrier Corp Operation of gas compression apparatus
US3713756A (en) * 1971-02-23 1973-01-30 Carrier Corp Control for gas compression apparatus
US3732038A (en) * 1971-02-23 1973-05-08 Carrier Corp Control for gas compression apparatus
US3737252A (en) * 1971-02-23 1973-06-05 Carrier Corp Method of and apparatus for controlling the operation of gas compression apparatus
US4462217A (en) * 1980-12-17 1984-07-31 Sueddeutsche Kuehlerfabrik Julius Fr. Behr Gmbh & Co. Kg Process and apparatus for the control of a volume of fluid moving through a duct system
US4502833A (en) * 1981-10-21 1985-03-05 Hitachi, Ltd. Monitoring system for screw compressor
US4526523A (en) * 1984-05-16 1985-07-02 Ingersoll-Rand Company Oil pressure control system
DE3540088A1 (en) * 1985-11-12 1987-05-14 Gutehoffnungshuette Man METHOD FOR DETECTING PUMPS IN TURBO COMPRESSORS
DE4202226A1 (en) * 1991-10-01 1993-04-08 Atlas Copco Energas METHOD FOR MONITORING THE PUMP LIMIT OF MULTI-STAGE, INTERCOOLED TURBO COMPRESSORS
US5290142A (en) * 1991-10-01 1994-03-01 Atlas Copco Energas Gmbh Method of monitoring a pumping limit of a multistage turbocompressor with intermediate cooling
US5716197A (en) * 1994-04-01 1998-02-10 Paul; Marius A. High pressure compressor with internal, inter-stage cooled compression having multiple inlets
US5769610A (en) * 1994-04-01 1998-06-23 Paul; Marius A. High pressure compressor with internal, cooled compression
US6123510A (en) * 1998-01-30 2000-09-26 Ingersoll-Rand Company Method for controlling fluid flow through a compressed fluid system
US6652241B1 (en) * 1999-07-20 2003-11-25 Linde, Ag Method and compressor module for compressing a gas stream
US20040013530A1 (en) * 2000-06-09 2004-01-22 Alexander Kelly Fluid control apparatus and method
US20100122808A1 (en) * 2008-11-19 2010-05-20 Wabtec Holding Corp. Temperature Management System for a 2CD Type Air Compressor
WO2015187230A3 (en) * 2014-03-17 2016-04-07 Eaton Corporation Actuation method and efficiency

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US2696345A (en) * 1949-10-14 1954-12-07 United Aircraft Corp Method of controlling supercharger to avoid pulsation
US2632307A (en) * 1949-11-01 1953-03-24 Bristol Aeroplane Co Ltd Flow-control system for rotaryvane compressors for conditioning air
US3027904A (en) * 1952-08-25 1962-04-03 Garrett Corp Pneumatic control apparatus
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Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3574474A (en) * 1969-07-31 1971-04-13 Carrier Corp Method of and apparatus for controlling the operation of gas compression apparatus
US3594093A (en) * 1969-07-31 1971-07-20 Carrier Corp Operation of gas compression apparatus
US3713756A (en) * 1971-02-23 1973-01-30 Carrier Corp Control for gas compression apparatus
US3732038A (en) * 1971-02-23 1973-05-08 Carrier Corp Control for gas compression apparatus
US3737252A (en) * 1971-02-23 1973-06-05 Carrier Corp Method of and apparatus for controlling the operation of gas compression apparatus
US4462217A (en) * 1980-12-17 1984-07-31 Sueddeutsche Kuehlerfabrik Julius Fr. Behr Gmbh & Co. Kg Process and apparatus for the control of a volume of fluid moving through a duct system
US4502833A (en) * 1981-10-21 1985-03-05 Hitachi, Ltd. Monitoring system for screw compressor
US4526523A (en) * 1984-05-16 1985-07-02 Ingersoll-Rand Company Oil pressure control system
DE3540088A1 (en) * 1985-11-12 1987-05-14 Gutehoffnungshuette Man METHOD FOR DETECTING PUMPS IN TURBO COMPRESSORS
DE4202226A1 (en) * 1991-10-01 1993-04-08 Atlas Copco Energas METHOD FOR MONITORING THE PUMP LIMIT OF MULTI-STAGE, INTERCOOLED TURBO COMPRESSORS
US5290142A (en) * 1991-10-01 1994-03-01 Atlas Copco Energas Gmbh Method of monitoring a pumping limit of a multistage turbocompressor with intermediate cooling
US5716197A (en) * 1994-04-01 1998-02-10 Paul; Marius A. High pressure compressor with internal, inter-stage cooled compression having multiple inlets
US5769610A (en) * 1994-04-01 1998-06-23 Paul; Marius A. High pressure compressor with internal, cooled compression
US6123510A (en) * 1998-01-30 2000-09-26 Ingersoll-Rand Company Method for controlling fluid flow through a compressed fluid system
US6652241B1 (en) * 1999-07-20 2003-11-25 Linde, Ag Method and compressor module for compressing a gas stream
US20040013530A1 (en) * 2000-06-09 2004-01-22 Alexander Kelly Fluid control apparatus and method
US20100122808A1 (en) * 2008-11-19 2010-05-20 Wabtec Holding Corp. Temperature Management System for a 2CD Type Air Compressor
US8128379B2 (en) * 2008-11-19 2012-03-06 Wabtec Holding Corp. Temperature management system for a 2CD type air compressor
WO2015187230A3 (en) * 2014-03-17 2016-04-07 Eaton Corporation Actuation method and efficiency
US20170107987A1 (en) * 2014-03-17 2017-04-20 Eaton Corporation Actuation method and efficiency
US10247190B2 (en) * 2014-03-17 2019-04-02 Eaton Intelligent Power Limited Actuation method and efficiency

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