Information
-
Patent Grant
-
6571566
-
Patent Number
6,571,566
-
Date Filed
Tuesday, April 2, 200222 years ago
-
Date Issued
Tuesday, June 3, 200321 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 062 149
- 062 126
- 062 127
- 062 129
- 062 208
- 062 209
- 062 125
-
International Classifications
-
Abstract
In accordance with the present invention, a method of determining refrigerant charge level in a space temperature conditioning system includes the steps of establishing a relationship between at least one selected system operating parameter and refrigerant charge level, independent of ambient temperature conditions; measuring the selected parameter(s) while the system is in operation; and using the established relationship and the measured parameter(s) to determine the refrigerant charge level. In one embodiment of the invention, both condenser subcooling and evaporator superheat parameters are measured and the predetermined relationship between charge level and each of these parameters is used to determine the actual refrigerant charge level.
Description
DESCRIPTION
1. Field of Invention
This invention relates generally to space temperature conditioning systems and in particular to a new and improved method of determining refrigerant charge level in a space temperature conditioning system.
2. Background Art
Space temperature conditioning systems of the type having a refrigerant as a heat transfer medium are well-known in the art. It is important that such systems have a proper charge of refrigerant in order to function properly. Various methods of determining refrigerant charge level are known in the art. Most of these prior art methods provide only a qualitative determination of whether the charge level is below or above acceptable limits or require inputs from multiple sensors, including ambient temperature and humidity sensors, in order to determine refrigerant charge level, which increases the cost and complexity of the system. Examples of such prior art refrigerant charge level determination methods are shown in U.S. Pat. Nos. 4,381,549; 4,677,830; 5,239,865; 5,987,903; and 6,101,820.
There is, therefore, a need for an improved method of determining refrigerant charge level in a space temperature conditioning system. There is also a need for a method of determining refrigerant charge level in a space temperature conditioning system that is both relatively inexpensive and reliable under a wide range of ambient temperature conditions.
SUMMARY OF INVENTION
In accordance with the present invention, a method for determining refrigerant charge level in a space temperature conditioning system is provided. The method is comprised of the following steps: (a) establishing a relationship between at least one system operating parameter and refrigerant charge level, independent of ambient temperature conditions; (b) operating the space temperature conditioning system; (c) measuring the operating parameter(s) while the system is in operation; and (d) determining refrigerant charge level based on the established relationship in response to the measuring step.
In accordance with one embodiment of the invention, the establishing step comprises: (i) operating the system; (ii) measuring the operating parameter(s) under a plurality of ambient temperature conditions for each of a plurality of known refrigerant charge levels; and (iii) correlating the measured values of the operating parameter(s) to establish a relationship between refrigerant charge level and the operating parameter(s), independent of the ambient temperature conditions.
In accordance with another embodiment of the invention, the system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser and the at least one system operating parameter includes refrigerant subcooling.
In accordance with yet another embodiment of the invention, the at least one operating parameter includes refrigerant subcooling and refrigerant superheat.
In accordance with still another embodiment of the invention, the at least one operating parameter includes refrigerant subcooling and refrigerant pressure at at least one selected location in the system.
In accordance with the preferred embodiment of the invention, the at least one system operating parameter includes refrigerant subcooling, refrigerant superheat, liquid refrigerant pressure on a discharge side of the condenser and vapor refrigerant pressure on a suction side of the compressor. These four parameters are measured while the system is operating at a relatively steady-state condition and the measured values of the parameters are used to determine refrigerant charge level based on the predetermined relationship between charge level and each of these parameters. A human-detectable indication is provided regarding whether the charge level is within acceptable limits and if it is not within acceptable limits, the amount of the undercharge or overcharge condition is indicated.
BRIEF DESCRIPTION OF DRAWINGS
FIG. 1
is a block diagram of a space temperature conditioning system embodying the present invention;
FIG. 2
is a graph of the relationship between the subcooling and superheat values at various known refrigerant charge levels and under different ambient temperature conditions for a space temperature conditioning system having a fixed expansion device;
FIG. 3
is a graph of predicted refrigerant charge level versus actual charge level, based on the data of
FIG. 2
, under different ambient temperature conditions;
FIG. 4
is a graph of subcooling versus refrigerant charge level under different ambient temperature conditions for a space temperature conditioning system having a thermal expansion valve;
FIG. 5
is a flow diagram of a refrigerant charge level determination algorithm in accordance with the present invention; and
FIG. 6
is a block diagram of an alternate embodiment of a space temperature conditioning system, according to the present invention.
BEST MODE FOR CARRYING OUT THE INVENTION
The best mode for carrying out the invention is described hereinbelow with reference to the accompanying drawings. The drawings are not necessarily to scale and in some instances proportions may have been exaggerated in order to more clearly depict certain features of the invention.
Referring to
FIG. 1
, a space temperature conditioning system
10
of the type normally installed in a residence or commercial building is comprised of a condenser
12
, an evaporator
14
, an expansion device
16
(which may be either a fixed expansion device, such as an orifice, or a controllable expansion device, such as a thermal expansion valve) and a compressor
18
. Compressor
18
is operative to circulate a vapor compression refrigerant between condenser
12
and evaporator
14
and to compress the vapor refrigerant before it enters condenser
12
. Condenser
12
, which is in heat exchange relationship with outdoor ambient air, is operative to substantially condense the vapor refrigerant. Evaporator
14
, which is in heat exchange relationship with the indoor air to be cooled, is operative to substantially evaporate the refrigerant. Expansion device
16
facilitates evaporation of the refrigerant by reducing the pressure thereof before the refrigerant enters evaporator
14
. The heat absorbed by the refrigerant during evaporation cools the air passing through evaporator
14
. The cooled air is supplied to an indoor conditioned space via an air supply duct (not shown). Although system
10
is described herein as a conventional air conditioning (cooling) system, one skilled in the art will recognize that
10
may also be configured as a heat pump system to provide both heating and cooling, by adding a reversing valve (not shown) so that the outdoor heat exchanger (condenser
12
in
FIG. 1
) functions as an evaporator in the heating mode and the indoor heat exchanger (evaporator
14
in
FIG. 1
) functions as a condenser in the heating mode.
In addition to the primary components of system
10
described hereinabove, condenser
12
has a fan
20
operatively associated therewith, which moves air (typically outdoor ambient air) across condenser
12
, as indicated by arrows
22
, to cool the refrigerant in condenser
12
and facilitate condensation thereof. Similarly, evaporator
14
has a fan
24
operatively associated therewith for moving indoor air to be cooled across evaporator
14
, as indicated by arrows
26
.
System
10
may also include various temperature and pressure sensors of the types normally used in space temperature conditioning systems. Temperature sensor
28
senses the temperature of the liquid refrigerant on a discharge side of condenser
12
between condenser
12
and expansion device
16
(said temperature being hereinafter referred to as the “liquid refrigerant temperature”). Pressure sensor
30
senses the pressure of the liquid refrigerant on the discharge side of condenser
12
between condenser
12
and expansion device
16
(said pressure being hereinafter referred to as the “liquid refrigerant pressure”). Temperature sensor
32
senses the temperature of the vapor refrigerant on a suction side of compressor
18
between evaporator
14
and compressor
18
(said temperature being hereinafter referred to as the “vapor refrigerant temperature”). Pressure sensor
34
senses the pressure of the vapor refrigerant on the suction side of compressor
18
between evaporator
14
and compressor
18
(said pressure being hereinafter referred to as the “vapor refrigerant pressure”). Sensors
28
and
30
are preferably located at a liquid service valve (not shown) between condenser
12
and expansion device
16
or, alternatively, at an inlet to expansion device
16
. Sensors
32
and
34
are preferably located at a suction service valve (not shown) between evaporator
14
and compressor
18
, but alternate locations are at an outlet from evaporator
14
or at an outlet from compressor
18
.
The temperature measurements from sensors
28
,
32
and the pressure measurements from sensors
30
,
34
are transmitted to an interface module
36
, which provides electrical power to sensors
28
,
30
,
32
,
34
and converts the analog data signals to digital signals for processing by a personal digital assistant (PDA)
38
. PDA
38
is programmed to perform the necessary calculations (including subcooling and superheat) to determine refrigerant charge level and to provide a human-detectable output to a service technician.
Referring now to
FIG. 2
, refrigerant charge level is a function of condenser subcooling (SC), evaporator superheat (SH), liquid refrigerant pressure (P
liqv
) and vapor refrigerant pressure (P
suct
). The subcooling value SC is determined by subtracting the liquid refrigerant temperature measured by sensor
28
(T
liqv
) from the liquid refrigerant saturation temperature (T
satl
) on the discharge side of condenser
12
, according to the following equation (1):
SC=T
satl
−T
liqv
(1)
The superheat value (SH) is determined by subtracting the vapor refrigerant saturation temperature (T
satv
) on the suction side of compressor
18
from the vapor refrigerant temperature (T
suct
) measured by temperature sensor
32
, according to the following equation (2):
SH=T
suct
−T
satv
(2)
Each of the liquid refrigerant saturation temperature (T
satl
) and the vapor refrigerant saturation temperature (T
satv
) is a function of the corresponding refrigerant pressure. For example, the saturation temperature for R
22
refrigerant may be determined according to the following equation (3):
In equation (3) T
sat
can be either the liquid refrigerant saturation temperature T
satl
or the vapor refrigerant saturation temperature T
satv
. For example, if T
sat
represents the liquid refrigerant saturation temperature T
satl
, then the pressure P in equation (3) corresponds to the liquid refrigerant pressure P
liqv
measured by sensor
30
. On the other hand, if T
sat
represents the vapor refrigerant saturation temperature T
satv
, then the pressure P in equation (3) corresponds to the vapor refrigerant pressure P
suct
measured by sensor
34
.
In accordance with the present invention, inputs from temperature sensors
28
,
32
and pressure sensors
30
,
34
are used to establish baseline data for determining refrigerant charge level. To establish this baseline data, system
10
is operated at various known refrigerant charge levels and under various known ambient temperature conditions, and the subcooling SC and superheat SH values are determined in accordance with equations (1), (2) and (3) and stored in PDA
38
.
FIG. 2
shows a relationship between subcooling and superheat plotted on a graph wherein the subcooling values are shown on the ordinate and the superheat values are shown on the abscissa.
FIG. 2
shows data plotted for three different refrigerant charge levels (85%, 100% and 115%) and for eleven different ambient temperature conditions for each charge level, so that each charge level has eleven different data points associated therewith. Charge level 100% represents the normal or desired charge level. The following Table I shows the eleven different ambient temperature conditions for which data was taken.
TABLE I
|
|
ID Amb
ID Amb
OD Amb
|
(DB) ° F.
(WB) ° F.
(DB) ° F.
|
|
65
51
70
|
65
51
95
|
65
51
115
|
80
62
95
|
80
67
70
|
80
67
95
|
80
67
115
|
80
71
95
|
95
84
70
|
95
84
95
|
95
84
115
|
|
The first column in Table I represents the indoor ambient dry bulb temperature, the middle column represents the indoor ambient wet bulb temperature and the right column represents the outdoor ambient dry bulb temperature. The data shown in
FIG. 2
is for an air conditioning system
10
in which expansion device
16
is a fixed orifice. The data in
FIG. 2
shows an approximately linear relationship between subcooling and superheat for three different refrigerant charge levels, as indicated by the three positive-sloped lines. Further, the three negative-sloped lines illustrate how the relationship between subcooling and superheat is affected by outdoor ambient temperature conditions. For example, when the outdoor ambient dry bulb temperature (OD Amb) temperature 70° F., the subcooling value is less for a given superheat value than when the outdoor ambient dry bulb temperature is 95° F. The subcooling value is even less for the same given superheat value when the outdoor ambient dry bulb temperature is 115° F. Therefore, by determining the relationship between subcooling and superheat under various ambient temperature conditions for a particular refrigerant charge level, the affects of both indoor and outdoor ambient temperature can be essentially eliminated in predicting the refrigerant charge level, which reduces the complexity and cost of the charge level determination method.
Referring also to
FIG. 3
, the predicted refrigerant charge level, as determined from the data of
FIG. 2
, is plotted against the known refrigerant charge level for three different ambient temperature conditions, to validate predicted charge level.
FIG. 3
shows that the predicted charge level is within 10% of the actual charge level over a range of charge levels from about 70% to 130%. The three ambient conditions for which data is plotted in
FIG. 3
correspond to (a) 65° F. indoor dry bulb temperature/51° F. indoor wet bulb temperature/70° F. outdoor dry bulb temperature; (2) 80° F. indoor dry bulb temperature/67° F. indoor wet bulb temperature/95° F. outdoor dry bulb temperature; and (3) 95° F. indoor dry bulb temperature/84° F. indoor wet bulb temperature/115° F. outdoor dry bulb temperature.
The baseline data shows that over a range of charge levels between 70% and 130% relative to normal charge level, refrigerant charge level (CL) is a function of subcooling, superheat, liquid refrigerant pressure and vapor refrigerant pressure. For example, the function can be represented by a first order linear approximation represented by the following equation (4), where a, b, c, d and e are coefficients based on the particular system
10
:
CL=a·SC+b·SH+c+d·P
liqv
+e·P
suct
(4)
PDA
38
is preferably equipped with a standard curve fitting program to determine the values of coefficients a, b, c, d and e, using the baseline data of FIG.
2
and the measured pressures (liquid refrigerant pressure and vapor refrigerant pressure).
Referring now to
FIG. 4
, if expansion device
16
is a thermal expansion valve, the superheat value usually is not needed to determine charge level so that charge level CL is a function of subcooling, liquid refrigerant pressure and vapor refrigerant pressure. For example, the function can be represented by a first order linear approximation as set forth in the following equation (5), where a, c, d and e are coefficients based on the particular system
10
:
CL=a·SC+c+d·P
liqv
+e·P
suct
(5)
FIG. 4
shows subcooling plotted against refrigerant charge level for a system
10
having a thermal expansion valve. The data was measured for five different charge levels (70%, 85%, 100%, 115% and 130%) under eleven different ambient temperature conditions (the same ambient temperature conditions shown in Table I). The data shows that there is an approximate linear relationship between charge level and subcooling, but that there is a greater deviation from the linear approximation at the higher charge levels. The curve fitting program determines the values of the coefficients a, c, d and e, using the baseline data of FIG.
4
and the measured pressures (liquid refrigerant pressure and vapor refrigerant pressure).
Referring now to
FIG. 5
, the refrigerant charge level determination algorithm in accordance with the present invention is shown. The algorithm will be described with reference to a system
10
having a fixed orifice expansion device. PDA
38
preferably includes a microcomputer (not shown), which is programmed to execute the algorithm and to determine the refrigerant charge level based on inputs from sensors
28
,
30
,
32
,
34
. Upon initiation of the charge determination algorithm (step
51
), sensors
28
,
30
,
32
,
34
are calibrated (step
53
). If the sensor calibration (step
55
) is not okay, a “sensor fault” condition is indicated, pursuant to step
57
. If the sensor calibration is okay, the service technician or other user is directed to install the sensors on the unit, pursuant to step
59
. The algorithm then prompts the service technician to input information on the air conditioning system, including the model number of the outdoor unit and the type of expansion device, pursuant to step
61
. The algorithm also directs the user to verify that the unit is operating (step
63
) and prompts the user to select “YES” when ready to proceed with the charge level determination test, pursuant to step
65
.
The program will then begin to record the values of liquid refrigerant temperature T
liqv,
liquid refrigerant pressure P
liqv
, vapor refrigerant temperature T
suct
and vapor refrigerant pressure P
suct
for a predetermined time period, using inputs from sensors
28
,
30
,
32
,
34
, respectively. The temperature and pressure measurements are taken and recorded (step
67
) and the subcooling and superheat values are computed according to step
69
until the system reaches steady-state operation, pursuant to steps
71
and
73
. When steady-state operation has been achieved, average values are calculated for the subcooling and superheat parameters, pursuant to step
75
. If the computed values are within predetermined acceptable limits for normal unit operation (step
77
), refrigerant charge level (CL) is predicted based on the computed values for subcooling (SC) and superheat (SH) and the inputs from pressure sensors
30
,
34
(P
liqv
, P
suct
) pursuant to step
81
. If the predicted charge level is within a predetermined desired range (e.g., between 98% and 102% of normal charge level), pursuant to step
83
, “charge OK, charging complete” is indicated to the user, pursuant to step
85
. However, if the predicted charge level is outside of the desired range (step
83
), the offset from normal charge level is computed and a charge level adjustment is indicated to the user, pursuant to step
87
. Therefore, the algorithm not only determines the refrigerant charge level, but also prompts a service technician or other user to add or subtract refrigerant charge to bring the charge level within acceptable limits.
Referring now to
FIG. 6
, an alternate embodiment of air conditioning system
10
is depicted, with only temperature sensors
28
,
90
,
92
being required to measure the data for determining refrigerant charge level. Sensor
90
measures refrigerant temperature within condenser
12
(T
cc
) and temperature sensor
92
measures the vapor refrigerant temperature on the discharge side of compressor
18
(T
dsc
). Subcooling (SC) is computed by subtracting the liquid refrigerant temperature T
liqv
measured by sensor
28
from the condenser refrigerant temperature (T
cc
) measured by sensor
90
, according to the following equation (6):
SC=T
cc
−T
liqv
(6)
The superheat value (SH) is determined by subtracting the condenser refrigerant temperature T
cc
from the compressor discharge refrigerant temperature (T
dsc
) measured by sensor
92
according to the following equation (7):
SH=T
dsc
−T
cc
(7)
In accordance with the alternate embodiment of
FIG. 6
, pressure sensors are not needed to establish the subcooling and superheat values. Further,
FIG. 6
shows a microcontroller
94
that receives inputs from sensors
28
,
90
,
92
and is programmed to compute refrigerant charge level based on inputs from these three sensors. Microcontroller
94
is also configured to receive an input from an indoor space thermostat
96
for controlling the temperature of the indoor space. Microcontroller
94
can be programmed to provide a visual or audible indication of an abnormal refrigerant charge level to alert an occupant of the space or service technician to the abnormal condition. Alternatively, microcontroller
94
can communicate with a personal digital assistant, either by hard-wire connection or wireless connection. In accordance with yet another embodiment of the invention, microcomputer
94
can communicate with a service technician's computer system via internet connection or modem connection, or by any other appropriate electronic or electromagnetic communication means.
The best mode for carrying out the invention has now been described in detail. Since changes in and additions to the above-described best mode may be made without departing from the nature, spirit or scope of the invention, the invention is not to be limited to the above-described best mode, but only by the appended claims and their proper equivalents.
Claims
- 1. In a space temperature conditioning system having a refrigerant as a heat transfer medium, a method of determining refrigerant charge level, comprising the steps of:establishing a relationship between at least one system operating parameter and refrigerant charge level, independent of ambient temperature conditions; operating the space temperature conditioning system; measuring said at least one system operating parameter while the system is in operation; and determining refrigerant charge level based on said relationship in response to said measuring.
- 2. The method of claim 1 wherein said establishing comprises:operating the system; measuring said at least one system operating parameter under a plurality of ambient temperature conditions for each of a plurality of known refrigerant charge levels; and correlating the measured values of said at least one system operating parameter to establish a relationship between refrigerant charge level and said at least one system operating parameter, independent of the ambient temperature conditions.
- 3. The method of claim 2 further including comparing a determined refrigerant charge level to actual charge level for each of a plurality of ambient temperature conditions, to validate said correlating.
- 4. The method of claim 1 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said at least one said system operating parameter including a refrigerant subcooling parameter.
- 5. The method of claim 1 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said at least one said system operating parameter including a refrigerant subcooling parameter and a refrigerant superheat parameter.
- 6. The method of claim 1 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said at least one said system operating parameter including a refrigerant subcooling parameter, a refrigerant superheat parameter and a refrigerant pressure parameter.
- 7. The method of claim 1 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said at least one said system operating parameter including a refrigerant subcooling parameter and a refrigerant pressure parameter.
- 8. The method of claim 1 wherein said operating comprises the step of operating the system at a relatively steady-state condition.
- 9. In a space temperature conditioning system having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, a method of determining refrigerant charge level, comprising the steps of:establishing a relationship between refrigerant charge level and a plurality of system operating parameters for a plurality of known refrigerant charge levels, independent of ambient temperature conditions; operating the system; measuring said plurality of system operating parameters while the system is in operation; determining the refrigerant charge level based on said relationship in response to said measuring.
- 10. The method of claim 9 wherein said establishing comprises:operating the system; measuring said plurality of system operating parameters under a plurality of ambient temperature conditions for each of a plurality of known refrigerant charge levels; and correlating the measured values of said plurality of system operating parameters to establish a relationship between refrigerant charge level and said plurality of system operating parameters, independent of the ambient temperature conditions.
- 11. The method of claim 10 further including comparing a determined refrigerant charge level to actual charge level for each of a plurality of ambient temperature conditions, to validate said correlating.
- 12. The method of claim 9 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said plurality of system operating parameters including refrigerant subcooling and refrigerant superheat.
- 13. The method of claim 12 wherein said plurality of system operating parameters further include refrigerant pressure at a selected location in the system.
- 14. The method of claim 9 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said plurality of system operating parameters including refrigerant subcooling and refrigerant pressure at a selected location in the system.
- 15. The method of claim 9 wherein said system is a space temperature conditioning system of the type having a condenser, an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, said plurality of system operating parameters including refrigerant subcooling, refrigerant pressure at a first selected location in the system and refrigerant pressure at a second selected location in the system.
- 16. The method of claim 15 wherein said plurality of system operating parameters further include refrigerant superheat.
- 17. The method of claim 9 wherein said operating comprises operating the system at a relatively steady-state condition.
- 18. In a space temperature conditioning system having a condenser, and an evaporator and a compressor for circulating a vapor compression refrigerant between the evaporator and the condenser, a method of determining refrigerant charge level, comprising the steps of:establishing a relationship between refrigerant charge level and at least first, second and third system operating parameters for a plurality of known refrigerant charge levels, independent of ambient temperature conditions, said first system operating parameter corresponding to refrigerant subcooling, said second system operating parameter corresponding to refrigerant pressure at a selected location on a discharge side of the condenser, said third system operating parameter corresponding to refrigerant pressure at a selected location on a suction side of the compressor; operating the system to cool air passing through the evaporator; measuring said first, second and third system operating parameters while the system is in operation; and determining refrigerant charge level based on said relationship in response to said measuring.
- 19. The method of claim 18 wherein said establishing further includes establishing a relationship between refrigerant charge level and a fourth system operating parameter for a plurality of known refrigerant charge levels, independent of ambient temperature conditions, said fourth system operating parameter corresponding to refrigerant superheat.
- 20. The method of claim 19 wherein said establishing comprises:operating system to cool air passing through the evaporator; measuring said first, second, third and fourth system operating parameters under a plurality of ambient temperature conditions for each of said plurality of known refrigerant charge levels; and correlating the measured values of said first, second, third and fourth system operating parameters to establish a relationship between refrigerant charge level and said first, second, third and fourth system operating parameters, independent of the ambient temperature conditions.
US Referenced Citations (16)