GAS ENERGY MEASURING METHOD AND CORRESPONDING DEVICE

Description

TECHNICAL FIELD

[0001] The present invention relates to gas energy measurements, and more particularly, to an improved vibratory meter and method for measuring gas energy.BACKGROUND OF THE INVENTION

[0002] The usage and combustion of hydrogen rich gases such as fuel gas, tail gas, and bio-gas is heavily dependent upon the energy content of the gas itself. The energy content of a gas may be described as how much energy can be generated upon combustion. Energy, often measured in British thermal units (BTU), is thus a critical measurement for gas suppliers, transporters and users alike. A BTU is defined as the amount of energy needed to cool or heat one pound of water by one degree Fahrenheit. Another commonly used parameter associated with the energy generated by the combustion of a gas (called calorific value or CV) is that of Wobbe Index (WI) or Wobbe number. This is an important parameter that indicates how easily a gas will burn, and not simply just how much energy can be generated by its combustion. The WI is employed because it is a reliable indicator of the interchangeability of fuel gases such as natural gas, liquefied petroleum gas (LPG), and other hydrocarbons, for example. The Wobbe index may be described by equation (1): WI = CV SG Where: WI is the Wobbe Index; CV is the calorific value; and SG is the specific gravity.

[0003] The calorific value, CV, is often defined by equation (2): CV = 0.0235 + 0.00197 − 0.000329 ⋅ Mco 2 + 0.000217 ⋅ Mn 2 G S Where: Mco 2 =% CO 2 content; and Mn 2 =% N 2 content.

[0004] The Wobbe Index is often used to compare the combustion energy output of different composition fuel gases for a given application. For example, should fuels have identical Wobbe Indices, then for a given pressure and process settings on a particular apparatus, the energy output will be the same between the fuels. This is particularly important in processes or apparatuses where gases may be substituted for each other or where gas composition does not remain constant.

[0005] For hydrogen rich gases, there are two common types of instrumentation that are used to calculate / measure CV or WI - Gas Chromatographs (GC's) and Wobbe Index meters. GCs are relatively slow, as they separate gas into constituent components and then calculate gas parameters by separately analyzing the properties of the individual mixture gases. Wobbe Index meters typically combust a gas to measure the energy or calculate CV or WI. However, for non-combustion Wobbe Index meters, a major problem in obtaining accurate measurements relates to the accounting for the percent of inert gases and percentage of Hydrogen (H 2 ) present in the gas mixture. Inert gases drastically change the energy content generated by the overall mixture-as does Hydrogen. The inert gases most often encountered in hydrogen-rich gas mixtures and fuel gases are Carbon Dioxide (CO 2 ), Carbon Monoxide (CO), and Nitrogen (N 2 ). Of these, CO 2 and CO are relatively easy to measure, as near infra-red (NIR) monitors are available for this purpose. Nitrogen measurements, however, remain cumbersome to measure, and typically require a GC.

[0006] When it comes to measuring hydrogen content, a number of thermal conductivity analyzers are available that can directly output this variable, so measurement of this parameter is relatively simple. In most Hydrogen-rich and fuel gas mixtures, Nitrogen content is a relatively small percentage of the mixture, and generally relatively constant. Therefore, a constant value of N 2 may often be employed in the determination of accurate energy measurement values. For CO, CO 2 and H 2, this is definitely not the case. Wild swings in concentration of these components is typical, often occurring over a period of mere seconds. This is a primary reason that GC technology fails to meet the market need for fast response gas energy and Wobbe Index (WI) measurement.

[0007] Gas Chromatographs are widely used in the gas measurement industry, and while they provide an accurate output of the full gas composition of the gas mixture under measurement, they have a number of significant limitations. First, GCs exhibit an extremely high cost of ownership. Systems and parts are expensive to buy, and a number of moving parts require significant and frequent servicing. Second, GCs require regular calibration. Third, the calibration gases needed for the calibration process must be generated, which is timely and expensive. Fourth, skilled and trained operators are required for GC operation, which increases operating costs. Fifth, the response time is typically extremely slow, with outputs typically updated about every 7 minutes.

[0008] As noted above, Wobbe Index meters or calorimeters can be used for fuel gas or H 2 rich gas mixtures, yet they also exhibit a number of limitations. First, there is a high cost of purchase and ownership. Second, due to the combustion often needed for measurements, such units must often be installed in non-hazardous areas. Third, these meters also require extensive utilities, such as high current electrical inputs and compressed air-gas bottle supplies. They are therefore expensive to install and operate. Along these lines, the waste gas exhausted by these units is typically around the order 800°C, which is potentially dangerous and expensive to mitigate in hazardous environments, such as those found in oil refineries, for example.

[0009] An alternative method and apparatus for calculating CV, WI, density, base density, SG, etc. is needed. A method and apparatus for these calculations that updates quickly is needed. Additionally, a method and apparatus is needed that minimizes safety risks. A non-combustive, fast-response method and apparatus is provided to address these and other issues, and an advance in the art is achieved. Embodiments disclosed provide an alternative method to determine gas energy and WI in a hydrogen-rich gas mixture. This method and apparatus is especially well-suited for a gas composition that is not known and / or where existing standards that relate gas specific gravity to energy content are not applicable.

[0010] Relevant prior art concerning a method for determining an energy content of a natural gas using a gas density meter is disclosed in J. Agar et al, "The Use Of Density Meters And Microprocessors For Energy Measurement And Control", in "First Industrial Energy Technology Conference", January 1979, pages 503-516, also available at http: / / hdl.handle.net / 1969.1 / 93842.SUMMARY OF THE INVENTION

[0011] A method is provided for determining an energy content of a fuel gas, tail gas, or bio-gas mixture using a vibratory gas density meter according to claim 1.

[0012] A system is provided for measuring gas energy using a vibratory gas density meter according to claim 3.ASPECTS

[0013] According to the invention, a method for determining an energy content of a gas mixture using a gas density meter comprises: providing a vibratory gas density meter; providing meter electronics with the gas density meter configured to communicate with at least one external input, wherein the external input comprises a percent H 2 value of the gas mixture, a percent CO value of the gas mixture, a percent CO2 value of the gas mixture, and a percent N2 value of the gas mixture; measuring a density of the gas mixture; measuring a specific gravity of the gas mixture; and deriving a calorific value of the gas mixture using the measured specific gravity and a plurality of constant values; wherein the calorific value (CV) is calculated, in Kj, according to an equation comprising: CV = A + (B · percent H 2 ) + (C · percent CO) + (D · percent CO 2 ) + (E · percent N 2 ) + (F · SG), where A-F comprise the constant values, and SG comprises the specific gravity; and calculating the specific gravity from the measured density.

[0014] Preferably, a Wobbe Index value of the gas mixture is calculated.

[0015] According to the invention, A is between about 144.8 and 150.8, wherein B is between about -2.5 and -2.6, wherein C is between about -12.15 and -12.65, wherein D is between about -47.7 and -49.65, wherein E is between about -24.68 and -25.69, and wherein F is between about 1528.7 and 1591.1.

[0016] Preferably, A is about 147.8458, B is about -2.55807, C is about -12.3963, D is about -48.685065, E is about -25.18546, and F is about 1559.94255.

[0017] Preferably, the external input comprises a percent H 2 value of the gas mixture.

[0018] Preferably, the external input comprises a percent CO value of the gas mixture.

[0019] Preferably, the external input comprises a percent CO 2 value of the gas mixture.

[0020] Preferably, the external input comprises a percent N 2 value of the gas mixture.

[0021] According to the invention, a system for measuring gas energy comprises: a vibratory gas density meter configured to calculate a specific gravity of a gas mixture; a communication line configured to connect to an external input; meter electronics for operating the vibratory gas density meter in communication with the communication line, wherein the meter electronics is configured to measure a density of the gas mixture and derive a calorific value of the gas mixture using the derived specific gravity and a plurality of constant values; providing meter electronics with at least one external input, wherein the external input comprises a percent H 2 value of the gas mixture, a percent CO value of the gas mixture, a percent CO2 value of the gas mixture, and a percent N2 value of the gas mixture; wherein the calorific value (CV) is calculated, in Kj, according to an equation comprising: CV = A + (B · percent H 2 ) + (C · percent CO) + (D · percent CO 2 ) + (E · percent N 2 ) + (F · SG), where A-F comprise the constant values, and SG comprises the specific gravity; and wherein the specific gravity is calculated from the measured density.

[0022] Preferably, the external input comprises at least one of a near infrared meter, a thermal conductivity meter, and a gas chromatograph.

[0023] Preferably, the meter electronics is configured to calculate a Wobbe Index value of the gas mixture.

[0024] According to the invention, A is between about 144.8 and 150.8, wherein B is between about -2.5 and -2.6, wherein C is between about -12.15 and -12.65, wherein D is between about -47.7 and -49.65, wherein E is between about -24.68 and -25.69, and wherein F is between about 1528.7 and 1591.1.

[0025] Preferably, A is about 147.8458, B is about -2.55807, C is about -12.3963, D is about -48.685065, E is about -25.18546, and F is about 1559.94255.BRIEF DESCRIPTION OF THE DRAWINGS

[0026] The same reference number represents the same element on all drawings. The drawings are not necessarily to scale. FIG. 1 illustrates a system for measuring gas energy according to an embodiment; and FIG. 2 illustrates meter electronics according to an embodiment. DETAILED DESCRIPTION OF THE INVENTION

[0027] FIGS. 1, 2, and the following description depict specific examples to teach those skilled in the art how to make and use the best mode of the invention. For the purpose of teaching inventive principles, some conventional aspects have been simplified or omitted. Those skilled in the art will appreciate variations from these examples that fall within the scope of the invention. Those skilled in the art will appreciate that the features described below can be combined in various ways to form multiple variations of the invention. As a result, the invention is not limited to the specific examples described below, but only by the claims.

[0028] FIG. 1 illustrates a system 100 for measuring gas energy according to an embodiment. A density meter 101 is provided to measure the specific gravity of a gas. To measure the specific gravity of a gas, the density meter 101 utilizes a resonating element 102 surrounded by a constant volume reference chamber 104 filled with a fixed quantity of gas. A separator diaphragm 106 inside the reference chamber ensures that the pressure of a sample gas, delivered by gas line 108, in the density meter 101 is equal to that of the reference gas by controlling a pressure control valve 110.

[0029] The density meter's 101 resonating element 102 is located at least partially within a housing 103. The housing 103 or the resonating element 102 may include flanges or other members for operatively coupling the density meter to a pipeline or similar gas delivering device in a gas-tight manner. Often, the resonating element 102 is cantilever mounted to the housing at one end of the housing, with the opposite end of the resonating element 102 free to vibrate. The resonating element 102 may, in an embodiment, define a plurality of gas apertures that allow gas to enter the density meter and flow between the housing and the resonating element 102. Therefore, the gas contacts the inside as well as the outside surfaces of the resonating element 102. This allows a greater surface area of the resonating element 102 to be exposed to gas, and therefore provide more accurate measurements. In other examples, apertures may be provided in the housing, and apertures in the resonating element 102 may not be required.

[0030] The resonating element 102 may be vibrated at or near to a natural (i.e., resonant) frequency. By measuring a resonant frequency of the member in a presence of a gas, the density of the gas may be determined.

[0031] A driver 105 and a vibration sensor 107 are typically positioned on a spool body positioned proximate the resonating element 102. The driver 105 receives a drive signal from a meter electronics 112 and vibrates the resonating element 102 at or near a resonant frequency. The vibration sensor 107 detects the vibration of the resonating element 102 and sends the vibration information to the meter electronics 112 for processing. The meter electronics 112 determines the resonant frequency of the resonating element 102 in combination with the gas under test, and generates a density measurement from the measured resonant frequency.

[0032] The specific gravity of a gas is the ratio of its molecular weight (M) to the molecular weight of standard dry air. In an embodiment, the density meter 101 yields a frequency output that is proportional to the gas specific gravity, and may also generate a gas molecular weight (M).

[0033] The most relevant parameters when measuring hydrogen-rich or fuel gases are: a. specific gravity (SG) b. temperature (T) c. pressure (P) d. molecular weight (M) e. Percent inert gas (e.g. % N, % CO 2 ) f. Calorific value / BTU (CV) g. Wobbe Index (WI) h. relative density (ρ rel )

[0034] An embodiment of the system 100 provides measurement and / or calculation of at least one of the parameters above, without the need for combusting a gas or relying on a GC. In an embodiment, the density meter 101 is calibrated to output SG - using the molecular weight of a plurality of calibrations gases. For example, without limitation, three calibration gases as the low, medium and high range points are contemplated. Calibrations with more or less than three gases is also contemplated.

[0035] In the present invention, the system accepts more than one external input 116. The external input 116 comprises measurements of, inter alia, percent CO 2 , percent CO, percent H 2 , and percent N 2 . This data is provided to meter electronics 112 via a communication line 114. In conjunction with separate external inputs 116 from analyzers such as, for example without limitation, thermal conductivity meters (that provide real time percent H 2 value), near infrared (NIR) meters (that provide real time percent CO and / or percent CO 2 values), and gas chromatographs (that provide percent N 2 values), the system 100 may produce an extremely accurate measurement of calorific value, BTU and Wobbe Index, and may effectively do so in roughly real-time. By providing a multi-meter / multi-technology approach, the system 100 produces an inherently fast response, yet does not require a known full composition of the gas being measured. Additionally, the need for gas combustion is obviated, which is otherwise the typical approach employed by calorimeters and Wobbe Index meters.

[0036] This multi-technology input embodiment relies upon an accurate fast response measurement of specific gravity that the density meter 101 provides. An embodiment has been derived by analyzing over 30 different hydrogen gas and fuel gas mixtures-all of which are outside the scope of standards where specific gravity is directly related to the energy content of the gas, such as the AGA5 standard, for example without limitation. The relationship below between energy content, specific gravity and percent N 2 , percent CO, percent CO 2 , and percent H 2 is derived according to an embodiment, as described by equation (3): CV = A + B ⋅ % H 2 + C ⋅ %CO + D ⋅ % CO 2 + E ⋅ % N 2 + F ⋅ SG Where A-F are constants: A = 147.8458 B = -2.55807 C = -12.3963 D = -48.685065 E = -25.18546 F = 1559.94255

[0037] Note that from the above coefficients, the greatest sensitivity to measurement is that of SG, hence an accurate measurement of SG, derived from the density meter 101 is critical. Using this equation, typical measurement errors are less than ±0.25%, with maximum observed deviations less than ±0.9%. It should be noted that constants A-F may be altered by as much as ±5%.

[0038] In an embodiment, once CV is determined, the Wobbe Index is calculated according to equation (1). It should be noted that other calculations to determine CV are also contemplated.

[0039] It will be appreciated by those skilled in the art that various modifications of that which is described above is possible without departing from the scope of the invention. By way of example only, constant A in equation (3) above could be trimmed or refined from time to time by separately measuring % CO using a sampling technique (e.g. NIR) and using that measurement to refine the calculation made according to a far more rapid time scale inherent in the claimed method.

[0040] FIG. 2 illustrates meter electronics 112 for the density meter 101 according to an embodiment. The meter electronics 112 may include an interface 201 and a processing system 203. The interface 201 transmits a drive signal to the resonating element 102. The meter electronics 112 receives and processes at least one sensor signal from a sensor, such as a vibration sensor 107 signal, that measures oscillations associated with the resonating element 102.

[0041] The interface 201 can perform any necessary or desired signal conditioning, such as any manner of formatting, amplification, buffering, etc. Alternatively, some or all of the signal conditioning can be performed in the processing system 203.

[0042] In addition, the interface 201 can enable communications between the meter electronics 112 and external devices, such as via the communication link 114, for example. The interface 201 can transfer measurement data to external devices via a communication link 118 and can receive commands, updates, data, and other information from external devices and external gas measurement apparatuses. The interface 201 and communication link 114 may be capable of any manner of electronic, optical, or wireless communication.

[0043] The interface 201 in one embodiment comprises a digitizer, wherein sensor signals comprise analog sensor signals. The digitizer samples and digitizes the analog sensor signals and produces corresponding digital sensor signals. The interface / digitizer can also perform any needed decimation, wherein the digital sensor signal is decimated in order to reduce the amount of signal processing needed and to reduce the processing time.

[0044] The processing system 203 conducts operations of the meter electronics 112 and processes gas measurements from the density meter 101. The processing system 203 executes an operating routine 210 and processes the density measurements in order to produce one or more density characteristics (or other density measurements). The processing routine comprises, inter alia, routines for determining gas specific gravity, gas density, gas temperature, gas pressure, gas molecular weight, percent inert gas, calorific value, and Wobbe Index.

[0045] The processing system 203 can comprise a general purpose computer, a microprocessing system, a logic circuit, or some other general purpose or customized processing device. The processing system 203 can be distributed among multiple processing devices. The processing system 203 can include any manner of integral or independent electronic storage medium, such as the storage system 204. The storage system 204 may be coupled to the processing system 203 or may be integrated into the processing system 203.

[0046] The storage system 204 can store information used for operating the density meter 101, including information generated during the operation of the density meter 101. The storage system 204 can store one or more signals that are used for vibrating the resonating element 102, and that are provided to a driver 105 for actuating the resonating element 102, such as a drive signal 212. In addition, the storage system 204 can store vibrational response signals 214 generated by a vibration sensor 107 as a result of the resonating element 102. Temperature signals 216 may also be utilized by meter electronics and related algorithms.

[0047] It will thus be appreciated that the embodiments utilize a density meter 101 in combination with commercially available gas meters to provide fast and accurate measurements of both Calorific Value and Wobbe Index. The embodiments described above provide Calorific Value and / or Wobbe Index measurements at a frequency of about every 5-10 seconds as opposed to the typical response time of around 7 minutes when using a gas chromatograph. In other embodiments, the frequency is greater or less than every 5-10 seconds. This fast response time optimizes combustion efficiency for combustion-requiring operations, and concomitantly minimizes NOx & SOx emissions, as well as related taxation. Embodiments also yield a stable steam heat supply for certain applications. Thus the present invention could be used in gas blending applications and is ideal for custody transfer applications. Since over 50% of a refinery's (or manufacturing plant's) operating costs is typically due to energy (i.e. steam) production, the present embodiments may lower operating costs in such applications. These benefits are realized, while eliminating safety risks inherent in incendive technologies.

[0048] The detailed descriptions of the above embodiments are not exhaustive descriptions of all embodiments contemplated by the inventor to be within the scope of the invention. Accordingly, the scope of the invention should be determined from the following claims.

Claims

1. A method for determining an energy content of a fuel gas, tail gas, or bio-gas mixture using a gas density meter, comprising the steps of: providing a vibratory gas density meter; providing meter electronics with the gas density meter configured to communicate with at least one external input, wherein the external input comprises a percent H2 value of the gas mixture, a percent CO value of the gas mixture, a percent CO2 value of the gas mixture, and a percent N2 value of the gas mixture; measuring a density of the gas mixture; measuring a specific gravity of the gas mixture; and deriving a calorific value of the gas mixture using the measured specific gravity and a plurality of constant values; wherein the calorific value (CV) is calculated, in, according to an equation comprising: CV = A + (B · percent H2) + (C · percent CO) + (D · percent CO2) + (E · percent N2) + (F · SG), wherein A is between about 144.8 and 150.8, wherein B is between about -2.5 and -2.6, wherein C is between about -12.15 and -12.65, wherein D is between about -47.7 and -49.65, wherein E is between about -24.68 and -25.69, and wherein F is between about 1528.7 and 1591.1, and SG comprises the specific gravity; and calculating the specific gravity from the measured density.

2. The method of Claim 1, wherein a Wobbe Index value of the gas mixture is calculated.

3. A system (100) for measuring gas energy, comprising: a vibratory gas density meter (101) configured to calculate a specific gravity of a fuel gas, tail gas, or bio-gas mixture; a communication line (114) configured to connect to an external input (116); meter electronics (112) for operating the vibratory gas density meter (101) in communication with the communication line (114), wherein the meter electronics (112) is configured to measure a density of the gas mixture and derive a calorific value of the gas mixture using the derived specific gravity and a plurality of constant values; providing meter electronics with at least one external input, wherein the external input comprises a percent H2 value of the gas mixture, a percent CO value of the gas mixture, a percent CO2 value of the gas mixture, and a percent N2 value of the gas mixture; wherein the calorific value (CV) is calculated, in, according to an equation comprising: CV = A + (B · percent H2) + (C · percent CO) + (D · percent CO2) + (E · percent N2) + (F · SG), wherein A is between about 144.8 and 150.8, wherein B is between about -2.5 and -2.6, wherein C is between about -12.15 and -12.65, wherein D is between about -47.7 and -49.65, wherein E is between about -24.68 and -25.69, and wherein F is between about 1528.7 and 1591.1, and SG comprises the specific gravity; and wherein the specific gravity is calculated from the measured density.

4. The system (100) of Claim 3, wherein the external input (116) comprises at least one of a near infrared meter, a thermal conductivity meter, and a gas chromatograph.

5. The system (100) of Claim 3, wherein meter electronics (112) is configured to calculate a Wobbe Index value of the gas mixture.

6. The system (100) of Claim 3, wherein at least one of the percent H2, percent CO, percent CO2, and percent N2 is provided to the meter electronics (112) from the external input (116).