Flowmeter fluid composition and temperature correction

Abstract: To correct the flow measurment of a gaseous or liquid fluid of interest for changes in the composition and temperature of that fluid in a flowmeter of the hot element type, an uncorrected flow value signal for the fluid of interest in relation to a hot element sensor output is corrected by applying a correction factor to the flow value signal based on certain unique physical parameters of the fluid of interest which nominally include thermal conductivity, k, specific heat, c p , and temperature, T.

Description: CROSS REFERENCE TO RELATED APPLICATION Reference is made to copending allowed application with Serial No. 07/285,897, with publication nr. US-A-4 961 348, filed December 16, 1988 and assigned to the common assignee of the present application. BACKGROUND OF THE INVENTION The present invention relates to fluid flow measurement and, more particularly, addresses overcoming inaccuracies in flow measurement. The invention provides a method for eliminating errors in mass and volumetric (and energy) flow rates measured for primarily gaseous fluid with respect to temperature changes in the gaseous fluids. Flow sensors that utilize a pair of thin film heat sensors and a thin film heater are known. An example of such a device is illustrated and described in U.S. Patent 4,501,144 to Higashi, et al. The thin film heat sensors may be arranged in a Wheatstone bridge so that the output of the bridge is representative of flow. These microanemometers or "microbridges" are produced using similar techniques to those used for producing integrated circuits and are thus quite inexpensive. As will be described in greater detail herein, such microanemometers or microbridges are capable of quite accurate flow sensing when directly exposed to a stream of fluid flowing past them. In this manner, such a sensor can be used to directly measure the flow velocity of the fluid. While such a sensing system can be used to approximately measure mass flow, a significant level of error has been experienced with respect to changes in composition of the measured fluid in prior devices using this system. Allowed patent application Serial No. 07/285,897 (publication nr. US-A- 4 961 348) entitled "Flow Meter Fluid Composition Correction" and assigned to the same assignee as the present application, describes in detail a method of correcting gaseous fluid flow measurement for changes in composition. Applying the composition corrections provided in application Serial No. 07/285,897 (publication nr. US-A- 4 961 348) will generally provide flow measurements accurate to within 10%. While this accuracy is sufficient for many nonprecision applications, there remain many precision applications that require a greater accuracy. Further investigation has resulted in the discovery of the algorithm of the present invention. The investigation showed that after applying the composition correction, there still remained an error due to the temperature difference of the gaseous fluid relative to the temperature of the calibration fluid. For illustration purposes, errors due to temperature of about 0.2% per °C were observed when the temperature of the gaseous fluid varied about ± 10° from the 23°C calibration temperature. This error of approximately 5% for a 10° temperature difference is unacceptable for many precision gas flow measurement applications. Thus a need exists for a method to correct gas flow measurements for variations in the temperature of the flowing gas from the temperature of the calibration gas. SUMMARY OF THE INVENTION The present invention solves these needs and problems in the field of hot element (wire or film) gas flow measurements by providing a method which can be used to correct the measured flow for changes in both the composition of the gas and the temperature of the gas relative to the calibration gas composition and temperature. The invention includes an equation for determining a gauge correction (C G ) which is applied to a measured gauge output (G) of the microbridge (MB) and an equation for determining a volumetric flow correction (C V ) which is applied to the measured volumetric flow (V). V = V(G) The C G and C V corrections are determined using preferred equations of the form: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 where: k e = thermal conductivity of the measured gas at the environment or calibration temperature and pressure k co = thermal conductivity of the calibration gas at the calibration gas at the calibration temperature and pressure c pe = specific heat of the measured gas at the environment or calibration temperature and pressure c pco = specific heat of the clalibration gas at the calibration temperature and pressure T e = absolute temperature of the measured gas environment T c = absolute temperature of the calibration gas n₁ through n₆ constants determined during a calibration process While the influence of pressure on k and c p is minor under most conditions, applications using high pressures i.e. over 100 psi (or over 7 atmospheric) would experience such influences, and would require the full power of equations (2) and (3) (1 psi = 6,89476·10⁻³MPa). After constants n₁ through n₆ have been determined in the calibration procedure, the equation for C G and C V may be used to determine the appropriate C G and C V for a gas flow measurement when the gas has a thermal conductivity k e , a specific heat c pe and a temperature T e . The use of the C G and C V correction is explained as follows. A measured volumetric flow, V, is determined according to: V = f(G C ) where G = microbridge output or gauge signal and G C = G/C G f(G C ) = polynomial function of G C The measured volumetric flow is then corrected to a corrected volumetric flow (V C ) according to: V C = V/C V The present invention includes the steps of a calibration process and of a user process. The calibration process begins by experimentally determining microbridge output values for known volumetric flows for several gases at several temperatures. Such data may be represented graphically as calibration curves, V = f(G). Each calibration curve is then compared to one specially selected or reference calibration curve. Correction factors C G for the microbridge gauge output signal and correction factors C V for the volumetric flows are experimentally determined in such a way as to achieve a best match between the reference calibration curve and all other curves. Values of thermal conductivity, specific heat and temperature for each of the gases at each of the temperatures are either theoretically determined from known thermodynamic data or measured. These values are normalized with respect to the reference condition. To complete the calibration process, the algorithm of the present invention is then derived to relate the experimentally determined correction factors C G and C V to the normalized values of k, c p and T. An algorithm is then available to a user for use to correct a gas flow measurement for composition and temperature changes. In the typical user process a gas flow measurement is being made. A measured microbridge output signal, G, is obtained. Using the thermal conductivity, specific heat and temperature also obtained with the microbridge during the gas flow measurement and the formula of the invention a gauge correction factor, C G is determined. A corrected gauge output value, G C , is determined by dividing the measured gauge output, G by the correction factor C G . The corrected gauge output, G C , is then used in an equation that calculates measured gas flow, V. This equation is of the form: V = a₀ + a₁G m 1 + a₂G m 2 + a₃G m 3 ... = V(G) where m i and a i = constants which represent the reference calibration curve After the measured volumetric flow, V, is determined, it must be corrected by a correction factor, C V . C V is determined by using the algorithm of the invention. The corrected volumetric flow, V C , is then determined by dividing V by C V . DESCRIPTION OF THE DRAWINGS Figure 1 is a diagrammatic representation of a method of composition and temperature compensation of gas flow measurements in accordance with the present invention. Figure 2 is a plot of the microbridge output signals as a function of volumetric flows for gas flow measurements using methane at temperatures at 9.2° C, 23° C and 35.3° C. Figure 3 is a plot of the error in percent of a microbridge flow measurement versus volumetric flow when the correction factors of the present invention are not used. The gas is methane at temperatures of 9.2° C, 23° C and 35.3° C. Figure 4 is a plot of the microbridge flow measurement error as a function of volumetric flow after the corrections of the present invention have been applied. The gas is methane at temperatures of 9.2° C, 23° C and 35.3° C. Figure 5 is a plot of the microbridge flow measurement error in percent as a function of volumetric flow with the corrections of the present invention applied. The gases are ethane at 9.2° C and 34.8° C, and nitrogen at 9.4° C and 35.2° C. Figure 6 is a plot of the microbridge flow measurement error only in percent as a function of volumetric flow for methane at 23° C, ethane at 22.5° C and nitrogen at 21.9° C. Figure 7 is a plot of the microbridge flow measurement error in percent as a function of the mass flow for methane at 9.2° C, 23° C and 35.3°, ethane at 22,5° C and nitrogen at 21.9° C. DESCRIPTION OF THE INVENTION Figure 1 illustrates one embodiment of applicant's invention of a method of temperature compensation for microbridge flow sensors. The system is depicted as a section of pipe, gas pipe, conduit or the like 12 through which a gaseous fluid 14 of interest is flowing. A microbridge or microanemometer sensor package for sensing flow through the system is shown generally at dynamic flow location 16. It includes an individual microbridge sensor for dynamic sensing of fluid flow. Semiconductor chip sensors or microbridges of the class described are treated in a more detailed manner in one or more of patents such as 4,478,076, 4,478,077, 4,501,144, 4,555,939, 4,651,564 and 4,683,159 all of common assignee with the present invention. To the extent necessary, additional details with respect to the microbridge sensors are incorporated by reference from these cited documents. Microbridge sensors typically require heated power control circuitry as identified in block 30. In addition, circuitry is needed for monitoring the difference in resistance of a resistor (R d ) located downstream of the heated elements and a resistor (R u ) located upstream of the heated elements as identified in block 30. In accordance with the present invention, a resistive temperature sensing element R is required for the purpose of measuring the temperature T g of the gas. Resistor R, is indicated in Figure 1 as being located at the dynamic flow location 16. Resistor R is a resistor element which may be located on the microbridge chip. In accordance with said US-A-4 961 348, a second microbridge location called a static microbridge location is indicated at 20. The method of determining the composition correction based on thermal conductivity, k, and specific heat, c p , identified in block 32 of Figure 1 is disclosed in the allowed application. An alternate location for resistor R is at static location 20. Figure 1 illustrates that information from block 32 on composition correction and information from block 30 including gas temperature information is provided to block 34. After calculations relating to flow and composition and temperature corrections, the flow at standard temperature and pressure is displayed as identified in block 36. Figure 2 is a plot of the measured microbridge output or gauge G versus the standard volume flow of methane at temperatures of 9.2° C, 23° C and 35.3° C. Ideally, the plots for the three temperatures would be identical. Actually, the error due to temperature is so small that it is not readily apparent from Figure 2. However, if only the error is plotted as in Figure 3, it is apparent that the error of the 9.3° C measurement and the 35.2° C measurement relative to the 23° C measurement are significantly greater than ± 1%. This invention teaches a method of correcting for the effects of temperature differences between the calibration gas at the time of the calibration and the test gas at the time of device use in the following overall compensation equation. V C = V(G/C G ) x (1/C V ) Where V = Volumetric flow rate as a function of G or G/C G G = the R d - R u microbridge output or gauge signal C G = correction of gauge output signal C V = correction of measured volumetric flow Equation 1a corrects for temperature effect errors by causing a y-axis shift of the calibration curve with the C G correction factor and for temperature effects by causing an x-axis shift of the calibration curve with the C V correction factor. A preferred complete temperature correction is of the following form: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 where: n₁ through n₆ = constants determined by the calibration procedure subscript e = during experiment or test subscript c = during calibration subscript o = for calibration gas (generally air or methane) k = thermal conductivity as measured by the composition correction MB c p = either specific heat in pressure independent units of, e.g. cal/(mol C) or its temperature derivative, also pressure independent T = absolute temperature It will be understood that other more general equations may be used to recognize the physics of the microbridge sensor structure. Particularly the thermal conductivity and specific heat of not only the gas, but also of solid substances of the sensor may be considered. Other more general forms of equation 2 are shown below: 1/C G = {(A₀ + k e )/(A₀ + k co )} n 1{(B₀ + c pe )/ (B₀ + c pco )} n 2{T e /T c } n 3 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...)/ (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...)/ (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 where constants A i , B i and m i are determined during the calibration procedure and allow for recognition of the thermal conductivity and specific heat of substances other than the gas. More general forms of equation 3 are shown below: 1/C V = {(C₀ + k e )/(C₀ + k co )} n 4{(D₀+ c pe )/ (D₀ + c pco )} n 5{T e /T c } n6 1/C V = {(C₀ + C₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n6 where constants C i , D i , q i and r i are determined during the calibration process and allow for recognition of the thermal conductivity and specific heat of substances other than the gas, and other heat transfer processes such as radioactive ones. The implementation of the correction provided by the present invention will now be explained. For illustration purposes we will use methane, ethane and nitrogen as the gases of interest and microbridge calibration data at approximately 5° C, 23° C and 35° C. It is understood that those are merely examples and the invention applies to other gases and calibration data at other temperatures. It is further understood that while this invention is described with respect to volumetric gas flow measurements, it is also applicable to mass flow measurements or energy flow measurements. For mass flow measurements, the uncorrected mass flow is designated M and the corrected mass flow is designated M C . For energy flow measurements, the uncorrected energy flow is designated E and the corrected energy flow is designated E C . For mass flow and energy flow measurements, the gauge correction (C G ) remains the same, but the mass correction is designated as C M and the energy correction is designated as C E . CALIBRATION PROCESS This process includes the following steps: 1) Determination of microbridge calibration curves for several gases of interest at several temperatures. Equations (2) and (3) for C G and C V , respectively, require for each the determination of 3 unknown exponents. Therefore, at least 3 calibration curves must be determined. The microbridge calibration curve is a plot of microbridge output values versus standard volume flows. 2) Selection of one gas, e.g. methane at 23° C as the reference operating condition and fitting the best possible calibration curve to the microbridge output values. This establishes a reference calibration curve for methane at 23° C, V(G). 3) Determining the correction factors C G and C V for other temperatures of methane and for other gases at other temperatures. This is accomplished by comparing the other calibration curves to the reference calibration curve and determining the gauge correction factors C G needed to cause the necessary y-axis shifts and the volumetric correction factors C V needed to cause the necessary x-axis shifts to allow the other calibration curves to conform to the chosen reference curve, i.e. the methane calibration curve at 23° C. The determination may be by visual comparison of the calibration curves or by using known data processing techniques. 4) Calculation from thermodynamic reference data or from measured data the values of k/k o , c p /c po and T/T o for the other gases and other temperatures. 5) Use the C G and C V values experimentally determined for other gases and temperatures and the normalized k, c p and T values calculated, and solve for the best n₁ through n₆ in equations (2) and (3). Equations (2) and (3) can then be used with the determined n₁ through n₆ to determine C G and C V for any gas at any temperature. Table 1 shows selected representative values obtained for methane, ethane and nitrogen when the described calibration process was used. Figure 4 illustrates the results of applying the temperature correction of the present invention to methane flow measurements at gas temperatures of 9.2° C, 23° C and 35.3° C. A very significant improvement over Figure 3 is noted with the error at flow above 30 liters per hour L/h being within about ± 1%. Figure 5 illustrates the applicability of applicant's invention to gases significantly different than methane such as ethane and nitrogen. Applicant has disclosed a method for correcting for the composition and temperature of a gas in order to achieve a corrected volumetric gas flow measurement. It will be apparent to those skilled in the art that this same methodology used to achieve volumetric flow corrections may be used to achieve mass flow corrections; values of n₄, n₅ and n₆ were found to need adjustment, while n₁-n₃ required none. Figure 7 illustrates the application of applicant's invention to mass flow measurements of methane, ethane and nitrogen. It will be noted that at flow rates above 100 g/h the error is generally less than ± 1%. It will further be appreciated to those skilled in the art that the same methodology used to achieve volumetric flow corrections may be used to achieve energy flow corrections for certain groups of like combustible fluids. In accordance with the foregoing description, applicant has developed a gas composition and gas temperature correction method that will provide very accurate gas flow measurements. Applicant's invention is applicable to volumetric flow measurements, mass flow measurements or energy flow measurements. Applicant's invention was accomplished by the recognition and solution of a long standing problem in gas flow measurements. Applicant's invention may readily be incorporated into those gas flow measurement applications requiring precision measurement.

Claims: A method for compensating the volumetric flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-related output signal, the method characterised by the steps of: (A) obtaining an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) obtaining the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) applying a gauge correction factor (C G ) to said sensor output G to obtain a corrected sensor output (G c ), said (C G ) being determined according to a known relationship among values of specific heat (C pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalised with respect to a reference gas; (D) obtaining an uncorrected volumetric flow value (V) for the fluid of interest in relation to the corrected sensor output, G c ; (E) applying a volumetric correction factor (C V ) to the flow value (V) to obtain the corrected volumetric flow value (V C ), C V being determined according to a known relationship, among values of specific heat (C pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalised with respect to the reference gas. A method according to Claim 1 characterised in that the gauge correction factor is determined according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co )} n1 {B₀ + c pe )/ (B₀ + c pco )} n 2 {T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...) / (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...)/ (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 and the volumetric correction factor (C V ) is determined according to a relationship selected from: C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C V = {(C₀ + k e )/(C₀ + k co )} n 4{D₀ + c pe )/ (D₀ + c pco )} n 5 {T e /T c } n 6 or 1/C V = {(C₀ + C₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , B i , m i , C i , D i , q i , and r i = constants determined by the calibration process, and k co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. A method according to Claim 1 or 2 characterised in that the gauge correction factor is determined according to the relationship: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 and the volumetric correction factor C V is determined according to the relationship: C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 and n₁ through n₆, respectively, are approximately equal to: -0.015331 -0.060124 0.387617 -0.85033 0.9845898 0.027236 A method for compensating the mass flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-related output signal, the method characterised by the steps of: (A) obtaining an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) obtaining the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) applying a gauge correction factor (C G ) to said sensor output (G) to obtain a corrected sensor output (G C ), said (C G ) being determined according to a known relationship among values of specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to a reference gas; (D) obtaining an uncorrected mass flow value (M) for the fluid of interest in relation to the corrected gauge output (G C ); (E) applying a mass correction factor (C M ) to the mass flow value to obtain the corrected mass flow value (M C ), C M being determined according to a known relationship, among values of specific heat (c pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to the reference gas. A method according to Claim 4 characterised in that the gauge correction factor is determined according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co )} n 1 {(B₀ + c pe )/ (B₀ + c pco )} n 2 {T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...)/ {(A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...) / (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 and the mass correction factor (C M ) is determined according to a relationship selected from: C M = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C M = (C₀ + k e )/(C₀ + k co ) }n 4{(D₀ + c pe ) / (D₀ + c pco )} n 5(T e /T c } n 6 or 1/C M = {(C₀ + C₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , B i , m i , c i , D i , q i , and r i = constants determined by the calibration process, and k co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. A method for compensating the energy flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-relating output signal, the method characterised by the steps of: (A) obtaining an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) obtaining the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) applying a gauge correction factor (C G ) to said sensor output (G) to obtain a corrected sensor output (G C ), said (C G ) being determined according to a known relationship among values of specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to a reference gas; (D) obtaining an uncorrected energy flow value (E) for the fluid of interest in relation to the corrected gauge output (G C ); (E) applying an energy correction factor (C E ) to the flow value to obtain the corrected energy flow value, (E C ), C E being determined according to a known relationship, among values of specific heat (c pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to the reference gas. A method according to Claim 6 characterised in that the gauge correction factor is determined according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co )} n 1{B₀ + c pe )/ (B₀ + c pco )} n 2{T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...)/ (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...)/ (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 and the energy correction factor (C E ) is determined according to a relationship selected from: C E = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C E = {(C₀ + k e )/(C₀ + k co )} n 4{(D₀ + c pe )/ (D₀ + c pco )} n 5{T e /T c } n 6 or 1/C E = {(C₀ + c₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , D i , m i , c i , D i , q i and r i = constants determined by the calibration process, and k co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. A method according to any preceding Claim, characterised in that c pe , k e and T e are determined by a second microbridge in relatively static communication with said fluid of interest. A method according to any preceding Claim characterised in that said C G determined in step (C) is determined according to a known relationship among variables selected from the group consisting of specific heat (c pe ), the differential of specific heat with respect to temperature (d cpe /dT), thermal conductivity (k e ), the differential of thermal conductivity with respect to temperature (dk e /dT), density, viscosity, speed of sound, optical absorption or diffusibility. A method according to any preceding Claim characterised in that said step (C) of determining C G is omitted and C G is set equal to unity. Apparatus for compensating the flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-related output signal, the apparatus characterised by operating according to the method of any of the preceding claims. Apparatus for compensating the volumetric flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-related output signal, the apparatus characterised by: (A) means to obtain an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) means to obtain the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) means to apply a gauge correction factor (C G ) to said output (G) to obtain a corrected sensor output (G c ), said (C G ) being determined according to a known relationship among values of specific heat (C pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalised with respect to a reference gas; (D) means to obtain an uncorrected volumetric flow value (V) for the fluid of interest in relation to the corrected sensor output, G c ; (E) means to apply a volumetric correction factor (C V ) to the flow value (V) to obtain the corrected volumetric flow value (V C ), C V being determined according to a known relationship, among values of specific heat (C pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalised with respect to the reference gas. Apparatus according to Claim 12 characterised by means to determine the gauge correction factor according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co )} n1 {B₀ + c pe )/ (B₀ + c pco )} n 2 {T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...) / (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...)/ (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 and the volumetric correction factor (C V ) is determined according to a relationship selected from: C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C V = {(C₀ + k e )/(C₀ + k co )} n 4{D₀ + c pe )/ (D₀ + c pco )} n 5 {T e /T c } n 6 or 1/C V = {(C₀ + C₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , B i , m i , C i , D i , q i , and r i = constants determined by the calibration process, and k co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. Apparatus according to Claim 12 or 13 characterised by means to determine the gauge correction factor according to the relationship: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 and the volumetric correction factor C V is determined according to the relationship: C V = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 and n₁ through n₆, respectively, are approximately equal to: -0.015331 -0.060124 0.387617 -0.85033 0.9845898 0.027236 Apparatus for compensating the mass flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-related output signal, the apparatus characterised by: (A) means to obtain an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) means to obtain the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) means to apply a gauge correction factor (C G ) to said sensor output (G) to obtain a corrected sensor output (G C ), said (C G ) being determined according to a known relationship among values of specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to a reference gas; (D) means to obtain an uncorrected mass flow value (M) for the fluid of interest in relation to the corrected gauge output (G C ); (E) means to apply a mass correction factor (C M ) to the mass flow value to obtain the corrected mass flow value (M C ), C M being determined according to a known relationship, among values of specific heat (c pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to the reference gas. Apparatus according to Claim 15 characterised by means to determine the gauge correction factor according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co ) } n 1{(B₀ + c pe )/ (B₀ + c pco )} n 2{T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...)/ (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...) / (B₀ + B₁c pco p 1 + ...)} n 2{T e /T c } n 3 and the mass correction factor (C M ) is determined according to a relationship selected from: C M = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C M = (C₀ + k e )/(C₀ + k co ) }n 4{(D₀ + c pe ) / (D₀ + c pco )} n 5{T e /T c } n 6 or 1/C M = {(C₀ + C₁k e q 1 + C₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , B i , m i , c i , D i , q i , and r i = constants determined by the calibration process, and K co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. Apparatus for compensating the energy flow measurement of a gaseous fluid of interest for changes in the composition, pressure and temperature of that fluid in a flowmeter having a first dynamic microbridge exposed to the flow and producing a flow-relating output signal, the apparatus characterised by: (A) means to obtaining an uncorrected dynamic microbridge sensor output (G) for the fluid of interest; (B) means to obtain the specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest; (C) means to apply a gauge correction factor (C G ) to said sensor output (G) to obtain a corrected sensor output (G C ), said (C G ) being determined according to a known relationship among values of specific heat (c pe ) thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to a reference gas; (D) means to obtain an uncorrected energy flow value (E) for the fluid of interest in relation to the corrected gauge output (G C ); (E) means to apply an energy correction factor (C E ) to the flow value to obtain the corrected energy flow value, (E C ), C E being determined according to a known relationship, among values of specific heat (c pe ), thermal conductivity (k e ) and temperature (T e ) of the fluid of interest normalized with respect to the reference gas. Apparatus according to Claim 17 characterised by means to determine the gauge correction factor according to a relationship selected from: C G = (k e /k co ) n1 (c pe /c pco ) n2 (T e /T c ) n3 or 1/C G = {(A₀ + k e )/(A₀ + k co )} n 1{(B₀ + c pe )/ (B₀ + C pco )} n 2{T e /T c } n 3 or 1/C G = {(A₀ + A₁k e m 1 + A₂k e m 2 + ...)/ (A₀ + A₁k co m 1 + A₂k co m 2 + ...)} n 1 {(B₀ + B₁c pe p 1 + B₂c pe p 2 + ...)/ (B₀ + B₁c pco p 1 + ...)} n 2(T e /T c } n 3 and the energy correction factor (C E ) is determined according to a relationship selected from: C E = (k e /k co ) n4 (c pe /c pco ) n5 (T e /T c ) n6 or 1/C E = {(C₀ + k e )/(C₀ + k co )} n 4{(D₀ + c pe )/ (D₀ + c pco )} n 5{T e /T c } n 6 or 1/C E = {(C₀ + c₁k e q 1 + c₂k e q 2 + ...)/ (C₀ + C₁k co q 1 + C₂k co q 2 + ...)} n 4 {(D₀ + D₁c pe r 1 + ...)/(D₀ + D₁c pco r 1 + ...)} n 5 {T e /T c } n 6 Where: n₁ through n₆, A i , B i , m i , c i , D i , q i , and r i = constants determined by the calibration process, and k co , c pco and T c = thermal conductivity, specific heat and temperature of the calibration gas. Apparatus according to any of Claims 12 to 18 characterised by a second microbridge, in relatively static communication with said fluid of interest, to determine c pe , k e and T e . Apparatus according to any of Claims 12 to 19 characterised in that the means to apply C G in step (C) comprises means to determine C G according to a known relationship among variables selected from the group consisting of specific heat (c pe ), the differential of specific heat with respect to temperature (dc pe /dT), thermal conductivity (k e ), the differential of thermal conductivity with respect to temperature (dk e /dT), density, viscosity, speed of sound, optical absorption or diffusibility.

Inventors: BONNE ULRICH, KUBISLAK DAVID, BONNE, ULRICH, KUBISLAK, DAVID
Applicants: HONEYWELL INC, HONEYWELL INC.
Application year: 1991
Main classification: G01F15
IPC codes: G01F1, G01F15