WO2000073713A1 - Method and means for controlling the generation of cold air - Google Patents

Method and means for controlling the generation of cold air Download PDF

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Publication number
WO2000073713A1
WO2000073713A1 PCT/SE1999/000912 SE9900912W WO0073713A1 WO 2000073713 A1 WO2000073713 A1 WO 2000073713A1 SE 9900912 W SE9900912 W SE 9900912W WO 0073713 A1 WO0073713 A1 WO 0073713A1
Authority
WO
WIPO (PCT)
Prior art keywords
expander
conduit
inlet
compressor
air
Prior art date
Application number
PCT/SE1999/000912
Other languages
French (fr)
Swedish (sv)
Inventor
Henrik ÖHMAN
Original Assignee
Svenska Rotor Maskiner Ab
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to SE9704707A priority Critical patent/SE510794C2/en
Application filed by Svenska Rotor Maskiner Ab filed Critical Svenska Rotor Maskiner Ab
Priority to EP99933317A priority patent/EP1181488B1/en
Priority to ES99933317T priority patent/ES2232151T3/en
Priority to PCT/SE1999/000912 priority patent/WO2000073713A1/en
Priority to DE69921368T priority patent/DE69921368T2/en
Publication of WO2000073713A1 publication Critical patent/WO2000073713A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/002Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
    • F25B9/004Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D13/08Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B49/00Arrangement or mounting of control or safety devices
    • F25B49/02Arrangement or mounting of control or safety devices for compression type machines, plants or systems

Definitions

  • the present invention relates to a method of controlling a device for generating cold air for cooling objects that need to be cooled, in accordance with the preamble of Claim 1.
  • the invention also relates to a device whose output cooling power can be regulated to generate cold air in accordance with Claim 6.
  • Cooling systems are based normally on a two-phase cycle in which a primary refrigerant, for instance freon, is caused to alternate between a liquid phase and a gas phase.
  • a system of this nature will generally have a high cooling capacity and will take up large quantities of heat as the primary refrigerant passes from its liquid phase to its gas phase. It is therefore the system that is most used and most preferred in the majority of applications, including air-conditioning.
  • the equipment required in such a system is both extensive and expensive.
  • gas normally air
  • gas is first compressed from ambient pressure, therewith significantly increasing the temperature of the gas.
  • the hot compressed gas is then cooled in a heat exchanger with small pressure losses and thereafter caused to expand to essentially ambient pressure, or preferably a somewhat higher pressure.
  • the heat exchange effected in the heat exchanger is normally with ambient air.
  • This expanded gas is colder than the gas introduced into the compressor and can therefore be used for cooling purposes, for instance air-conditioning, which normally takes place at ambient pressure, in other words at the same pressure as the compressor inlet pressure.
  • Cooling systems that operate in accordance with the cold air principle for gener- ating cold air for the purpose of cooling objects that need to be cooled, for instance electronic components in aircraft and also aircraft cabins are known to the art.
  • a cooling system is described in Swedish Patent Specification 9403966-6 (publication number 504967).
  • the system described in the Swedish patent specification includes two parallel compressors having inlet and outlet means, a heat exchanger, an expander having inlet and outlet means, compressor inlet conduits, connecting conduits that extend from the compressors to a common heat exchanger inlet, and a conduit that extends from the expander outlet means to the object in need of cooling, for instance electronic components.
  • This described known system is still expensive, because it requires two compres- sors.
  • the use of two compressors enables the gas supply to the expander to be adjusted, since at least one of the compressors is driven by a separate drive means and since its compressed gas volume can be varied with time.
  • Another described method of adjusting the flow to an object in need of being cooled is to release expanded cold air to the surroundings via a valve in a branch conduit, optionally in heat exchanging contact with the heat exchanger of the system.
  • an object of the present invention is to provide a controllable sys- tem for generating a cold air flow whose temperature can be regulated in accordance with cooling requirements.
  • Another object is to provide a controllable system that includes only one compressor and a helical screw expander, and also a method for controlling such a system.
  • a device for generating cold air for cooling objects that require cooling said arrangement including a compressor having inlet and outlet means, a heat exchanger, a helical screw expander having inlet and outlet means, and a first conduit that connects the compressor outlet means to the heat exchanger, a second conduit that connects the heat exchanger to the expander inlet means, and a third conduit that extends from the expander outlet means to the object that needs to be cooled.
  • the compressor and the helical screw expander operate with a generally constant volumetric flow.
  • the compressor may conveniently be a helical screw compressor.
  • the present invention is characterised in that a temperature sensor is placed in the expander outlet means or in the third conduit, and in that the temperature sensor functions to actuate means for regulating the flow to the ex- pander inlet means in accordance with the sensed temperature.
  • the method of controlling the inventive arrangement comprises sensing the temperature of air exiting from the expander in a position in or downstream of the expander outlet, and by adjusting the flow of air to the expander on the basis of the sensed temperature.
  • a change in the air flow to the expander will result in a change in the extent to which the pressure is lowered in the expander and therewith also to a change in the temperature of the outgoing air.
  • a reduction in the air flow to the expander inlet will result in a lower expander inlet pressure and therewith in lower pressure reduction during the expansion phase. This lower pressure reduction results in a lower temperature drop, i.e. in a higher temperature of the outgoing air.
  • One advantage afforded by the present invention is that the system pressure, that is to say the pressure between the compressor outlet means and the inlet means of the helical screw expander, can be reduced when cooling requirements decrease. Because the compression in a cold air system requires the highest mechanical effect, less power is required when the system pressure can be reduced.
  • Figure 1 is a schematic illustration of a first embodiment of an inventive cold air system
  • Figure 2 is a schematic illustration of a second embodiment of an inventive cold air system
  • Figure 3 is a schematic illustration of a third embodiment of an inventive cold air system
  • Figure 4 is a schematic illustration of a fourth embodiment of an inventive cold air system.
  • Figure 1 illustrates schematically an embodiment of an inventive arrangement which includes in series a compressor 1 which operates with a substantially constant volume flow, a heat exchanger 2 which is in heat exchange contact with ambient atmos- phere, and a helical screw expander 3.
  • the expander 3 also operates with a substantially constant volume flow.
  • a first conduit 4 connects the compressor outlet means with the heat exchanger inlet means
  • a second conduit 5 is disposed between the heat exchanger outlet means and the inlet means of the helical screw expander 3.
  • a third conduit 6 extends from the expander outlet means to an object or objects (not shown) that needs/need to be cooled, for example electronic components of a stationary aircraft on the hard- standing.
  • the object that needs to be cooled may be included as part of the conduit 6.
  • An inlet conduit 15 may be connected to the inlet means of the compressor 1.
  • the compressor 1 is driven by a drive means, not shown.
  • a regulating valve 9 is mounted in the branch line 10. The regulating valve 9 can be adjusted between a closed position and a fully open position.
  • a temperature sensor 11 is placed in the third conduit 6, although it may alternatively be placed in the outlet means of the expander 3.
  • the sensor 11 is connected electrically to a processor 7 which, in turn, is connected to a control device 8.
  • the control device 8 adjusts the throughflow area of the regulating valve 9 in re- lation to the temperature sensed by the temperature sensor 11.
  • air is delivered to the inlet means of the compressor 1, via the inlet conduit 15.
  • the supply air is compressed in the compressor 1 to a pressure of up to 3 bar, for instance.
  • This compression means that the temperature of the air leaving the compressor outlet means will be much higher than the temperature of the air delivered to the compressor 1.
  • the compressed air is delivered through the conduit 4 to the heat exchanger 2, in which an exchange of heat takes place with the ambient atmosphere with only slight pressure losses, therewith cooling the air.
  • the cooled, compressed air is delivered to the expander 3 through the conduit 5.
  • the valve 9 is closed, so that no air can flow through the branch conduit 10.
  • the pressure of the air is reduced in the helical screw expander 3, wherewith the temperature of the air falls significantly to a temperature that lies beneath the temperature of the compressor inlet air.
  • the air leaving the expander 3 has a higher pressure than the ambient atmosphere, for instance a pressure of 0.11 -0.15 MPa.
  • the processor 7 sends a signal to the control device 8 which responds by opening the valve 9. Air can then flow through the branch-conduit 10 to the conduit 6. As air begins to flow through the valve 9, the pressure downstream of the compressor 1 drops. This means that the power required to drive the compressor 1 decreases. The pressure drop across the helical screw expander 3 also decreases, result- ing in a lower temperature drop.
  • the temperature of the air flowing through the branch conduit 10 is higher than the temperature of the air that has expanded in the expander 3.
  • the temperature of the air in the conduit 6 increases after combining the air flows from the expander 3 and the branch conduit 10. This temperature change in the conduit 6 results in a reduction in the throughflow area of the valve 9.
  • FIG. 2 is a schematic illustration of an embodiment of the arrangement illustrated in Figure 1. Similar to the Figure 1 arrangement, the Figure 2 arrangement in- eludes a compressor 1 , a heat exchanger 2 which is in heat exchange contact with ambient atmosphere, and a helical screw expander 3, these components being connected in series.
  • the branch conduit 10 of the Figure 1 embodiment is replaced with a branch conduit 12.
  • the branch conduit 12 is also provided with a regulating valve 9 which is actu- ated by the control device 8.
  • the branch conduit 12 extends from the conduit 5 and opens into a closed working chamber of the helical screw expander 3. In a helical screw expander, a working chamber has its smallest volume when closing against the expander inlet. During continued rotation of the expander, the volume of the closed working chamber will increase until the chamber comes into contact with the outlet of said ex- pander 3.
  • the branch conduit 12 opens into a working chamber when its volume is greater than the smallest volume at the moment of closure.
  • Figure 3 illustrates schematically an arrangement which differs from the aforede- scribed arrangements by virtue of the fact that the compressor is a helical screw compressor 14 and that the branch conduit 10 of Figure 1 has been replaced with a branch conduit 16. Other components are identical to those of the Figure 1 embodiment.
  • the branch conduit 16 of the Figure 3 embodiment also includes a regulating valve 9 which is actuated by the control device 8.
  • the branch conduit 16 connects the supply conduit 15 to the outlet means of the compressor 14 or to the first conduit 4.
  • the pressure of the air is reduced in the expander 3, wherewith the temperature falls drastically to a temperature which lies beneath the temperature of the compressor supply air.
  • the pressure of the air leaving the expander 3 is higher than the pressure of the ambient atmosphere, e.g. a pressure of 0.11-0.15 MPa.
  • the processor 7 sends a signal to the control device 8 which responds by opening the valve 9. Air is then able to flow back to the inlet conduit 15, through the branch conduit 16.
  • the pressure downstream of the compressor 14 falls as air begins to flow through the valve 9. This means that less power is required to drive the compressor 14.
  • the temperature of the air flowing through the branch conduit 16 is much higher than the temperature of the ambient air supplied to the compressor 14. Consequently, the air entering the compressor 14 will have a higher temperature than the ambient atmos- phere and that the output temperature will also be higher.
  • the volume of air delivered to the heat exchanger and the helical screw expander 3 decreases, as does also the pressure upstream of the expander 3. The net result is that the air from the expander 3 obtains a higher temperature, which results in adjustment to the throughflow area of the regulating valve.
  • the embodiment illustrated in Figure 4 is similar to the Figure 3 embodiment, but differs therefrom by virtue of the branch conduit 16 in Figure 3 having been replaced with a branch conduit 17.
  • the branch conduit 17 in Figure 4 connects a closed working chamber in the compressor 14 with said inlet conduit 15.
  • a working chamber has its greatest volume when closing against the inlet means. As rotation continues, the volume of the closed working chamber decreases until the other end of said working chamber establishes fluid communication with the compressor outlet means.
  • the branch conduit 17 is arranged in the compressor 14 so that a working chamber will come into contact with the orifice of the branch conduit prior to fluid connection with the outlet means being established and subsequent to establishing fluid connection with the inlet means.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Devices That Are Associated With Refrigeration Equipment (AREA)

Abstract

The invention relates to a method of controlling an arrangement designed for generating cold air for cooling objects that are in need of being cooled, and an arrangement for carrying out the method. The arrangement includes a compressor (1) having air inlet means and compressed air outlet means, a heat exchanger (2) connected to the compressor outlet means via a first conduit (4) and functioning to cool the compressed air, a helical screw expander (3) which is connected to the heat exchanger (2) via a second conduit (5) and which includes an outlet for expanded and cooled air, and a third conduit (16) which extends from the outlet of said expander (3) to the object in need of being cooled. The method is characterised by sensing the temperature of air exiting from the expander (3) at a position in or downstream of the expander outlet, and by controlling the mass flow of air to the expander (3) in accordance with the temperature sensed. The arrangement for generating cold air for cooling objects that are in need of being cooled is characterised by a temperature sensor (11) positioned in the expander outlet or in the third conduit (6), and by a device (7, 8, 9; 10) which is actuated by the temperature sensor (11) and which functions to adjusts the mass flow through the expander (3) in accordance with the temperature sensed.

Description

Method and means for controlling the generation of cold air
The present invention relates to a method of controlling a device for generating cold air for cooling objects that need to be cooled, in accordance with the preamble of Claim 1. The invention also relates to a device whose output cooling power can be regulated to generate cold air in accordance with Claim 6.
Cooling systems, or refrigerating systems, are based normally on a two-phase cycle in which a primary refrigerant, for instance freon, is caused to alternate between a liquid phase and a gas phase. A system of this nature will generally have a high cooling capacity and will take up large quantities of heat as the primary refrigerant passes from its liquid phase to its gas phase. It is therefore the system that is most used and most preferred in the majority of applications, including air-conditioning. However, the equipment required in such a system is both extensive and expensive.
These known systems require a closed circuit for a typical environmentally hazardous refrigerant, which must be isolated from the surroundings. Actual cooling of the objects is achieved with a secondary medium, for instance air, which is cooled by the primary medium in the closed circuit, through the medium of a heat exchanger.
It has long been known that cooling can also be achieved with a cooling system that operates in accordance with the cold air cycle, designated the open reversed Joule-Brayton cycle. Air (or some other gaseous substance) is the only working medium used in the cooling cycle of this system.
In a cooling system according to the cold air cycle, gas, normally air, is first compressed from ambient pressure, therewith significantly increasing the temperature of the gas. The hot compressed gas is then cooled in a heat exchanger with small pressure losses and thereafter caused to expand to essentially ambient pressure, or preferably a somewhat higher pressure. The heat exchange effected in the heat exchanger is normally with ambient air. This expanded gas is colder than the gas introduced into the compressor and can therefore be used for cooling purposes, for instance air-conditioning, which normally takes place at ambient pressure, in other words at the same pressure as the compressor inlet pressure. In a system that operates in accordance with the cold air cycle, there is therefore no need to circulate a primary medium that is cyclically condensed and vaporised and from which cold is transferred to a secondary medium, such as air. The system operating in accordance with the cold air principle has a lower cooling capacity than a conventional cooling system that has a closed circuit which includes a primary refrigerant such a freon. Consequently, the components of a system operating in accordance with the cold air principle will be relatively large and also expensive in relation to cooling capacity.
If a cooling cycle according to the cold air principle is used in a system where the nature of the objects that need to be cooled is such that a relatively large pressure drop will be obtained, the requirements placed on the cooling equipment components will be higher, since the pressure from the cooling equipment must be significantly higher than the ambient pressure. As a result of the requisite overpressure, the temperature at the expander outlet will be higher than if the expander outlet pressure had been closer to the inlet pressure of the cooling equipment. It is necessary to compensate for this temperature difference, by means of correspondingly higher compression in the compressor, so as to obtain a satisfactorily low expander outlet temperature. One situation in which this problem arises is when the cold air is used to cool electronic equipment, for instance electronic equipment in aircraft. Since the air has to pass through a large number of very confined ducts in this latter application, the air that leaves the expander will have a significant overpressure due to the flow resistance in the ducts.
Cooling systems that operate in accordance with the cold air principle for gener- ating cold air for the purpose of cooling objects that need to be cooled, for instance electronic components in aircraft and also aircraft cabins are known to the art. For instance, such a cooling system is described in Swedish Patent Specification 9403966-6 (publication number 504967). The system described in the Swedish patent specification includes two parallel compressors having inlet and outlet means, a heat exchanger, an expander having inlet and outlet means, compressor inlet conduits, connecting conduits that extend from the compressors to a common heat exchanger inlet, and a conduit that extends from the expander outlet means to the object in need of cooling, for instance electronic components.
This described known system is still expensive, because it requires two compres- sors. The use of two compressors enables the gas supply to the expander to be adjusted, since at least one of the compressors is driven by a separate drive means and since its compressed gas volume can be varied with time. Another described method of adjusting the flow to an object in need of being cooled is to release expanded cold air to the surroundings via a valve in a branch conduit, optionally in heat exchanging contact with the heat exchanger of the system.
Accordingly, an object of the present invention is to provide a controllable sys- tem for generating a cold air flow whose temperature can be regulated in accordance with cooling requirements.
Another object is to provide a controllable system that includes only one compressor and a helical screw expander, and also a method for controlling such a system. These objects have been achieved in accordance with the invention with a device for generating cold air for cooling objects that require cooling, said arrangement including a compressor having inlet and outlet means, a heat exchanger, a helical screw expander having inlet and outlet means, and a first conduit that connects the compressor outlet means to the heat exchanger, a second conduit that connects the heat exchanger to the expander inlet means, and a third conduit that extends from the expander outlet means to the object that needs to be cooled. The compressor and the helical screw expander operate with a generally constant volumetric flow. The compressor may conveniently be a helical screw compressor. The present invention is characterised in that a temperature sensor is placed in the expander outlet means or in the third conduit, and in that the temperature sensor functions to actuate means for regulating the flow to the ex- pander inlet means in accordance with the sensed temperature.
The method of controlling the inventive arrangement comprises sensing the temperature of air exiting from the expander in a position in or downstream of the expander outlet, and by adjusting the flow of air to the expander on the basis of the sensed temperature. A change in the air flow to the expander will result in a change in the extent to which the pressure is lowered in the expander and therewith also to a change in the temperature of the outgoing air. A reduction in the air flow to the expander inlet will result in a lower expander inlet pressure and therewith in lower pressure reduction during the expansion phase. This lower pressure reduction results in a lower temperature drop, i.e. in a higher temperature of the outgoing air.
One advantage afforded by the present invention is that the system pressure, that is to say the pressure between the compressor outlet means and the inlet means of the helical screw expander, can be reduced when cooling requirements decrease. Because the compression in a cold air system requires the highest mechanical effect, less power is required when the system pressure can be reduced.
Preferred embodiments of the present invention will be apparent from the de- pending Claims.
The invention will now be described in more detail with reference to a detailed description of preferred embodiments and also with reference to the accompanying drawings, in which
Figure 1 is a schematic illustration of a first embodiment of an inventive cold air system;
Figure 2 is a schematic illustration of a second embodiment of an inventive cold air system;
Figure 3 is a schematic illustration of a third embodiment of an inventive cold air system; and Figure 4 is a schematic illustration of a fourth embodiment of an inventive cold air system.
Figure 1 illustrates schematically an embodiment of an inventive arrangement which includes in series a compressor 1 which operates with a substantially constant volume flow, a heat exchanger 2 which is in heat exchange contact with ambient atmos- phere, and a helical screw expander 3. The expander 3 also operates with a substantially constant volume flow. A first conduit 4 connects the compressor outlet means with the heat exchanger inlet means, a second conduit 5 is disposed between the heat exchanger outlet means and the inlet means of the helical screw expander 3. A third conduit 6 extends from the expander outlet means to an object or objects (not shown) that needs/need to be cooled, for example electronic components of a stationary aircraft on the hard- standing. The object that needs to be cooled may be included as part of the conduit 6. An inlet conduit 15 may be connected to the inlet means of the compressor 1. The compressor 1 is driven by a drive means, not shown.
A branch conduit 10, which short-circuits the expander inlet and outlet means, is disposed between the second conduit 5 and the third conduit 6. A regulating valve 9 is mounted in the branch line 10. The regulating valve 9 can be adjusted between a closed position and a fully open position. In the illustrated case, a temperature sensor 11 is placed in the third conduit 6, although it may alternatively be placed in the outlet means of the expander 3. The sensor 11 is connected electrically to a processor 7 which, in turn, is connected to a control device 8. The control device 8 adjusts the throughflow area of the regulating valve 9 in re- lation to the temperature sensed by the temperature sensor 11.
When starting-up the arrangement, air is delivered to the inlet means of the compressor 1, via the inlet conduit 15. The supply air is compressed in the compressor 1 to a pressure of up to 3 bar, for instance. This compression means that the temperature of the air leaving the compressor outlet means will be much higher than the temperature of the air delivered to the compressor 1. The compressed air is delivered through the conduit 4 to the heat exchanger 2, in which an exchange of heat takes place with the ambient atmosphere with only slight pressure losses, therewith cooling the air. The cooled, compressed air is delivered to the expander 3 through the conduit 5. The valve 9 is closed, so that no air can flow through the branch conduit 10. The pressure of the air is reduced in the helical screw expander 3, wherewith the temperature of the air falls significantly to a temperature that lies beneath the temperature of the compressor inlet air. The air leaving the expander 3 has a higher pressure than the ambient atmosphere, for instance a pressure of 0.11 -0.15 MPa.
When the temperature sensed by the temperature sensor 11 is lower than a pre- determined lowest temperature, the processor 7 sends a signal to the control device 8 which responds by opening the valve 9. Air can then flow through the branch-conduit 10 to the conduit 6. As air begins to flow through the valve 9, the pressure downstream of the compressor 1 drops. This means that the power required to drive the compressor 1 decreases. The pressure drop across the helical screw expander 3 also decreases, result- ing in a lower temperature drop.
The temperature of the air flowing through the branch conduit 10 is higher than the temperature of the air that has expanded in the expander 3. Thus, the temperature of the air in the conduit 6 increases after combining the air flows from the expander 3 and the branch conduit 10. This temperature change in the conduit 6 results in a reduction in the throughflow area of the valve 9.
Figure 2 is a schematic illustration of an embodiment of the arrangement illustrated in Figure 1. Similar to the Figure 1 arrangement, the Figure 2 arrangement in- eludes a compressor 1 , a heat exchanger 2 which is in heat exchange contact with ambient atmosphere, and a helical screw expander 3, these components being connected in series. The branch conduit 10 of the Figure 1 embodiment is replaced with a branch conduit 12. The branch conduit 12 is also provided with a regulating valve 9 which is actu- ated by the control device 8. The branch conduit 12 extends from the conduit 5 and opens into a closed working chamber of the helical screw expander 3. In a helical screw expander, a working chamber has its smallest volume when closing against the expander inlet. During continued rotation of the expander, the volume of the closed working chamber will increase until the chamber comes into contact with the outlet of said ex- pander 3. The branch conduit 12 opens into a working chamber when its volume is greater than the smallest volume at the moment of closure.
Figure 3 illustrates schematically an arrangement which differs from the aforede- scribed arrangements by virtue of the fact that the compressor is a helical screw compressor 14 and that the branch conduit 10 of Figure 1 has been replaced with a branch conduit 16. Other components are identical to those of the Figure 1 embodiment. The branch conduit 16 of the Figure 3 embodiment also includes a regulating valve 9 which is actuated by the control device 8. The branch conduit 16 connects the supply conduit 15 to the outlet means of the compressor 14 or to the first conduit 4.
When starting-up the arrangement shown in Figure 3, air is delivered to the inlet means of the compressor 14 via the inlet conduit 15. The supply air is compressed in the compressor 1 to a pressure of, e.g., 3 bar. As a result of this compression, the temperature of the air leaving the outlet means of the compressor 14 will be much higher than the temperature of the air supplied to said compressor. The valve 9 is closed, so that no air is able to flow through the branch conduit 16. The compressed air is delivered to the heat exchanger 2 through the conduit 4 and a heat exchange takes place in the heat exchanger with the ambient atmosphere with only small pressure losses, therewith cooling the air. The cooled compressed air is delivered to the expander 3 through the conduit 5. The pressure of the air is reduced in the expander 3, wherewith the temperature falls drastically to a temperature which lies beneath the temperature of the compressor supply air. The pressure of the air leaving the expander 3 is higher than the pressure of the ambient atmosphere, e.g. a pressure of 0.11-0.15 MPa. When the temperature sensed by the temperature sensor 11 is lower than a predetermined lowest temperature, the processor 7 sends a signal to the control device 8 which responds by opening the valve 9. Air is then able to flow back to the inlet conduit 15, through the branch conduit 16. The pressure downstream of the compressor 14 falls as air begins to flow through the valve 9. This means that less power is required to drive the compressor 14.
The temperature of the air flowing through the branch conduit 16 is much higher than the temperature of the ambient air supplied to the compressor 14. Consequently, the air entering the compressor 14 will have a higher temperature than the ambient atmos- phere and that the output temperature will also be higher. At the same time, the volume of air delivered to the heat exchanger and the helical screw expander 3 decreases, as does also the pressure upstream of the expander 3. The net result is that the air from the expander 3 obtains a higher temperature, which results in adjustment to the throughflow area of the regulating valve. The embodiment illustrated in Figure 4 is similar to the Figure 3 embodiment, but differs therefrom by virtue of the branch conduit 16 in Figure 3 having been replaced with a branch conduit 17. Instead of connecting the first conduit 4 with the inlet conduit 15, the branch conduit 17 in Figure 4 connects a closed working chamber in the compressor 14 with said inlet conduit 15. In a helical screw compressor, a working chamber has its greatest volume when closing against the inlet means. As rotation continues, the volume of the closed working chamber decreases until the other end of said working chamber establishes fluid communication with the compressor outlet means. The branch conduit 17 is arranged in the compressor 14 so that a working chamber will come into contact with the orifice of the branch conduit prior to fluid connection with the outlet means being established and subsequent to establishing fluid connection with the inlet means.
The arrangement according to Figure 4 operates in a manner corresponding to the arrangement according to the Figure 3 embodiment.

Claims

Claims
1. A method of controlling an arrangement for generating cold air for cooling objects that need to be cooled, said arrangement including in series a compressor (1 ; 14) having inlet and outlet means and functioning to compress air at ambient pressure, a heat exchanger (2) having air inlet and outlet means, a helical screw expander (3) having inlet and outlet means, and in which arrangement a first conduit (4) connects the compressor (1; 14) outlet means with the heat exchanger (2) inlet means, a second conduit (5) connects the heat exchanger (2) outlet means with the inlet means of the helical screw expander (3), and which includes a third conduit (6) that connects the outlet means of said helical screw expander (3) with the object that needs to be cooled, characterised by sensing the temperature of the air exiting from the helical screw expander (3) at a position in or downstream of the expander (3) outlet means; and adjusting the flow of air to the expander (3) inlet means in accordance with the sensed temperature.
2. A method according to Claim 1, characterised by adjusting the air flow to the expander inlet means by decreasing the flow delivered from the compressor (1 ; 14) to the heat exchanger (2).
3. A method according to Claim 2, characterised by returning part of the air that has been partially or fully compressed in the compressor (1; 14) to the compressor inlet means.
4. A method according to Claim 1 , characterised by adjusting the air flow to the expander (3) inlet means by taking out a part-flow at a point between the heat exchanger (2) and the expander inlet means and causing said part-flow to by-pass the expander (3).
5. A method according to Claim 1 , characterised by adjusting the air flow to the expander inlet means by taking out a part-flow at a point between the heat exchanger and the expander inlet means and passing said part-flow to a closed working chamber in the expander.
6. An arrangement for generating cold air for cooling objects that are in need of being cooled, said arrangement comprising in series a compressor (1; 14) having inlet and outlet means, a heat exchanger (2) having inlet and outlet means, a helical screw ex- pander (3) having inlet and outlet means, a first conduit (4) which connects the compressor outlet means to the heat exchanger inlet means, a second conduit (5) which connects the heat exchanger outlet means with the expander inlet means, and a third conduit (6) which extends from the expander outlet means to the object that is in need of being cooled, characterised by a temperature sensor (11) located in the expander outlet means or in the third conduit (6), and by means ([7, 8, 9; 10], 12, 16, 17) which is actuated by the temperature sensor (11) and which adjusts the flow of air to the expander inlet means in accordance with the sensed temperature.
7. An arrangement according to Claim 6, characterised in that the device ([7, 8, 9
10], 12, 16, 17) actuated by said temperature sensor (11) includes a control valve (9) mounted in a conduit (10) that connects the second conduit (5) to the expander outlet means or to the third conduit (6). 8. An arrangement according to Claim 6, characterised in that the device ([7,
8, 9; 10], 12, 16, 17) that is actuated by the temperature sensor (11) includes a control valve (9) mounted in a conduit (12) that connects the second conduit (5) with a closed working chamber in the helical screw expander (3).
9. An arrangement according to Claim 6, characterised in that the device ([7, 8, 9; 10], 12, 16, 17) that is actuated by the temperature sensor (12) includes a control valve
(9) mounted in a conduit (16) that connects the compressor outlet means or the first conduit (4) to the compressor inlet means or to the inlet conduit (15).
10. An arrangement according to one or more of Claims 6-9, characterised in that the compressor (1; 14) is a helical screw compressor (14).
11. An arrangement according to Claim 10, characterised in that the device ([7, 8, 9,; 10], 12, 16, 17) that is actuated by the temperature sensor (11) is a control valve (9) mounted in a conduit (17) that connects a closed working chamber in the compressor (14) with the compressor inlet means or with the inlet conduit (15).
PCT/SE1999/000912 1997-12-17 1999-05-28 Method and means for controlling the generation of cold air WO2000073713A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
SE9704707A SE510794C2 (en) 1997-12-17 1997-12-17 Methods and apparatus for controlling cooling effect in cold air systems
EP99933317A EP1181488B1 (en) 1997-12-17 1999-05-28 Method and means for controlling the generation of cold air
ES99933317T ES2232151T3 (en) 1997-12-17 1999-05-28 METHOD AND MEANS TO CONTROL THE GENERATION OF COLD AIR.
PCT/SE1999/000912 WO2000073713A1 (en) 1997-12-17 1999-05-28 Method and means for controlling the generation of cold air
DE69921368T DE69921368T2 (en) 1997-12-17 1999-05-28 METHOD AND DEVICE FOR REGULATING COLD-AIR GENERATION

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9704707A SE510794C2 (en) 1997-12-17 1997-12-17 Methods and apparatus for controlling cooling effect in cold air systems
PCT/SE1999/000912 WO2000073713A1 (en) 1997-12-17 1999-05-28 Method and means for controlling the generation of cold air

Publications (1)

Publication Number Publication Date
WO2000073713A1 true WO2000073713A1 (en) 2000-12-07

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PCT/SE1999/000912 WO2000073713A1 (en) 1997-12-17 1999-05-28 Method and means for controlling the generation of cold air

Country Status (5)

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EP (1) EP1181488B1 (en)
DE (1) DE69921368T2 (en)
ES (1) ES2232151T3 (en)
SE (1) SE510794C2 (en)
WO (1) WO2000073713A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005005254A1 (en) * 2003-04-29 2005-01-20 Honeywell International Inc. Aircraft ground support air conditioning unit with temperature-biased flow control
EP1780478A1 (en) * 2004-07-07 2007-05-02 Daikin Industries, Ltd. Freezing device
JP2007522389A (en) * 2004-02-17 2007-08-09 スベンスカ・ロツタア・マスキナア・アクチボラグ Method and means for controlling flow rate through expander
WO2016132820A1 (en) * 2015-02-19 2016-08-25 株式会社 豊田自動織機 Air conditioning system
CN106438110A (en) * 2015-08-05 2017-02-22 北京意科瑞思能源技术有限公司 Cooling and power generating system and method by using gas pressure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3221511A (en) * 1964-12-14 1965-12-07 British Oxygen Co Ltd Cooling systems for gases
US3878692A (en) * 1974-04-22 1975-04-22 Garrett Corp Aircraft cabin cooling method and apparatus
US4771612A (en) * 1986-01-29 1988-09-20 Imatran Voima Oy Method and apparatus for the utilization of heat energy released in a cooling process of water
GB2273349A (en) * 1992-11-21 1994-06-15 Normalair Garrett Air cycle air conditioning systems
US5600965A (en) * 1996-03-14 1997-02-11 Solar Turbines Incorporated Air conditioning system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3221511A (en) * 1964-12-14 1965-12-07 British Oxygen Co Ltd Cooling systems for gases
US3878692A (en) * 1974-04-22 1975-04-22 Garrett Corp Aircraft cabin cooling method and apparatus
US4771612A (en) * 1986-01-29 1988-09-20 Imatran Voima Oy Method and apparatus for the utilization of heat energy released in a cooling process of water
GB2273349A (en) * 1992-11-21 1994-06-15 Normalair Garrett Air cycle air conditioning systems
US5600965A (en) * 1996-03-14 1997-02-11 Solar Turbines Incorporated Air conditioning system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005005254A1 (en) * 2003-04-29 2005-01-20 Honeywell International Inc. Aircraft ground support air conditioning unit with temperature-biased flow control
JP2007522389A (en) * 2004-02-17 2007-08-09 スベンスカ・ロツタア・マスキナア・アクチボラグ Method and means for controlling flow rate through expander
EP1723310B1 (en) * 2004-02-17 2009-04-29 Svenska Rotor Maskiner Ab Method and means for controlling a flow through an expander
AU2005213593B2 (en) * 2004-02-17 2010-09-09 Svenska Rotor Maskiner Ab Method and means for controlling a flow through an expander
EP1780478A1 (en) * 2004-07-07 2007-05-02 Daikin Industries, Ltd. Freezing device
EP1780478A4 (en) * 2004-07-07 2014-12-24 Daikin Ind Ltd Freezing device
WO2016132820A1 (en) * 2015-02-19 2016-08-25 株式会社 豊田自動織機 Air conditioning system
CN106438110A (en) * 2015-08-05 2017-02-22 北京意科瑞思能源技术有限公司 Cooling and power generating system and method by using gas pressure

Also Published As

Publication number Publication date
DE69921368T2 (en) 2006-02-02
DE69921368D1 (en) 2004-11-25
SE9704707L (en) 1999-06-18
EP1181488B1 (en) 2004-10-20
SE9704707D0 (en) 1997-12-17
EP1181488A1 (en) 2002-02-27
SE510794C2 (en) 1999-06-21
ES2232151T3 (en) 2005-05-16

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