WO2008009870A1 - Détecteur de flux gazeux - Google Patents

Détecteur de flux gazeux Download PDF

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Publication number
WO2008009870A1
WO2008009870A1 PCT/GB2006/002763 GB2006002763W WO2008009870A1 WO 2008009870 A1 WO2008009870 A1 WO 2008009870A1 GB 2006002763 W GB2006002763 W GB 2006002763W WO 2008009870 A1 WO2008009870 A1 WO 2008009870A1
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WO
WIPO (PCT)
Prior art keywords
gas flow
gas
wave
loop
conductor
Prior art date
Application number
PCT/GB2006/002763
Other languages
English (en)
Inventor
Edward Colby
Alan Syrop
Kimon Roussopoulos
Original Assignee
Sentec Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sentec Limited filed Critical Sentec Limited
Priority to EP06765090A priority Critical patent/EP2052220A1/fr
Priority to PCT/GB2006/002763 priority patent/WO2008009870A1/fr
Publication of WO2008009870A1 publication Critical patent/WO2008009870A1/fr

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/66—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by measuring frequency, phase shift or propagation time of electromagnetic or other waves, e.g. using ultrasonic flowmeters
    • G01F1/662—Constructional details

Definitions

  • the present invention relates to a gas flow detector and meter, method, computer program, and system for measuring gas flow and in particular to gas flow detection utilizing a transducer and detector system that is operating in an acoustic range.
  • Ultrasonic meters which measure flow rate by measuring the "time of flight” of an acoustic pulse in the moving flow, inherently give an electronic reading, and much effort has been dedicated to attempts to make a viable and affordable ultrasonic meter.
  • accuracy requirements are such that a plurality of individually matched and calibrated transducers must be used in such meters, something which increases costs significantly.
  • Ultrasound flow measurement techniques have been known for years, and are very accurate for large applications (pipe diameter greater than 5 cm, say). For smaller gas pipes and flows they are, however, not yet generally available.
  • European patent application EP 0566859 discloses an ultrasonic flowmeter for fluid media, having an ultrasonic measurement section in a measuring channel through which the fluid medium flows and preferably two ultrasonic transducers functioning as transmitter and/or receiver, as well as an electronic evaluating system for determining the flow rate of the fluid medium on the basis of the transit time or phase difference of an ultrasonic signal, the measuring channel being wound in a worm-like or helical fashion.
  • the transducer act as a wall between two adjacent parts of the flow channel; the same transducer is used for exciting and for measuring ultrasonic signals in the fluid media. In order to provide an accurate signal the sensor configuration need to be carefully optimized and calibrated.
  • a gas flow detector comprising a gas flow conductor which comprises a substantially loop-shaped part cooperating with a gas inlet part and a gas outlet part for the flow of gas from the gas inlet part through the substantially loop-shaped part of the gas flow conductor to the gas outlet part; where the gas flow detector additionally comprises at least one wave generating device for generating mechanical waves in the gas which flows in the gas flow conductor and at least one wave detection device for detection of the mechanical waves which are generated in the gas flow conductor by the wave generating device and wherein the gas flow conductor is arranged to form a continuous path for the mechanical waves and where the at least one wave generation device is located between two or more adjacent pipe sections which form the substantially loop-shaped part of the gas flow conductor in order to generate the mechanical wave substantially simultaneously in the at least two adjacent pipe sections and where the at least one wave detection device is positioned within at least one of the pipe sections of the at least two adjacent pipe sections in the loop-shaped part of the gas flow conductor.
  • the location of the wave generating device in the pipe sections which form the loop- shaped part of the gas flow conductor makes it possible to generate an acoustic response in both sections of the loop-shaped part of the gas flow conductor.
  • the wave generating device may form part of a wall common to two adjacent pipe sections of the loop-shaped part of the gas flow conductor.
  • One advantage of this arrangement of the wave generating device is that it is intrinsically a seal against gas flow between the adjacent pipe sections.
  • the wave generating device may be attached to a wall common to two adjacent sections of the loop-shaped part of the gas flow conductor. This would give the advantage of a less complicated mounting procedure for the wave generating device onto the gas flow conductor.
  • the embodiment where the wave generating device forms part of a wall common two adjacent pipe sections is to be preferred.
  • the wave generating device is able to produce mechanical wave in the form of acoustic waves, i.e. sound waves, which may or may not be audible to the human ear.
  • the wave generating device generates sound waves in the frequency range between 20 Hz - 20 kHz and in another embodiment the sound waves are produced in a frequency range from 20 kHz and higher, i.e. in the ultrasound frequency range.
  • the sound waves generated by the wave generating device are pulsed acoustic signals.
  • the advantage of this type of signal is that it would enable non-ambiguous determination of flight times for the pulsed acoustic signals.
  • the wave generation device may in this case operate with pulse centre frequencies in the range 20 Hz - 20 kHz.
  • acoustic pulse propagation is mainly single-mode
  • the use of acoustic pulses would minimise the dispersion of the pulse during propagation through the gas flow conductor.
  • the pulsed acoustic signals may be sent with an envelope which may be chosen to be a Raised Cosine, a Hamming or a Hanning or some similar envelope which has a low bandwidth for a given duration.
  • the envelope of the launched acoustic pulse which can have the envelope shapes described above, is preserved.
  • wave generating devices may be used and they may be chosen from the group of piezoelectric, piezo resistive, magneto elastic, capacitive, moving coil or diaphragm motion devices.
  • the wave generating device may for example comprise a diaphragm of elastic material, such as a metal disc with an actuator, such as a piezoelectric actuator or some other electro-mechanical actuator.
  • the wave detecting device mentioned above is adapted for detection of mechanical waves, and in particular pulsed acoustic mechanical waves in the same frequency range as the acoustic pulses sent out by the wave generation device.
  • wave detection devices which may be used in the gas flow detector according to the present invention. Some of the possible choices for such wave detection devices may comprise one of the following types of detecting devices: piezoelectric, piezo resistive, magneto elastic, capacitive, moving coil or diaphragm motion detection devices.
  • the wave detecting device is adapted to detect the time of flight for the acoustic mechanical waves and of acoustic pulses in particular. Additionally, the wave detection device may comprise a matched correlation filter in order to perform signal processing on the received sound pulse and to determine the timing of the sound pulse. This would have the advantage of only letting the energy in the pulsed sound signal received pass that corresponds to the sound pulse launched by the wave generating device.
  • the gas flow detector may comprise two wave detection devices which are located inside two adjacent pipe sections of the loop-shaped part of the gas flow conductor. These wave detection devices are adapted to measure both the sound pulses generated by the wave generating device and the sound pulses that are received after propagation through the loop-shaped part of the gas-flow conductor.
  • these two wave detection devices are located flush with the walls of the gas flow conductor in the vicinity of the wave generating device. In particular, they may be placed directly opposite the wave generation device. By placing the two detectors in such a fashion, one could minimise the effects of different pulse times when the first pulses are sent out by the wave generating device.
  • these two wave detecting devices may be preferably be located flush with the wall of the each of at least two adjacent pipe sections belonging to the loop-shaped part of the gas flow conductor, but offset from the wave generating device and towards each other by a distance less than the diameter of the gas flow pipe.
  • the two wave detecting devices could be located flush with the wall of each of the at least two adjacent pipe sections belonging to the loop-shaped part of the gas flow conductor, but offset from said wave generating device and towards each other by a distance larger than the diameter of the gas flow conductor.
  • the at least one wave detection device may be located in the loop-shaped part of the gas flow conductor substantially at 90 degrees clockwise or counter clockwise from the wave generating device and perpendicular to the direction of flow of gas in the gas flow conductor.
  • the gas flow conductor may also be constructed so that its gas inlet and gas outlet parts are of greater length than the loop-shaped part of the gas flow conductor. Constructing the gas flow conductor in this fashion would minimise the impact of reflections of the sound pulse on the measurement of the sound pulses propagating in the loop-shaped part of the gas flow conductor, since reflections occurring at the ends of the gas inlet and gas outlet parts would arrive later at the wave detecting devices than the sound pulses propagating in the loop-shaped part of the gas flow conductor.
  • the gas inlet and outlet parts each has a length equal or larger than: where LGMIN is the minimum length of the gas inlet or the gas outlet pipe sections, n the number of loops of the loop-shaped pipe section, L the length of the loop-shaped pipe section, t P the duration of the sound pulse generated by the sounder and v s the speed of sound in the gas flow pipe.
  • the loop-shaped portion of the gas flow conductor may have a number of different shapes, among which it could take the shape of a toroid, a spiral, an ellipsoid, an oval shape, a rectangle with or without smoothed corners, rhomboid or other quadrilateral, or other topological ⁇ multilateral shapes.
  • the gas flow conductor may be manufactured from a number of different materials, among which there may be at least one of the following materials: metal, plastic, and ceramic based pipes.
  • the object of the invention is achieved by a method of measuring gas flow comprising the steps of:
  • a gas flow conductor which comprise a substantially loop-shaped part cooperating with a gas inlet part, a gas outlet part and arranging the mechanical wave so as to flow with a flow of gas between the gas inlet part, the substantially loop-shaped part and the gas outlet part;
  • the method according to the present invention may further comprise the step of measuring the mechanical wave both when it is generated in the gas flow conductor and when it is received after having travelled along the gas flow conductor. Measuring the time of flight for the pulsed sound wave in this fashion would have the advantage of accurate matching of the wave detecting devices and the signal processing performed in these devices when there is more than one wave detecting device present in the pipe section forming the loop-shaped part of the gas flow conductor.
  • the timing analysis for the received pulse shaped signal may for example comprise phase determination for the sound pulses in the direction of the gas flow and in the opposite flow direction using a complex correlation function for each detected pulse
  • the object of the present invention is achieved by a gas flow meter comprising a gas flow detector in turn comprising a gas flow conductor which comprise a substantially loop-shaped part cooperating with a gas inlet part and a gas outlet part for the flow of gas from the gas inlet part, through the substantially loop-shaped part of the gas flow conductor to said the gas outlet (3) part, where the gas flow meter additionally comprises at least one wave generating device which generates mechanical waves in gas flowing in the gas flow conductor, at least one wave detection device for detecting the mechanical waves generated in said gas flow conductor by said wave generating device, wherein the gas flow conductor is arranged to form a continuous path for the mechanical waves and where the at least one wave generation device is located between two or more adjacent pipe sections which form the substantially loop-shaped part of the gas flow conductor to generate the mechanical wave substantially simultaneously in the at least two adjacent pipe sections and where the at least one wave detection device is positioned inside at least one of the pipe sections of the at least two adjacent pipe sections in the loop-shaped part
  • the object of the present invention is achieved by a system for supplying gas in a building which comprises the above described gas flow meter; a main gas inlet connected the gas flow meter at an upstream position relative to the flow meter, at least one gas conduit which is arranged to distribute gas within the building, wherein the at least one gas conduit is connected to the gas flow meter at a downstream position relative to the flow meter and at least one gas appliance receiving gas via the gas conduit.
  • the object of the invention is achieved by a computer program which determines gas flow and further comprises instruction sets which generate at least one mechanical wave which is transmitted in gas flowing in a gas flow conductor which comprise a substantially loop-shaped part cooperating with a gas inlet part, a gas outlet part and where the mechanical wave is arranged so as to flow with a flow of gas between the gas inlet part, the substantially loop-shaped part and the gas outlet part, transmits the mechanical wave in substantially opposite directions and substantially simultaneously in two or more adjacent pipe sections which form the substantially loop-shaped part of the gas flow conductor, detect said mechanical wave with at least one detector which is positioned inside the at least one of the pipe sections of the at least two adjacent pipe sections in the loop-shaped part of the gas flow conductor, analyse the waves for timing characteristics; and determine gas flow using these timing characteristics, wherein the analysis comprises measuring the times between detected signals.
  • the timing analysis comprises phase determination by using a complex correlation function for each detected pulse.
  • Fig. 1 illustrates schematically a perspective side view of an embodiment of the present invention
  • Fig. 2 illustrates schematically a cross sectional view of the embodiment in Fig. 1
  • Fig. 3 illustrates schematically a number of pulses detected during measurement using the embodiment according to Fig. 1 and Fig. 2;
  • Fig. 4 illustrates schematically a perspective side view of a second embodiment of the present invention
  • Fig. 5 illustrates schematically a cross sectional view of a fourth embodiment of the 5 present invention
  • Fig. 6 illustrates schematically a cross sectional view of a fifth embodiment of the present invention
  • FIG. 7 illustrates schematically a computational device according to the present invention
  • Fig. 8 illustrates schematically a flow diagram representing a method according to the present invention.
  • FIG. 9 illustrates schematically a building having a flow meter according to the present invention
  • FIG. 1 illustrates a perspective side view of a first embodiment of a gas flow detector 100, showing a gas flow pipe 110 comprising a gas inlet part 120, a loop-shaped section of the gas flow pipe 130 and a gas outlet part 140.
  • the direction of gas flow is indicated by the arrows in Fig. 1, where the first arrow 125 indicates the inflow of gas into the gas inlet part 120 and the second arrow 145 the direction of outflow of gas from the gas outlet part 140
  • the pipe sections 160 and 170 are shown in Fig. 1 as substantially straight portions of the loop-shaped section 130 of the gas flow pipe sharing a common wall; however these sections 160, 170 may also be formed as curved portions, for instance as part of a continued loop together with the looped shaped section 130 forming a multi looped gas detector 100. Also, a sounder 180 for producing mechanical waves, for
  • 30 instance sound pulses is located between the first substantially straight pipe section 160 and the second substantially straight pipe section 170.
  • Fig. 2 illustrates a cross section of the first embodiment of the present invention along the line X-X.
  • a sounder 180 is installed, which in this embodiment forms part of the common wall for the two pipe sections. Having the sounder 180 built into the common wall 151 in the manner described above has the advantage that two sound pulses can be launched at two distinct flow locations along the gas flow pipe. It also minimises cavity resonances in a coupling system between the sounder and the gas flow tube.
  • the sounder may 180 for example be constructed as a diaphragm of elastic material, such as in the form of a metal disc, with an actuator, such as a piezo-electric element bonded to it.
  • an actuator such as a piezo-electric element bonded to it.
  • the sounder may be bonded to the common wall and at the same time present a seal against gas leakage from one pipe section to the other. In this fashion, it is possible to control sounder motion and therefore manage resonance effects stemming from the natural frequencies of vibration for the sounder.
  • the material for the sounder 180 may be chosen so as to be able to resist the pressure difference between the two pipe sections 160 and 170.
  • a first microphone 153 and a second microphone 154 are arranged flush with the walls belonging to the first and the second pipe sections 160 and 170.
  • the function of the microphones is to receive the sound pulses launched by the sounder 180 in both the first pipe section 160 and the second pipe section 170.
  • perturbations introduced in the sound pulse measured by the microphones stemming from the interaction between the gas flow and the microphone or interaction between the pulses travelling in the gas and the microphone (or the microphone mounting) when the microphones are located at the inner walls of the pipe which may negatively affect the measurements; for instance in a position of the microphone on the inner side of the wall thus protruding into the flow path of gas in the gas flow pipe 110.
  • These perturbations may be, for example, due to the acoustic mismatch between the pipe section leading to the location of the microphone and the microphone position or due to the occurrence of flow turbulence around or nearby the microphones,
  • the incorporation of the microphones flush with the gas pipe walls may serve to avoid cavity resonances in a possible coupling pipe between the gas flow pipe 110 and the microphone.
  • a continuous gas flow entering the gas inlet part 120 in the direction of the arrow 125 passes through the loop-shaped pipe section 130 of the gas flow pipe 110 and exits the gas flow pipe 110 through the gas outlet pipe section 140 in the direction of the of the second arrow 145.
  • the sounder 180 launches a sound pulse in the direction of the gas flow 125 and in the counter-flow direction (not shown) through the substantially straight pipe sections 170 and 180 forming part of the loop-shaped section 130 in the gas flow pipe 110 and sharing a common wall 151.
  • the first microphone 153 and second microphone 154 register the sound pulse almost immediately after it is launched at time instants t1 and t3.
  • the pulse launched by the sounder 180 in the direction of gas flow 125 arrives at the second microphone 154 and at a time instant t4 the sound pulse launched against the direction of gas flow 125 in the second pipe section 170 arrives at the first microphone 160 after having travelled one or more turns in the loop-shaped pipe section 130 of the gas flow pipe 110.
  • the loop-shaped pipe section of the gas flow pipe may comprise more than one loop, it is here chosen for the sake of clarity to illustrate the one-loop version of the gas flow pipe 110.
  • the pulses travelling with the flow of gas and against the flow of gas may be measured simultaneously.
  • the mechanical wave pulses sent out by the sounder 180 may be generated in the acoustic range, i.e. within the 20 Hz - 20 kHz audible range, where there exists a number of wave generating and detecting devices on the market that may readily be utilized and at an advantageous price.
  • a sounder 180 which produces sound pulses in the ultrasound range, i.e. from 20 kHz and above. This would, of course, necessitate the use of transducers receptive to sound pulses in this frequency area.
  • an acoustic wavelength at which only planar waves propagate in the waveguide is advantageous to use.
  • the frequency will depend on the size of the pipe.
  • a suitable combination for low speed gas for example, is to use a 0.4 m long loop-shaped pipe section 180 of diameter 16mm with a pulse consisting of a Hanning windowed sine wave of length 6 cycles and frequency 8 kHz.
  • a pulse consisting of a Hanning windowed sine wave of length 6 cycles and frequency 8 kHz.
  • other combinations of lengths, cycles, pulse shapes and frequencies will be applicable depending on gas composition, flow speed ranges and required (or desired) resolution of gas flow measurements.
  • the sounder 180 may produce sound pulses from the group of Raised Cosine, Hamming or similar pulses which have a low bandwidth for a given pulse duration.
  • the important aspect here is to use a pulse shape that will minimise pulse duration and bandwidth. Using such a bandwidth-limited pulse in the gas flow detector 100 minimises the risk of giving rise to undesired parasitic resonances in the gas flow pipe 110 which occur at frequencies adjacent to the pulse.
  • Another aspect of avoiding resonant frequencies for the sound pulse will also make sure that the envelope of the sound pulse during travel though the gas flow pipe will not change significantly due to temperature variations of the gas inside the pipe or the gas flow pipe itself and the variations in the sounder mounting.
  • Fig. 3 illustrates a signal registered by the wave detection devices 160, 170 at various times after a pulse has been transmitted from the sounder 180.
  • a first pulse A1 to be registered is a pulse which is sent downstream, i.e. in the direction of the arrow 190, from the sounder 180 in the first straight pipe section 160 into the loop-shaped pipe section 130 of the gas flow pipe 100.
  • the second pulse B1 is generated by the sounder 180 in the second straight pipe section 170 and sent into the direction of the arrow 191 opposite to the direction 190 of the pulse A1 into the loop-shaped pipe section 130, which is the pulse that has travelled in the other direction through one or more loops of the loop-shaped pipe section 130 and upstream, 145.
  • the third pulse A2 to be registered is from the downstream travelling pulse after it has travelled through one or more loops of the loop- shaped pipe section 130 and the fourth pulse B2 to be registered is from the upstream travelling pulse after it has travelled upstream through one or more loops of the loop- shaped pipe section 130.
  • Pulse times between consecutive pulses of the same character i.e. pulses travelling in the same direction
  • a number of pulses from reflections at the ends of the gas inlet and gas outlet pipe sections 120 and 140 or other sections of the pipe will also be detected and thus need to be dealt with by an electronic controller.
  • Such an electronic controller is used for synchronizing measurements, controlling excitation pulses, acquiring signals from the detector, and analysing measurements.
  • the difference ⁇ t2- ⁇ t1 between pulse arrival times for the pulse going in the flow direction and the pulse travelling against the flow will be used for determining the flow of the gas since the speed of the acoustic pulses are generally known and it is possible to approximate the arrival times of pulses as a function of flow rate and length of the travelled distance between detector locations.
  • the accuracy of the flow measurement will depend on the accuracy to which the pulse timings can be determined. To obtain the accuracy generally required for fiscal metering it is necessary to use a phase measurement technique, such as described herein below.
  • signal processing involving a correlation operation on the received signal is performed by a matched correlation filter which is loaded with filter coefficients that match the launched sound pulse shape sent to the sounder.
  • a matched correlation filter which is loaded with filter coefficients that match the launched sound pulse shape sent to the sounder.
  • the matched correlation filter may be loaded with coefficients for the pulse sent to the sounder convolved with the frequency response of the sounder. This way the received sound pulses will be processed to match a signal that better approximates the actual pulse propagating in the gas flow pipe.
  • the correlation filter may be loaded with filter coefficients that are adapted to match the first pulse received by the microphones 153, 154. Then the subtraction of the first and second pulse timings is processed to match a pulse that actually propagates in the gas flow tube convolved with the frequency response of the microphone. Also, the second pulse (the pulse that has travelled through the loop-shaped pipe section and arrived at the other microphone) is processed to match a pulse that actually propagates in the gas flow tube convolved with the frequency response of the microphone.
  • the microphone if it is positioned away from the sounder it will measure the first signal (A1 and B1) as a more fully developed signal, i.e. any near field variations will be reduced; however, if the microphone is located to far away other effects will start to distort the signal, such as temperature variations, flow disturbances and so on. This means that there will be an optimal distance between the microphone and the sounder for optimal signal detection.
  • Fig. 4 illustrates a different embodiment of the present invention, where the two microphones 153 and 154 have been moved a distance D from the sounder 180 towards each other in the direction of the loop-shaped pipe section 130 of the gas flow pipe 110.
  • the width of the gas flow pipe is set to d and the distance D between the microphones 153 and 154.
  • the embodiment of the present invention shown in Fig. 5 is similar to the first embodiment of the gas flow detector 100 from figure 1 , in that the two microphones 153, 154 are located at the same streamwise location as the sounder 180 . However, the microphones are positioned at 90 degrees from the sounder 180 and perpendicular to the direction of gas flow into the gas flow pipe 110 indicated by the arrow 125. The microphones may also be positioned either at 90 degrees counter clockwise in relation to the sounder 180 or clockwise. Also, they need not be positioned at the same streamwise location as the sounder 180, but instead at a distance D from the sounder 180 and towards each other either such that either D ⁇ d or D>d, where d is the width of the pipe 110. Even though the microphones are depicted as being mounted on the inside of the pipe walls they may alternatively be mounted flush with the wall as is the case illustrated in Fig. 2.
  • non-planar modes for the pulse propagation may occur due to the response of the pipe and they may be minimised by the placement of the microphones 153, 154 in the way illustrated in Fig. 5.
  • the sounder may be instead of forming part of the common wall 151 for the two flat pipe sections 160 and 170 of the gas flow tube 110, be located outside the common wall 151 and attached to it.
  • This arrangement has the added advantage of the overall easier construction of the gas flow meter, since mechanical modification of the straight pipe sections 160 and 170 can be avoided. It may however not give equally good measurement values for the launched and received sound pulses generated by such a sounder 180.
  • One other means for improving the quality of received signals is choosing the length of the gas inlet and gas outlet pipe sections 120 and 140 to be at least as long as the length of the loop-shaped pipe section 130 or even longer. This would eliminate degradation in the received pulses due to reflections of sound pulses sent in the directions 192 and 191 from the pipe ends. Choosing their length in this fashion would ensure that the sound pulses travelling in the loop-shaped pipe section 130 of the gas flow pipe 110 would arrive at the two microphones 153 and 154 before the sound pulses reflected from the two pipe- ends arrive at the microphones. More specifically, the minimum length for the gas inlet and gas outlet pipe sections 120 and 140 can be calculated from the expression below:
  • LQMIN is the minimum length of the gas inlet or the gas outlet pipe sections 120 and 140
  • n the number of loops of the loop-shaped pipe section 130
  • L the length of the loop- shaped pipe section 130
  • t P the duration of the sound pulse generated by the sounder 180 and Vs the speed of sound in the gas flow pipe 110.
  • the amplitude of the sound pulses generated by the sounder 180 may be increased in order to account for increasing flow rates which may introduce acoustic flow noise into the gas flow pipe 110, thus maintaining a desired Signal-to-Noise ratio when measuring the received sound pulses.
  • the overall power consumption of the gas flow meter 100 is reduced.
  • a similar argument may be used for optimizing the repetition rate of the sound pulses, with a higher repetition rate of the sound pulses a higher accuracy may be obtained on the expense of power consumption, i.e. it is possible to dynamically alter either or both of the amplitude or and repetition rate to find a suitable signal to noise ration for the specific application or installation. This may also be adjusted over time for a specific installation due to changes of the system or the environment, for instance temperature changes, wear, ageing, changed components and so on.
  • Another measure which may improve the overall quality of the measured sound pulse is the modification of the shape of the inlet and outlet pipe sections 120 and 140.
  • an acoustic miss-match for the sound pulses travelling in these two directions is introduced at a minimal pressure loss. Due to the acoustic mismatch the most part of the arriving sound pulses will be reflected at the area where the mismatch occurs back into the flat pipe sections 160 and 170. In this way acoustic propagation is mostly contained in the gas flow detector 100 without propagating further into other parts of the pipe system where the gas flow detector 100 according to the present invention is installed.
  • One other possible way of solving the above-mentioned problem may also be to have the sectional area for the gas inlet and gas outlet pipe sections 120 and 140 increase exponentially with distance from the straight pipe sections 160 and 170 with an appropriate expansion coefficient for the frequencies which are used for the sound pulses launched by the sounder 180. In this fashion, the change from the straight to the expanding pipe section would minimise acoustic reflections for the launched sound pulses.
  • some form of protection for the sounder 180 in order to guard it against interference from other external acoustical sources. This may be achieved by constructing the sounder 5 180 out of metal or some other suitably rigid material and with walls having a thickness which would prevent interference from external acoustic sources.
  • Another variant of insulation for the sounder 180 may be to build the sounder or the flow meter into a box with air isolating the sounder or flow meter from the walls. Enclosing the flow meter in such a manner will also provide security from tampering means in the form of inducing0 sound pulses in the piping of the flow meter.
  • the present invention is not limited to gas flow pipes of any particular length or width. It is possible to use it in pipes with a relatively small width which are relatively short in length for instance residential gas delivery pipes, but also pipes with5 a diameter of one meter or more and lengths of 100 meters or more if necessary for instance gas pipes from gas wells.
  • the computational device 300 comprises a computational unit 801 , such as e.g. a microprocessor, a DSP (Digital Signal Processor), an ASIC (Application Specific Integrated Circuit) or an FPGA (Field Programmable Gate Array) or a combination of these.
  • the computational device may further comprise a storage unit (e.g. volatile or non-volatile memory) 802 and/or a5 communication unit 803.
  • the communication unit 803 may use any suitable communication method and protocol, including different forms of wired or wireless communication methods; the communication unit 803 may actually comprise a combination of communication methods and/or protocols, each used for different types of communication links (e.g. a short ranged wireless protocol for service communication and0 a long range wireless protocol for sending metering data to a billing system).
  • the computational device 800 has a control interface 804 and a detector interface 805.
  • the control interface 804 is used for sending control signals to the wave generating device 180 or to an intermediate pulse generator (not shown) in turn driving the wave generating device 180.
  • the detector interface receives signals directly or indirectly from the wave5 detecting devices 153, 154, for instance in some cases a signal conditioning device (not shown) may be needed in order to provide the computational device 800 with appropriate signal types and levels, or for reducing noise levels.
  • the invention is not limited to any special communication types or protocols for communicating measured flow data, but may include for instance short range wireless standards as WLAN (Wireless Local Area Network) protocols (e.g. from the IEEE 802.11 family, IEEE 802.16 family, or IEEE 802.15.4 family) or WPAN (Wireless Personal Area Networks) such as for instance the Bluetooth protocol or any proprietary wireless solution (e.g. low power solutions that may be run on battery for long periods of time).
  • WLAN Wireless Local Area Network
  • WPAN Wireless Personal Area Networks
  • Bluetooth protocol Wireless Personal Area Networks
  • any proprietary wireless solution e.g. low power solutions that may be run on battery for long periods of time.
  • wireless communication may be using long range wireless communication methods, including but not limited to NMT (Nordic Mobile Telephone), GSM (Global System for Mobile Communication), GPRS (General Packet Radio Service), EDGE (Enhanced Data rate for Global Evolution), UMTS (Universal Mobile Telecommunications Service), variations of CDMA (Code-Division Multiple Access), and future similar communication types.
  • Communication may also utilize wired solution, including but not limited to Ethernet link, serial connection, parallel connection, and power line communication.
  • Fig. 8 illustrates a flow chart representing a method according to the present invention of measuring gas flow, comprising the steps of: - generating at least one mechanical wave transmitted in gas flowing in a gas flow conductor consisting of an substantially loop-shaped part cooperating with a gas inlet part, a gas outlet part and arranging said mechanical wave so as to flow with a flow of gas between said gas inlet part, said substantially loop- shaped part and said gas outlet part (901); - transmitting said mechanical wave in substantially opposite directions and substantially simultaneously in two or more adjacent pipe sections forming said substantially loop-shaped part of the gas flow conductor of the substantially loop-shaped part of said gas flow conductor (902);
  • a gas flow meter 1001 meters the amount of gas entering the building 1000 via an incoming gas conduit 1004.
  • gas conduits 1005 conduct gas to different appliances, such as a boiler 1002 for generating warm water and a central heating unit 1003 for generating heat to the building 1000.
  • the gas flow detector may of course also be used in gas flow applications such as within industrial processes where it is desirable to determine the amount of gas delivered to a certain process but not used for billing purposes in a metering application.
  • the loop-shaped pipe section 130 of the gas flow pipe 110 for example, need not be round, as shown in Figure 1. It can be any closed shape, although the corners should not be too sudden or abrupt. Other shapes include, but the invention is not limited to these shapes, ellipsoid, oval, rectangle with or without smoothed corners, and rhomboid, or other quadrilateral, or other topological ⁇ multilateral shapes.
  • actuator and detector technologies including for example piezoelectric, piezo resistive, magneto elastic, capacitive, moving coil, or diaphragm motion (detection) devices.
  • the working frequency can be in the acoustic range, making use of the transducers (earpieces) manufactured for personal entertainment systems and low cost miniature microphones as used, for example, in mobile telephones.
  • gas flow detector and method may be utilized in a gas flow meter for use in measuring gas flow volumes in both residential and industrial applications.
  • the gas flow meter sends measured and/or stored flow measurements to a central aggregating device (such as a billing server) for later billing to customers acquiring gas volumes. Data may be sent as flow data together with time data and later converted to volumes or as volume data converted by the flow meter itself.
  • the gas flow meter may be used in a system, for instance in a residential home, for measuring the amount of gas domestic appliances (e.g. water heating, stove, and heating of living area) consume.
  • gas domestic appliances e.g. water heating, stove, and heating of living area
  • All the above described embodiments of the present invention may be built into a gas leak proof containment unit in order to provide a convenient box for mounting purposes and protection purposes; it may also provide extra safety against gas leaks.
  • An additional advantage of the present invention is that it permits the use of relatively low- cost transducer components, such as low cost microphones since measurements are based on arrival times of pulses from a single source.

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  • Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)
  • Electromagnetism (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)

Abstract

L'invention concerne un procédé et des appareils permettant de déterminer un flux gazeux, par exemple sous la forme d'un détecteur de flux gazeux (100) comprenant : un conducteur de flux gazeux (110) comprenant une partie sensiblement en forme de boucle (130) coopérant avec une entrée de gaz (120) et une sortie de gaz (140), pour le flux gazeux s'écoulant de l'entrée de gaz (120) à travers la partie sensiblement en forme de boucle (130) du conducteur de flux gazeux (110) jusqu'à la sortie de gaz (140), au moins un dispositif de génération d'ondes (180) destiné à générer des ondes mécaniques dans le flux de gaz s'écoulant dans le conducteur de flux gazeux (110), au moins un dispositif de détection d'ondes (153, 154) destiné à détecter les ondes mécaniques générées dans le conducteur de flux gazeux (110) par le dispositif de génération d'ondes (180), et ce conducteur de flux gazeux (110) est agencé de façon à former un trajet continu pour les ondes mécaniques et ce dispositif de génération d'ondes (180) étant situé entre les parties de tuyaux contigues formant la partie sensiblement en forme de boucle (130) du conducteur de flux gazeux (110) afin de générer l'onde mécanique sensiblement simultanément dans ces deux parties de tuyaux contigues et, ce dispositif de détection d'ondes (153, 154) est positionné à l'intérieur d'au moins une des parties de tuyau de ces parties de tuyaux contigues de la partie en forme de boucle (130) du conducteur de flux gazeux 110).
PCT/GB2006/002763 2006-07-21 2006-07-21 Détecteur de flux gazeux WO2008009870A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP06765090A EP2052220A1 (fr) 2006-07-21 2006-07-21 Détecteur de flux gazeux
PCT/GB2006/002763 WO2008009870A1 (fr) 2006-07-21 2006-07-21 Détecteur de flux gazeux

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/GB2006/002763 WO2008009870A1 (fr) 2006-07-21 2006-07-21 Détecteur de flux gazeux

Publications (1)

Publication Number Publication Date
WO2008009870A1 true WO2008009870A1 (fr) 2008-01-24

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PCT/GB2006/002763 WO2008009870A1 (fr) 2006-07-21 2006-07-21 Détecteur de flux gazeux

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EP (1) EP2052220A1 (fr)
WO (1) WO2008009870A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
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CN102192767A (zh) * 2010-03-18 2011-09-21 西克工程有限公司 用于测量流体流动速度的超声波测量装置和方法
JP2021015024A (ja) * 2019-07-11 2021-02-12 旭有機材株式会社 螺旋式超音波流量計

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US5168762A (en) * 1988-06-09 1992-12-08 British Gas Plc Speed measurement device
US5247826A (en) * 1992-11-12 1993-09-28 Devilbiss Health Care, Inc. Gas concentration and/or flow sensor
EP0566859A1 (fr) * 1992-04-22 1993-10-27 Hydrometer Gesellschaft mbH Débitmètre ultrasonique avec canal de mesure hélicoidal
US5461931A (en) * 1991-09-16 1995-10-31 British Gas Plc Measurement system
EP0763717A2 (fr) * 1995-09-13 1997-03-19 IWK Regler und Kompensatoren GmbH Dispositif de mesure ultrasonique de débit
US5777238A (en) * 1996-06-12 1998-07-07 Welch Allyn, Inc. Driver-receiver apparatus for use with ultrasonic flowmeters

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DE2833793A1 (de) * 1978-08-02 1980-02-14 Daimler Benz Ag Ultraschall-durchflussmesseinrichtung
US5168762A (en) * 1988-06-09 1992-12-08 British Gas Plc Speed measurement device
US5461931A (en) * 1991-09-16 1995-10-31 British Gas Plc Measurement system
EP0566859A1 (fr) * 1992-04-22 1993-10-27 Hydrometer Gesellschaft mbH Débitmètre ultrasonique avec canal de mesure hélicoidal
US5247826A (en) * 1992-11-12 1993-09-28 Devilbiss Health Care, Inc. Gas concentration and/or flow sensor
US5247826B1 (en) * 1992-11-12 1995-07-18 Devilbiss Health Care Inc Gas concentration and/or flow sensor
EP0763717A2 (fr) * 1995-09-13 1997-03-19 IWK Regler und Kompensatoren GmbH Dispositif de mesure ultrasonique de débit
US5777238A (en) * 1996-06-12 1998-07-07 Welch Allyn, Inc. Driver-receiver apparatus for use with ultrasonic flowmeters

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CN102192767A (zh) * 2010-03-18 2011-09-21 西克工程有限公司 用于测量流体流动速度的超声波测量装置和方法
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EP2375224A1 (fr) 2010-03-18 2011-10-12 SICK Engineering GmbH Dispositif de mesure des ultrasons et procédé de mesure de la vitesse d'écoulement d'un liquide
CN102192767B (zh) * 2010-03-18 2013-07-24 西克工程有限公司 用于测量流体流动速度的超声波测量装置和方法
US8776613B2 (en) 2010-03-18 2014-07-15 Sick Engineering Gmbh Ultrasonic measurement apparatus having a deflection unit forming a loop
JP2021015024A (ja) * 2019-07-11 2021-02-12 旭有機材株式会社 螺旋式超音波流量計
JP7246275B2 (ja) 2019-07-11 2023-03-27 旭有機材株式会社 螺旋式超音波流量計

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