The present invention generally relates to a method and system for accurately measuring carbon dioxide gas concentration. More specifically, the present invention relates to measuring the thermal conductivity of carbon dioxide gas in a substantially saturated or non-saturated gaseous environment, e.g., a cell-culture incubator, and compensating for relative humidity and temperature variations.
Measurement and control of carbon dioxide gas concentration in laboratory cell-culture incubators is most commonly accomplished by means of a thermal conductivity detection system. The thermal conductivity cell, or detector, is a differential thermometer, set up as an electronic bridge circuit that is balanced to be equal, with two thermistors in a common block or metallic housing to add thermal stability. (See U.S. Pat. No. 3,929,584 (Mansfield)). This cell is most commonly placed in a working environment that is isolated from the surrounding area, but is not restricted to its placement.
Moreover; U.S. Pat. No. 5,418,131 (Butts) shows a unique system for detecting or measuring CO2 gas concentration in an enclosed environment using a thermal conductivity sensor.
In some instances, a detector cell is located in an air flow path external from the working environment, but contiguous with the environment. One thermistor sensor is enclosed in the block/housing and detects chamber temperature only. The other thermistor sensor is exposed to the chamber environment. The measured difference between the two thermistor sensors is the thermal conductivity (density) of the atmosphere, or its ability, when moved at an even rate, to remove the small amount of heat from the exposed sensor. If all other factors remain constant and only the carbon dioxide content is varied, the “TC” cell output (when properly calibrated) will indicate changes in carbon dioxide gas concentration. Unfortunately, the TC cell is affected by barometric pressure, temperature, humidity and the velocity of air flow past the sensor cell. These variables are controlled or compensated for with the use of electronic zeroing circuitry to compensate for changes in temperature and relative humidity levels. In monitoring the effects of carbon dioxide gas in an atmosphere, absolute humidity must be held constant so any change in thermal conductivity is caused only by a change in the carbon dioxide gas concentration. Under the worst circumstances, a change in absolute humidity can cause such a significant change in thermal conductivity that the controller can shift the carbon dioxide gas content by as much as 4%.
To maintain a stable humidity level in laboratory incubators, a pan of water is placed within the working environment and its temperature allowed to equilibrate. The incubator, working atmosphere, must reach a point of near saturation in order to maintain an absolute humidity level that will not change with ambient conditions.
For the laboratory investigator that does not want to operate their incubator in a saturated condition, but does want accurate carbon dioxide gas control, the drifting of the thermal conductivity sensor's reference becomes a problem with regard to the accuracy of the carbon dioxide gas concentration in the incubator. That is, as the absolute humidity changes, so does the reference base of the carbon dioxide gas sensor.
When operating a dry incubator, as opposed to a saturated one, ambient humidity fluctuations will effect carbon dioxide gas zero calibration. Since the fluctuations possible in extreme ambient temperature changes have less effect on the total absolute humidity, the carbon dioxide gas calibration can be affected as much as 1.5% in the worst case which does not represent as severe a problem, but does create an error that could prove critical in the pH level of the cell media being cultured within the incubator working chamber.
The two factors that contribute to inaccuracies in a thermal conductivity gas control system, i.e., relative humidity and dry-bulb temperature, are taken into consideration in the measurement system of the present invention to arrive at the absolute humidity and temperature compensated carbon dioxide gas concentration.
The present invention provides a method to compensate for humidity and temperature in a controlled environment.
The present invention also provides a method of quantifying an absolute humidity sensor for three dependent variables and isolating the desired variable e.g., CO2.
The present invention includes a method of thermal conductivity measurement of CO2 with relative humidity and temperature compensation as herein disclosed. In accordance with one embodiment of the present invention, this method ensures accurate readings without being sensitive to any specific hardware or sensors being utilized.
The present invention provides a humidity and temperature compensated carbon dioxide gas detection and control system in a controlled atmosphere environment, having a humidity sensor, a temperature sensor and a carbon dioxide adjustment control circuit.
Further, the present invention provides a method of humidity and temperature compensated carbon dioxide gas detection and control system in a controlled atmosphere environment, which includes sensing humidity level outputs, sensing thermal conductivity level outputs, comparing the humidity levels and the thermal conductivity levels to find carbon dioxide gas levels and adjusting the carbon dioxide gas levels.
The present invention provides a humidity and temperature compensated carbon dioxide gas detection and control system in a controlled atmosphere environment, having means for sensing humidity level outputs, means for sensing thermal conductivity level outputs, means for comparing the humidity levels and the thermal conductivity levels to find carbon dioxide gas levels and means for adjusting the carbon dioxide gas levels.
There has thus been outlined, rather broadly, the more important features of the invention in order that the detailed description thereof that follows may be better understood, and in order that the present contribution to the art may be better appreciated. There are, of course, additional features of the invention that will be described below and which will form the subject matter of the claims appended hereto.
In this respect, before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein, as well as the abstract, are for the purpose of description and should not be regarded as limiting.
As such, those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
The present invention provides a compensation method and system employing a quantification of the absolute humidity sensor 20 (e.g., the Mitsubishi HS-6 absolute humidity sensor) to measure the carbon dioxide response for each of the three dependent variables under consideration namely, absolute humidity (D), temperature (T) 32, and carbon dioxide gas 34 in an incubator or other controlled environment.
Referring to
Vm(D,T)=(aD2+bD)(cT2+dT+e)f
with,
Thus if D and T are known, then Vm(D, T) can be obtained, i.e. the voltage response of the absolute humidity sensor for measuring carbon dioxide to absolute humidity and temperature.
Referring to
D(T)=4E-06T4+2E-05T3+0.0158T+0.2313T+5.5676
Again, referring to
Referring to
Referring to
The many features and advantages of the invention are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirit and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.
This application claims priority to the provisional patent application 60/347,237 filed Jan. 14, 2002, the disclosure of which is incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
3929584 | Mansfield | Dec 1975 | A |
5025619 | Cannon | Jun 1991 | A |
5418131 | Butts | May 1995 | A |
5540077 | Benning et al. | Jul 1996 | A |
5897836 | Martell et al. | Apr 1999 | A |
6010243 | Hessler et al. | Jan 2000 | A |
6503751 | Hugh | Jan 2003 | B2 |
Number | Date | Country | |
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20030131653 A1 | Jul 2003 | US |
Number | Date | Country | |
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60347237 | Jan 2002 | US |