A METHOD AND AN APPARATUS FOR DETERMINING THE VELOCITY, DIRECTION AND OTHER MAGNITUDES OF A FLOW, IN PARTICULAR A GAS FLOW

Abstract: A method and an apparatus for determining the veloc­ ity, direction and other magnitudes of a flow (30), in particu­ lar a gas flow, in which a strongly damped acoustic signal (1) is emitted by a first transducer (12) in a first direction through the flow (30) towards a second transducer (13) pro­ ducing a damped electric signal, the first deflection (4) thereof being compared with a threshold value (5) which is lower than the peak value of said deflection (4), and exceed­ ing said threshold value (5) being used as the end of the time measurement period started at the emission of the acoustic signal (1) by said first transducer (12). In particular a single first transducer (12) is used, and a reflecting body (28) is placed in front of said first transducer (12), adapted to reflect the acoustic pulses (1) emitted by said transducer (12) through the flow (30) in different directions towards one or more second transducers (13).

Description: The invention relates to a method as defined in the preamble of claim 1, as well as to an apparatus according to the preamble of claim 6. From DE-A 2 641 772, a method and an apparatus are known, in which the electric signals generated on reception of acoustic signals have a substantially symmetric envelope, i.e. have peaks with initially increasing heights, before the peak height decreases again. The object of the invention is to provide a method and an apparatus for these purposes, which allows to improve the accuracy of the measurements in a simple manner, as characterised in claims 1 band 6 respectively. Advantageous embodiments are mentioned in the respective dependent subclaims. The invention will be elucidated below by reference to a drawing, showing in: Figs. 1A, B and C representations of waveforms used in an apparatus according to the invention; Fig. 2 a block diagram of an embodiment of the apparatus according to the invention; and Fig. 3 a diagrammatical representation of a special arrangement of the piezo-electric transducers of such an apparatus. Fig. 1A shows an acoustic pulse 1, having a first peak 2 in a given sense, which is shown here as the negative sense, followed by a number of peaks in alternating senses with strongly decreasing height. Such a pulse can be produced by discharging a charged capacitor through a piezo-electric transducer. This is repeated with a relatively low frequency, e.g. 500 Hz, so that the interval between successive pulses 1 is large in respect of the pulse width. Fig. 1B shows a corresponding representation of the output signal 3 of a piezo-electric transducer on which an acoustic pulse 1 of Fig. 1A is incident. This signal comprises, again, a first peak 4, shown here in the negative sense, as well as a number of subsequent peaks in alternate senses and with decreasing heights. The first peak 4 of the signal 3 has the largest deflection, so that, if only the negative peaks are used for the measurement, the peaks following on the first peak 4 can be excluded by selecting a suitable threshold value 5. By measuring the time lapse between the emission of the emittor pulse 1 and the reception of a signal 3 the transit time can be determined. The interval between the pulses 1 is, then, substantially larger than the duration of the signal 3. The measurement of the transit time can, for instance, take place by means of clock pulses 6 shown in Fig. 1C. These pulses can, for instance, have a repetition frequency of 10 MHz. The transit time is, then, given by the number of clock pulses 6 counted between the instant t₀ at which the pulse 1 was emitted and the instant t₁ at which the first peak 4 of the signal 3 exceeds the threshold value 5. According as the repetition frequency of the pulses 6 is higher, the accuracy of the measurement will be better, but a practical limit is imposed thereon. In practice a frequency of about 10 MHz will be used, so that the time interval Δt between two pulses will be about 0,1 µs. Another restriction of the accuracy is caused by the fact that as well the enabling instant t₀ as the disabling instant t₁ of the used counter can be in an arbitrary point between two pulses 6. In order to remove said inaccuracy the measurements will be repeated a sufficient number of times in order to obtain a dependable average. In view of the repetition frequency of the pulses 1, which is, for instance, 500 Hz, dependable statistics can be obtained within a short time. Even if a subsequent peak of the signal 3 would exceed the threshold value 5, this has no influence on the count, since, at the instant t₁, counting is interrupted. Also plural echo signals will not have a noticeable influence on these statistics, since such signals will arrive later and, therefore, will not have an effect, and the distance between the pulses 1 is sufficiently large for allowing echo signals to decay before a subsequent measurement takes place. The clock pulses 6 are continuously produced, but the counter used for counting them is enabled at the instant t₀, and is disabled on the instant t₁, as the case may be by the intermediary of suitable gates. The flow velocity can be derived from transit time differences in two different directions, and in particular in opposite directions, and the flow direction can be determined from a plurality of measurements at different angles. There exists, moreover, a relationship between the propagation speed of the acoustic waves in a gas and the latter's temperature, which relationship is a substantially linear one. Therefore, also the temperature of the gas can be derived from the average of a number of transit time measurements if the relationship between the propagation speed and the temperature is known. The humidity of the gas influences the attenuation of the acoustic pulses in the gas. Said attenuation can be determined by comparing the peak value 4 of the signal 3 with a reference value for dry gas. This peak value can, for instance, be determined by means of a plurality of additional thresholds 5', the just exceeded threshold then substantially corresponding to said peak value. It is also possible to use, to that end, a periodically shifting threshold, which, for instance, is controlled by means of a suitable saw-tooth voltage, and it is also possible that this threshold is a so-called self-learning threshold in that in a series of consecutive measurements the preceding measurement is used as the initial value, so that, again, a dependable average can be determined. In this manner it becomes possible to measure in a quick and dependable way all the variables of the gas flow to be examined by means of a single apparatus. Fig. 2 shows a block diagram of an electric circuit suitable for this purpose. This circuit comprises a trigger 10 fixing the repetition period of the pulses 1. This trigger controls a supply circuit 11 for a piezo-electric pulse generator 12 or a plurality of such generators, adapted to emit the acoustic pulses in the desired number of directions; for simplicity's sake only two directions are indicated in Fig. 2, but the number thereof can also be larger or smaller. The acoustic pulses are received by a corresponding number of transducers 13, and are transformed thereby in electric signals 3. The signals 3 are forwarded towards a threshold circuit 14 applying the above-mentioned threshold 5. On reception of a trigger pulse the circuit 11 causes, for instance, the discharge of a capacitor through the transducer 12, and forwards, moreover, via a line 15 an enabling pulse towards a counter 16 which, on the other hand, can receive via a line 17 a disabling pulse from the associated threshold circuit 14. Moreover each counter 16 receives from a clock pulse source 18 via a line 19 the clock pulses 6, so that in the period between enabling and disabling the counter the received clock pulses can be counted. If necessary means not shown can reset the counters 16 after processing the counts in question. The outputs of the counters 16 are connected with a processing circuit 20 in which the various transit time measurements are processed for computing the flow velocity and, as the case may be, flow direction of the gas flow to be examined, and the results thereof are displayed on a display apparatus 21. On the other hand the output signals of the counters 16 are forwarded towards an additional processing circuit 22, which can be a summing circuit, by means of which a result corresponding to the average transit time or a result proportional thereto can be determined, which is a measure for the temperature of the gas, which result can be displayed on an associated display apparatus 23. Moreover the output signal 3 of one of the transducers 13 can be forwarded to a special threshold circuit 24 by means of which the peak value of the peak 4 of the signal 3 can be determined, which peak value is compared, in a stage 25, with a reference value supplied to a reference input 26 and corresponding to the attenuation with the dry gas, the difference therebetween being a measure for the humidity of the gas, which result can be displayed on a display apparatus 27. The threshold circuit 24 can be a multiple threshold circuit or a circuit with a variable threshold value, as has already been remarked above. If required also one of the threshold circuits 14 can be used for this purpose. It will be clear that Fig. 2 shows only the fundamental structure of a circuit suitable for the present purpose, and that many modifications can be made therein. If a smaller number of magnitudes is to be determined, a corresponding part of this circuit can be left out. Although, in Fig. 2, separate threshold circuits 14 and counters 16 are shown, it is also possible to store the output signals 3 of the transducers 13 in a memory, and to process them during the time between two successive pulses 1, which allows a simplification of the circuit. For determining the velocity and direction of the gas flow to be examined, various assemblies of transducers 12 and 13 can be used. In particular transducer pairs with mutually crossed directions can be used, and, in a given direction, also measurements in two opposite senses can be used. If the character of the transducers is such that they can be used as well as a pulse emittor and as a pulse receiver, a measurement in both senses can be obtained by a simple commutation. It is, of course, also possible to use, for a given direction, two pairs, each being intended for one sense of propagation. The number of pairs depends, of course, from the fact whether the direction of the flow factor is to be determined in two or in three dimensions. Fig. 3 shows, furthermore, a special embodiment of an apparatus suitable for the present purposes. This embodiment comprises a single piezo-electric pulse generator 12 which is arranged at one side of a flow portion to be examined, and in front of this pulse generator 12 a reflection body 28 is arranged which, for the sake of simplicity, is represented as a triangle. The emitted pulses 1 are reflected against the oblique planes 29 of this body 28 towards an associated transducer 13. The acoustic pulses proceed, therefore, through the gas flow first in one and then in the other sense. If required a symmetrical geometry of the pulse tracks before and after reflection can be obtained by a suitable design of the pulse generator 12 and of the body 28. In particular the body 28 is made in the form of a three-sided pyramid or tetrahedron, in which case three transducers 13 are to be used, and then an accurate determination of the flow vector 30 can be obtained. It is also possible to use a larger number of piezo-electric transducers than is required for a direction measurement, in particular if the flow to be examined can originate from all directions, and, in certain directions, certain transducers or transducer pairs are less favourably situated for obtaining a good transit time measurement. In that case the transducers with the least favourable position can be switched off, and then sufficient transducers remain for obtaining an unambiguous determination of the direction. Switching off can, for instance, take place on the basis of a preceding coarse direction measurement, for instance at the beginning of a measurement series. Although in the preceding description gas flows have been discussed, it will be clear that also in the case of liquid flows similar measurements can be formed. For measuring the humidity of a gas also use can be made of less attenuated oscillations, and then the amplitude decay of the envelope is determined.

Claims: A method for determining the velocity of a flow (30), in particular a gas flow, in which a damped acoustic signal (1) is emitted by a first transducer (12) in a first direction or sense through said flow (30) towards a second transducer (13), which, on reception, produces a corresponding damped electric signal (3), which is also done in a different direction or sense, the transit time, in each of the directions, of the acoustic signal (1) between the transducers (12, 13) in question being measured by measuring the time lapsed between the emission and the reception of the acoustic signal, each of the transit time measurements being started at the emission of the acoustic signal (1) by the first transducer (12), the velocity of the flow being derived from the difference between said transit time measurements, characterised in that the acoustic signal (1) emitted by the first transducer (12) is a strongly damped pulse which, in the second transducer (13), gives rise to a damped alternating electric signal, the first deflection (4) of which in the one sense has a larger amplitude than the subsequent deflections in the same sense, which signal is compared with a threshold value (5) which is lower than the peak value of the first deflection (4), exceeding said threshold value (5) being used as the end of the time measurement period. The method of claim 1, characterised in that the emission of the acoustic pulse (1) enables a timing pulse counter (16) adapted to count timing pulses (6) produced by an independent source (18), said counter (16) being stopped at the reception of a threshold excession signal, the emission of acoustic pulses (1) taking place at an arbitrary instant in respect of the fixed time pulses (6). The method of claim 2, characterised in that the repetition frequency of the acoustic pulses (1) is substantially lower than the decay frequency of the signal (3) emitted by the second transducer (13), and in that the frequency of the timing pulses (6) is substantially higher than said decay frequency. The method of claim 2 or 3, characterised in that a plurality of time measurements is performed successively, and in that the transit time is determined by a statistic interpolation of the various separate measurement results. The method of any one of claims 1 to 4, characterised in that the transit time measurements are made by means of acoustic signals emitted and received under different angles, and in that the velocity and temperature of the flow are derived from these measurements made under different angles. An apparatus for performing the method of any one of claims 1 to 5, comprising at least a first (12) and a second (13) transducer for emitting and receiving respectively of an acoustic signal (1), and means (14) for comparing the electric signals (3) produced by the second transducer (13) with a threshold value (5), and means (16) for determining the time lapse between the emission of an acoustic signal by said first transducer (12) and the instant on which the threshold value (5) is exceeded, characterised in that the first transducer (12) is adapted for emitting strongly damped acoustic signals, in that the threshold value (5) is lower than the first deflection (4) of the electric signal produced by said second transducer (13), and in that the energising circuit of said first transducer (12) is connected with the enabling input of a pulse counter (16), and the output of the threshold circuit (14) is connected to the disabling input of said counter (16), the counting input of said counter (16) being connected with a source (18) of timing pulses (6). The apparatus of claim 6, comprising a plurality of second transducers adapted to receive acoustic pulses originating from different directions, characterised in that the means connected therewith for determining the transit time of the acoustic pulses (1) in question are connected with a summing circuit (22) which is connected with means for computing the temperature of the flow from the sum of transit times. The apparatus of claim 6 or 7, characterised in that at least one second transducer (13) is connected with a threshold circuit (24) with different thresholds (5'), adapted for determining the highest value of the first deflection (4) of the produced electric signal (3), which threshold circuit (24) is connected with a circuit (25) for comparing the highest value thus determined with a reference value (26), and for computing the humidity of the flow therefrom. The apparatus of any one of claims 6 to 8, characterised by a single first transducer (12) and a reflection body (28) placed in front of said transducer (12), this in such a manner that the flow to be examined (30) can flow through the interspace therebetween, which reflection body (28) is adapted to reflect the acoustic pulses (1) emitted by said first transducer (12) through said flow (30) along differently oriented paths through said flow towards one or more second transducers (13). The apparatus of claim 9, characterised in that the reflection body (28) is a pyramid, its apex being directed towards the centre of said first transducer (12). The apparatus of any one of claims 6 to 10, characterised in that the number of transducers is larger than required for determining the direction of the flow, and in that means are provided for switching off those transducers with the least favourable orientation in respect of said flow, as well as means for determining the flow direction for controlling the first-mentioned means.

Inventors: BREEUWER, RENE, Breeuwer, René
Applicants: LEICA B.V.
Application year: 1986
Main classification: G01P5
IPC codes: G01P5, G01K11, G01P13, G01N29, G01F1