A DEVICE FOR MEASURING THE FLOW VELOCITY OF FLUIDS

Abstract: A device for measuring the flow velocity of fluids including at least one pair of electro-acoustic transducers (tr1, tr2) at the ends of a measurement path, said transducers simultaneously transmitting acoustic pulses and receiving the same at first and second times, a transmission circuit, a receiving circuit, at least one integration circuit having an integration capacitor (C3), the charge and discharge circuits of which are controlled by the transit times of the acoustic pulses, the starting point of which being sharply defined by a control circuit of both transducers.

Description: - A device for measuring the flow velocity of fluida - The invention relates to a deviςe for measuring the flow velocity of fluids including at least one pair of electro-acoustic transducers to be positioned at the ends of a measurement path, each pair of said transducers si- multaneously transmitting acoustic pulses and receiving the same at first and second times dependent on the ve¬ locity of the fluid, a clock pulse generator., a trans¬ mission circuit, a receiving circuit including an ampli¬ fier and a detection circuit for each of the transducers separately, at least one integration circuit including an integration capacitor for use in processing the diffe¬ rence in propagation time of the acoustic pulses, wherein the transmission and reception times for each of the transducers are determined. A device of this type is of practical knowledge in the pertaining field. In the fluid flow technics several applications of devices for measuring the flow velocity of a liquid or gas in pipes, ducts and the like are generally known, all utilising the physical property that pressure or sound waves propagate in a fluid at a velocity that applies with re * spect to said fluid. Hence the effective propaga¬ tion velocity with respect to a stationary reference po¬ sition is the resultant of the flow velocity of the fluid with respect to said reference position .plus the propa- gation velocity of the sound in said fluid. When presuming for instance a measurement path AB within a fluid having a length L the resultant velocity in the direction from A to B is:.L/t.-g = C + Vcos φ and the resultant velocity in the direction from B to A is: = C - Vcos , in which V is the flow velocity of the fluid and 0 is the angle between the low direction of the fluid and the measurement path AB. Where the sound velocity C is not constant, said velocity being dependent among others from the temperature and the salt conσentra- ^^Tfj- tion and the value of said velocity is not always known r either it is prefered to use the equation X V T cos < aϋ . = -Lx . - t rAB - " — t rBA - ~ τ AB x τ BA In accordance with the known technics both the elec tro-acoustic transducers provided at opposite ends of th measurement path simultaneously emit short acoustic pul¬ ses. In this way one avoids moreover disturbing effects o interferences through reflections and other paths than the measurement path as occur when using continuous sound tones. Where both the transducers provided at opposite end of the measurement path function as a transmitter and also as a receiver the same value of L applies to both sound transmissing directions. This equality is an im- portant advantage when measuring flow velocities V of a small value with respect to the sound velocity C. When very accurately determining the transmission times as well as the reception times the propagation times as wel as the difference in propagation time of both transits may be determined wherein the sound velocity C is inclu¬ ded in the calculation. « An object of the invention is now to provide a de¬ vice having a very simple construction for determining the above function and by means of which at low flow ve- locities of the fluid a high accuracy of the measurement and a very good zero stability are obtained. In a device of the type mentioned above the object is attained in accordance with the invention in thaff-rfn- tegration capacitor is connected to a potential divider connected to a gate circuit and having in each leg there of a switching means conductive in the rest condition after the transmission time, two different potentials being supplied in the rest condition to the one leg and to the other leg of said divider whereby the capacitor adjusts itself to the middle of the potential difference OMPI _ while controlled by the gate circuit the switching means associated with the one transducer is blocked after the first reception time and subsequently the switching means associated with the other transducer is blocked after the second reception time. The invention will now ' be described on the basis of an embodiment thereof having reference to the drawings in which: Fig; 1 shows an example of a measurement path pro- vided within a flowing fluid; Figs. 2a and 2b represent a diagram of the trans¬ mission circuit associated with the two transducers as well as of a receiving circuit including an amplifier and a detection circuit associated with the one or the other of said transducers, respectively; Fig. 3a represents a diagram of the gate circuit connected to both receiving circuits and the subsequent integration circuit for the difference in transit time including sampling and hold circuits; Fig. 3b shows a possible embodiment of the integra¬ tion circuit; Fig. 3c shows an other possible embodiment of the integration circuit; Fig. _■ represents a diagram of the propagation time integration circuit; Fig. 5 shows a diagram of the clock pulse generator of the device; Fig. 6 shows a number of rectangular waves for elu¬ cidating the operation of the device; Figs. ?a and 7b exemplify possible flow velocity distributions of the fluid within a pipe; and Fig. represents a cross section of a pipe in which it has been indicated that the measurement path is located at a certain distance from the axis of the pipe. * In fig. 1 there has been shown an example of the general location of a measurement path AB that has been arranged within a fluid flowing at a velocity V and making an angle § ( with respect to the direction of the flow. At both the opposite ends there has been provided an electro-acoustic transducer. For the velocity compo¬ nent the above derived equation applies. As has already been indicated above it is very im¬ portant that the exact time of transmission of the acous¬ tic pulses as well as of the receipt of the received sig¬ nal in both receiving circuits be determined as accura¬ tely as possible. When transmitting by means of electro- acoustic transducers it is first of all important to have a transmission power as high as possible as well as a transmission time and a transmission signal for both the transducers or crystals that are as accurate and identical as possible. With reference to Fig. 2 there will be described • the transmission circuit associated with both the elec¬ tro-acoustic transducers as well as a receiving circuit including an amplifier and detection circuit associated with one of said transducers. A coil is included in the load circuit of an end transistor T3. The base of the end transistor T2 is connected to a control transistor T1 through a EC network (G1 , E1). For obtaining a high transmission power i.e. a high transmission potential a not sharply changing current should run through the coil L during a short time. The potential across the coil and hence on the crystals is thereby small due to the gra¬ dually increasing current. The current control through the coil L occurs by means of the end transistor T2, the base of which is connected to the said RC network. By supplying a clock or reset pulse from the clock pulse generator (vide Fig. 5) to the control transistor T1 this transistor T1 is cut off whereby the potential at the base of the transistor T2 increases with an e-power and the current in the load circuit of the same transistor T2 increases slowly, while the control transistor T1 is cut off. The thus caused current running through the coil is deter¬ mined by the elements R , C , R2 and the width of the reset pulse. The gradual increase of the current through the coil L in accordance with the e-power of the RC-net- work serves to avoid already before the said transmission time a pulse though small is transmitted that might cause disturbances. The current through the coils is not limi¬ ted to a maximum value but dependent on the maximum power dissipation of the end transistor T2. When the clock potential becomes positive the con¬ trol transistor T1 is rendered conductive whereby the base of the end transistor T2 is connected to ground. Consequently the current in this transistor T2 and hence also through the coil is abruptly cut off. As a conse- quence thereof there is generated a high induction poten¬ tial across the coil this potential being supplied to the transducer tr 1 through a condenser and to antiparallelly arranged diodes e.g. D1 and D2. The transducer or the crystal will then oscillate in its own resonance fre- quency and hence emit a transmission pulse in the fluid. By means of this control method the crystals during the transmission, are supplied with an identical signal. Du¬ ring the reception the crystals are separated from each other by means of the two pairs of antiparallelly ar- ranged diodes. Instead of these diodes there may also be used electronically controlled switches. After the transmission by the first transducer tr 1 and the second transducer tr 2, respectively, the acous¬ tic pulses are received by the second transducer tr 2 and the first transducer tr 1, respectively, after a cer¬ tain transit time. From the transducers the received sig¬ nals are supplied through a commutator T3 to a receiving circuit comprising an optionally selfcontrolling ampli¬ fier circuit T and a detection circuit T5, T6, T7, T8, T9, T10. The transducers tr 1 and tr 2, respectively, are connected alternately per repetition period to the one and to the other receiving circuit. For clearness sake there has been shown only one receiving circuit (T , T5, T6, T7, T8, T9, T10) in Fig. 2b. After amplification by the amplifier circuit T .the received signal is supplied to two differential ampli¬ fiers T5, T8 each one functioning as a potential compa^ rator. To the plus-input of the differential amplifier T5 there is adjusted a level corresponding to noise level by means -of which the threshold for the lowest adjustable level is determined that has to be surpassed by the re¬ ception signal. Upon supplying the reception signal con¬ sisting of different successive waves to the minus-input a detection signal having a climbing front will be sup¬ plied at the output of the level detector when the said adjusted level is surpassed for the first time. The detection circuit operates continuously and therefore also during the transmission. It being known approximately within which time intervalafter the trans¬ mission time the reception of a signal may be expected, the output signal of the level detector T5 will only be transmitted within said time interval indicated by a time window supplied by the clock pulse generator. To that effect there is inserted a switching transistor T6 be¬ tween the output of the level detector T5 and ground, said switching transistor only being blocked during said time window (vide Fig. 6; signal T) supplied by the clock pulse generator so that the detection signal emana¬ ting from T5 may be transmitted to the gate circuit T7. The gate circuit T7 consisting of a gate combination of two Not-OR-gates operates as follows: by supplying the reset pulse (vide Fig. 6) to the upper Not-0R-gate of the gate combination there is generated the leading edge associated to the transmission time of the switching sig¬ nal D obtained at the output. The trailing edge of the signal is determined by the detection signal of T5. Such a gate circuit has the important advantage that upon the detection after the " reset pulse i.e. aft* -gfRE_ OMPI the transmission there may only be given one change from zero to puls or the reverse thereof. Consequently the ad¬ vantage of this gate circuit is that positively and nega¬ tively going edges may be obtained simultaneously with- out any switching of a separate gate being required for obtaining the second edge when starting from a certain first edge. If for instance from a positive edge a nega¬ tive edge would have to be derived then an extra gate should be incorporated in one of the lines that is to say a time delay of 20 nanoseconds. The puls-input of the second differential amplifier T8 is grounded. The output of this zero point detector T8 is supplied across a resistor to a gate circuit T10 that is identical with T7. By means of T9 under the con- trol of T7 the output of T8 is grounded. Upon receipt of a signal T9 will be blocked so that T8 may transmit its signal to T10. The edge of this control signal from T10 ■ now corresponds in time to the first zero crossing of the received signal occuring after the first surpassment of the level adjusted by means of T . In this way the time position of the (detection) trailing edge of T10 (signal P) is independent from the amplitude of the re¬ ceived _ignal. In this way detection signals indicating the first and the second reception time are alternately per repe¬ tition period supplied to the lines B and B' . In Fig. 3a there is represented a transit time dif¬ ference integration circuit by means of which the diffe¬ rence in propagation t between the two propaga- tion times is converted into a potential difference \ Y, which conversion will have to be as accurately as pos¬ sible in order to render for instance the measurement of a difference of 0.1 nanosecond well feasible. In Fig. 3b there is shown a first embodiment of the integration circuit as well as the subsequent sampling and hold circuit, whereas in Fig. 3c there is shown a second embodiment of the integration circuit. In Fig. " - _ the gate combinations T10, T10' respec¬ tively are again shown to which gate combinations the de¬ tection signals B and B'are supplied. Upon application of the reset pulse (vide Fig. 6) to each upper Not-OR-gate of each gate combination there is generated the leading or front edge associated with the starting time of the switching signals P1 and P2 (vide Fig. 6) received from the.output of T10, T10' . The back edges of both said switching signals are determined by the first and by the second detection signal, respectively. The gate combina¬ tion T10, T10' is followed by the potential divider of the integration circuit, to the middle of which the in¬ tegration capacitor C3 is connected. It will now be elucidated that in the rest condition there is supplied to the upper leg (R3 . E5) of the poten¬ tial divider a positive potential P1 (comparable with a voltage source) with respect to the potential ___ sup¬ plied to the lower leg (R , D6) of the potential divider (for instance +w with respect o -w = zero Volt). In the rest condition the potential at point on the capacitor 03 equals then the middle between P1 and P2. Upon detec¬ tion of _. potential the potentials P1 and P2 will then subsequently change such that the potential between P1 and P2 is reversed. Thereby it is possible that at first P1 and thereafter P2 or the reverse will change in mag¬ nitude. The potentials P1 and P2 are controlled independent¬ ly, that is to say that the potential P1 is controlled by the receiving circuit connected at that time to the transducer tr 1 and the potential P2 is controlled by the receiving circuit connected at that time to the trans¬ ducer tr 2, said receiving circuits being alternated per repetition period as has been discussed already. When the transmitted sound waves arrive at the same time that is to say when the flow velocity of the fluid is zero m/sec the points P1 and P2 will be subject to a potential change at the same time whereby the diodes D5 and D6 are blocked. Thereby the potential on the capaci¬ tor C3 will not change. When the transmitted signals do not arrive at the same time the detection signals emitted by both receiving circuits will not occur at the same time whereby.P1 and P2 will not be subject simultaneously to a potential change so' that for instance D5 is blocked first, whereas the diode D6 is blocked only at a time being a time in¬ terval corresponding to the difference in propagation time later after the first reception time. Within this time interval corresponding to the difference in propa¬ gation time the potential on the capacitor C3 may change in positive or in negative direction. This change is also a measure of the flow velocity of the fluid-. It is of importance that the potential at point Q is as stable as possible and that this potential will not be changed by other causes. To that effect the point should be terminated by a high ohmic impedance. This may for instance be attained by connecting the capacitor C3 to a buffer amplifier T12. The buffer amplifier may then be followed by a DC amplifier. The rate of change of the potential on the capacitor C3 is dependent on the ele- ments R3, R , C3 as well as on the potentials +w and -vv. In Fig. 3c there is shown another embodiment. There¬ in the potentials +w and -w are supplied by a fixed power source. In the potential divider there have now been included no diodes but switches G1 and G2 in series which are conductive in rest condition. Like in Fig. 3b the capacitor C3 at point Q will acquire in the rest con¬ dition a potential that is adjusted to the middle of the potential difference. Upon detection in the detection circuit and from the receiving circuits the switches G1 and G2 are opened by the switching signals P1 and P2 from the gate circuit. ^O EΛ O.-PI ( Within the time interval, corresponding to the .diffe¬ rence in propagation time between the opening of the switch G1 (or G2) and the opening of the switch G2 (or G1) the potential at point may change. This potential change is again also a measure of. the flow velocity of the fluid. Electronic switches but also other components, for instance field effect transistors, may be used as the switches -G1 and G2. From point Q the potential of the capacitor is sup¬ plied through a buffer amplifier to a double sampling switch T13. Starting from the equation V 1 c C o 0 s S PiD = £2 ' t tj ^ LB x ' t t ] B 3A A this being approximately equal to Vcos = constant .—5- t now the flow velocity V of the fluid may be measured by determining the quantity \t and the quantity t . Ap- proximately t.g. g. may be assumed to be equal to t so that it is thus sufficient to determine one of the pro¬ pagation times. Starting from the buffer amplifier T12 it would therefore be sufficient to determine only the quantity Δ.V because apart from a constant this potential change is proportional to the difference in propagation time. However, in order to compensate all balance phenomena caused by time and potential variations within the recei¬ ving circuits and within the gate and integration circuit there are utilized the said switches T3 and T13. The commutator T3 (vide Fig. 2a) and the commutator T13 (vide Fig. 3a) consist of electronic switches. The switch 1 changes the transducer connections from the one amplifier circuit to the other and in reverse, and is controlled by J.K. flipflop T19 shown in Fig. 5 that has been arranged as a two-divider. This two-divider divides the reset signal (vide Fig. 6) from the base clock cir- cuit T18 so that the signals Q and Q are supplied to the control terminals of the commutator T3. Where each of the receiving circuits is now alter¬ nately connected to the transducer tr 1 and the trans- ducer tr 2 this will result in the propagation time dif¬ ference convertor (At— _~ Δ^) that the potential at point Q alternately becomes above and below the rest po¬ tential. This alternating potential is, however, proces¬ sed with ' difficulty. By means of the double sampling switch T13 this al¬ ternating potential is again converted into two poten¬ tials, i.e. one positive with respect to the rest poten¬ tial and one negative with respect to the re?wl§ p^mt Q. When this potential delivered by the capacitor C3 and sampled by means of the sampling switches is by turns- supplied to a hold circuit T1 , T15 and these potentials are then subtracted from each other in a subsequent dif¬ ferential amplifier T16 there only remains two times the potential change _ V for the rest potential is eli ina- ted in the differential amplifier. The double sampling switch T13 (vide Fig. 3a) is controlled by the pulse signals S2 and S3 supplied by a gate circuit T20 in the clock circuit of the Fig. 5» The douple sampling switch operates thereby as follows: the switch T13a is energized by the S2 signal when the Q signal (vide Fig. 6) from the two-divider T1 is zero and both the detection signals are present, i.e. both the acoustic pulses are received. The switch T 3d is ener¬ gized by the S3 signal when the Q signal from two-divi- der is +vv and both the detection signals are present. - The two sampling switches a and d remain closed only for a short while so that a sampled potential is supplied to the subsequent hold circuits. In Fig. •_ ■ there is shown a propagation time integra- tion circuit by means of which the quantity t is deter¬ mined. This determination of the propagation or transit time is performed by means of a potential integration -gTTfEΛ> OMPI circuit. Therefore to a gate circuit T17 having Not-AND-gates there is supplied a reset pulse provided by the clock pulse generator to one of the ΪTot-AND-gates, whereas to the other input thereof there is supplied the P2 swit¬ ching signal. The P2 switching signal is likewise sup¬ plied ' to a second Not-AND-gate, to the other input of which the P1 switching signal is supplied. The output signal obtained at the output of this gate through a ca- -pacitor is supplied to a third Not-AND-switch, from the output of which the S1 pulse signal (vide Fig. 6) is ob¬ tained the leading edge of which coincides with the se¬ cond detection signal, i.e. with the end of the time in¬ terval corresponding to the difference in propagation times. Through a second gate circuit T18 having NOt-AHD- gates a potential -w is supplied to the input of the in¬ tegration circuit T19, the time interval for supplying this potential running from the transmission time to the reception time of one of the two detection signals. Where the supplied potential is constant the output potential of the integration circuit T19 is direct pro¬ portional to the propagation time t. In Fig. ' 5 there has been shown a clock circuit in which starting from a trigger circuit T17 there is ob¬ tained a reset pulse that is also supplied through one of the Not-AND-gates of the gate circuit T1S for obtaining an inverse reset pulse. From the output of this Not-AND- gate the signal is supplied through a delay circuit to both the inputs of a second MOt-AND-gate in T18, from the output of which the output signal is supplied through a capacitor to both the inputs of a third Not-AND-gate in T18. From the output of the third Not-AND-gate the time window T is obtained for controlling the switching ele- ments T6 provided at both the outputs of the detection circuits T5. The reset pulse obtained from the output of the first Not-AND-r-gate is supplied to the input of a J.K. flipflop T19, from the outputs of which the two mutually opposite Q-signals are obtained. The flipflop T19 is yet followed by a gate circuit T20 comprising two gate com¬ binations. The Q-signal is supplied to the inputs of a Not-OR-gate in both the gate combinations, whereas like¬ wise the S1 signal is supplied to the second Not-OR-gate of one of said gate combinations. The signal obtained at the output of this Not-OR-gate is therein supplied to the input of the associated Not-OR-gate of this combination and to an input of a Not-OR-gate of the second gate com¬ bination to which the Q-signal is not supplied. The S2 and S3 pulse signals are then obtained from the two out- puts of the Not-OR-gates to which the Q-signal is sup¬ plied. With reference to the mutual time relations of the different signals reference is made to Fig. 6 in which the transmission time is marked with the reference ST. The potentials obtained from the propagation time integration circuit (Fig. 4) and from the propagation time difference circuit (Fig. 3a) are supplied to an analogous computation unit. The mean velocity of the fluid across the measurement path is then calculated from . dividion may be adjusted by means of the combination R3, R4 and C3 in the integration circuit, the amplifier in - Fig. 3a/b and the gain of the different amplifiers in Fig. 4. When measuring the flow velocity of the fluid through ajpipe or duct a further important factor is yet the relation between the mean flow velocity measured a- cross a measurement path at a location within the pipe or duct, and the real mean flow velocity across t entire surface of the cross section of the pipe, or duct. In general it will prove to be necessary to apply a cor¬ rection faktor in order to convert the mean flow ' velo¬ city measured across a certain measurement path into the real mean flow velocity across the entire surface of the cross section. As is well known the correction factor i.e. the ra¬ tio between the measured and the real mean flow velocity across the surface of a section in the pipe, is dependent on the flow velocity profile of the fluid. Hence two flow technically different cases may be considered having re¬ ference to Figs. 7a and b in which the pipe wall is in¬ dicated with the reference BW. 1. The fluid is a non-Newtonian liquid such as for instance tooth paste (a Bingham liquid). For most of the non-Newtonian liquids there may " be observed a phenomenon called plug flow. The distribution of the flow velocities within the pipe then take the course of a straight line, vide Fig. 7a. Only close to the wall the velocity de- creases whereas the velocity at the wall will then be ze¬ ro. The mean velocity across a measurement path within the pipe is therefore almost exactly equal to the mean flow velocity across the cross section of the pipe. This means that in this case K = 1. 2. The fluid is a Newtonian liquid whereby three possibilities may be distinguished: 2a) a laminar flow in which the velocity distribu¬ tion within the pipe takes a parabolic course (vide Fig. 7b). To a- laminar flow, omitting some derivations, there applies the equation K = 1/(4/3 - 4/3b 2 ) . The relative • displacement of the measurement path with respect to the axis of the pipe is therein b = B.R. in which R is the radius of a circular cross section of the pipe and B is a factor smaller than 1. 2b) a turbulent flow, vide Fig. 7a in which the ve¬ locity distribution across the pipe is substantially ho¬ mogeneous. However, only close to the wall of the pipe a_ liquid film having a laminar flow is found. The. thickness of this film is dependent on the Reynolds number. Espec¬ ially it may be derived that K = 0.889 + 0.0091 log Re t 0.0001 (log Re) . To a measurement path ML at a distance B.R. with respect to the axis of the pipe there applies after derivation the equation (vide Fig. 7c): wherein 1/n = 0.250 + 0,023 log Re. By means of a computer the mean flow velocity may be determined as a function of B and Re whereupon may be calculated in a simple manner. 2c) a flow without a known velocity ..distribution in which the flow may be within the transitional area be¬ tween laminar and turbulent flow ( 2000 {Re <4000) , in which Case the correction factor __ varies from 0.75 to 0.93. The flow velocity profile may also be disturbed, for instance due to anobstacle within the pipe, a bend, a valve and the like. In such a case no correction factor can be calculated. This problem may, however, be elimina-- ted by t allowing a stabilization of the flow. To that ef¬ fect there is required a pipe length having a length of at least twenty times the pipe diameter. According to a further alternative solution for performing a measurement that is completely independent from the ' velocity profile, the flow velocity of a liquid will be measured across several measurement paths at different locations within the cross section of the pipe. The different values of V may then be integrated numerically for obtaining a total mean velocity. This requires, however, a certain number of measurement paths and many electronic circuits. According to another alternative solution it is, however, very well possible to find a measurement path within the pipe for which the correction factor for la- minar flow equals about the correction factor for turbu- ' KEJQT c:?ι lent flow. Thus is has already been calculated.that if the measurement path is located at a distance from the axis of the pipe being between 0.497 s and 0.523 B the correction factor K will be the least dependent on the flow velocity profile. At this location the correction factor Σ- would then equal 1. According to the invention it has, however, become apparent experimentally that the above mentioned adjust¬ ment range of 0.497 ^. b ^ 0.523 is not correct. This is due to the fact that the extensiveness of the electro- acoustic transucers per se was not accounted for. If, however, this extensiveness is included in the theoreti¬ cal model it appears that the calculations correspond to the results of the experiments. In accordance with the above it has become apparent that the K-factor being the most independent from the flow velocity profile -is ob¬ tained when the displacement of the measurement path wit respect to the axis of the pipe or duct is between 0.45 and 0.49 R. This displacement is thereby in accordance with the invention dependent on the ratio between the diameter of the pipe and the diameter of the transducer. OMPI

Claims: C L A I M S . A device for measuring the flow velocity of fluids including at least one pair of electro-acoustic transducers to be positioned at the ends of a measurement path, each pair of said transducers simultaneously trans- mitting acoustic pulses and receiving the same at. first and second times dependent on the velocity of the fluid, a ςlock pulse generator, a transmission circuit, a recei¬ ving circuit including an amplifier and a detection cir¬ cuit for each of the transducers separately, at least one integration circuit including an integration capaci¬ tor for use in processing the difference in propagation time of the acoustic pulses wherein the transmission and reception times for each of the transducers are determi¬ ned, c h a r a c t e r i z e d i n t h a t said inte- gration capacitor (C3) is connected to ajpotential divider connected to a gate circuit (T10, T10') and having in each leg thereof a switching means conductive in the rest condition after the transmission time, two different po¬ tentials being supplied in the rest condition to the one leg and to the other leg of said divider whereby the ca¬ pacitor adjusts itself to the middle of the potential difference, while controlled by the gate circuit (T10, T10 ! ) the switching means associated with the one trans¬ ducer is blocked after the first reception time and sub- sequently the switching means associated with the other transducer is blocked after the second reception time. 2. The device of claim 1 in which the clock pulse generator supplies a clock pulse associated with the transmission time, c h a r a c t e r i z e d i n t h a t the gate circuit (10, T10') comprises two gate combina¬ tions to each of which there is supplied the clock pulse, and in that to the one leg of the potential divider the detection signal supplied by the one detection circuit and to the other of which having its output connected to the other leg of the potential divider there is supplied the detection signal supplied by the other detection cir¬ cuit such that each gate combination at its output sup¬ plies a switching signal corresponding to the propagation time of the pertaining acoustic pulse so that the capaci- • tor is subject to a potential variation corresponding to the difference in propagation time (Fig. 2a). 3. The device of claim 2, c h a r a c t e r i z e d i n t h-a t at its terminals the potential divider is inserted between the outputs of said two gate combina¬ tions and that the switching means are diodes (D5, D6; Fig. 3b). 4. The device of claim 2, c h a r a c t e r i z e d i n t h t at its terminals the potential divider is inserted between two different DC-potentials and that -the switching means (G1, G2) each via its control terminal is connected to the output of the associated gate combina¬ tion (Fig. 3c). 5. The device of anyone of the preceding claims, c h a r a c t e r i z e d i n t h a t in each of the receiving circuits the detection circuit comprises in series a level detector (T5) adjusted to noise level and a zero ,point detector (T8) adjusted to zero level, to bot of which detectors (T5, T8) the reception signal is sup- plied and both of which are interconnected such that the zero point detector (T8) can only supply a detection sig¬ nal upon a detection signal supplied by ' the level detec¬ tor (T5) when the noise level is surpassed. 6. The device of claim 5 . c h a r a c t e r i z e d i n t h a t each of both said detectors consists of a • differential amplifier (D5, D8), the plus-inputs of which are connected to noise level and zero level, respectively whereas to the minus-inputs thereof there is supplied the reception signal, whereby apart from being connected to the gate circuit (T10, T10') the output of the zero point detector (T8) is connected to mass through a switching means (T9) which is blocked only upon receipt of a detec- OMP tion signal from the level detector (T5). 7. The device of claim 6, c h a r a c t e r, i z e d i n t h a t between the output of the level detector (T5) and the switching means (T9) there is inserted a gate combination (T7) of two Not-OR-gates wherein the clock pulse (R) from the clock pulsegenerator is supplied to an input of the first Not-OR-gate and the detection signal from the level detector (T5) is supplied to an in-r- put of the second Not-OR-gate, and wherein the other in- put of the first and the second Not-OR-gate, respectively, is connected to the output of the second and the first Not-OR-gate, respectively. 8. The device of anyone of claims 5 . 6 and 7. c h a r a c t e r i z e d i n t h a t the output of the level detector (T5) is also connected to mass through a switching means (T6), said switching means (T6) being - controlled into conductive condition except during a time window (T) provided by the clock pulse generator within which the reception signal is expected. 9- The device of anyone of the preceding claims in which both the transducers in the transmission circuit are controlled by means of the same clock pulse, said trans¬ mission, circuit comprising at least one transistor having a coil included in the load circuit across which coil a transducer is connected, c h a r a c t e r i z e d i n t h a t both the transducers (tr 1, tr 2 ) are connec¬ ted to the same said coil (L) each of them by means of a pair of antiparallelly arranged diodes (D1 , D2; D3, D4) , that said transistor (T2) in its base circuit is connec- ted to a controlling transistor (T1) through a RC-net- work, said controlling transistor (T1) being cut-off du¬ ring the clock pulse and opened upon termination of said clock pulse so that in said transistor (T2) the current is. thereby abruptly interrupted whereby a high induction voltage is produced in said coil (L). 10. The device of anyone of the preceding claims in which the integration capacitor is connected to the further part of the propagation time difference integra¬ tion circuit through a buffer, c h a r a c t e r i z e d i n t h a t between both the outputs of the transducer (tr 1, tr 2) and both the receiving circuits a commutato (T3) and connected to the output of the buffer (T12) a double sampling switch (T13) are included, the same bein controlled such that per repetition period each of the transducers is connected alternately to the first and th second receiving circuit, respectively, and that upon termination of the second detection signal alternately i one of the two repetition periods the output potential o the buffer (T12) is supplied by means of the first or th second sampling switch, respectively, to a hold circuit (T15) for positive voltage variations and to a hold cir- cuit (T14) for negative voltage variations, respectively the outputs of both said hold circuits being connected t a differential amplifier (T16). 11. The device of anyone of the preceding claims used for measuring .the flow velocity of a fluid within a pipe or duct having a generally circular cross section (radius R), c h a r a c t e r i z e d i n t h a t the measurement paths employed in a number of one or more are arranged at a position displaced over a distance of from 0.45 R to 0.49 R with respect to the axis of the pipe or duct.

Inventors: HOOGENDIJK C, YMKER L
Applicants: HOOGENDIJK C, RHEOMETRON AG, YMKER L, PRODUCTIEBEDRIJF RHEOMETRON AG
Application year: 1979
Main classification: G01F1
IPC codes: G01F1, G01P5, G01S11