Arrangement and Field Device of Process Measurements Technology

Abstract

An arrangement comprising an ultrasonic transducer and a damping element with a longitudinal axis, which damping element connects the ultrasonic transducer with a housing- or measuring tube wall. The transducer has an end piece with a medium-contacting surface, from which ultrasonic signals are transferred into a gaseous or liquid medium. The damping element has at least two annular grooves and an annular mass segment arranged therebetween, characterized in that the damping element has a first eigenfrequency, in which the annular mass segment executes an axial movement parallel to the longitudinal direction of the damping element. This first eigenfrequency is the highest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which the annular mass segment executes an axial movement parallel to the longitudinal direction of the damping element, and the damping element has a second eigenfrequency, in which the annular mass segment executes a rotary movement. This second eigenfrequency is the lowest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which the annular mass segment executes a rotary movement, will and wherein the ratio of the first eigenfrequency to the second eigenfrequency is less than 0.75; and a field device of process measurements technology.

Claims

1-10. (canceled)

11. An arrangement, comprising: an ultrasonic transducer; and a damping element with a longitudinal axis, which damping element connects said ultrasonic transducer with a housing- or measuring tube wall, wherein: said ultrasonic transducer has an end piece with a medium-contacting surface, from which ultrasonic signals are transferred into a gaseous or liquid medium; said damping element has at least two annular grooves and an annular mass segment arranged therebetween; said damping element has a first eigenfrequency, in which said annular mass segment executes an axial movement parallel to the longitudinal direction of said damping element; this first eigenfrequency is the highest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which said annular mass segment executes an axial movement and said damping element has a second eigenfrequency, in which the annular mass segment executes a rotary movement; this second eigenfrequency is the lowest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which said annular mass segment executes a rotary movement; and the ratio of the first eigenfrequency to the second eigenfrequency is less than 0.75.

12. The arrangement as claimed in claim 11, wherein: the ratio of the first eigenfrequency to the second eigenfrequency is less than 0.55, especially preferably less than 0.4.

13. The arrangement as claimed in claim 11, wherein: said damping element has at least in the region of a first of the at least two annular grooves a first average separation from the outer wall of a hollow cylindrical portion to the longitudinal axis; said damping element has at least in the region of the first of the at least two annular grooves a second average separation from the inner wall of the hollow cylindrical portion to the longitudinal axis; said damping element has in the region of the annular mass segment between the annular grooves an average length, wherein the expression $\frac{0.093.Math.\left(r_2-r_1\right)}{1.Math..Math.\mathrm{mm}}+{0.0016\left[\left(l_3/1.Math..Math.\mathrm{mm}\right)-12.5\right]}^2+0.057$ is less than 0.55, especially preferably less than 0.40, wherein the data for r.sub.1, r.sub.2 and l.sub.3 are in millimeters.

14. The arrangement as claimed in claim 11, wherein: said hollow-cylindrical portion is rotationally symmetric.

15. The arrangement as claimed in claim 11, wherein: said ultrasonic transducer and said damping element are connected with one another by material bonding.

16. The arrangement as claimed in claim 11, wherein: said damping element has less than five annular grooves.

17. The arrangement as claimed in claim 11, wherein: the lengths of said at least two annular grooves in the axial direction are equally long and the length of said annular mass segment is greater, preferably at least 1.5 times greater, than the length of one of said two annular grooves.

18. The arrangement as claimed in claim 11, wherein: said ultrasonic transducer has terminally a bending plate, which has said medium-contacting surface, from which the ultrasonic signal is transferred into the medium, which bending plate is embodied edgewise to freely oscillate.

19. The arrangement as claimed in claim 11, wherein: the arrangement has in a frequency range, in which the ratio of the wanted frequency f.sub.n to the first eigenfrequency f.sub.a is greater than 1.6 and in which the ratio of the wanted frequency f.sub.n to the second eigenfrequency f.sub.r is less than 0.7, no axial eigenfrequency or rotational eigenfrequency.

20. A field device of process measurements technology, especially an ultrasonic, flow measuring device for measuring gaseous media, wherein the field device has a measuring tube or a supply container, on which an arrangement is placed, said arrangement comprises: an ultrasonic transducer; and a damping element with a longitudinal axis, which damping element connects said ultrasonic transducer with a housing- or measuring tube wall, wherein: said ultrasonic transducer has an end piece with a medium-contacting surface, from which ultrasonic signals are transferred into a gaseous or liquid medium said damping element has at least two annular grooves and an annular mass segment arranged therebetween; said damping element has a first eigenfrequency, in which said annular mass segment executes an axial movement parallel to the longitudinal direction of said damping element; this first eigenfrequency is the highest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which said annular mass segment executes an axial movement and said damping element has a second eigenfrequency, in which the annular mass segment executes a rotary movement; this second eigenfrequency is the lowest eigenfrequency, in the case that a plurality of eigenfrequencies are present, in the case of which said annular mass segment executes a rotary movement; and the ratio of the first eigenfrequency to the second eigenfrequency is less than 0.75.

Description

[0031] The present invention will now be explained in greater detail based on the appended drawings:

[0032] The figures of the drawing show as follows:

[0033] FIG. 1 an arrangement of the invention comprising an ultrasonic transducer and a damping element;

[0034] FIG. 2 an arrangement according to the state of the art;

[0035] FIG. 3 a frequency spectrum of the arrangement of FIG. 1 and the arrangement according to FIG. 2;

[0036] FIG. 4 a representation of the oscillatory behavior of the arrangement of the invention at an excitation frequency in the case of the wanted frequency;

[0037] FIG. 5 a representation of the oscillatory behavior of the arrangement of the invention at an excitation frequency in the region of an axial mode; and

[0038] FIG. 6 a representation of the oscillatory behavior of the arrangement of the invention in the case of an excitation frequency in the region of a rotational mode.

[0039] The present arrangement can be applied both in the case of fill level measuring devices as well as also in the case of flow measuring devices. In the following, however, the construction, operation and advantages resulting therefrom will be described primarily for an ultrasonic, flow measuring device. The arguments can, however, for the most part, also be transferred to ultrasonic, fill level measurement.

[0040] Ultrasonic, flow measuring devices are widely applied in process and automation technology. They permit simple determination of volume flow and/or mass flow of a measured medium in a pipeline. Known ultrasonic, flow measuring devices frequently work according to the travel-time difference principle. In the travel-time difference principle, the different travel times of ultrasonic waves, especially ultrasonic pulses, so-called bursts, are evaluated relative to the flow direction of the liquid. For this, ultrasonic pulses are sent at a certain angle to the tube axis both with as well as also counter to the flow. From the travel-time difference, the flow velocity, and therewith, in the case of known diameter of the pipeline section, the volume flow, can be determined.

[0041] Ultrasonic waves are produced and received with the assistance of so-called ultrasonic transducers. For this, ultrasonic transducers are solidly connected with the tube wall of the relevant pipeline section. This device type is known to those skilled in the art also as an inline, flow measurement device. Also clamp-on ultrasonic, flow measuring systems exist, which are placed, e.g. secured, externally on the measuring tube. Clamp-on ultrasonic, flow measuring devices are, however, not subject matter of the present invention

[0042] Ultrasonic transducers normally include an electromechanical transducer element, e.g. one or more piezoelectric elements.

[0043] Both in the case of clamp-on-systems, as well as also in the case of inline-systems, the ultrasonic transducers are arranged in a shared plane on the measuring tube, either on oppositely lying sides of the measuring tube, in which case the acoustic signal travels, projected on a tube cross section, once along a secant through the measuring tube, or on the same side of the measuring tube, in which case the acoustic signal is reflected on the oppositely lying side of the measuring tube, whereby the acoustic signal traverses the measuring tube twice along the secant projected on the cross section through the measuring tube.

[0044] In the concrete example of an embodiment of FIG. 1, an arrangement with a corresponding ultrasonic transducer 1 is embodied with two electromechanical transducer elements 2, especially two piezo elements, arranged on top of one another. The ultrasonic transducer 1 includes additionally an end piece 4 with a medium-contacting surface 5. At this surface 5, the ultrasonic waves produced by one or more electromechanical transducer elements 2 are transferred to the measured medium.

[0045] The end piece 4 shown in FIG. 1 includes a pedestal 6, which is in contact, especially in shape-interlocking contact, with the electromechanical transducer elements 2. Furthermore, the end piece 4 includes a bending plate 7 with the medium-contacting surface 5.

[0046] The pedestal 6 of the end piece 4 includes an interface 16 to a damping element 15. This damping element 15 is embodied as a cylindrical body with at least two annular grooves 10 and 12 extending parallel to one another. Interface 16 can be embodied e.g. as a welded connection.

[0047] Arranged between the interface 16 and a first of the two annular grooves 10 is a first annular mass segment 9, which has a greater wall thickness, especially at least two times thicker, than the annular groove 10.

[0048] Arranged between the two annular grooves 10 and 12 is additionally a second annular segment 11, which has a greater wall thickness, especially at least two times thicker, then the annular grooves 10 and 12.

[0049] As evident from FIG. 1, the damping element 15 is essentially defined by three radii. There is a first radius r.sub.1, which extends from a longitudinal axis L of the damping element 15 to an inner wall of the cylindrical body. Furthermore, a second radius r.sub.2 is provided, which describes the separation of the outer wall from the longitudinal axis in the region of the annular grooves 10, 12. Finally, there is a third radius r.sub.3, which describes the radial separation between the longitudinal axis and the outermost point of the second annular mass segment 11.

[0050] After the second annular groove 12, the damping element 15 is connected via an interface 17 in the region of the third radius r.sub.3 with a housing wall 14. Also here, the interface 17 can be embodied as a welded connection. The interface is arranged in FIG. 1 radially outside of the second radius r.sub.2 and in the region of the third radius r.sub.3.

[0051] The annular grooves 10 and 12 extend over length sections l.sub.1 and l.sub.2, respectively, along the longitudinal axis L. These length sections l.sub.1 and l.sub.2, are dimensioned equally large in FIG. 1. The second annular mass segment 11 extends over a length section l.sub.3, which in the example of an embodiment of FIG. 1 is greater than the length of sections l.sub.1 and l.sub.2.

[0052] The first annular mass segment 9 is connected at its radially outermost point with an annular segment 8, which extends from the interface 16 to the annular mass 9. This annular segment 8 has a smaller wall thickness than that of the first annular mass segment 9. Preferably, it is at least twice as small.

[0053] The annular mass segment 9 transitions at its radially innermost point into the annular groove. In this way, there occurs in the case of an axial force a diversion of this force through the annular mass segment from the outside to the inside.

[0054] FIG. 2 shows a damping element from the state of the art as exemplified by EP 1 340 964 B1. The damping characteristics of this damping element were examined and compared with the damping characteristics of the arrangement of FIG. 1.

[0055] FIG. 3 shows the damping behavior of the arrangement of FIG. 1 based on the spectrum S1 with the solid line oscillation spectra in comparison with the spectrum S2 with the dashed line for the damping characteristics of the arrangement of FIG. 2.

[0056] A wanted signal A-n, which is required for determining the fill level or the flow, lies in the spectrum S1 at, for instance, 82000 Hz. As can be seen from FIG. 3, the frequency range of the wanted signal A-n for the arrangement of FIG. 1 can be selected in a very broad region. The frequency range of the wanted signal can be in the range from 45000 to, for instance, 120000 Hz, without experiencing greater superimposings of the wanted signal A-n with the eigenfrequencies A-a1, A-a2, A-r1 of the damping element 15. The peaks in the spectrum S1 at 28000 and at 35000 Hz represent axial oscillations, while the peak at, for instance, 136000 Hz is a rotary oscillation.

[0057] In contrast, the spectrum of the damping element of FIG. 2 has, in the case of to scale conversion, an entire series of eigenoscillations, which superimpose on a wanted signal at, for instance, 82000 Hz. The peaks at 25000 and at 55000 Hz represent, in such case, axial oscillations B-a1 and B-a2. The peaks at 71000 and 73000 Hz represent, in contrast, rotational oscillations B-r1 and B-r2. Both the axial-as well as also the rotational oscillations lie in the case of the variant illustrated in FIG. 3 below the wanted frequency of 82000 Hz.

[0058] FIG. 4 shows the oscillatory behavior of the damping element in the case of sending and/or receiving an ultrasonic signal in the wanted frequency range. One can see that primarily the ultrasonic transducer 1, thus the electromechanical transducer elements 2 and 3 and the end piece 4 with the pedestal 6 and the bending plate 7, are oscillating. The bending plate 7 undergoes during operation of the ultrasonic flow device a radial deflection A1. This deflection A1 is, however, not transferred to a following damping structure, but, instead, the bending plate 7 oscillates freely and is not disturbed in its radial deflection by a damping structure. In this way, the radiated ultrasonic signal transfers especially well and unimpeded to the medium.

[0059] FIG. 5 shows the oscillatory behavior of the arrangement of the invention in the illustrated embodiment according to FIG. 1 in the state of the eigenfrequency A-a2 (axial mode at about 35000 Hz.). Primarily, the annular mass segment 11 executes an axial movement between the two parallel annular grooves 10 and 12. The back and forth movement of the annular mass segment 11 results in a temporary material wall deformation in the region of the annular grooves 10 and 12 in the form of a temporary thinning or thickening.

[0060] FIG. 6 shows the oscillatory behavior of the arrangement of the invention in the illustrated embodiment according to FIG. 1 in the state of the eigenfrequency A-r1 (rotational mode at about 137000 Hz.). Primarily, the annular mass segment 11 executes a rotary movement between the two parallel annular grooves 10 and 12. The oscillatory movement of the annular mass segment 11 causes a temporary material wall deformation in the region of the annular grooves 10 and 12 in the form of a wave shaped bending of the material wall.

[0061] The embodiment shown in FIG. 1 can also be further modified in the context of invention. Thus, instead of a cylindrical basic structure, also a prismatic basic structure, preferably with unitary prism surfaces, provides an option. Also, individual segments of the basic structure, thus especially also the annular mass segment 11, can be embodied polygonally in two-dimensional section perpendicular to the longitudinal axis L.

[0062] Due to the sequence of annular mass segments 9 and 11 and annular grooves 10 and 12, a decoupling of the one or more rotational modes from the axial modes can be achieved, so that a broad frequency range between these individuals eigenfrequencies is available for the wanted signal.

[0063] On the whole, the arrangement can be of one- or multipiece construction. The damping element and the end piece are rotationally symmetric and are of metal. In such case, the end piece can preferably be of stainless steel or titanium. The damping element is preferably composed of stainless steel.

LIST OF REFERENCE CHARACTERS

[0064] 1 ultrasonic transducer [0065] 2 transducer element [0066] 4 end piece [0067] 6 surface [0068] 5 pedestal [0069] 7 bending plate [0070] 8 annular segment [0071] 9 annular mass segment [0072] 10 annular groove [0073] 11 annular mass segment [0074] 12 annular groove [0075] 13 section [0076] 14 housing wall [0077] 15 damping element [0078] 16 interface [0079] 17 interface [0080] L longitudinal axis [0081] r.sub.1 radius longitudinal axis to inner wall [0082] r.sub.2 radius longitudinal axis to outer wall (annular groove) [0083] r.sub.3 radius longitudinal axis to outer wall (annular mass segment) [0084] l.sub.1 length of annular groove [0085] l.sub.2 length of annular groove [0086] l.sub.3 length of annular mass segment [0087] f.sub.n wanted frequency [0088] f.sub.a axial mode [0089] f.sub.r rotational mode