ULTRASONIC METER AND METHOD FOR SENSING A FLOW VARIABLE

Abstract

An ultrasonic meter for recording a flow quantity dependent on a flow of a fluid, has a control device, a measuring tube having a plurality of side walls, mutually adjacent side walls being at an angle to one another, and through which the fluid can flow in a longitudinal direction of the measuring tube, and first and second ultrasound transducers which are arranged at a distance from one another in the longitudinal direction on the measuring tube. The first and second ultrasound transducers respectively contain one transducer element or a predetermined arrangement of a plurality of transducer elements. The ultrasound transducer can be driven by the control device in order to excite an acoustic wave conducted in a side wall of the measuring tube, and conducted through the fluid to the other ultrasound transducer and recorded there by the control device to determine a signal time of flight.

Claims

1. An ultrasonic meter for recording a flow quantity dependent on a flow of a fluid, the ultrasonic meter comprising: a control device; a measuring tube having a plurality of side walls, mutually adjacent ones of said side walls being at an angle to one another, and through said measuring tube the fluid can flow in a longitudinal direction of said measuring tube; and ultrasonic transducers, including a first ultrasonic transducer and a second ultrasound transducer, which are disposed at a distance from one another in the longitudinal direction on said measuring tube, said first and said second ultrasound transducers respectively contain one transducer element or a predetermined configuration of a plurality of transducer elements, at least one of said first ultrasound transducer and said second ultrasound transducer is drivable by said control device to excite an acoustic wave conducted in one of said side walls of said measuring tube, the acoustic wave being conducted through the fluid to a respective other of said ultrasound transducers and can be recorded there by said control device in order to determine a signal time of flight, wherein an excitation width of at least one of said first ultrasound transducer or said second ultrasound transducer, over which said transducer element or said configuration of said transducer elements extends, is at least 50% of a width of an inner surface of one of said side walls on which a respective one of said ultrasound transducers is disposed, and/or wherein a propagation direction of a conducted wave which can be excited by at least one of said first ultrasound transducer or said second ultrasound transducer is at an angle to the longitudinal direction of said measuring tube, and/or wherein said conducted wave can be emitted over a predetermined angle range by said first ultrasound transducer and/or said second ultrasound transducer.

2. The ultrasonic meter according to claim 1, wherein said measuring tube has a rectangular tube cross section.

3. The ultrasonic meter according to claim 1, wherein said transducer element or said transducer elements is or are deformable in order to excite the conducted wave, said transducer element or said transducer elements respectively having a round or elliptical contact surface for coupling with said one side wall.

4. The ultrasonic meter according to claim 1, wherein said transducer elements of at least one of said first ultrasound transducer or of said second ultrasound transducer are disposed linearly, parabolically, in a concave arc or in a v-shape.

5. The ultrasonic meter according to claim 1, wherein said transducer element is deformable in order to excite the conducted wave and has a rectangular contact surface for coupling with said one side wall, two sides of said rectangular contact surface being perpendicular to the propagation direction, and side lengths of said two sides corresponding to the excitation width.

6. The ultrasonic meter according to claim 1, wherein the propagation direction of the conducted wave which can be excited by at least one of said first ultrasound transducer or said second ultrasound transducer is at an angle of between 10 and 80 with respect to the longitudinal direction of said measuring tube.

7. The ultrasonic meter according to claim 1, wherein the predetermined angle range is 360.

8. The ultrasonic meter according to claim 1, wherein the excitation width of at least one of said first ultrasound transducer or of said second ultrasound transducer is at least 70% of a width of said inner surface of said one side wall on which said respective ultrasound transducer is disposed.

9. The ultrasonic meter according to claim 1, wherein at least one of said first ultrasound transducer or said second ultrasound transducer is drivable by said control device in such a way that two conducted waves with mutually perpendicular propagation directions can be excited simultaneously or with a time offset by said respective ultrasound transducer.

10. The ultrasonic meter according to claim 9, wherein excitation widths are a same for the two conducted waves which can be excited by said respective ultrasound transducer.

11. The ultrasonic meter according to claim 1, wherein said control device and at least one of said first ultrasound transducer or said second ultrasound transducer are adapted to excite a Lamb wave.

12. The ultrasonic meter according to claim 1, wherein at least one of said first ultrasound transducer or said second ultrasound transducer are disposed on an outer side of said measuring tube.

13. The ultrasonic meter according to claim 1, wherein at least one of said first ultrasound transducer or said second ultrasound transducer is drivable by said control device in such a way that the conducted wave with precisely one mode and/or two conducted waves each with precisely one mode and with mutually perpendicular propagation directions can be excited.

14. The ultrasonic meter according to claim 1, wherein the propagation direction of the conducted wave which can be excited by at least one of said first ultrasound transducer or said second ultrasound transducer is at an angle of between 40 and 50 with respect to the longitudinal direction of said measuring tube.

15. The ultrasonic meter according to claim 8, wherein the excitation width is at least 80% of the width of said inner surface of said one side wall on which said respective ultrasound transducer is disposed.

16. A method for recording a flow quantity dependent on a flow of a fluid, which comprises the steps of: providing an ultrasonic meter having a control device, a measuring tube being formed by a plurality of side walls, mutually adjacent ones of the side walls being at an angle to one another, and through which the fluid flows in a longitudinal direction of the measuring tube, and a first ultrasound transducer and a second ultrasound transducer which are disposed at a distance from one another in the longitudinal direction on the measuring tube, wherein the first ultrasound transducer and the second ultrasound transducer respectively have one transducer element or a predetermined configuration of a plurality of transducer elements; and driving at least one of the first ultrasound transducer or the second ultrasound transducer by the control device to excite an acoustic wave conducted in a side wall of the measuring tube, the acoustic wave being conducted through the fluid to a respective other one of the first and second ultrasound transducers and is recorded there by the control device in order to determine a signal time of flight, wherein the flow quantity is determined as a function of the signal time of flight, wherein an excitation width, over which the transducer element or the configuration of the transducer elements extends, is at least 50% of a width of an inner surface of the side wall on which a respective ultrasound transducer is disposed, and/or the conducted wave is excited with a propagation direction which is at an angle to the longitudinal direction of the measuring tube, and/or the conducted wave is emitted over a predetermined angle range by the first and/or the second ultrasound transducer.

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING

[0042] FIG. 1 is a diagrammatic, longitudinal sectional view of an exemplary embodiment of an ultrasonic meter according to the invention, using which an exemplary embodiment of the method according to the invention may be carried out;

[0043] FIG. 2 is an end view of the ultrasonic meter shown in FIG. 1;

[0044] FIG. 3 is a top view of the ultrasonic meter shown in FIG. 1;

[0045] FIGS. 4 to 8 are top view of further exemplary embodiments of the ultrasonic meter according to the invention; and

[0046] FIG. 9 is a sectional view of a further exemplary embodiment of the ultrasonic meter according to the invention.

DETAILED DESCRIPTION OF THE INVENTION

[0047] Referring now to the figures of the drawings in detail and first, particularly to FIG. 1 thereof, there is shown an ultrasonic meter 1 for recording a flow quantity dependent on a flow of a fluid. The ultrasonic meter 1 contains a control device 2, a measuring tube 3 and a first and a second ultrasound transducer 5, 6. The fluid is guided in an internal space 4 of the measuring tube 3 in a longitudinal direction 14 of the measuring tube 3.

[0048] In order to determine a flow quantity, in particular a flow volume, a time-of-flight difference of the signal time of flight from the first ultrasound transducer 5 to the second ultrasound transducer 6 and vice versa may be determined by the control device 2. Here, use is made of the fact that this time of flight depends on a velocity component of the fluid parallel to a propagation direction of an ultrasound beam 12 through the fluid. From this time of flight, it is therefore possible to determine an averaged fluid velocity in the direction of the respective ultrasound beam 12 over the path of the respective ultrasound beam 12, and therefore approximately an averaged flow velocity in the volume through which the ultrasound beam 12 passes. A problem with conventional ultrasonic meters, which use a single ultrasound beam for this measurement, is that the latter only passes through a very small part of the flow cross section of the measuring tube 3, so that no information is available regarding regions outside the ultrasound beam 12.

[0049] In order to counteract this, an ultrasound beam 12, i.e. a pressure wave, is not induced directly in the fluid by the first ultrasound transducer 5. Instead, a conducted wave (represented schematically by its propagation direction 11), of the measuring tube 3, or in particular of the side wall 7, shown in FIG. 2, of the measuring tube 3 is excited by the ultrasound transducer 5. To this end, an ultrasound transducer 5 is used which contains a transducer element that is deformable perpendicularly to the side wall 7 and/or in the longitudinal direction 14 of the measuring tube 3. The transducer element is coupled with the side surface 7 via a rectangular contact surface, the dimension of which correspond to the plan view, shown in FIG. 3, of the ultrasound transducer 5, in such a way that a deformation of the transducer element also leads to a deformation of the side wall in the region of the contact surface. The excitation is carried out with a frequency which is selected in such a way that a Lamb wave is excited in the side wall 7. Such waves can be excited when the thickness 15 of the side wall 7 is comparable to the wavelength of the transverse wave of the solid, which is given by the ratio of the speed of sound of the transverse wave of the solid and the excited frequency.

[0050] A Lamb wave is a combined shear and pressure wave. A local deformation of the internal surface 8 of the side wall 7 therefore results from the conducted wave traveling along the side wall 7. This in turn results in the emission of a pressure wave into the fluid in the entire region inside which the conducted wave propagates. This is schematically represented in FIG. 1 by the ultrasound beams 12 spaced apart in the longitudinal direction 14. The emission of the corresponding pressure waves takes place at the Rayleigh angle 27, which depends on the speed of sound in the fluid and the phase velocity of the conducted wave. For a particular excitation mode, in the case of a known fluid being examined, a known emission angle therefore results. As is conventional with other ultrasonic meters, in this case as well a signal time of flight may therefore be determined for the signal and, for example, a flow may be calculated therefrom. In contrast to conventional flow meters, however, in this case averaging is also carried out over the propagation section of the conducted wave along the propagation direction 11.

[0051] On the reception side, the principal of conducted waves is also used. As indicated by the arrow 13, by the incident pressure waves from the fluid in the region of the second ultrasound transducer 6, a conducted wave traveling in the direction of the second ultrasound transducer 6 is induced, which can be recorded by the control device by means of the second ultrasound transducer 6. The procedure described therefore leads to the flow velocities being taken into account in a larger part of the measurement region in the measuring tube 3 between the first and the second ultrasound transducers 5, 6.

[0052] As is represented in FIG. 2, a rectangular tube cross section of the measuring tube 3 is used (in which case the corners may be configuredinternally and/or externallyto be rounded to a greater or lesser extent). In order also to take into account maximally large parts of the flow cross section perpendicularly to the propagation direction 11 of the conducted wave, an ultrasound transducer 5 is used whose excitation width extends over a large part of the width 9 of the internal surface 8 of that side wall 7 on which it is arranged. Large parts of the flow profile are therefore also jointly taken into account in the transverse direction of the measuring tube 3 in the scope of determining the signal time of flight and therefore, for example, the flow velocity or the volume flow.

[0053] FIG. 3 shows an external plan view of the side wall 7 of the measuring tube 3 in the region of the ultrasound transducer 5. The width 9 of the internal surface 8 of the side wall 7 is illustrated by the dashed lines. As can be seen clearly in FIG. 3, selection of a sufficient excitation width 10 of the ultrasound transducer 5 makes it possible to take into account almost the entire flow profile of the fluid in the scope of taking into account the signal time of flight and therefore the flow quantity. Furthermore, it may readily be seen that even larger excitation widths may be selected for the ultrasound transducer 5. For example, the excitation width 10 may extend over the entire width 9 of the internal surface 8, or even beyond this.

[0054] In particular when a measuring tube 3 with a large tube cross section is intended to be used, the use of an ultrasound transducer with a sufficiently large width may be technically relatively elaborate. In the following exemplary embodiments, which are represented in FIGS. 4 and 5, however, even in these cases it is possible to achieve the effect that essentially the entire width of the cross section is taken into account during the determination of the signal time of flight and therefore of the flow quantity. In the exemplary embodiment shown in FIG. 4, the excitation width 17 of the ultrasound transducer 16 is significantly smaller than the width of the internal surface 8 of the side wall 7 of the measuring tube 3. In order nevertheless to record the flow profile over its entire width 9, the ultrasound transducer 16 is arranged on the side surface 7, or is driven by the control device (not shown), in such a way that a conducted wave is emitted with a propagation direction 18 that makes the emission angle 19 with the longitudinal direction 14. The conducted wave, or the pressure waves initiated by it in the fluid, therefore has/have a propagation direction which is at an angle to the longitudinal direction 14. The conducted wave, or the pressure waves, therefore propagate(s) as far as the lateral side walls of the measuring tube 3, are reflected on these and change their propagation direction. The width 9 is therefore covered by the pressure waves reflecting between the lateral side walls, or the conducted wave reflected between the latter.

[0055] In order to improve the measurement accuracy of the ultrasonic meter, an additional time-of-flight measurement may optionally be carried out with the aid of a further ultrasound transducer 34. This may, as is represented in FIG. 1, for example be arranged on a side wall lying opposite the ultrasound transducer 5.

[0056] The coverage of the width 9, or of the entire internal space of the measuring tube 3, may be further improved if, as shown in FIG. 5, an ultrasound transducer 20 is used which is driven by the control device in such a way that two conducted waves with mutually perpendicular propagation directions 21, 22 are emitted simultaneously or with a time offset. These conducted waves may preferably be emitted with a respective emission angle 23, 24 of about 45 with respect to a longitudinal direction 14 of the measuring tube 3. In this way, symmetrical propagation is achieved. The wavelengths of the emitted conducted waves and the excitation widths 25, 26 are equal.

[0057] In a further exemplary embodiment (not shown), it would also be possible to use a rectangular ultrasound transducer 20 whose excitation widths 25, 26 are different to one another. In this case, conducted waves with mutually different wavelengths are emitted in the two propagation directions 21, 22.

[0058] FIG. 6 shows a detail view of a further exemplary embodiment of an ultrasonic meter. The representation corresponds substantially to the representation shown in FIG. 3, although instead of the ultrasound transducer 5 shown in FIG. 3 with a single wide rectangular excitation element, an ultrasound transducer 28 is used which has a multiplicity of individual, in particular round or cylindrical, or even rectangular or cuboid, square or cubic or elliptical transducer elements 29. The transducer elements 29 are arranged linearly and the arrangement of the transducer elements 29 extends over an excitation width 30 which is only slightly narrower than the width 9 of the side wall 7.

[0059] In the simplest case, the individual transducer elements 29 may be driven with the same control signal, which results in a conducted wave in the side wall 7 which essentially travels in the longitudinal direction of the measuring tube 3. It is, however, also possible to invite the conducted wave at an angle into the side wall 7, for example by specifying a defined phase offset for the individual transducer elements 29. In an alternative exemplary embodiment (not shown), it would also be possible to arrange the linear arrangement of the transducer elements 29 at an angle to the transverse direction of the measuring tube 3, in order to achieve angled emission with respect to the longitudinal direction 14 of the measuring tube 3.

[0060] FIG. 7 shows a variant of the exemplary embodiment shown in FIG. 6. In this case, an ultrasound transducer 31 is used whose transducer elements 32 are arranged in a V-shape (a parabolic or concave arrangement is likewise possible). The excitation width 33 in this case again corresponds approximately to the width 9 of the side wall 7. By the V-shaped arrangement, in the case of common driving of the transducer elements 32 with the same excitation signal, in the longitudinal direction 14 of the measuring tube 3 a phase offset is achieved between the various emitted conducted waves, so that these can be superimposed in such a way that an emission angle is adapted.

[0061] A further exemplary embodiment for an ultrasonic meter is represented in FIG. 8. In this case, an ultrasound transducer 35 is used which comprises a single cylindrical transducer element. Because of the cylindrical shape of the transducer element, emission of the conducted wave in the angle range 36 of 360 takes place. In other words, emission takes place isotropically in all spatial directions. By reflections at the edge of the side wall 7, as has been explained with reference to FIG. 4, in this case as well propagation of the conducted wave essentially over the entire width 9 of the side wall 7 is achieved, so that oscillations are also input into the fluid over the entire width 9. This therefore makes it possible, with little technical outlay, to take into account the flow velocity of the fluid essentially in the entire flow cross section of the measuring tube 3.

[0062] The explanations so far assumed that a time of flight is measured after the compression wave conducted through the fluid has been reflected at least once at a side wall. For the measurement principle explained, however, this is not necessary, so that it is also possible to use an arrangement as shown in FIG. 9. The basic structure in this case corresponds to the structure shown in FIG. 1, the first and second ultrasound transducers 5, 6 in this case being arranged on mutually opposite side walls. In one exemplary embodiment which is not shown, it would also be possible to use such an arrangement with the ultrasound waves being reflected several times at the side walls during the propagation through the fluid.

[0063] The following is a summary list of reference numerals and the corresponding structure used in the above description of the invention: [0064] 1 ultrasonic meter [0065] 2 control device [0066] 3 measuring tube [0067] 4 internal space [0068] 5 first ultrasound transducer [0069] 6 second ultrasound transducer [0070] 7 side wall [0071] 8 internal surface [0072] 9 width [0073] 10 excitation width [0074] 11 propagation direction [0075] 12 ultrasound beam [0076] 13 arrow [0077] 14 longitudinal direction [0078] 15 thickness [0079] 16 ultrasound transducer [0080] 17 excitation width [0081] 18 propagation direction [0082] 19 emission angle [0083] 20 ultrasound transducer [0084] 21 propagation direction [0085] 22 propagation direction [0086] 23 emission angle [0087] 24 emission angle [0088] 25 excitation width [0089] 26 excitation width [0090] 27 Rayleigh angle [0091] 28 ultrasound transducer [0092] 29 transducer element [0093] 30 excitation width [0094] 31 ultrasound transducer [0095] 32 transducer element [0096] 33 excitation width [0097] 34 ultrasound transducer [0098] 35 ultrasound transducer [0099] 36 angle range