US3797266A - Air conditioning control system - Google Patents
Air conditioning control system Download PDFInfo
- Publication number
- US3797266A US3797266A US00269638A US3797266DA US3797266A US 3797266 A US3797266 A US 3797266A US 00269638 A US00269638 A US 00269638A US 3797266D A US3797266D A US 3797266DA US 3797266 A US3797266 A US 3797266A
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- Prior art keywords
- pressure
- temperature
- refrigerant
- evaporator
- air
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B41/00—Fluid-circulation arrangements
- F25B41/30—Expansion means; Dispositions thereof
- F25B41/31—Expansion valves
- F25B41/33—Expansion valves with the valve member being actuated by the fluid pressure, e.g. by the pressure of the refrigerant
- F25B41/335—Expansion valves with the valve member being actuated by the fluid pressure, e.g. by the pressure of the refrigerant via diaphragms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2500/00—Problems to be solved
- F25B2500/26—Problems to be solved characterised by the startup of the refrigeration cycle
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2600/00—Control issues
- F25B2600/25—Control of valves
- F25B2600/2513—Expansion valves
Definitions
- the constant pressure expansion device at system start up, is operated at a relatively high pressure to maximize the refrigeration effect and increase cooling capacity.
- a temperature sensing element which is sensitive to a variable indicative of air temperature within the cooled space, is operative to reset the control point of the expansion device to reduce the temperature and pressure of the evaporator.
- the improvement of the subject invention is directed to a system in which the temperature sensing element comprises a temperature responsive bulb and capillary charged with a fluid having a pressure difference over its temperature range which approximately matches the pressuredifference of the system refrigerant over its range of operating conditions.
- the critical part of the system is in the compressor.
- the efficiency of the compressor is materially reduced in that the refrigeration taken in the suction side of the compressor is in a smaller quantity and less work can be performed on the refrigerant.
- Automotive applications also present a problem with respect to start-up conditions. For example, the temperature of the air in an enclosed vehicle space, if the auto is parked in the sun with the airconditioning off, is often 145 F. and may be as high as 180 F.
- the system should be operated in such a manner as to reduce this temperature as fast as possible to minimize discomfort of the occupants.
- the evaporator pressure should be kept relatively high. This allows more refrigerant to be taken into the compressor suction and provides for effective use of the entire evaporator coil surface.
- the refrigerant will completely evaporate in the first section of the evaporator coil. Beyond this point the temperature of the refrigerant vapor rises (is superheated) and then passes to the compressor suction port.
- the pressure can be raised to effectively increase thecapacity of the compressor and utilize most of the evaporator coil surface.
- the evaporator pressure should then be lowered to a point slightly above the temperature at which ,coil freeze up can occur.
- the thermal bulb capillary system which, for the pull-down temperature range, matches the pressure-temperature characteristics of the refrigerant employed in the system. For example, if it is desired to operate the evaporator at 55 F. upon initiation of the refrigeration system and at 28 F. after the desired air temperature in the control space has been reached, this is effectively a 15.2 psi difference in refrigeration pressure. If the thermal bulb is placed in contact with the air circulating in the passenger compartment, the temperature drop from 145 to F. should be about equal to the previously mentioned pressure difference i.e., 15.2 psi.
- 15.2 psi One advantage flowing from this is that further decrease in the temperature of air within the vehicle space would have very little effeet on the thermal bulb-capillary system.
- FIG. 1 is a schematic or diagrammatic view of the air conditioning system constructed in accordance with the present invention.
- FIG. 2 is a graph in which refrigeration'system capacity(Q) is plotted against evaporator temperature (T).
- the airconditioning system of the present invention includes a compressor 10, a condenser 12, an expansion device 14 and an evaporator 16 all connected to provide a closed circuit refrigeration system.
- Refrigerant compressed by the compressor 10 is delivered to the condenser through line 18.
- the liquified refrigerant is then passed through line 28 to expansion device 14, which will be discussed in more detail below.
- expansion device 14 which will be discussed in more detail below.
- the refrigerant passes through the expansion device from high pressure side to low pressure side, it flows through line 22 to the evaporator 16 which cools the air circulated over it by fan 17.
- the refrigerant then flows through line 24, commonly referred to as the suction gas line, to the suction connection of compressor 10.
- a superheat regulating valve 25 is located between the evaporator and the compressor in line 24. Since the construction and operation is described in detail in the above-identified Newton application it is incorporated by reference.
- Expansion device 14 comprises a valve having a casing 30, a valve member 32 adapted to be seated on valve seat 34, inlet 36 and outlet 37.
- Valve member 32 is connected to a stem 38 which is secured at its opposite end to an actuating diaphragm 40.
- Spring 42 is seated upon a spring support member 43 and tends to urge the valve member toward a closed position against seat 34.
- Spring 44 located in the upper portion of the casing 30 engages the diaphragm 40 and biases the same in a downward position tending to open the valve by urging valve member 32 away from the seat.
- an important feature of the inven tion is the provision of means for establishing a control signal indicative of the interior air temperature and using such signal to vary the control point of the expansion device 14.
- a fluid connection by means of capillary tube 50, to thermal bulb 52.
- FIG. 2 shows a plot of temperature in the evaporator vs. capacity of a system using refrigerant R-12
- the two lines running across the graph with a downward slope indicate the characteristics of the 90 F. wet bulb condition and the 65 F. wet bulb condition, as indicated by the legends.
- the two curves with the positive slope identified as A and B respectively indicate the compressor capacity pressure conditions at maximum discharge pressure and at normal discharge pressure.
- the intersection (C) of the 90 F. wet bulb line and capacity curve A approximates the conditions at initiation of the pull-down phase and results in a 55 F. evaporator pressure.
- wet bulb line is the desired operating point on the assumption that the air temperature and humidity have been adjusted to this value after several minutes of operation. This produces the desired evaporator temperature of about 28 F. It is obvious from inspection of FIG. 2 that the compressor must shift operation between points C and D along the dashed line C-D. In order to establish this shift it is desirable to use a fluid in the thermal bulb-capillary system which has the same pressure drop between an assumed high interior vehicle space condition, about 145 F. and the desired air temperature, about 75 F. It can be seen that whil jhgevaporator pressure is being shifted from 66.7 psia (corresponding to 55Fij and 41.5 psia (corresponding to 28 F.) the bulbcapillary system must operate over an appreciably larger temperature range.
- a desirable fluid for use in the bulb-capillary system would be refrigerant R-l 13.
- this refrigerant has a pressure of 23.9 psia and at 75 F. a pressure of 6.2'psia resulting in a difference of 17.7 psi.
- R-l or R-216 can be used in the bulb-capillary system. The net result of this matching of pressures within the control system forces the shift of operating conditions along a line approximating line C-D on FIG. 2.
- the bulb 50 which as previously noted may be located in a position to sense interior air temperature, will be relatively warm. Accordingly, the fluid charge in the bulb and capillary will be at a high pressure, tending to establish arelatively high pressure. not only within the bulb itself but also in chamber 56 which is part of the same closed system. This pressure acting against the upper surface of diaphragm 40 will tend to bias the valve member to its open position and establish a control point effecting a relatively high pressure on the downstream side of the valve, and in the evaporator itself. After the system has been operating for a few minutes the pressure on the downstream side will be maintained constant by the pressure acting against the under side of the diaphragm 40.
- the bulb temperature will be reduced tending to reduce the pressure in chamber 56 to relieve the pressure on the upper surface of the diaphragm. This will gradually shift control point at lower and lower pressures until such time as the pull-down phase has been completed.
- the evaporator pressure will be established at a point slightly above the temperature at which freeze up can occur but at a low enough temperature to effect the desired dehumidification of air passing through the evaporator coil.
- the fluid to be used for the thermal bulb fill it is preferred that such fluid have a pressure change between 145 and 75 F. of between 75 and 125 percent of the pressure change of the system refrigerant between 55 and 28 F.
- a fluid for the thermal bulb-capillary system which exhibits little pressure change upon further change in the temperature of the compartment.
- refrigerant R-113 for a system utilizing refrigerant R-l2 meets this need.
- the average pressure change from 145 F. bulb temperature to 75 F. bulb temperature is approximately 0.25 psi/ F., whereas for the next 10 F. (down to F.) there would be only 0.12 psi/ F. pressure change for further reduction in temperature.
- An air conditioning system comprising a compressor, a condenser, a constant pressure expansion device, and an evaporator all connected to provide a closed, vapor cycle refrigeration circuit through which a refrigerant is circulated; means for circulating air within a cooled space through said evaporator; a control system including a thermal bulb-capillary unit for establishing a control signal which is a function of the temperature of air within said cooled space; means for applying said signal to said constant pressure expansion device to vary the control point thereof, and the corresponding evaporator pressure, whereby the evaporator pressure is established at a lower value when the temperature of the cooled space is below some predetermined value, said thermal bulb-capillary unit being filled with an expansible, halocarbon fluid having a pressure change in the range of 145 and F of between 75 and percent of the pressure change of said refrigerant in the range between 55 and 28 F, whereby the temperature range of air within the controlled space during normal operation matches the temperature-pressure characteristics of said refrigerant over the range
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Air-Conditioning For Vehicles (AREA)
- Temperature-Responsive Valves (AREA)
Abstract
A refrigerant control system, particularly useful for air conditioning apparatus, including means for operating the system with a relatively high evaporator pressure during the time the temperature within the cooled space is being reduced to its desired level. The constant pressure expansion device, at system start up, is operated at a relatively high pressure to maximize the refrigeration effect and increase cooling capacity. A temperature sensing element, which is sensitive to a variable indicative of air temperature within the cooled space, is operative to reset the control point of the expansion device to reduce the temperature and pressure of the evaporator. The improvement of the subject invention is directed to a system in which the temperature sensing element comprises a temperature responsive bulb and capillary charged with a fluid having a pressure difference over its temperature range which approximately matches the pressure difference of the system refrigerant over its range of operating conditions.
Description
United States Patent 1 Newton Mar. 19, 1974 AIR CONDITIONING CONTROL SYSTEM [75] Inventor: Alwln B. Newton, York. Pa.
[73] Assignee: Borg-Warner Corporation, Chicago,
[22] Filed: July 7, 1972 [21] App]. No; 269,638
[52] US. Cl. 62/223, 62/224 [51] Int. Cl. F25b 41/04 [58] Field of Search 62/204, 210, 211, 222, 62/225 [56] References Cited UNITED STATES PATENTS 1,408,744 '3/1922 Keen... 62/224 1,618,815 2/1927 Cory 62/223 Primary Examiner-Meyer Perlin Attorney,-Agent, 0r FirmDonald W. Banner [57] ABSTRACT A refrigerant control system, particularly useful for air conditioning apparatus, including means for operating the system with a relatively high evaporator pressure during the time the temperature within the cooled space is being reduced to its desired level. The constant pressure expansion device, at system start up, is operated at a relatively high pressure to maximize the refrigeration effect and increase cooling capacity. A temperature sensing element, which is sensitive to a variable indicative of air temperature within the cooled space, is operative to reset the control point of the expansion device to reduce the temperature and pressure of the evaporator. The improvement of the subject invention is directed to a system in which the temperature sensing element comprises a temperature responsive bulb and capillary charged with a fluid having a pressure difference over its temperature range which approximately matches the pressuredifference of the system refrigerant over its range of operating conditions.
3 Claims, 2 Drawing Figures 2 2 a 14 f' I PAIENTEBuAR 19 I974 3; 791,266
cow: MAX. DISCHARGE TEMPERATU R E EVAPORATOR CAPACITY COMF?@ NORMAL DISCH.
AIR CONDITIONING CONTROL SYSTEM BACKGROUND AND SUMMARY OF THE INVENTION In U. S. Pat. No. 3,260,064 issued to A. B. Newton on July 12, 1966 there is described an air conditioning system including a compressor, a condenser, an expansion device, and an evaporator, all connected in a closed, vapor cycle refrigeration circuit. An important feature described and claimed in the aforementioned patent is the use of means for sensing the superheat of gas leaving the evaporator and means varying thecapacity of the compressor operated in response to the amount of superheat to maintain the correct balance between the compressor capacity and the refrigeration load. This system also uses a constant pressure expansion device between the condenser and evaporator to maintain the evaporator pressure at a predetermined value.
In certain automotive air conditioning applications, especially in the larger size vehicles, which are conventionally furnished with adequately sized evaporator coils, the critical part of the system is in the compressor. At low suction pressures the efficiency of the compressor is materially reduced in that the refrigeration taken in the suction side of the compressor is in a smaller quantity and less work can be performed on the refrigerant. Automotive applications also present a problem with respect to start-up conditions. For example, the temperature of the air in an enclosed vehicle space, if the auto is parked in the sun with the airconditioning off, is often 145 F. and may be as high as 180 F. During the time which is required to bring this temperature down to the desired level, commonly referred to as pull-down, the system should be operated in such a manner as to reduce this temperature as fast as possible to minimize discomfort of the occupants. On the other hand, it is desirable to operate the system to provide adequate dehumidification of the air being circulated within the vehicle space.
In order to satisfy the first objective, i.e., rapid pull down, the evaporator pressure should be kept relatively high. This allows more refrigerant to be taken into the compressor suction and provides for effective use of the entire evaporator coil surface. In other words, during pull-down under normal conditions the refrigerant will completely evaporate in the first section of the evaporator coil. Beyond this point the temperature of the refrigerant vapor rises (is superheated) and then passes to the compressor suction port. With an adequately sized evaporator coil the pressure can be raised to effectively increase thecapacity of the compressor and utilize most of the evaporator coil surface. To satisfy the requirement of dehumidification after pulldown has been completed, the evaporator pressure should then be lowered to a point slightly above the temperature at which ,coil freeze up can occur.
In the related copending application Ser. No. 269,637 by Kenneth W. Cooper filed July 7, 1972, there is described an automatic control for adjusting the balance point of the automatic expansion device which permits the evaporator to operate at a substantially higher temperature (and pressure) during the pull-down phase of operation. When the temperature of the air within the controlled space reaches its desired level, the balance point of the expansion device is reset to produce a pressure and temperature in the evaporator slightly above the temperature at which coil freeze up could occur. Actually, the readjusting of the balance point is a continuous process as the pressure opposing the evaporator pressure control. force rises continuously throughout the pull-down period. In the present invention, it has been found that it is very desirable to utilize a fluid in the thermal bulb capillary system which, for the pull-down temperature range, matches the pressure-temperature characteristics of the refrigerant employed in the system. For example, if it is desired to operate the evaporator at 55 F. upon initiation of the refrigeration system and at 28 F. after the desired air temperature in the control space has been reached, this is effectively a 15.2 psi difference in refrigeration pressure. If the thermal bulb is placed in contact with the air circulating in the passenger compartment, the temperature drop from 145 to F. should be about equal to the previously mentioned pressure difference i.e., 15.2 psi. One advantage flowing from this is that further decrease in the temperature of air within the vehicle space would have very little effeet on the thermal bulb-capillary system.
DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic or diagrammatic view of the air conditioning system constructed in accordance with the present invention; and
FIG. 2 is a graph in which refrigeration'system capacity(Q) is plotted against evaporator temperature (T).
DETAILED DESCRIPTION OF THE INVENTION As shown in FIG. 1, the airconditioning system of the present invention includes a compressor 10, a condenser 12, an expansion device 14 and an evaporator 16 all connected to provide a closed circuit refrigeration system. Refrigerant compressed by the compressor 10 is delivered to the condenser through line 18. The liquified refrigerant is then passed through line 28 to expansion device 14, which will be discussed in more detail below. After the refrigerant passes through the expansion device from high pressure side to low pressure side, it flows through line 22 to the evaporator 16 which cools the air circulated over it by fan 17. The refrigerant then flows through line 24, commonly referred to as the suction gas line, to the suction connection of compressor 10.
As previously described in copending application Ser. No. 99,806, A. B. Newton filed Dec. 21, 1970, now U.S. Pat. No. 3,688,517 issued Sept. 5, 1972, a superheat regulating valve 25 is located between the evaporator and the compressor in line 24. Since the construction and operation is described in detail in the above-identified Newton application it is incorporated by reference.
As noted-above, an important feature of the inven tion is the provision of means for establishing a control signal indicative of the interior air temperature and using such signal to vary the control point of the expansion device 14. At the upper portion of the casing 30 there is provided a fluid connection, by means of capillary tube 50, to thermal bulb 52. The chamber 56 formed between the casing 30 and diaphragm 40 together with the capillary and bulb form a closed system.
Referring now to FIG. 2, which shows a plot of temperature in the evaporator vs. capacity of a system using refrigerant R-12, the two lines running across the graph with a downward slope indicate the characteristics of the 90 F. wet bulb condition and the 65 F. wet bulb condition, as indicated by the legends. The two curves with the positive slope identified as A and B respectively indicate the compressor capacity pressure conditions at maximum discharge pressure and at normal discharge pressure. The intersection (C) of the 90 F. wet bulb line and capacity curve A approximates the conditions at initiation of the pull-down phase and results in a 55 F. evaporator pressure. The intersection (D) of line B and the 65 F. wet bulb line is the desired operating point on the assumption that the air temperature and humidity have been adjusted to this value after several minutes of operation. This produces the desired evaporator temperature of about 28 F. It is obvious from inspection of FIG. 2 that the compressor must shift operation between points C and D along the dashed line C-D. In order to establish this shift it is desirable to use a fluid in the thermal bulb-capillary system which has the same pressure drop between an assumed high interior vehicle space condition, about 145 F. and the desired air temperature, about 75 F. It can be seen that whil jhgevaporator pressure is being shifted from 66.7 psia (corresponding to 55Fij and 41.5 psia (corresponding to 28 F.) the bulbcapillary system must operate over an appreciably larger temperature range. In this case, a desirable fluid for use in the bulb-capillary system would be refrigerant R-l 13. At 145 F., this refrigerant has a pressure of 23.9 psia and at 75 F. a pressure of 6.2'psia resulting in a difference of 17.7 psi. Corresponding relationships can be found for the other refrigerant systems. For example, if the system is utilizing R-22, then R-ll or R-216 can be used in the bulb-capillary system. The net result of this matching of pressures within the control system forces the shift of operating conditions along a line approximating line C-D on FIG. 2.
Assuming that the vehicle is in a condition where the interior space is relatively warm, the bulb 50 which as previously noted may be located in a position to sense interior air temperature, will be relatively warm. Accordingly, the fluid charge in the bulb and capillary will be at a high pressure, tending to establish arelatively high pressure. not only within the bulb itself but also in chamber 56 which is part of the same closed system. This pressure acting against the upper surface of diaphragm 40 will tend to bias the valve member to its open position and establish a control point effecting a relatively high pressure on the downstream side of the valve, and in the evaporator itself. After the system has been operating for a few minutes the pressure on the downstream side will be maintained constant by the pressure acting against the under side of the diaphragm 40. For example, if the load is changed so as to increase the downstream pressure this pressure will be applied through channel 45 to the under side of the diaphragm 40 tending to close the valve. If the pressure is reduced for some reason, the opposite result occurs. After the system has been operating for a while at the higher evaporator pressure, the bulb temperature will be reduced tending to reduce the pressure in chamber 56 to relieve the pressure on the upper surface of the diaphragm. This will gradually shift control point at lower and lower pressures until such time as the pull-down phase has been completed. At this point, the evaporator pressure will be established at a point slightly above the temperature at which freeze up can occur but at a low enough temperature to effect the desired dehumidification of air passing through the evaporator coil.
In the selection of the fluid to be used for the thermal bulb fill, it is preferred that such fluid have a pressure change between 145 and 75 F. of between 75 and 125 percent of the pressure change of the system refrigerant between 55 and 28 F. As noted above in the preliminary remarks, it is also desirable to select a fluid for the thermal bulb-capillary system which exhibits little pressure change upon further change in the temperature of the compartment. The choice of refrigerant R-113 for a system utilizing refrigerant R-l2 meets this need. The average pressure change from 145 F. bulb temperature to 75 F. bulb temperature is approximately 0.25 psi/ F., whereas for the next 10 F. (down to F.) there would be only 0.12 psi/ F. pressure change for further reduction in temperature.-
Likewise, with refrigerant R-ll as the thermal bulb fill, the average change in pressure for bulb temperature decreases from 145 to 75 F. is 0.48 psi/ F., whereas the change in the next 10 F. below 75 F. is 0.26 psi/ F. Even if an operator should set the temperature control in his car as low as F he would affect the evaporator temperature by only about 05 F., which is an acceptable deviation.
While this invention has been described in connection with a certain specific embodiment thereof, it is to be understood that this is by way of illustration and not by way of limitation; and the scope of the appended claims should be construed as broadly as the prior art will permit.
What is claimed is:
1. An air conditioning system comprising a compressor, a condenser, a constant pressure expansion device, and an evaporator all connected to provide a closed, vapor cycle refrigeration circuit through which a refrigerant is circulated; means for circulating air within a cooled space through said evaporator; a control system including a thermal bulb-capillary unit for establishing a control signal which is a function of the temperature of air within said cooled space; means for applying said signal to said constant pressure expansion device to vary the control point thereof, and the corresponding evaporator pressure, whereby the evaporator pressure is established at a lower value when the temperature of the cooled space is below some predetermined value, said thermal bulb-capillary unit being filled with an expansible, halocarbon fluid having a pressure change in the range of 145 and F of between 75 and percent of the pressure change of said refrigerant in the range between 55 and 28 F, whereby the temperature range of air within the controlled space during normal operation matches the temperature-pressure characteristics of said refrigerant over the range of its operating pressure.
2. A system as defined in claim 1 wherein said expansible fluid is refrigerant R-ll3 and said system refrigerant is refrigerant R-12.
3. A system as defined in claim 1 wherein said expansible fluid is refrigerant R-ll and said system refrigerant is refrigerant R-22.
Claims (3)
1. An air conditioning system comprising a compressor, a condenser, a constant pressure expansion device, and an evaporator all connected to provide a closed, vapor cycle refrigeration circuit through which a refrigerant is circulated; means for circulating air within a cooled space through said evaporator; a control system including a thermal bulb-capillary unit for establishing a control signal which is a function of the temperature of air within said cooled space; means for applying said signal to said constant pressure expansion device to vary the control point thereof, and the corresponding evaporator pressure, whereby the evaporator pressure is established at a lower value when the temperature of the cooled space is below some predetermined value, said thermal bulb-capillary unit being filled with an expansible, halocarbon fluid having a pressure change in the range of 145* and 75* F of between 75 and 125 percent of the pressure change of said refrigerant in the range between 55* and 28* F, whereby the temperature range of air within the controlled space during normal operation matches the temperature-pressure characteristics of said refrigerant over the range of its operating pressure.
2. A system as defined in claim 1 wherein said expansible fluid is refrigerant R-113 and said system refrigerant is refrigerant R-12.
3. A system as definEd in claim 1 wherein said expansible fluid is refrigerant R-11 and said system refrigerant is refrigerant R-22.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US26963872A | 1972-07-07 | 1972-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3797266A true US3797266A (en) | 1974-03-19 |
Family
ID=23028070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00269638A Expired - Lifetime US3797266A (en) | 1972-07-07 | 1972-07-07 | Air conditioning control system |
Country Status (5)
Country | Link |
---|---|
US (1) | US3797266A (en) |
JP (2) | JPS4951654A (en) |
CA (1) | CA990087A (en) |
GB (1) | GB1429873A (en) |
IT (1) | IT990887B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3866430A (en) * | 1973-12-17 | 1975-02-18 | Robert C Webber | Method and apparatus for controlling refrigerant flow in cryogenic systems |
US7076964B2 (en) * | 2001-10-03 | 2006-07-18 | Denso Corporation | Super-critical refrigerant cycle system and water heater using the same |
FR2905633A1 (en) * | 2006-09-08 | 2008-03-14 | Valeo Systemes Thermiques | Air conditioning loop for motor vehicle, has coolant release unit allowing overheating of evaporator till specific temperature, where evaporator has air temperature gap between zones of evaporator comprised between specific degrees |
CN110953401A (en) * | 2019-12-17 | 2020-04-03 | 天津商业大学 | Thermal actuator |
US20210180842A1 (en) * | 2016-10-28 | 2021-06-17 | Mitsubishi Electric Corporation | Air conditioner |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1408744A (en) * | 1920-01-09 | 1922-03-07 | Keen Harold Perot | Thermostatically-operated ammonia expansion valve |
US1618815A (en) * | 1922-08-11 | 1927-02-22 | Cash A W Co | Refrigerating system and appliance |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5219433B2 (en) * | 1971-08-16 | 1977-05-27 |
-
1972
- 1972-07-07 US US00269638A patent/US3797266A/en not_active Expired - Lifetime
-
1973
- 1973-05-29 GB GB2539873A patent/GB1429873A/en not_active Expired
- 1973-06-04 CA CA173,095A patent/CA990087A/en not_active Expired
- 1973-07-03 IT IT26135/73A patent/IT990887B/en active
- 1973-07-07 JP JP48077006A patent/JPS4951654A/ja active Pending
-
1982
- 1982-03-09 JP JP1982033172U patent/JPS57172376U/ja active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1408744A (en) * | 1920-01-09 | 1922-03-07 | Keen Harold Perot | Thermostatically-operated ammonia expansion valve |
US1618815A (en) * | 1922-08-11 | 1927-02-22 | Cash A W Co | Refrigerating system and appliance |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3866430A (en) * | 1973-12-17 | 1975-02-18 | Robert C Webber | Method and apparatus for controlling refrigerant flow in cryogenic systems |
US7076964B2 (en) * | 2001-10-03 | 2006-07-18 | Denso Corporation | Super-critical refrigerant cycle system and water heater using the same |
FR2905633A1 (en) * | 2006-09-08 | 2008-03-14 | Valeo Systemes Thermiques | Air conditioning loop for motor vehicle, has coolant release unit allowing overheating of evaporator till specific temperature, where evaporator has air temperature gap between zones of evaporator comprised between specific degrees |
US20210180842A1 (en) * | 2016-10-28 | 2021-06-17 | Mitsubishi Electric Corporation | Air conditioner |
CN110953401A (en) * | 2019-12-17 | 2020-04-03 | 天津商业大学 | Thermal actuator |
Also Published As
Publication number | Publication date |
---|---|
JPS4951654A (en) | 1974-05-20 |
IT990887B (en) | 1975-07-10 |
JPS57172376U (en) | 1982-10-29 |
CA990087A (en) | 1976-06-01 |
GB1429873A (en) | 1976-03-31 |
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