Method and apparatus for determining supercritical pressure in a heat exchanger

• US 20050066675A1
• Filed: 07/29/2004
• Published: 03/31/2005
• Est. Priority Date: 09/25/2003
• Status: Active Grant

• Current Assignee: Tecumseh Products Company
• Original Assignee: Tecumseh Products Company
• Inventors: Manole, Dan M., Frostick, Alicia
• Granted Patent: US 7,216,498 B2
• Time in Patent Office: Days
• US Class Current: 62/228.300
• CPC Class Codes: F25B 2309/061 with cycle highest pressure above the supercritical pressure
• CPC Class Codes: F25B 2500/19 Calculation of parameters
• CPC Class Codes: F25B 2600/17 by controlling the pressure of the condenser
• CPC Class Codes: F25B 2700/2102 at the outlet of the gas cooler
• CPC Class Codes: F25B 9/008 the refrigerant being carbon dioxide

Abstract

A method and apparatus to determine the pressure of a supercritical refrigerant within a heat exchanger of a transcritical vapor compression system. A plurality of measurements, e.g., temperature, are obtained at spaced locations on the heat exchanger and the location of the minimum temperature gradient, i.e., maximum specific heat value of the refrigerant, is determined (“the inflection point”). Obtaining the refrigerant temperature at the inflection point allows the refrigerant pressure to be determined. Alternatively, the temperature of the refrigerant at a second point can be determined together with the change in specific enthalpy between the inflection point and the second point to thereby determine the pressure of the refrigerant. The system can be regulated by controlling the location of the inflection point or by controlling the temperature difference of the refrigerant at the inflection point and a second point, e.g., the outlet of the heat exchanger.

Claims

1. A method of determining the supercritical pressure of a refrigerant in a heat exchanger in a transcritical vapor compression system, said method comprising:

obtaining a plurality of measurements representative of the temperature of the refrigerant at spaced locations on the heat exchanger;

identifying a first location based upon said plurality of measurements wherein said first location is the approximate location of the minimum temperature gradient of the refrigerant within the heat exchanger; and

determining the pressure of the refrigerant within the heat exchanger based upon the identification of said first location.

2. The method of claim 1 wherein determining the pressure of the refrigerant comprises determining the approximate temperature of the refrigerant at said first location and determining the pressure at which the refrigerant has a maximum specific heat at a temperature equivalent to the temperature of the refrigerant at the first location.

3. The method of claim 2 wherein determination of the pressure comprises the use of a look-up table.

4. The method of claim 1 wherein determination of the pressure comprises determining a value that is a function of the approximate change in specific enthalpy of the refrigerant between said first location and an outlet of said heat exchanger.

5. The method of claim 4 wherein determination of the pressure further comprises determining the approximate temperature of the refrigerant at said outlet.

6. The method of claim 1 wherein determining the pressure of the refrigerant comprises:

determining the approximate temperature of the refrigerant at a second location spaced from said first location;

determining a value that is a function of the approximate change in specific enthalpy of the refrigerant between said first location and said second location;

determining the pressure of the refrigerant at said first location based upon said approximate temperature of the refrigerant at said second location and said value that is a function of the approximate change in specific enthalpy between said first and second locations.

7. The method of claim 6 wherein the heat exchanger is cooled using ambient air and said second location is the heat exchanger outlet;

and wherein the temperature of the refrigerant at said second location is estimated to be equivalent to the temperature of the ambient air.

8. The method of claim 6 wherein the value that is a function of the approximate change in specific enthalpy is the approximate change in specific enthalpy between said first and second locations and determining the value includes using the following equation:

$\mathrm{\Delta <br><br>}<br><br>\text{\hspace{1em}<br><br>}<br><br>h_{\mathrm{INF}}=\frac{1}{\stackrel{.}{m}}<br><br>\frac{\partial <br><br>Q}{\partial <br><br>L}<br><br>{|}_{\mathrm{avg}}<br><br>\left(\mathrm{\Delta <br><br>}<br><br>\text{\hspace{1em}<br><br>}<br><br>L_{\mathrm{INF}}\right)$

wherein;

 

Δ

h_INF is the change in specific enthalpy;

{dot over (m)} is the mass flow rate of refrigerant through the heat exchanger;

$\frac{\partial <br><br>Q}{\partial <br><br>L}<br><br>{❘<br><br>}_{\mathrm{avg}}$

is the average heat transfer rate of the heat exchanger;

 

Δ

L_INF is the length between the first and second locations.

9. The method of claim 1 wherein the step of obtaining a plurality of measurements representative of the temperature of the refrigerant at spaced locations on the heat exchanger comprises obtaining temperature measurements on the exterior surface of the heat exchanger.

10. The method of claim 1 wherein the step of obtaining a plurality of measurements representative of the temperature of the refrigerant at spaced locations on the heat exchanger comprises obtaining strain measurements of the heat exchanger structure.

11. The method of claim 1 wherein the step of identifying said first location comprises comparing adjacent measurements of said plurality of measurements and selecting a pair of adjacent measurements that define the minimal difference between said adjacent measurements.

12. The method of claim 1 wherein the step of identifying said first location comprises defining a curve based upon said plurality of measurements and the position of said measurements on said heat exchanger.

13. A method of controlling the operation of a transcritical vapor compression system wherein the vapor compression system defines a closed loop circuit through which a refrigerant is circulated and including therein, in serial order, a compressor, a first heat exchanger, an expansion device and a second heat exchanger wherein the refrigerant is at a supercritical pressure within the first heat exchanger;

said method comprising;

identifying a first location on the first heat exchanger wherein said first location is the approximate location of the minimum temperature gradient of the refrigerant within the heat exchanger;

regulating the operation of the transcritical vapor compression system by controlling at least one characteristic of said first location.

14. The method of claim 13 wherein a first distance separates said first location from an outlet of said first heat exchanger and said at least one characteristic of said first location includes said first distance.

15. The method of claim 14 wherein said step of regulating the operation of the transcritical vapor compression system comprises maintaining said first distance between said first location and said outlet of said first heat exchanger at a relatively constant value.

16. The method of claim 13 wherein said at least one characteristic of said first location includes the temperature of refrigerant at said first location.

17. The method of claim 16 wherein said step of regulating the operation of the transcritical vapor compression system comprises maintaining a desired temperature difference between refrigerant at said first location and refrigerant at an outlet of said first heat exchanger.

18. The method of claim 17 wherein said first heat exchanger utilizes ambient air as a cooling medium and the temperature of refrigerant at said outlet of said first heat exchanger is assumed to be equivalent to the temperature of the ambient air.

19. The method of claim 17 wherein said desired temperature difference is non-variable.

20. A transcritical vapor compression system, said system comprising:

a closed loop circuit through which a refrigerant is circulated, said circuit including, in serial order, a compressor, a first heat exchanger, an expansion device and a second heat exchanger and wherein the refrigerant is at a supercritical pressure within said first heat exchanger;

a plurality of sensing devices mounted on said first heat exchanger at spaced locations each of said devices generating a signal representative of the temperature of the refrigerant within said first heat exchanger at a respective one of said spaced locations;

means for identifying a first location based upon said signals wherein said first location is the approximate location of the minimum temperature gradient of the refrigerant within said first heat exchanger; and

means for determining the pressure of the refrigerant within said first heat exchanger based upon the identification of said first location.

21. The transcritical vapor compression system of claim 20 wherein said means for determining the pressure of the refrigerant comprises measuring the temperature of the refrigerant at said first location and determining the pressure at which the refrigerant has a maximum specific heat at a temperature equivalent to the temperature of the refrigerant at said first location.

22. The transcritical vapor compression system of claim 20 wherein said means for determining the pressure of the refrigerant comprises determining the approximate temperature of the refrigerant at a second location spaced from said first location;

determining the approximate change in specific enthalpy of the refrigerant between said first location and said second location; and

determining the pressure of the refrigerant at said first location based upon said approximate temperature of the refrigerant at said second location and said approximate change in specific enthalpy between said first and second locations.

23. The transcritical vapor compression system of claim 20 wherein said plurality of sensing devices sense the temperature of said first heat exchanger at said spaced locations.

24. The transcritical vapor compression system of claim 20 wherein said plurality of sensing devices sense the strain of said first heat exchanger at said spaced locations.

25. The transcritical vapor compression system of claim 20 wherein said means for identifying said first location comprises comparing signals of adjacent ones of said plurality of measuring devices and selecting a pair of adjacent devices that define the minimal difference between said signals of said adjacent devices.

26. The transcritical vapor compression system of claim 20 wherein said means for identifying said first location comprises defining a curve based upon said plurality of signals and the respective positions of said sensing devices generating said signals.