AU631491B2 - Creación de Inventos y Patentes con Inteligencia Artificial

AU631491B2 – Acoustic transducers
– Google Patents

AU631491B2 – Acoustic transducers
– Google Patents
Acoustic transducers

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Publication number
AU631491B2

AU631491B2
AU74135/91A
AU7413591A
AU631491B2
AU 631491 B2
AU631491 B2
AU 631491B2
AU 74135/91 A
AU74135/91 A
AU 74135/91A
AU 7413591 A
AU7413591 A
AU 7413591A
AU 631491 B2
AU631491 B2
AU 631491B2
Authority
AU
Australia
Prior art keywords
plate
transducer
transducer system
driver assemblies
driver
Prior art date
1990-05-18
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)

Ceased

Application number
AU74135/91A
Other versions

AU7413591A
(en

AU631491C
(en

Inventor
Jozef Tabin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Siemens Canada Ltd

Original Assignee
Milltronics Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
1990-05-18
Filing date
1991-04-08
Publication date
1992-11-26

1991-04-08
Application filed by Milltronics Ltd
filed
Critical
Milltronics Ltd

1991-11-21
Publication of AU7413591A
publication
Critical
patent/AU7413591A/en

1992-01-23
Assigned to MILLTRONICS LTD.
reassignment
MILLTRONICS LTD.
Alteration of Name(s) of Applicant(s) under S113
Assignors: FEDERAL INDUSTRIES INDUSTRIAL GROUP INC.

1992-11-26
Application granted
granted
Critical

1992-11-26
Publication of AU631491B2
publication
Critical
patent/AU631491B2/en

1994-09-15
Publication of AU631491C
publication
Critical
patent/AU631491C/en

2001-05-10
Assigned to SIEMENS MILLTRONICS PROCESS INSTRUMENTS INC.
reassignment
SIEMENS MILLTRONICS PROCESS INSTRUMENTS INC.
Alteration of Name(s) in Register under S187
Assignors: MILLTRONICS LTD.

2011-04-08
Anticipated expiration
legal-status
Critical

Status
Ceased
legal-status
Critical
Current

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Classifications

B—PERFORMING OPERATIONS; TRANSPORTING

B06—GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS IN GENERAL

B06B—METHODS OR APPARATUS FOR GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS OF INFRASONIC, SONIC, OR ULTRASONIC FREQUENCY, e.g. FOR PERFORMING MECHANICAL WORK IN GENERAL

B06B1/00—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency

B06B1/02—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy

B06B1/06—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy operating with piezo-electric effect or with electrostriction

B06B1/0607—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy operating with piezo-electric effect or with electrostriction using multiple elements

B06B1/0622—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy operating with piezo-electric effect or with electrostriction using multiple elements on one surface

G—PHYSICS

G10—MUSICAL INSTRUMENTS; ACOUSTICS

G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR

G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general

G10K11/02—Mechanical acoustic impedances; Impedance matching, e.g. by horns; Acoustic resonators

Abstract

A broadly tuned transducer system for pulse echo ranging systems has a rigid plate (1), to a planar radiating front surface of which is applied at least one layer of acoustic coupling material (6) having a density intermediate between that of the plate and an atmosphere into which the transducer is to be coupled. Three or more driver assemblies spaced apart in a two dimensional array are rigidly secured to a rear surface of the plate, each assembly having a loading block (3) and a piezoelectric element (2) compressed between the block and the plate (1). The driver assemblies all have the same resonant frequency on axes perpendicular to the plate and are driven in phase; they occupy not less than one fifth and not more than four fifths of the area of the rear surface of the plate, which is rigid enough to prevent the excitement of significant flexural oscillations. The arrangement permits the transducer to have a large planar radiating surface whilst using quite small piezoelectric elements (2).

Description

41 COMMONWEALTH OF AUSTRALIA Patents Act 1952 Name of Applicant(s): Address of Applicant(s) PDER.L 1NDUSTRIEZIUUTRA GROUP Canad 3 4~
S.
S S 9*e S 55 95
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9 9 *S 59 59 9 5** Actual Inventor(s): Address for Service: JOZEF TABIN CULLEN COMPANY, Patent Trade Mark Attorneys, 240 Queen Street, Brisbane, Qld. 4000, Australia.
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COMPLETE SPECIFICATION FOR THE INVENTION ENTITLED: ACOUSTIC TRANSDUCERS The following statement is a full description of the invention including the best method of performing it known to us:
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.5 Ii bbi This invention relates to acoustic transducers for use in pulse-echo ranging applications.
5 United States Patent No. 4,333,028 (Panton) issued June 1, 1982 discloses a transducer for use in such applications which provides good performance and has received widespread commercial acceptance. The Panton invention,’as set forth in claim 25 of Patent No. 4,333,028, provides a broadly tuned directional transducer system comprising a radiating plate having a higher flexural mode resonance at substantially the operating frequency of the system, a transducer element of much smaller effective area than the plate and coupled thereto, and coupling means formed of lowloss acoustic propagation material of much lower acoustic impedance than the plate and applied to alternate antinodal zones of the radiating surface thereof such as to avoid substantial cancellation in the far field of sound radiated from said alternate antinodal zones of the plate by sound radiated from the remaining antinodal zones of the plate.
Various different ways in which this invention can be implemented are described, depending variously on enhancing or reducing radiation from alternate antinodal zones as compared to adjacent antinodal zones, and/or adjusting the A
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*0 *r 9 g 09 a Br B te phase of radiation from adjacent antinodal zones to reduce or eliminate far-field cancellation. A particular advantage of the Panton transducer is that, as compared to transducers of previous designs, for example those disclosed in United States Patent No. 3,674,945, (Hands), issued July 4, 1972, it utilizes very much smaller quantities of piezoelectric material, particularly in transducers operating at low frequency. This in turn permits the cost and weight of the transducer to be greatly reduced without any performance penalty. It has however been found that, in certain industrial environments involving high temperatures and/or chemically aggressive atmospheres, the low loss acoustic coupling materials utilized to couple the transducer to the atmosphere, which are usually fabricated from foamed synthetic plastics or rubbers, can be subject to unacceptably rapid deterioration in service. In some applications, this latter problem has required the use of transducers of the older design, despite the substantial cost and weight penalty.
20 In an endeavour to overcome the problems involved in forming the coupling means of the Panton transducer from foam materials, United Kingdom Patent Application No.
2186465A (Endress Hauser), published August 12, 1987, discloses a version of the Panton transducer as set forth above in which a grid is applied to the front of the radiating plate so as to define concentric rings and channels, the rings and channels being in front of alternate antinodal zones of the plate. The channels contain shaped bodies of air applied to the plate, which bodies provide the coupling means formed from low loss acoustic propagation material having a much lower acoustic impedance than the plate. The rings, which are not mechanically coupled to the plate, block radiation from the remaining alternate antinodal zones. The channels in the grid configure the air which they contain so that the latter provides the required coupling II~ILILIIIILIIsl~llllllllLl~e~llll
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means. There is no necessity for using vulneLable foamed materials: the grid itself, which acts largely as a mask, may be made from heat and corrosion resistant material. On the other hand, the confinement of a portion of the ambient atmosphere to form the coupling means provides less than ideal coupling between the plate and the far field, making it more difficult to control ringing of the transducer. It is also difficult to ensure that material does not become lodged between the grid and the radiating plate, with severe effects upon the performance of the transducer, whilst multiple reflections between the radiating plate and the grid may also degrade transducer performance.
It is known to increase the effective area of an axial mode transducer by applying to its front surface a 15 frustoconical radiating plate and a loading plate: U.S.
g Patent No. 4,183,007 (Baird) issued June 8, 1980 is exemplary of such transducers. There are however fairly severe limits upon the extent to which the size of the radiating surface can be extended in this manner, since the periphery of the 20 radiating plate will commence to produce flexural mode Oo se responses with deleterious effects on transducer performance and polar response.
Besides the Hands patent mentioned above, various proposals have been made for transducer assemblies comprising multiple transducer arrays in which the transducers are Se operated in unison or near unison in order to provide the effect of a single much larger transducer, and/or to enable manipulation of the polar radiation pattern of the transducer. Examples of such transducers are disclosed in U.S. Patent No. 2,567,407 (Slaymaker), 4,122,725 (Thompson), and 4,211,948 (Smith et al). Although such array may be provided with common matching layers, the transducers operate essentially independently, and a large quantity of piezoelectric material is required. U.S. Patent No.
I I 4
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2,406,767 shows, in Figure 10, an array of closely adjacent piezoelectric transducers submerged in liquid between front and rear plates. Shear effects in the liquid together with the closeness of the transducers are relied upon to maintain phase coherence and piston like operation of the plates.
Again, a large quantity of piezoelectric material is required, the elements having together substantially the same area as that of the radiating plate of the transducer.
It is also known to provide the matching layer of a transducer with a protective membrane: in addition to the Hands patent already mentioned, exemplary arrangements are shown in U.S. Patent No. 4,297,607 (Lynnworth et al), who also show in Figure 5 a multitransducer array of the type already discussed, and U.S. Patent No. 4,523,122 (Tone) (see 15 Figure 2).
An object of the present invention is to provide a transducer which can, to a substantial degree, retain the cost, weight and performance advantages of the Panton transducer, but which at the same time is more robust and better suited to use in high temperature and chemically aggressive environments.
Accordingly the invention provides a broadly tuned directional transducer system for pulse-echo ranging systems comprising a substantially rigid plate having a continuous substantially planar radiating front surface, coupling means applied to the radiating surface and comprising at least one layer of acoustic propagation material of acoustic impedance intermediate between that of the material of the plate and that of an atmosphere into which the plate is to radiate, at least three driver assemblies spaced apart in a two dimensional array upon and rigidly secured to an opposite surface of the plate, each driver assembly comprising a loading block, a piezoelectric element between the loading 555555 v:
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I block and the plate, and means maintaining the piezoelectric element acoustically coupled to the plate and to the loading block state of compression therebetween, each driver assembly having substantially the same resonant frequency as the others on an axis perpendicular to the radiating surface of the plate, and means establishing electrical connections to the piezoelectric transducers to permit excitement of the latter in phase with one another, substantially at their resonant frequencies and on said perpendicular axes, the rigidity of the plate and the proximity of the driver assemblies being sufficient to prevent the excitement of significant flexural oscillations in the plate.
😮 to Further features of the invention will be apparent from the following description of a preferred embodiment 0 Go*. 15 thereof with reference to the accompanying drawings, in *69: which: Figure 1 is a diametrical cross-section through a transducer system in accordance with the invention; and Figures 2 5 are diagrammatic rear views of 20 transducer systems in accordance with the invention, without 0. 0 their outer casings, illustrating different arrangements of .0:0 driver assemblies within the system.
Referring to Figure 1, a transducer system is based upon a thick rigid circular plate 1, typically of aluminum.
S 25 The dimensions of the plate will vary according to the frequency and beamwidth of the transducer. For example, the plate may be 2 cm thick and 20 cm in diameter for a transducer operating at 22 kHz; other dimensions given hereafter are based upon these, and are exemplary only. The plate is drilled and tapped at four points, spaced 5 cm from the centre of the plate and arrayed at the corners of a square concentric with the plate, to receive screws 4 used to secure piezoelectric elements 2 and steel loading blocks 3 to I i i 6 the plate. The piezoelectric elements and steel loading blocks are each cylindrical with a central bore to pass the shank of a screw 4 and form a symmetrical arrangement of four driver assemblies secured by the screws 4 to the plate 1.
Conductive washers 5 and 5a with integral solder tabs at their periphery are located between the elements 2 and both the plate 1 and the loading blocks 3, whilst a lock washer I and an insulating washer 16 are placed between the head of each screw 4 and its associated loading block 3. The 1 0 insulating washer 16, together with an insulating sleeve 18 which may be shrunk onto the shank of the screw, prevents the screw from establishing a short circuit between the conductive washers 5 and 5a. The washers 5 are connected *o 0o together and to one terminal of the secondary of a matching transformer 17, and the washers 5A are connected together and to the other terminal of the transformer secondary. This enables the piezoelectric elements 2 to be energized, for vibration in an axial mode, simultaneously and in parallel, by the application of an alternating potential to the primary of the transformer 17 at a frequency which equals or is close to the resonant frequency of each assembly formed by a Sloading block 3 and an element 2 secured by a screw 4 to the plate 1.
ig The screws 4 are torqued so that, even when the lements 2 are energized at a maximum rated potential of the i device, and even at extremes of the rated temperature range i’ of the device, the elements 2 remain under compression. This I prevents distortion of the oscillatory waveform produced by the assembly through momentary loss or variation of acoustic coupling between the parts, and reduces the risk of fracture of the elements 2.
The side and rear surfaces of the transducer system are wrapped with layers 7, 8, 9, 10 and 11 of vibration damping material, preferably cork, and located within an I i I r 7 open-fronted housing 21 by being embedded in a potting compound 20, typically an epoxy resin. Layers 12, 13 and 14 of cork or silicone rubber are located between the resin and the housing to provide further vibration damping. A coupling layer 6_is formed in front of the plate either by pouring a foamable resin into the housing, and foaming and curing the resin in situ, or by adhesively applying a layer of a rigid, closed celled foam selected so as to withstand temperatures to which the system is likely to be subjected.
The layer may be formed from a single bulk material or formed of two or more physically different materials either laminated or admixed. The layers may be provided with an integral or separately formed protective membrane resistant to aggressive chemicals: for example, the coupling layer may 15 be machined and covered by a thin membrane 19 in the form of a protective layer of impervious material such as stainless steel. The protective membrane may be specified so as to meet regulations applicable to transducers for operation in explosive atmospheres. In each case, the configuration is selected to provide effective coupling, typically arranging that the coupling layer represents, together with any S* membrane layer, the ecuivalent of a quarter wavelength matching layer at the resonant frequency of the transducer 0:60 system; its effective acoustic impedance should be *to 25 intermediate between that of the plate 1 and the ambient atmosphere, thus providing impedance matching in a manner similar to that provided by the Hands patent discussed above.
The thickness of the plate 1, and the relatively close’spacing of the driver assemblies, together with their operation in synchronism, result in the plate oscillating with a piston like action, without any substantial flexural mode response, comparable to that produced by a single very large cylindrical piezoelectric element, or an array of large elements energized in unison. The provision of the relatively massive plate 1 and the massive loading blocks 3 c i i 8 enables the resonant frequency of the system in the axial mode to be reduced very substantially, as compared to that of the relatively small piezoelectric elements 2 when unloaded, to a level comparable to that achieved by using a relatively thin plate operating in flexural mode as in the Panton patent. Whilst the use of multiple driver assemblies together with the thick plate 1 and the loading blocks 3 means that the reduction in weight and in the use of piezoelectric material is not quite as spectacular as that achieved by the Panton transducer assembly, it is sufficient that neither the mass of the unit nor the amount of piezoelectric material utilized presents a significant problem.
0 The loading blocks 3 are preferably but not 15 necessarily of steel, which is cheap, strong and massive, whilst the plate 1 is preferably of aluminum so that the too necessary flexural resistance may be achieved without unduly increasing the mass of the plate. If too much of the mass of the assembly is concentrited in the plate, as opposed to the loading blocks, this will reduce the amplitude of radiation P as from the plate. In transducers operating over a very wide temperature range, it may be advantageous to select the materials used to compensate for thermal expansion effects.
According to the size of the elements 2 and the 25 loading blocks 3, the diameter of the plate 1 and the desired h *frequency of operation, arrangements of the driver assemblies other than that shown in Figure 2 may be employed. Thus in Figure 3, only 3 driver assemblies are employed, arranged at the apices of an equilateral triangle concentric with the plate, whilst in Figures 4 and 5 respectively six and seven assemblies are used, with one assembly at the centre of the plate and the remainder distributed around it in a ring.
9 In order to avoid the generation of excessive flexural vibration of the plate 1, it is preferable to observe certain dimensional relationships. Firstly, the piezoelectric elements 2 should have a size and number such as to engage at least one fifth and less than four fifths of the area of the rear surface of the plate 1. Secondly, no more than one sixth of the area of the rear surface of the plate should be distant from an element 2 by more than /77 2 0. 2 7jfh w(1-q where f is the frequency of operation, h is the thickness of the plate 1, and E, q and w are respectively the Young’s modulus, the Poisson’s ratio and the !.;pecific gravity of the material of the plate.
Goes woo: 060 006:0, No

Claims (11)

1. A broadly tuned directional transducer system for pulse-echo ranging systems comprising a substantially rigid plate having a continuous substantially planar radiating front surface; coupling means applied to the radiating surface and comprising at least one layer of acoustic propagation material of acoustic impedance intermediate between that of the material of the plate and that of an atmosphere into which the plate is to radiate; at least three driver assemblies spaced apart in a two dimensional array upon and .igidly secured to an opposite surface of the plate, .9 each driver assembly comprising a loading block, a piezoelectric element between the loading block and the plate, and means maintaining the piezoelectric element acoustically coupled to the plate and to the loading block, and each driver assembly having substantially the same resonant frequency as the others on an axis perpendicular to the radiating surface of the plate; and means establishing electrical connect.his to the piezoelectric elements of the driver assemblief to permit excitement of the latter in phase S* with one another substantially at their resonant frequency and on said perpendicular axes; the rigidity of the plate and the proximity of the driver assemblies being sufficient to prevent the excitement of significant flexural oscillations in the plate. *9

2. A transducer system according to claim 1, wherein the rigid plate is circular, and the driver assemblies are attached thereto in a symmetrical arrangement.

3. A transducer system according to claim 1 or 2, wherein the piezoelectric elements and the loading blocks are cylindrical with central bores, and the means for maintaining the piezoelectric elements acoustically coupled to the plate and to the loading blocks are bolts passing through the bores wiuLi one anotner sun.tantially at their resonant frequency /2 ~i~ii i 1 t -J; M-~ -al w I S. a S a S *SS a* S *oa. a a 550 *aa. i S a a’ a, a.. 2 ar a i 11 in the block and elements and engaged with threaded bores in the plate under sufficient torque that the piezoelectric elements are maintained under cuntinuous compression during operation of the system.

4. A transducer system according to claim 3, wherein the bolts are provided with insulative washers and sleeves to prevent their establishing short circuits between the loading blocks and the plates. A transducer system according to any one of the preceding claims, wherein the driver assemblies are spaced from each other and from the periphery of the plate such that the piezoelectric elements cover at least one fifth but less than four fifths of the area of the rear surface of the plate.

6. A transducer assembly according to any one of the preceding claims, wherein at least five sixths of the area of rear surface of the plate is distant from a piezoelectric element by less than 0.27 fh/ w(-q 2 where f is the frequency of operation of the transducer, h is the thickness of the plate, and E, q and w are respectively the Young’s modulus, the Poisson’s ratio and the specific gravity of the material of the plate.

7. A transducer system according to any one of the preceding claims, wherein the driver assemblies are three in number with their axes at the apices of an equilateral triangle concentric with the plate.

8. A transducer system according to any one of claims 1 6, wherein the driver assemblies are four in number with I i I 12 their axes at the corners of a square concentric with the plate.

9. A transducer system according to any one of claims 1 6, wherein the driver assemblies are five to eight in number, with one assembly at the centre of the plate and the remainder surrounding it in a concentric ring. one A transducer system according to any, of the proceeding claims, further including a rigid enclosure open at its front surrounding the plate and the driver assemblies, the acoustic coupling means attached to the radiating surface including an environmental seal across the open front of the enclosure. e

11. A transducer system according to claim 10, wherein the coupling means incorporates an external membrane S* resistant to atmospheric conditions expected to be encountered by the transducer. or

12. A transducer system according to claim 10 11 .sr-4 wherein the means establishing electric connections to the piezoelectric elements includes a trarnformer encapsulated within the enclosure.

13. A transducer system substantially as herein described with reference to the accompanying drawings. DATED this 8th day of April 1991 Mi-,TSoqiis LrO. FEDERAL INDUSTRIES I&NUBRH^PPRN.–P-Ne By their Patent Attorneys CULLEN CO. SSEC. S113 i j

AU74135/91A
1990-05-18
1991-04-08
Acoustic transducers

Ceased

AU631491C
(en)

Applications Claiming Priority (2)

Application Number
Priority Date
Filing Date
Title

US07/524,915

US5038067A
(en)

1990-05-18
1990-05-18
Acoustic transducer

US524915

1990-05-18

Publications (3)

Publication Number
Publication Date

AU7413591A

AU7413591A
(en)

1991-11-21

AU631491B2
true

AU631491B2
(en)

1992-11-26

AU631491C

AU631491C
(en)

1994-09-15

Family
ID=
Citations (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US4011472A
(en)

1975-05-13
1977-03-08

Becton, Dickinson Electronics Company

Acoustic emission transducer

US4333028A
(en)

1980-04-21
1982-06-01

Milltronics Ltd.

Damped acoustic transducers with piezoelectric drivers

Patent Citations (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US4011472A
(en)

1975-05-13
1977-03-08
Becton, Dickinson Electronics Company
Acoustic emission transducer

US4333028A
(en)

1980-04-21
1982-06-01
Milltronics Ltd.
Damped acoustic transducers with piezoelectric drivers

Also Published As

Publication number
Publication date

EP0457467B1
(en)

1995-03-01

ES2069822T3
(en)

1995-05-16

DE69107675T2
(en)

1995-06-29

EP0457467A2
(en)

1991-11-21

ZA913224B
(en)

1992-02-26

DK0457467T3
(en)

1995-05-22

CA2042623C
(en)

1994-07-05

AU7413591A
(en)

1991-11-21

ATE119081T1
(en)

1995-03-15

US5038067A
(en)

1991-08-06

EP0457467A3
(en)

1992-11-25

JPH04230199A
(en)

1992-08-19

CA2042623A1
(en)

1991-11-19

DE69107675D1
(en)

1995-04-06

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