DEVICE FOR PRODUCING A STANDARD ULTRASONIC FIELD

Abstract

Various embodiments of the present disclosure are directed to a device and a method for producing a standing ultrasonic field having the frequency f in a liquid. In one example embodiment, the device includes at least one oscillation element, a substantially dimensionally stable vessel having an outside wall and a substantially circular-cylindrical interior, the vessel receiving the liquid and the at least one oscillation element. The at least one oscillation element acoustically connected to the outside wall of the vessel and electrically excited at the frequency f. The substantially circular-cylindrical interior receives liquid with an inner radius r.sub.o at least in the region of the oscillation element. The oscillation element has a mean thickness p and a width b in the direction orthogonal to a main axis of the interior, and the width b is not greater than the inner diameter 2r.sub.o.

Claims

1. Device for producing a standing ultrasonic field at the frequency f in a liquid, the device comprising: at least one oscillation element; a substantially dimensionally stable vessel including an outside wall and a substantially circular-cylindrical interior, the vessel configured and arranged for receiving the liquid and the at least one oscillation element; wherein the at least one oscillation element is acoustically connected to the outside wall of the vessel and configured and arranged to be excitable at the frequency f; wherein the substantially circular-cylindrical interior is configured and arranged for receiving the liquid with an inner radius r.sub.o at least in the region of the oscillation element; and wherein the oscillation element has a mean thickness p and a width b in the direction orthogonal to a main axis of the interior, and the width b is not greater than the inner diameter 2r.sub.o, the oscillation element has at least one substantially flat lateral surface, and in that the oscillation element is acoustically connected via this one flat lateral surface to a substantially flat connection surface of the outside wall of the vessel in the region of the circular-cylindrical interior, wherein the connection surface is arranged parallel both to the main axis of the circular-cylindrical interior and to the oscillation element.

2-4. (canceled)

5. The device according to claim 1, characterized in that the outside wall of the vessel has a substantially circular-cylindrical shape in the region of the circular-cylindrical interior apart from the connection surface.

6. The device according to claim 1, characterized in that the width b of the oscillation element is less than or equal to 3.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2, preferably lies between (r.sub.P.Math.v.sub.C/f).sup.1/2 and 2.5.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2 and more preferably lies between 1.5.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2 and 2.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2, wherein r.sub.P=r.sub.o+c.sub.o applies, r.sub.o is the inner radius of the interior, c.sub.o is the minimum wall thickness of the vessel wall section in the region of the oscillation element, and v.sub.C is the sound velocity in the vessel wall section.

7. The device according to claim 1, further including a transducer array having the at least one oscillation element and a vessel wall section of the vessel in the region of the at least one oscillation element, wherein the vessel wall section has a minimum wall thickness c.sub.o in the region of the at least one oscillation element in the region of the center of the connection surface, and has a maximum radial wall thickness c.sub.max=c.sub.o+Δc in the peripheral region of the oscillation element, and an equivalent mean wall thickness c.sub.equ of the vessel wall section is defined by c.sub.equ=c.sub.o+Δc/3, wherein the difference Δc between the maximum radial wall thickness c.sub.max and the minimum wall thickness c.sub.o is determined by the width b of the oscillation element via the relationship Δc=(b.sup.2/4+r.sub.P.sup.2).sup.1/2 r.sub.P, wherein r.sub.P=r.sub.o+c.sub.o applies, and r.sub.o is the radius of the circular-cylindrical interior.

8. The device according to claim 7, wherein the transducer array includes a plurality of layers, characterized in that the thicknesses of the layers of the transducer array are selected such that natural resonance frequencies f.sub.er of the transducer array to the desired frequency f of the ultrasonic field have distances which are greater than one fifth of the distance f.sub.er,1−f.sub.er,2, wherein f.sub.er,1 and f.sub.er,2 are the two closest natural resonance frequencies f.sub.er with respect to the frequency f.

9. The device according to claim 7, wherein the transducer array includes a plurality of layers acoustically coupled in the thicknesses direction of the oscillation element, and characterized in that the thickness of the layers of the transducer array are selected such that the half-wave number κ of the transducer array satisfies the condition $κ = 1 / 2 + n \pm Δ n$ wherein n is a natural number, and the tolerance value Δn is at least less than 0.3, and the half-wave number κ of the transducer array is substantially given by $κ = 2 f .Math. (c_{e q u} / v_{C} + p / v_{P} + d_{1} / v_{d 1} + d_{2} / v_{d 2} + .Math. + d_{i} / v_{di}),$ wherein v.sub.C is the sound velocity in the vessel wall section in the region of the oscillation element, v.sub.P is the sound velocity in the thickness direction in the oscillation element, and d.sub.1 to d.sub.i are the thicknesses and v.sub.d1 to v.sub.di are the sound velocities of further layers of the transducer array acoustically coupled in the thickness direction, if present, and the index number “i” is a natural number indicating the number of these further layers of the transducer array.

10. The device according to claim 1, characterized in that the thickness p of the oscillation element is substantially equal to the value v.sub.P/(2f), wherein v.sub.P is the sound velocity in the thickness direction in the oscillation element.

11. The device according to claim 1, characterized in that the width b of the oscillation element is in the range between (r.sub.P.Math.p.Math.v.sub.C/v.sub.P).sup.1/2 and 4.Math.(r.sub.P.Math.p.Math.v.sub.C/v.sub.P).sup.1/2, wherein r.sub.P=r.sub.o+c.sub.o applies, r.sub.o is the inner radius of the interior, c.sub.o is the minimum wall thickness of the vessel wall section in the region of the oscillation element, and wherein v.sub.C is the sound velocity in the vessel wall section, and where v.sub.P is the sound velocity in the thickness direction in the oscillation element.

12. The device according to claim 7, wherein a plurality of layers of the transducer array includes coupling layers, characterized in that the thicknesses d′.sub.1 to d′.sub.j of coupling layers, which are arranged to be acoustically coupled between the oscillation element and the vessel wall section in the thickness direction, and the minimum wall thickness c.sub.o of the vessel wall section are selected such that the condition $c_{o} / v_{c} + ({(b^{2} / 4 + r_{P}^{2})}^{1 / 2} - r_{P}) / (3 v_{C}) + d_{1}^{'} / v_{d^{'} 1} + d_{2}^{'} / v_{d^{'} 2} + .Math. + d_{j}^{'} / v_{d^{'} j} = p / v_{P} .Math. (1 / 2 + q \pm Δ q)$ is satisfied, wherein v.sub.d″1 to v.sub.d″k are the sound velocities of the coupling layers, wherein the index number j is a natural number indicating the number of coupling layers of the transducer array arranged between the oscillation element and the vessel wall section, and q is a natural number, and the tolerance value Δq is at least less than 0.3.

13. (canceled)

14. The device according to claim 7, characterized in that the thicknesses d″.sub.1 to d″.sub.k of outer layers, acoustically coupled in the thickness direction, of the transducer array, which are arranged on the side of the oscillation element facing away from the vessel, are selected such that the condition $(d_{1}^{″} / v_{d^{″} 1} + d_{2}^{″} / v_{d^{″} 2} + .Math. + d_{k}^{″} / v_{d^{″} k}) = p / v_{P} .Math. (s \pm Δ s)$ is satisfied, wherein v.sub.d″1 to v.sub.d″k are the sound velocities of the outer layers, wherein the index number k is a natural number indicating the number of outer layers of the transducer array which are arranged on the side of the oscillation element facing away from the vessel, and s is a natural number, and the tolerance value Δs is at least less than 0.3.

15. The device according to claim 1, characterized in that the vessel has, outside the region of the oscillation element and at least at the level of the oscillation element, a wall thickness c which satisfies the condition c=v.sub.C/2f.Math.(½+m±Δm), wherein m is a natural number, and the tolerance value Δm is at least less than 0.3.

16-19. (canceled)

20. Method for producing a standing ultrasonic field with frequency f in a liquid, the method including the following steps: exciting at least one oscillation element with at least one frequency f and the oscillation element forms a standing ultrasonic field within the vessel that causes the vessel and the liquid arranged in a circular-cylindrical interior to oscillate, and in response to the standing ultrasonic field, concentrating dispersed particles in the liquid or separating dispersed particles from the liquid, wherein the oscillation element has a mean thickness p and the interior has an inner radius r.sub.o and the oscillation element has a width b in an orthogonal direction to a main axis of the interior, wherein the width b is not greater than the inner diameter 2r.sub.o, characterized in in that the at least one oscillation element transmits the oscillations to the vessel via a substantially flat side wall via a substantially flat connection surface of the outside wall of the vessel in the region of the circular-cylindrical interior, and in that the connection surface is arranged parallel both to the main axis of the circular-cylindrical interior and to the oscillation element.

21-23. (canceled)

24. The method according to claim 20, characterized in that the frequency f is chosen such that the width b of the oscillation element is less than or equal to 3.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2, wherein r.sub.P=r.sub.o+c.sub.o applies, r.sub.o is an inner radius of the interior, c.sub.o is a minimum wall thickness of a vessel wall section (10) in the region of the oscillation element, and v.sub.C is the sound velocity in the vessel wall section.

25. The method according to claim 20, characterized in that the frequency f is selected to lie outside the natural resonance frequencies f.sub.er of a transducer array including at least the oscillation element and a vessel wall section of the vessel in the region of the oscillation element, and in that the distance between the selected frequency f and the natural resonance frequencies f.sub.er is greater than one fifth of the distance f.sub.er,1−f.sub.er,2, wherein f.sub.er,1 and f.sub.er,2 are the two closest natural resonance frequencies f.sub.er with respect to the frequency f.

26. The method according to claim 20, further including the step of selecting the frequency f such that the half-wave number κ of the transducer array satisfies the condition $κ = 1 / 2 + n \pm Δ n,$ wherein n is a natural number and the tolerance value Δn is at least less than 0.3, and the half-wave number κ of a transducer array is substantially given by $κ = 2 f .Math. (c_{e q u} / v_{C} + p / v_{P} + d_{1} / v_{d 1} + d_{2} / v_{d 2} + .Math. + d_{i} / v_{di}),$ wherein the equivalent mean wall thickness c.sub.equ of a vessel wall section in the region of the oscillation element is defined by c.sub.equ=c.sub.o+Δc/3, wherein the difference Δc between the maximum radial wall thickness cmax and the minimum wall thickness co in the region of the center of the connection surface (11) is determined by the width b of the oscillation element via the relationship Δc=(b.sup.2/4+r.sub.P.sup.2).sup.1/2−r.sub.P, wherein r.sub.P=r.sub.o+c.sub.o applies, v.sub.C is the sound velocity in the vessel wall section in the region of the oscillation element, v.sub.P is the sound velocity in the thickness direction in the oscillation element and d.sub.1 to d.sub.i are the thicknesses and v.sub.d1 to v.sub.di are the sound velocities of further layers of the transducer array acoustically coupled in the thickness direction, if present, and the index number i is a natural number representing the number of said further layers of the transducer array, and in that the transducer array comprises at least the oscillation element and a vessel wall section in the region of the oscillation element.

27. The method according to claim 20, further including the step of selecting the frequency f such that a thickness p of the oscillation element corresponds approximately to v.sub.P/2f and v.sub.P is the sound velocity in the oscillation element.

28. The method according to claim 20, characterized in that at least one coupling layer is arranged between the oscillation element and a vessel wall section in the region of the oscillation element, wherein the minimum wall thickness c.sub.o of the vessel wall section and the thickness d′ of the at least one coupling layer are such that the condition $c_{o} / v_{c} + ({(b^{2} / 4 + r_{P}^{2})}^{1 / 2} - r_{P}) / (3 v_{C}) + d_{1}^{'} / v_{d^{'} 1} + d_{2}^{'} / v_{d^{'} 2} + .Math. + d_{j}^{'} / v_{d^{'} j} = p / v_{P} .Math. (1 / 2 + q \pm Δ q)$ is satisfied, wherein v.sub.d′1 to v.sub.d′j are the sound velocities of the coupling layers, wherein q is a natural number, the index number j is a natural number indicating the number of coupling layers of the transducer array and the tolerance value Δq is at least less than 0.3.

29. (canceled)

30. The method according to claim 20, characterized in that further layers of the transducer array include acoustically coupled outer layers arranged on the side of the oscillation element facing away from the vessel in the thickness direction, the thicknesses d″.sub.1 to d″.sub.k of which are selected such that the condition $(d_{1}^{″} / v_{d^{″} 1} + d_{2}^{″} / v_{d^{″} 2} + .Math. + d_{k}^{″} / v_{d^{″} k}) = p / v_{P} .Math. (s \pm Δ s)$ is satisfied, wherein v.sub.d″1 to v.sub.d″k are the sound velocities of the outer outer layers, the index number k is a natural number indicating the number of the outer layers of the transducer array, and s is a natural number, and the tolerance value Δs is at least less than 0.3.

31. The method according to claim 20, further including the step of choosing the frequency f such that the condition c=v.sub.C/2f.Math.(½+m±Δm) is satisfied, wherein m is a natural number, and the tolerance value Δm is at least less than 0.3, and in that the wall thickness c is that of the vessel outside the range of the oscillation element.

32. The method according to claim 20, further including the steps of measuring, using a signal generator, at least the voltage amplitude, or current amplitude, or the phase relationship between current and voltage amplitude of the emitted signal, or a combination of these electrical quantities, via a control circuit, and fine-tuning the frequency f to a resonance frequency f.sub.opt, determined from these measured quantities, of the device filled with the liquid.

Description

[0118] In the following, the invention will be explained in more detail with reference to non-limiting exemplary embodiments shown in the figures, wherein:

[0119] FIG. 1A shows a prior art vessel having a square cross-section;

[0120] FIG. 1B shows a side view of the vessel of FIG. 1A;

[0121] FIG. 2A shows a vessel according to the prior art having a circular cross-section and an oscillation element extending continuously around the cross-section;

[0122] FIG. 2B shows a vessel according to the prior art having a circular cross-section and a plurality of curved oscillation elements distributed about the cross-section;

[0123] FIG. 3A shows a vessel of a device according to the invention in a first embodiment having four oscillation elements in cross-section;

[0124] FIG. 3B shows a vessel of a device according to the invention in a second embodiment having two oscillation elements in cross-section;

[0125] FIG. 3C shows the embodiment of FIG. 3B with detailed designations of the geometric dimensions relevant to the invention;

[0126] FIG. 3D shows an embodiment of the oscillation element;

[0127] FIG. 4 shows the electrical resonance spectrum of the second embodiment as a function of frequency f;

[0128] FIG. 5A shows a vessel of a device according to the invention in a third embodiment having only one oscillation element in cross-section;

[0129] FIG. 5B shows a side view of the vessel of FIG. 5A;

[0130] FIG. 5C shows an array of a plurality of vessels of a device according to the invention in a fourth embodiment;

[0131] FIG. 6A shows a vessel of a device according to the invention in a fifth embodiment having three oscillation elements in cross-section;

[0132] FIG. 6B a vessel of a device according to the invention in a sixth embodiment with six oscillation elements in cross-section;

[0133] FIG. 6C shows an array of a plurality of vessels of a device according to the invention in a seventh embodiment;

[0134] FIG. 7A shows an array of a plurality of vessels of a device according to the invention in an eighth embodiment;

[0135] FIG. 7B shows an array of a plurality of vessels of a device according to the invention in a ninth embodiment;

[0136] FIGS. 8A to 8E show arrays of a plurality of vessels of devices according to the invention in various further embodiments;

[0137] FIG. 9A shows a vessel of a device according to the invention in a tenth embodiment having only one oscillation element in cross-section;

[0138] FIG. 9B shows an array of a plurality of vessels according to FIG. 9A of a device according to the invention in an eleventh embodiment;

[0139] FIG. 10A shows a vessel of a device according to the invention in a twelfth embodiment having only one oscillation element in cross-section;

[0140] FIG. 10B shows a vessel of a device according to the invention in a thirteenth embodiment having two opposing oscillation elements in cross-section;

[0141] FIGS. 11A-11D show schematic views of various implementations with devices according to the invention in a further embodiment;

[0142] FIG. 12 shows a device according to the invention in one embodiment having two vessels in a sectional view;

[0143] FIG. 13A shows a device according to the invention in one embodiment with inserted sample container in a cross-section;

[0144] FIG. 13B shows a longitudinal section of the embodiment of FIG. 13A.

[0145] FIGS. 1A and 1B illustrate a typical prior art acoustic device for producing a flat standing acoustic field in a vessel 1 filled with a dispersion 100. The dispersion 100 represents a liquid (the dispersion medium) and particles such as cells contained therein. The transducer array 200 is formed by a flat piezoelectric oscillation element 2 coated with electrode surfaces, and by a flat vessel wall 10a. The oscillation element 2 is acoustically precisely coupled to the vessel wall 10a from the outside (e.g. by bonding of precisely defined often highly thin layer thickness, or by an interposed acoustically coupling gel or liquid layer). The opposite reflecting, likewise flat vessel wall 10b serves as an acoustic reflector wall and is oriented with its inner surface 13b parallel to the emitting surface 13a of the transducer array. Between transducer wall 10a and reflector wall 10b, a parallel pattern of alternating sonic bulge planes 111 and sonic node planes 112 is formed in dispersion 100. Adjacent nodes and bulges are spaced apart by a quarter wavelength; the bulge-to-bulge or node-to-node spacing is half a wavelength.

[0146] Depending on the acoustic contrast and specific gravity of the particles relative to the dispersion medium, acoustic radiation forces drive the dispersed particles (which may be solid, liquid, or gaseous) into the sonic bulge planes 111 and sonic node planes 112, respectively. Accordingly, most solid particles (as shown here) are driven into the sonic bulge planes, while gaseous particles (bubbles) would collect in the sonic node planes.

[0147] In the illustrated embodiment, the acoustic field is generated by applying an AC voltage U˜ to the electrodes of the oscillation element 2. If an integer multiple of half wavelengths fits into the acoustic system (formed here by transducer array dispersion reflector wall), the standing wave field is in resonance and the system can be excited particularly effectively. If the distance L between the transducer wall 10a and the reflector wall 10b is significantly greater than the thickness of the transducer array or the reflector wall, the frequency spacing Δf.sub.res between adjacent resonance frequencies can be approximately estimated by the relationship Δf.sub.res=v.sub.M/(2L), wherein v.sub.M is the sound velocity of the medium of dispersion 100.

[0148] The vessel walls (transducer wall 10a, reflector wall 10b, side walls 10c) are typically made of glass or metal. As a possible measure for attenuating randomly excited transverse standing wave fields, the inner surfaces 13c of the side walls are shown here with an acoustically attenuating coating 15. Suitable materials for such a coating include silicone, rubber, and other materials compatible with the medium such as biocompatible plastics. Alternatively, the entire sidewall 13c, or all of the vessel walls if sufficiently thin, may be made of application-specific suitable plastics (e.g., forms of PEEK, polycarbonates, polyethylenes, polypropylenes, polystyrenes, etc.). Likewise, depending on the material, the vessel may also be cast, injection molded, fused, or milled in one piece. These embodiments regarding the material and the cushioning coating may also apply to embodiments according to the invention.

[0149] Analogous to FIG. 1A, FIG. 2A illustrates the fundamental structure of a device according to the prior art for producing a circular-cylindrical standing acoustic field. The vessel 1 is circular-cylindrical and continuously surrounded on an outside wall 12 by an equally circular-cylindrical oscillation element 2, which is designed as a piezoelectric tube. The cylinder axis or main axis H lies in the viewing direction z of the observer. The transducer array 200 is formed by the piezoelectric tube 2 and by the vessel 1 enclosed therein and serving as a carrier tube. The piezoelectric tube and the carrier tube are acoustically coupled to each other (e.g., by bonding, or by an interposed acoustically coupling gel or liquid layer). Within the carrier tube, a parallel pattern of alternating sonic bulge cylindrical shell surfaces 111 and sonic node cylindrical shell surfaces 112 is formed in the dispersion medium or liquid 100. Adjacent node shell surfaces and bulge shell surfaces are spaced apart by a quarter wavelength in the fluid 100; the spacing of adjacent bulge-bulge shell surfaces and node-node shell surfaces, respectively, is one-half wavelength λ/2.

[0150] In the illustrated embodiment, the acoustic field is generated by applying an AC voltage U˜ to the electrodes of the piezoelectric tube 2. If an integer multiple of half wavelengths fits into the acoustic system (here formed by transducer array medium), the standing wave field is in resonance and the system can be excited particularly effectively. If the inner radius r.sub.o of the carrier tube 1 is significantly greater than the wall thickness of the transducer array 200, the frequency spacing Δf.sub.res between adjacent resonance frequencies can be estimated approximately by the relationship Δf.sub.res=v.sub.M/(2r.sub.o), wherein v.sub.M is the sound velocity of the medium.

[0151] Due to the concentric excitation of the circular-cylindrical standing wave field, the acoustic energy density is inversely proportional to the distance r between the cylinder axes. Due to the increasing acoustic energy density, the pressure amplitude and thus the risk of cavitation in the area of the cylinder axis H also increases significantly. Especially for the separation of living cells, this poses a risk to the viability of the cells.

[0152] FIG. 2B illustrates a measure for reducing this risk of cavitation along the cylinder axis H, which is known from the prior art. In the illustrated variant of the cylindrical device, the piezo tube is divided into four cylinder shell segments, resulting in four oscillation elements 2A.sub.1, 2A.sub.2, 2B.sub.1, 2B.sub.2 which are curved in cross-section. They are electrically wired in such a way that the excitation of two opposing piezo shell segments is synchronous in time, but the pair of piezo shell segments orthogonal thereto is antisynchronous. That is, while piezo shell segments 2A.sub.1 and 2A.sub.2 expand, piezo shell segments 2B.sub.1 and 2B.sub.2 contract, and vice versa. This at least partially compensates for the acoustic pressure amplitudes increasing towards the center in the region of the axis, and the risk of cavitation is reduced.

[0153] FIG. 3A shows a possible embodiment variant according to the invention of a vessel 1 according to the device according to the invention, wherein the oscillation elements 2 are designed as flat piezoelectric plates and are acoustically coupled (e.g. by bonding) to connecting walls 11, which are held flat, of an outside wall 12 of the vessel 1 designed as a carrier tube. Thereby, the interior 14 is circular-cylindrical as shown in FIG. 2B, i.e. has a circular cross-section with an inner radius r.sub.0. The interior 14 is bounded by a continuous, smooth inner wall 13 of the vessel 1. Outwardly, the vessel 1 has a rectangular, preferably square, cross-section, resulting in an outside wall 12 of four flat partial walls that are parallel or at right angles to each other. Four oscillation elements 2 are arranged centered on each partial wall, whereby the partial walls serve at least partially as connection surfaces. Each partial wall has a minimum wall thickness c.sub.o at which the vessel 1 is thinnest, namely halfway across the width b of each oscillation element 2 and partial wall. This results in a radial distance r.sub.p of the oscillation elements 2 from the main axis H with r.sub.p=r.sub.o+c.sub.o.

[0154] FIG. 3B shows a second embodiment according to the invention, wherein the vessel 1 has a circular shell and thus cylindrical outside wall 12. Thus, the vessel 1 is essentially a hollow cylinder with an overall wall thickness c. On two sides the outside wall 12 is flattened, resulting in two flat connection surfaces 11. In this embodiment, the connection surfaces 11 are arranged parallel to each other and thus face each other. An oscillation element 2 is arranged on each connection surface 11, which are preferably excited with the same frequency f or the same frequency spectrum. Such an arrangement on two opposite sides is particularly advantageous for vessels which are made of plastic. Possible asymmetries of the wave field in the interior 14 of the vessel caused by damping in the vessel wall can thus be prevented.

[0155] For this purpose, the oscillation elements 2 can be electrically connected in series (as shown) or also electrically connected in parallel, wherein in FIG. 3B the polarity of the respective electrical contacting of the oscillation elements is selected in such a way that the oscillation elements expand or contract synchronously. For this purpose, the side of an oscillation element 2 facing away from the vessel 1 is connected to a first signal cable of a signal generator, and the side of the other oscillation element 2 facing towards the vessel 1 is connected to a second signal cable. The other sides of the oscillation elements 2 are connected to each other by a cable. In this case, the negatively polarized side of both oscillation elements 2 faces the vessel 1. In FIG. 3A it can be seen that such an electrical interconnection is of course also possible with several oscillation elements 2.

[0156] Due to such a rotationally symmetrical arrangement of a plurality of oscillation elements 2, a standing wave field 111 formed substantially radially about the main axis H occurs in the interior 14 within the dispersion 100 in the region between two oppositely arranged oscillation elements 2, and thus the dispersed particles are compacted. Corresponding compaction also occurs transversely to this region as a result of a standing wave field which is likewise substantially radially formed but oscillates in an inverted manner, as a result of which a weakening of the radial standing wave field can occur in the transition regions 113 between the wave regions, but this is insignificant for the practical functionality of the device.

[0157] According to the invention, an effective excitation of an—in spite of the flat formed oscillation elements 2—essentially still dominant cylindrical standing wave field within the interior 14 filled with liquid is possible by the fact that the oscillation elements 2 have a width b which approximately does not substantially exceed the relation b=2.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2.

[0158] According to the invention, it is sufficient that the width b is less than 3.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2, and preferably has a value within (r.sub.P.Math.v.sub.C/f).sup.1/2<b<2.5.Math.(r.sub.P.Math.v.sub.C/f).sup.1/2, wherein v.sub.C is the sound velocity in the vessel wall section 10 in the region of the oscillation element 2.

[0159] For the normally practical case where a piezoelectric plate for excitation at its thickness mode fundamental frequency is used as the oscillation element 2 (i.e., the oscillation element has a thickness p=v.sub.P/(2f), and v.sub.p is the sound velocity in the thickness direction in the oscillation element 2), an embodiment according to the invention of the width b is also given when it is less than 4.Math.(r.sub.P.Math.p.Math.v.sub.C/v.sub.P).sup.1/2 or preferably within a range 1.5.Math.(r.sub.P.Math.p.Math.v.sub.C/v.sub.P).sup.1/2<b<3.5.Math.(r.sub.P.Math.p.Math.v.sub.C/v.sub.P).sup.1/2.

[0160] FIG. 3C illustrates further key geometric dimensions of an embodiment according to the invention, which must be observed in the design in order to optimize the excitation of a circular-cylindrical acoustic field in sufficient approximation despite the use of flat sound emitting oscillation elements 2. The plate-shaped oscillation element 2 has a thickness p and is acoustically connected to the flat connection surface 11 of the outside wall 12 of the vessel via a coupling layer 23 of thickness d (e.g. by bonding, or by an interposed acoustically coupling gel or liquid layer). The oscillation element thus forms, together with the coupling layer 23 and the vessel wall section 10 located in the region of the coupling layer, a transducer array 200 acoustically coupled in the thickness direction of the oscillation element 2. Thereby, the vessel wall section 10 has a minimum wall thickness c.sub.0 in its center and a maximum radial wall thickness c.sub.max=c.sub.0+Δc at the edge of the coupling layer, where the radial wall thickness of c.sub.0 has expanded by Δc. In this embodiment, the total wall thickness c of the vessel is greater than c.sub.max, since the coupling surfaces 11 are made larger than the width b of the oscillation elements 2, and therefore project beyond them. The difference Δc is determined by the width b of the oscillation element (2) via the relationship Δc=(b.sup.2/4+r.sub.P.sup.2).sup.1/2−r.sub.P.

[0161] It is advantageous to define an equivalent thickness c.sub.equ for the vessel wall section 10 belonging to the transducer array 200, given by c.sub.equ=c.sub.0+Δc/3, which is substantially equal to the mean radial wall thickness of this vessel wall section 10.

[0162] According to the invention, in the embodiment variant illustrated with FIG. 3C, the thickness p of the oscillation element 2, the thickness d of the coupling layer 23, and the equivalent thickness c.sub.equ of the vessel wall section 10 have an overall thickness of the transducer array 200, so that the occurrence of natural resonances of the transducer array 200 is avoided when the transducer array 200 is excited at the desired operating frequency f. This is achieved in that the thickness p of the oscillation element, thickness d of the coupling layer 23, and the equivalent thickness c.sub.equ of the vessel wall section 10 have values which come as close as possible to the condition

[00014] $2 f .Math. (c_{equ} / v_{c} + p / v_{P} + d / v_{d}) = 1 / 2 + n,$

[0163] which is equivalent to the condition that the half-wave number of the acoustic wave extending in the thickness direction over the entire transducer array is as close as possible to no natural number n (0, 1, 2, . . . ). Here, v.sub.c is the sound velocity in the vessel wall section 10 in the region of the oscillation element 2, v.sub.p is the sound velocity in the thickness direction in the oscillation element 2, and v.sub.d is the sound velocity in the coupling layer.

[0164] For the normally practical case that a piezoelectric plate for excitation at its thickness mode fundamental frequency is used as the oscillation element 2 (i.e., that the oscillation element has a thickness p=v.sub.P/(2f)), and while observing the width b of the oscillation element 2 which is preferable according to the invention and as explained for FIGS. 2A and 2B, the excitation of natural resonances of the transducer array is avoided, in particular, if the minimum thickness c.sub.o of the vessel wall section 10 and the thickness d of the coupling layer have values which satisfy the condition

[00015] $c_{o} / v_{c} + d / v_{d} + ({(b^{2} / 4 + r_{P}^{2})}^{1 / 2} - r_{P}) / (3 v_{C}) = p / v_{P} .Math. (1 / 2 + n \pm Δ n),$

[0165] wherein n is a natural number (0, 1, 2, . . . ), and the tolerance value Δn is at least less than 0.3, preferably 0.2, and particularly preferably less than 0.1.

[0166] According to the invention, the coupling layer may have a thickness d so thin that it can be neglected and thus d is substantially equal to 0.

[0167] In a preferred embodiment of the device according to the invention, the wall thickness c of the vessel 1 around the interior 14 but outside the region of the connection surface 11 satisfies the condition

[00016] $c = v_{C} / 2 f .Math. (1 / 2 + m \pm Δ m),$

[0168] wherein m is a natural number (0, 1, 2, . . . ), and the tolerance value Δm is at least less than 0.3, preferably 0.2, and particularly preferably less than 0.1. This is equivalent to the condition that the vessel has a wall thickness c in this region which is not equal to an integer multiple of half a wavelength.

[0169] For the normally practical case where the oscillation element 2 is a piezoelectric plate for excitation at its thickness mode fundamental frequency (i.e., the oscillation element has a thickness p=v.sub.P/(2f)), the condition can also be expressed as

[00017] $c = ρ .Math. v_{C} / v_{P} .Math. (1 / 2 + m \pm Δ m) .$

[0170] FIG. 3D illustrates one of the possible embodiments of the oscillation element 2 according to the invention with thickness p and width b as an arrangement of two piezoelectric plates 20a and 20b of the same thickness p, which are adjacent to each other on the same plane and polarized in the thickness direction. Each of the two plates 20a, 20b has an electrode surface 21a, 21b facing the vessel (vessel not shown here) and an electrode surface 22a, 22b facing away from the vessel. For the purpose of accessibility of electrical contacting, the electrode surfaces 21a, 21b facing the vessel each have a region overlapping on the side facing away from the vessel.

[0171] In the embodiment shown here, the electrode surfaces 21a, 21b, 22a, 22b of the two piezo plates 20a and 20b are electrically connected in series with each other and connected to an electrical signal source U˜.

[0172] It is understood that in alternative embodiments an oscillation element 2 may have only a single piezoelectric plate, or may have a mosaic-like arrangement of any number of piezoelectric plates electrically connected to each other in series, or in parallel, or in a suitable combination thereof, to achieve a suitable overall electrical impedance of the oscillation element 2 for connection to the signal source U˜.

[0173] Further, a piezoelectric plate may have a plurality of separate electrode surface areas on one or both sides, which in turn are electrically connected to each other in such a way as to achieve a suitable overall electrical impedance of the oscillation element 2. Where a plurality of piezoelectric plates 20a, 20b are provided for the oscillation element 2, they may be directly acoustically connected to each other. For this purpose, it may be provided that the at least two piezoelectric plates are arranged with a base body of the oscillation element. In this respect, the base body may extend substantially only in the region between the piezoelectric plates. This may require that the mean thickness p of the oscillation element corresponds to the thickness of the piezoelectric plates. Alternatively, no main body may be provided and the piezoelectric plates may also be acoustically connected only via the vessel.

[0174] Further, the electrical connection between the signal source U˜ and one or more piezoelectric plates may also be supported by one or more signal transformers having suitable electrical transformation ratios to provide an overall electrical impedance of the oscillation element 2 suitable for connection to the signal source U˜.

[0175] FIG. 4 presents the frequency response of a device built according to the invention as shown in FIG. 3C, which has dimensions according to the invention that obey the conditions presented for FIG. 3C:

[0176] Width of the swing element: b=15 mm

[0177] Thickness of the oscillation element: p=1.2 mm (basic thickness mode at 1.7 MHz)

[0178] Minimum vessel wall thickness: c.sub.o=2.0 mm

[0179] General wall thickness: c=4.2 mm

[0180] Radii of the vessel: r.sub.o=15 mm and r.sub.P=r.sub.o+c.sub.o=17 mm

[0181] The coupling layer 23 is formed of a thin liquid cured adhesive whose thickness d is of the order of only one hundredth of a wavelength, and is thus negligible (d≈0). The oscillation element consists essentially of only one piezoelectric plate, whereby the thickness and width of this plate represent the thickness and width of the oscillation element.

[0182] Material Parameters:

[0183] Sound velocity Medium (water): v.sub.M=1500 m/s Sound velocity of the carrier tube: v.sub.C=5640 m/s Sound velocity of the piezo plate: v.sub.P=4100 m/s (for longitudinal oscillation mode in the direction of thickness p of the piezo plate).

[0184] A first plot 901 (thin solid line) represents the conductance spectrum of the acoustic system 300 (vessel 1 filled with medium), a second plot 902 (thick dashed line) represents the conductance spectrum of the transducer array 200 (empty vessel 1). In the case of excitation with an alternating electrical signal with primarily impressed voltage amplitude, the first plot 901 is to be equated with the resonance spectrum of the acoustic system 300, while the second plot 912 corresponds to the natural resonance spectrum of the transducer array 200.

[0185] In the range of the desired operating frequency of about 1.7 MHz, strongly pronounced radial resonance frequencies f1, f2 and f3 occur at the expected spacing of Δf.sub.res≈v.sub.M/(2r.sub.o)=50 kHz as a consequence of the production according to the invention. These radial resonance frequencies f1, f2, f3, and to a limited extent also f4 stand out significantly from the remaining non-radial background resonance behavior (typically recognizable by the smaller but dense and irregular resonance peaks), which is particularly pronounced in the frequency ranges 911 and 912 around the natural resonance frequencies f.sub.er1 (at 1550 kHz) and f.sub.er2 (at 1900 kHz) of the transducer array.

[0186] According to the invention, with a distance of greater than 70 kHz from these two closest natural resonance frequencies f.sub.er1 and f.sub.er2 (corresponds to about 20% or one fifth of the frequency separation between these two natural resonance frequencies), the resonance frequencies f1, f2, f3 and f4 of the acoustic system 300 are also sufficiently far away from the natural resonance frequencies of the transducer array, with a distance of more than 105 kHz (corresponds to about 30% of the frequency separation between the two nearest natural resonance frequencies f.sub.er1 and f.sub.er2), the frequencies f1, f2, f3 are to be preferred over f4; and among these in turn the frequencies f1 and f2 with a spacing of more than 140 kHz (corresponds to about 40% of the frequency spacing between the two nearest natural resonance frequencies f.sub.er1 and f.sub.er2).

[0187] Preferably, the alternating electrical signal source includes a device for:

[0188] (1) detecting resonance frequencies (such as by directly measuring the active electrical power absorbed by the vessel 1, thus detecting the frequencies for which there are local maxima of absorbed active power) and/or

[0189] (2) for automated frequency tuning to such resonance frequencies of maximum active electrical power absorption by the acoustic system 300.

[0190] With such a device, it is therefore possible to manually or even automatically fine-tune the operating frequency f to the preferred resonance frequency of the acoustic system 300 that most closely matches the assumed operating frequency (in this example, 1.7 MHz) on which the design is based.

[0191] It is remarkable that in the example presented, pronounced and largely mode-free radial resonances are formed only within a relatively narrow frequency range 910 of about 1650 to 1750 kHz; a clear indication that only for this narrow frequency range around 1.7 MHz a largely mode-pure cylindrical standing wave field is built up in the radial direction, in which no significant coupling with standing wave fields dependent on other dimensions occurs.

[0192] It should be emphasized that over the entire measured range from 1400 kHz to 2050 kHz, far-reaching mode-pure excitation of a radial standing acoustic cylinder field is possible only at f1, f2, and f3 (i.e., at only 3 of about 15 possible radial resonance frequencies); it is therefore very unlikely that with only random selection of the values for width b and thickness p of the piezo plate, as well as minimum and other wall thicknesses of the carrier tube (c.sub.o and c), a mode-pure radial resonance frequency could be found afterwards purely by frequency tuning, which would come sufficiently close to the desired operating range around 1.7 MHz, and at the same time would be sufficiently far away from natural resonances of the transducer array. This underlines that the present invention is indeed a device.

[0193] For vessels 1 with smaller circular-cylindrical inner diameter 14 (typically less than 50 wavelengths in the medium at operating frequency), it is sufficient for many only weakly attenuating dispersions (such as aqueous suspensions with a solids content of typ. <10% v/v) to excite the acoustic system 300 only on one side. By way of example, FIGS. 5A and 5B illustrate such a one-sided-only configuration of the vessel 1, which is designed as a circular-cylindrical tube, with piezoelectric excitation on one side only. The criteria according to the invention for the design of the thickness and width of the oscillation element 2, as well as the general wall thickness and minimum wall thickness of the carrier tube (i.e. for b, p, c and c.sub.o) remain as described for FIG. 3C.

[0194] In this regard, it is visible in FIG. 5B that the oscillation element 2 extends over a major part of the section of the vessel 1 which has a round cross-section. In this case, however, the oscillation element 2 does not extend to the ends of these sections—nor do the connection surfaces 11 extend as far—but this may be provided in alternative embodiments. This also applies to other embodiments with several oscillation elements 2.

[0195] FIG. 5C illustrates one way of increasing the total flow cross-section by arranging a plurality of circular-cylindrical vessel tubes 1 in parallel, each fitted with an oscillation element 2. Alternatively, of course, in other embodiments, the fitting of a plurality of oscillation elements 2 may be provided. If all vessel tubes 1 and oscillation elements 2 are of identical construction, the oscillation elements 2 may be electrically interconnected (e.g. serially, in parallel, or in a combination thereof) and operated by a common alternating electrical signal. For uniform separation performance of all such parallel acoustic systems 300 when operated from a common electrical source, it is advantageous if the inner diameters of the carrier tubes 1 differ from each other by at least no more than 0.3%, preferably no more than 0.1%; and if the minimum wall thicknesses c.sub.o of the carrier tubes 1 and the thicknesses p of the oscillation elements 2 differ from each other by at least no more than 5%, preferably no more than 2%. The individual vessel tubes 1 are held at their ends in two receiving plates 30.

[0196] FIGS. 6A and 6B show by way of example further embodiments according to the invention with acoustic excitation from more than 2 directions, here for 3 and 6 directions, respectively. Common to all such star-shaped forms of excitation from 3 or more directions is that the piezo plates are of identical size, these are arranged rotationally symmetrical to the axis of the circular-cylindrical interior 14 of the carrier tube, and for the dimensions of the oscillation elements 2 and of the vessel (i.e. for b, p, and c.sub.o) the same geometrical criteria according to the invention apply as in the case described for FIG. 3C, so that an essentially cylindrical acoustic standing wave field can likewise be formed, the rotationally symmetrical wave antinode/wave node periodicity of which in all excitation directions can again be described essentially alone by the one-dimensional radial dimension r.

[0197] In the embodiments shown in FIG. 6A-C, the oscillation elements are of the same thickness p and the same width b. In alternative embodiments, however, oscillation elements of different sizes may also be provided.

[0198] FIG. 6C illustrates a coupling of several parallel acoustic vessels 1 according to FIG. 6B into a honeycomb-shaped arrangement acoustically coupled via the oscillation element 2 as a way of increasing the total flow cross-section and further uniform acoustic energy distribution when operating on a common alternating electrical signal. In this regard, two vessels 1 are adjacent to each oscillation element 2, wherein each vessel 1 located inside the honeycomb-like structure is adjacent to a total of six oscillation elements 2.

[0199] FIG. 7A illustrates another way of increasing the total flow area by acoustically coupling multiple circular-cylindrical acoustic volumes drilled side-by-side in a common block. In other words, multiple vessels have a common shell that has a common outside wall 12. This results in an array of vessels 5, with six vessels 1 being evenly distributed in cross-section around a central vessel 1, thus being at an angle of 60° to their adjacent vessels 1. The outside wall 12 has connection surfaces 11 on which the oscillation elements 2 are arranged, with the connection surfaces being equally evenly arranged around the central vessel 1, corresponding to the vessels 1. All vessels 1 have the same inner radius r.sub.0 and thus the same interior 14, and all oscillation elements 2 have the same dimensions. Optimal acoustic coupling is achieved when the equivalent wall thickness c.sub.1+2.Math.Δc/3 between two adjacent vessels 2 corresponds to an integral multiple of half a wavelength, i.e. preferably corresponds approximately to the relation c.sub.1+2.Math.Δc/3=n.Math.v.sub.C/(2f).

[0200] In contrast, it is preferred that the outside wall 12 bounding the vessel array to the outside be as acoustically opaque as possible. This can be achieved, for example, by removing unnecessary volumes (such as the regions marked “A” in FIG. 7A) from the overall vessel wall, and the remaining equivalent wall thickness (e.g., in the case shown, c.sub.2+2.Math.Δc/3) corresponds to an odd multiple of a quarter wavelength, i.e., c.sub.2+2.Math.Δc/3=(2n−1).Math.v.sub.C/(4f). All other characteristic dimensions (b, p, and c.sub.o) preferably correspond to the case already discussed for FIG. 3A to 3C.

[0201] FIG. 7B illustrates one of the possible acoustic couplings of several vessel arrays 5, as for example in FIG. 7A, as a possibility of further enlarging the flow cross-section and furthermore of distributing the acoustic energy as evenly as possible when operating on a common electrical alternating signal. In this case, corresponding to FIG. 6C, the oscillation elements 2 are acoustically connected to two vessel arrays 5 each, whereby a honeycomb-like structure is created.

[0202] FIGS. 8A-8E illustrate further of the many possibilities for acoustically coupling a plurality of acoustic cylinders according to the invention to increase flow cross-section and uniform acoustic energy distribution when operating from a common alternating electrical signal. Again, the same criteria as discussed earlier preferably apply to the characteristic dimensions b, p, c.sub.o, c.sub.1, c.sub.2. FIG. 8A shows an embodiment of a composite vessel 5 with oscillation elements 2 arranged uniformly on the outside wall 12, while the embodiment of FIG. 8C has only two oscillation elements 2 on each of two sides, each of which is associated with a vessel 1. It should be emphasized that either vessels 1 may be coupled to individual shells via the oscillation elements 2, see for example FIG. 8B. On the other hand, vessel arrays 5 can also be coupled to each other via oscillation elements 2, see FIG. 8D and FIG. 8E.

[0203] FIG. 9A illustrates a general structure of a transducer array 200 formed by the oscillation element 2 and the vessel wall section 10, as well as further acoustically coupled layers 23a, 23b, 24, 25, 26, wherein one or more coupling layers 23a, 23b, 24 may be arranged between the side 21 facing the vessel of the oscillation element 2 essentially consisting of a piezoelectric plate 20 and the vessel wall section 10. These coupling layers 23a, 23b, 24 may be necessary, for example, in order to fix the oscillation element 2 to a stationary support plate 24 by means of an adhesive layer 23a instead of permanently bonding it directly to the vessel wall 10, in order to be able to acoustically couple the vessel 1 to the oscillation element 2 via this support plate 24 for only temporary use (for example, with a gel layer 23b serving as a bonding layer and applied to the support plate 24). This makes it possible, for example, to be able to manufacture the vessel 1 from plastic materials for single use, but to provide the oscillation element 2 for frequent use. In this regard, the bonding layers 23a, and/or 23b may be so thin as to be negligible.

[0204] Similarly, one or more outer layers 25, 26 may be arranged on the side 22 of the oscillation element 2 facing away from the vessel 1 in the thickness direction of the oscillation element 2. This can serve, for example, to apply a counter-mass 25 to the oscillation element 2 outwardly via a connecting layer 26 for reasons of acoustic symmetry. However, the outer layers 25, 26 can also serve, for example, to electrically and/or acoustically insulate the oscillation element 2 outwardly from a surrounding cooling liquid. The outer layers 25, 26 can thereby represent insulating layers 25 on the one hand and connecting layers 26, (for example made of adhesive) on the other hand. The connecting layers may be so thin as to be negligible. The outer layers 25, 26 are acoustically coupled layers of the transducer array 200.

[0205] Analogous to the trivial case illustrated in FIG. 3C, according to the invention the acoustically coupled layers 2, 10, 23a, 23b, 24, 25, 26 of a multilayer transducer array 200 illustrated as in FIG. 9A have thicknesses such that none of the natural resonances of the transducer array lies in the vicinity of the desired operating frequency f, and preferably occupy as large a frequency spacing as possible from the desired operating frequency f, thus the thicknesses of the layers come as close as possible to the condition

[00018] $2 f .Math. (c_{equ} / v_{c} + p / v_{P} + d_{1} / v_{d 1} + d_{2} / v_{d 2} + .Math. + d_{i} / v_{di}) = 1 / 2 + n$ $n = {0, 1, 2, 3, .Math.},$

[0206] wherein v.sub.c is furthermore the sound velocity in the vessel wall section 10 in the region of the oscillation element 2 and v.sub.p is the sound velocity in the thickness direction in the oscillation element 2, while d.sub.1 to d.sub.i are the thicknesses and v.sub.d1 to v.sub.di are the sound velocities of further layers 23a, 23b, 24, 25, 26 of the transducer array 200 acoustically coupled in the thickness direction, and the index number “i” is a natural number which indicates the number of these further layers 23a, 23b, 24, 25, 26 of the transducer array.

[0207] Furthermore, in a preferred embodiment, the thicknesses of the one or more outer layers 25, 26 coupled to the side 22 of the oscillation element 2 facing away from the vessel satisfy, as far as possible, in themselves the condition

[00019] $2 f ({d^{″}}_{1} / v_{d^{″} 1} + {d^{″}}_{2} / v_{d^{″} 2} + .Math. + {d^{″}}_{k} / v_{d^{″} k}) = s s = {0, 1, 2, 3, .Math.},$

[0208] which is equivalent to the condition that, if possible, an integer half-wave number falls on the total thickness of these outer layers 25, wherein d″.sub.1 to d″.sub.k are the thicknesses and v.sub.d″1 to v.sub.d″k are the sound velocities of these outer layers 25, 26, and the index number “k” is a natural number indicating the number of these outer layers.

[0209] For the normally practical case where a piezoelectric plate is used as the oscillation element 2 for excitation at your thickness mode fundamental frequency (i.e., the oscillation element has a thickness p=v.sub.P/(2f)), two latter conditions can also be expressed as

[00020] $(c_{equ} / v_{c} + p / v_{P} + d_{1} / v_{d 1} + d_{2} / v_{d 2} + .Math. + d_{i} / v_{di}) = p / v_{P} .Math. (1 / 2 + n \pm Δ n), and (d_{1}^{″} / v_{d^{″} 1} + d_{2}^{″} / v_{d^{″} 2} + .Math. + d_{k}^{″} / v_{d^{″} k}) = p / v_{P} .Math. (s \pm Δ s),$

[0210] where n={0, 1, 2, 3, . . . } and s={0, 1, 2, 3, . . . }, wherein the tolerance values Δn and Δs are each at least less than 0.3, preferably 0.2, and particularly preferably less than 0.1.

[0211] The width b of the oscillation element 2 preferably corresponds to the case already discussed for FIGS. 3A to 3C.

[0212] FIG. 9B shows a possible embodiment variant according to the invention, in which several identically constructed tubular vessels 1 with transducer array 200 are arranged in parallel and surrounded by a common cooling medium 400. In this case, a transducer array 200 has, in addition to the vessel wall section 10 and the oscillation element 2, two further layers 25a and 25b which are acoustically connected (via coupling layers of negligible thickness) to the side of the oscillation element facing away from the vessel wall. In this regard, the material of these two outer layers 25a and 25b is selected such that the layer 25a located between the outermost layer 25b and the oscillation element 2 has a significantly lower acoustic impedance than the oscillation element 2 and the outermost layer 25b. This provides an acoustic isolation effect that minimizes unwanted transmission of acoustic energy into the surrounding medium 400. Preferably, the two outer layers 25a and 25b each have thicknesses corresponding to an odd multiple of a quarter wavelength at the desired operating frequency f.

[0213] FIG. 10A shows a possible embodiment variant according to the invention, in which the transducer array 200 comprises the vessel wall section 10, the oscillation element 2, an intermediate support plate 24, a negligible (therefore not shown) thin adhesive layer between the oscillation element 2 and the support plate 24, and a temporarily applied coupling layer 23 between the support plate 24 and the vessel wall section 10. This embodiment allows the vessel 1 to be acoustically coupled to the support plate 24 (for example with an acoustically transparent gel 23) only temporarily for operation. This may be useful, for example, if the vessel is intended for one-time use only, but the oscillation element is designed for frequent operation.

[0214] In this case, the vessel wall section 10, the coupling layer 23, the support plate 24, and the oscillation element 2 each have thicknesses according to the invention, which satisfy the criteria already discussed with respect to FIG. 9A. The width b of the oscillation element 2 and the wall thickness c of the vessel 1 preferably correspond to the case already discussed for FIGS. 3A to 3C.

[0215] FIG. 10B shows a further possible embodiment variant according to the invention as a two-sided variant of the device presented in FIG. 10A, with transducer arrays 200 arranged in mirror symmetry around a detachable vessel 1. This two-sided variant of FIG. 10A is particularly useful when the detachable (disposable) vessel is made of a material (e.g., plastic) that significantly dampens acoustics, and therefore a single-sided input of acoustic oscillations only cannot sufficiently ensure symmetry of incoming and reflected waves to produce an effective standing wave field within the dispersion 100. All characteristic dimensions (b, p, c.sub.o and c) preferably correspond to the case already discussed for FIG. 10A.

[0216] FIGS. 11A-11D illustrate some of the numerous ways in which devices according to the invention can be implemented in practical use.

[0217] FIG. 11A illustrates a simple way of implementing a device according to the invention for separating dispersion medium from a dispersion 100, wherein the dispersed particles have a higher specific gravity than the medium of the dispersion 100, such as is the case with biological cells dispersed in a nutrient medium.

[0218] In the illustrated arrangement, the vessel 1 forms a transducer array 200 with the oscillation element 2. The transducer array 200, the opposing acoustically reflective wall of the vessel 1, and the dispersion 100 located in the interior 14 of the vessel form an acoustic system 300. The influence region 16 of the vessel 2 located directly below the acoustic system 300 is immersed directly in the dispersion 100 without any further pipe or hose routing. A pump 62 is connected to the outflow region 17 of the vessel 1 located above the acoustic system 300. When the pump 62 is operated in the forward direction, dispersion 100 is drawn from the vessel 50 into the acoustic system 300 substantially against the force of gravity 800. The signal generator 4 is electrically connected to the oscillation element 2 and excites a standing ultrasonic field with frequency f in the acoustic system 300. This results in immobilization and compaction of the dispersed particles in the region of the sonic bulges 110, and possibly also in the formation of particle aggregates.

[0219] At the level of the transducer array 200, the vessel 1 has no significant change in the cross-section of influence with respect to its region of influence 16, so that particle compacts 110 caused by the acoustic field can sediment directly back into the container 50 under the influence of gravity 800 without being hindered by any constrictions in the region of influence 16 of the vessel 1, as soon as the regions of the particle compacts 110 (or, optionally, of the particle aggregates 110) have reached a size (or weight) which allows them to overcome the acoustic forces (and, optionally, the hydrodynamic entrainment forces of the dispersion 100 flowing into the vessel 1).

[0220] Precipitation of particle compacts 110 from the acoustic field by gravity 800 may additionally be assisted by periodic shutdown of the signal generator 4 by a timer or central process control unit 40, during which time the ultrasonic field may additionally be interrupted, the pump 62 may also be stopped or operated in reverse, so that areas of dispersion 101 with accumulated higher particle concentration are more effectively flushed back into the container 50 in and below the acoustic system 300.

[0221] In contrast to FIG. 11A, the exemplary arrangement illustrated in FIG. 11B has a narrowed inflow orifice 16 which allows, for example, the use of a pipe or hose line between vessel 1 and dispersion container 50 to operate the acoustic system 300 at a greater distance from the dispersion container 50. In this regard, the optional periodic shutdown of the signal generator 4 described for FIG. 11A, synchronized with the reversal of the pump 62, becomes a necessary process step to be provided, for example by a process control unit 40, to flush the concentrated dispersion 101 back into the dispersion vessel.

[0222] FIG. 11C illustrates a typical extension of the embodiment variant shown in FIG. 11B, in which the vessel 1 provides, in addition to the lower and upper inflow/outflow regions 16 and 17, a lateral inflow port 18 disposed substantially below the acoustic system 300 and above the lower port 16. A pump 60 transports dispersion 100 from the vessel 50 through the lateral inflow port 18 and into the vessel 1, wherein the flow rate of the pump 60 is selected to be less than the delivery line of the pump 62, thereby allowing continuous effective removal of particulate enriched dispersion 101 back into the dispersion vessel 50 via the lower outflow region 16.

[0223] Optionally, precipitation of particle compacts 110 retained in the acoustic field may be further promoted by periodically shutting down the signal generator 4, possibly also upon synchronized reversal of the pump 62 (as already optionally presented in FIG. 11A). Further optionally, it may be provided that the particle concentrate 101 is not returned to the original dispersion vessel 50 (as is, for example, useful for the application of cell retention in a bioreactor), but is collected in a separate vessel 51 (as is, for example, useful when the recovery of a particle concentrate 101, and not, or not only, the recovery of the purified medium 102 is of interest). By way of example, the application of bioreactor “harvesting” is mentioned, in which, after completion of a cell culture run, as many cells (also referred to as “biomass”) as possible must be separated from the entire contents (i.e., from the entire cell suspension 100) of a bioreactor serving as a dispersion vessel 50, in order to feed the medium 102 freed from biomass to the further biotechnological downstream process. Returning the already separated cell concentrate 101 to the bioreactor, and thus remixing it with the cell suspension 100 still to be processed, would of course be impractical.

[0224] Especially if it is important to achieve a dispersion 101 of as high as possible, (or precisely defined) particle concentration at the lower outflow orifice 16, it may be useful to use a pump 61 between the lower outflow orifice 16 and its own collection container 51 for the concentrate instead of the pump 60 in the circuit of the lateral inflow 18 (or alternatively instead of the pump 62 at the upper outflow orifice 17). In this way, the flow rate (and hence the particle concentration) of the concentrate 101 withdrawn therefrom is not dependent on the difference between the flow rates of the pumps 60 and 62, but is determined by the directly definable flow rate of the pump 61 (which is more accurate especially for smaller flow rates). If, for example, a certain quantity of biological cells is to be withdrawn from a bioreactor 50 in a controlled manner (e.g. in order not to allow the concentration of the cell suspension 100 in the dispersion container 50 to rise above a certain limit), it is particularly important to lose as little medium as possible, and therefore to achieve as highly concentrated a cell suspension 101 as possible in the collection container 51 by means of a precisely defined delivery rate at the orifice of the lower discharge region 16, for which purpose the use of the pump 61 at this orifice is particularly advantageous.

[0225] FIG. 11D illustrates an alternative arrangement with (as already presented in FIG. 11C) lateral inflow 18. However, in this arrangement variant, the lateral pump 60 shown in FIG. 11C is dispensed with, and instead a valve 72 is provided in the inflow line between dispersion container 50 and vessel 1. Furthermore, a valve 51 is also provided in the discharge line between the lower discharge area 16 and the dispersion vessel 50 (or alternatively the separate collection vessel 51 for the concentrate). Furthermore, in addition to the pump 62 which conveys the filtrate 102 from the upper orifice region 17 of the vessel 1 into the filtrate collection container 52, a further pump 61 is provided which, when activated, flushes liquid or gaseous, flushing medium suitable for the particular application from a flushing source 70 (possibly also via a separate port not shown) into the upper orifice region 17. By suitable control of the pumps 61 and 62, the valves 71 and 72, as well as the signal generator 4, the following operative states can thus be achieved via a control unit 40:

[0226] Forward mode: Pump 61 off, valve 71 closed [0227] Pump 62 on, valve 72 open [0228] Signal generator 4 activated

[0229] Backwash mode: Pump 61 on, valve 71 open [0230] Pump 62 off, valve 72 closed [0231] Signal generator 4 deactivated

[0232] In the forward mode, the dispersion 100 flows from the vessel 1 to the acoustic system 300 via the lateral port 18. The particle regions 110 compacted by the ultrasonic field precipitate as a particle concentrate 101 into the lower port region 16, wherein a particle concentrate 101 and possibly also at least partially a particle sediment 103 may be formed.

[0233] In the backwash mode, the formed particulate concentrate 101 is flushed into the dispersion container 50, or alternatively into a dedicated collection container 51, together with any sediment 103 that may also have formed.

[0234] The particular advantage of the device presented in FIG. 11D is that it avoids pumping of the particle-laden dispersion 100, 101, since pump 62 conveys only the dispersion stream 102 cleaned of particles. This is particularly advantageous in biotechnological applications, since pumping cell culture suspensions can cause damage to the suspended living cells.

[0235] All devices according to FIGS. 11A-11D, but of course not limited only to the possible forms of implementation of the device according to the invention shown in these figures, may of course also comprise several oscillation elements 2 and transducer arrays 200. These can both be arranged at substantially the same height of the vessel 1 and thus be part of a common acoustic system 300 excited by the same signal generator 4, and also be arranged at different heights of the vessel 1 and thus be part of their own acoustic systems, and then possibly also excited by different signal generators at different frequencies.

[0236] Depending on the particular application, a variety of other configurations of pumps, valves and possible additional (optionally widening or tapering) inlet and outlet ports around the acoustic system are of course possible in addition to the arrangements shown in FIGS. 11A-11D. This includes, by way of example, identical or similar arrangements as described with the figures of WO 2017/063080 A1, and of course other alternative configurations known or readily derivable from those previously mentioned and from other sources.

[0237] Further, the orientation of the exemplary devices of FIGS. 11A to 11D with respect to the direction of gravity 800 is such as to enable retention or separation of dispersed particles having a higher specific gravity than the medium of dispersion 100. It is obviously possible to arrange these and similar devices rotated 180 degrees with respect to gravity to enable retention or separation of dispersed particles having a lower specific gravity than the medium of dispersion 100, which is apparent to the average person skilled in the art of separation by sedimentation or flotation and is hereby anticipated.

[0238] FIG. 12 is an exemplary detailed illustration as a longitudinal section of a device according to the invention, such as may be used in the arrangements described in FIGS. 11C and 11D.

[0239] A possible cross-section of the device presented in FIG. 12 has already been substantially presented in FIG. 9B. Accordingly, the device consists of six similar acoustic systems 300 according to the invention and operated in parallel at the same height, each of them comprising at least one vessel 1 formed as a circular-cylindrical tube and an oscillation element 2. According to the invention, each oscillation element 2 forms with the vessel wall section located in its region (and possibly further layers having an acoustically and electrically insulating effect with respect to a possible cooling medium 400) an identical transducer array 200, so that (if desired) all 6 parallel acoustic systems 300 can also be excited by a common signal generator with the same frequency.

[0240] According to FIG. 12, the dispersion 100 flows into the device through the lateral inflow port 18 and is distributed as uniformly as possible in all directions of the common lower orifice region 16 of the device, which is designed as a sedimentation funnel, by an influence distributor 19 designed here as a circular-cylindrical funnel. In the acoustic standing wave fields of the interiors of the respective vessel tubes 1 of all six acoustic systems 300 (in FIG. 12 two of these six acoustic systems 300 are visible in cross-section), which are arranged above the inflow distributor 19 and are circular-cylindrical in design according to the invention, the regions 110 compacted with particles occur, which can subsequently be removed as dispersion concentrate 101 at the lowest point of the orifice area 16 of the device. At the same time, the dispersion medium 102 cleaned of particles can be removed from the device via a common upper outflow region 17.

[0241] FIGS. 13A and 13B show transverse and longitudinal sections of a further device according to the invention for separating dispersed particles by sedimentation 103 from a dispersion 100 present in a sample container 31 (or by flotation, if the specific gravity of the dispersed particles is less than that of the dispersion medium). In this case, the sample container 31 is introduced into the interior of the vessel 1, which is essentially circular-cylindrical in accordance with the invention, as coaxially as possible with the main axis H of the interior, wherein the sample container 31 preferably also has a circular-cylindrical shape. Spacers 33, in the embodiment shown or in another expedient embodiment, may be provided to ensure as constant as possible an intermediate space 32 between the sample container 31 and the inner wall of the vessel 1. The intermediate space 32 itself is filled with an acoustically transparent liquid or gel to provide acoustic coupling between the sample container 31 and the inner wall of the vessel 1. Inlets and outlets 39 of this or other convenient design may be provided to ensure a level of liquid in the intermediate space 32 at least as high as the area of dispersion 100 to be sonicated in the sample container 31.

[0242] The embodiment shown in FIG. 13B provides three acoustic systems 300A, 300B, and 300C arranged one above the other, each of which is typically delimited by two transducer arrays 200A-200A, 200B-200B, and 200C-200C (which are symmetrically opposite one another with respect to the main axis H of the interior of the vessel 1), and further comprising the respective intermediate sections of the liquid or gel in the intermediate space 32 and the wall of the sample container 31, as well as the respective section of the dispersion 100 at the level of the respective acoustic system. According to the invention, the transducer arrays 200A, 200B, and 200C are respectively formed by the oscillation elements 2A, 2B, 2C and by the respective sections of the wall of the vessel 1 in the region of the respective oscillation elements.

[0243] In the illustrated case, the three acoustic systems 300A, 300B, and 300C are each driven by a signal generator 4A, 4B, 4C with a respective alternating electrical signal U.sub.A˜, U.sub.B˜, U.sub.C˜. The wall thickness of the sample container 31 with respect to the three frequencies of these signals (and vice versa) is preferably provided to correspond to approximately an integer multiple of half a wavelength in the wall of the sample container 31 for each of these three frequencies, so as to provide uniform acoustic transparency through the wall of the sample container 31. This is especially true for sample containers 31 made of glass or acoustically even harder material, such as metals. On the other hand, in the case where the sample container 31 is made of plastic (such as for the purpose of single use) or another acoustically absorbent material, the wall of the sample container 31 should preferably be made thin enough to just ensure sufficient mechanical stability. In this case, the condition according to a wall thickness of the sample container 31 of half a wavelength is secondary. A suitable wall thickness of a sample container 31 made of plastic is typically in the range of 1 mm or less.

[0244] In the case shown in FIG. 13B, all signal generators 4A, 4B, 4C are activated and deactivated by a central control unit. In this case, the such individual activation/deactivation of ultrasonic fields in the acoustic systems 300A, 300B, and 300C (as one of many alternatives) can be provided, for example, in a periodically recurring sequence A-B-C-A-B-C- . . . so that first a standing wave field is formed in the highest acoustic system 300A and areas of particle compaction and/or particle aggregates 110 are formed there first, which can then be lowered in a controlled manner by subsequent activation of the lower-lying ultrasonic field in acoustic system B (when system A is switched off), and then C (when B is switched off), so that finally, after deactivation of system C, a particularly dense sediment 103 is formed at the bottom of the sample container 31.

[0245] The sequential activation/deactivation of the acoustic regions A-B-C described by way of example can be optimized, for example, by also providing periods of simultaneous activation of two or all three regions, or generally simultaneous activation of the regions A, B, C with temporally staggered deactivation; or by any other appropriate combination of activated/deactivated states of the acoustic systems 300A, 300B, 300C that optimizes such accelerated sedimentation of dispersed particles with such minimized resuspension of precipitating particle compacts and/or particle aggregates 110.

[0246] Alternatively, instead of having three acoustic systems 300A, 300B, 300C, a device according to the invention as shown in FIGS. 13A and B may have only two, one, or more than three acoustic systems.

[0247] Alternatively, a control system 40 may be omitted and the ultrasonic field in the one or more acoustic systems may be activated for a fixed duration.

[0248] Further, the particles dispersed in the dispersion 100 may have a lower specific gravity than the dispersion medium of the dispersion 100, in which case sedimentation 103 of the particles to the bottom of the sample container 31 does not occur, but instead the particles are precipitated to the surface by flotation against gravity 800.

DEVICE FOR PRODUCING A STANDARD ULTRASONIC FIELD

Inventors

Cpc classification

Classification Explorer

B01D21/283

PERFORMING OPERATIONS; TRANSPORTING

Classification Explorer

B06B1/02

PERFORMING OPERATIONS; TRANSPORTING

Classification Explorer

C12M47/04

CHEMISTRY; METALLURGY

Classification Explorer

Y02P10/20

GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Classification Explorer

B06B2201/76

PERFORMING OPERATIONS; TRANSPORTING

Classification Explorer

B06B1/20

PERFORMING OPERATIONS; TRANSPORTING

Classification Explorer

B01D2221/10

PERFORMING OPERATIONS; TRANSPORTING

International classification

Classification Explorer

B06B1/20

PERFORMING OPERATIONS; TRANSPORTING

Classification Explorer

B01D21/28

PERFORMING OPERATIONS; TRANSPORTING

Abstract

Claims

Description