US3331970A - Sonic transducer - Google Patents

Sonic transducer Download PDF

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US3331970A
US3331970A US400009A US40000964A US3331970A US 3331970 A US3331970 A US 3331970A US 400009 A US400009 A US 400009A US 40000964 A US40000964 A US 40000964A US 3331970 A US3331970 A US 3331970A
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transducer
transducer assembly
impedance
assembly
housing
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US400009A
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Dundon Thomas Martin
Joseph M R Frappier
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Honeywell Inc
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Honeywell Inc
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04RLOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
    • H04R17/00Piezoelectric transducers; Electrostrictive transducers
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K9/00Devices in which sound is produced by vibrating a diaphragm or analogous element, e.g. fog horns, vehicle hooters or buzzers
    • G10K9/12Devices in which sound is produced by vibrating a diaphragm or analogous element, e.g. fog horns, vehicle hooters or buzzers electrically operated
    • G10K9/122Devices in which sound is produced by vibrating a diaphragm or analogous element, e.g. fog horns, vehicle hooters or buzzers electrically operated using piezoelectric driving means

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Acoustics & Sound (AREA)
  • Signal Processing (AREA)
  • Multimedia (AREA)
  • Piezo-Electric Transducers For Audible Bands (AREA)

Description

3 18, 1967 T. M. DUNDON ETAL 3,331,970
SONIC TRANSDUCER Filed Sept. 29, 1964 2 Sheets-Shem- 1 INVENTORS THO/W145 MART/IV DU/VDU/V RNEYS Filed Sept. 29, 1964 T. M. DUNDON ETAL SONIC TRANSDUCER 2 Sheets-Sheet 2 CE H M 'vvvx H I ELECTRICAL C MECHANICAL TERMINALS M TERMINALS INVENTORS THOMAS MART/N DU/VDO/V United States Patent 3,331,970 SONIC TRANSDUCER Thomas Martin Dundon, Sudbury, and Joseph M. R.
Frappier, Holliston, Mass, assignors, by mesne assignments, to Honeywell Inc., a corporation of Delaware Filed Sept. 29, 1964, Ser. No. 400,009 9 Claims. (Cl. 3109.1)
This invention relates to vibratory sonic transducers and more particularly to an improved method of coupling the vibrating element to the atmosphere.
Ceramic ferroelectric materials such as barium titanate or other similar materials are desirable as sonic transducers because of their high degree of piezoelectric activity. However, these materials are also noted by the fact that they exhibit high internal losses and thus, by themselves, represent relatively inefficient transducers. It
is well known that when the piezoelectric or vibrating element is mounted on a metallic plate or disc, the combination is then capable of vibrating with higher efliciencies at some frequency other than the natural frequency of the piezoelectric element alone. The medium on which the piezoelectric material is mounted is usually metal having a high elastic modulus and a relatively low density.
When resorting to this technique, it has been noted that the acoustic impedance of the resulting device is in ordinately high. Since the acoustic impedance of the surrounding ambient medium (i.e.: air) is relatively low, it is desirable to interpose some sort of impedance matching device between the transducer element and the air so that the maximum energy will be transferred with the least amount of losses.
One matching approach is to place a transducer at one end of a tube whose length is about A wavelength (M4) at the operating frequency. The transducer then looks into a higher impedance (in the tube) than it would if it faced the air directly. Assuming for example a transducer impedance of Z and an air impedance of Z it will be seen that the tube then acts as a transformer to match the impedance of Z and Z with lower losses than if no transformer were used. While under ordinary circumstances this is highly desirable, the use of the tube alone does not quite achieve the most desirable match and in fact, there is a noticeable mismatch although not as much as there would be if no tube were present. At best, this impedance match leaves much to be desired.
It must be realized that transducer-to-air impedance matching is not the sole consideration. Another important fact that must be faced is that commercially available transducers have such a high impedance that matching with a A wave tube is virtually impossible. It is, however, highly desirable to utilize the transducers that have the higher impedance since it represents a significant saving in manufacturing costs.
We propose loading the transducer so that the impedance of the transducer element is substantially lowered to provide a better acoustic transformation between the transducer and the ambient atmosphere.
At this point, it might be wise to review the action of a transducer which by definition transforms energy of one form to energy of another form. In our particular situation, we are interested in transforming electrical energy to mechanical energy and the system may be viewed as an electromechanical transformer. That is, the transformer action associated with a pair of coupled coils (note FIG. 5 of the appended drawings). The primary or input winding is connected to the electrical terminals through a series capacitor Ce. The coils perform .the coupling. In the output or secondary Winding, there is a shunt capacitor Cm, with an inductor M in series between the secondary winding and the mechanical terminals. In this particular situation, Ce represents the capacity of the piezoelectric material and is usually determined by parameters such as the area (A), the thickness (1) and the dielectric constant (K) and may be expressed approximately by the formula Ce=KA/t. The capacitor Cm across the output winding or mechanical terminals represents the stiffness of the Vibrating element while the series inductor M represents in this particular instance the moment of inertia of the transducer-disc combination. (In expanding type transducers, this element would be equal to the mass.) The coupling, represented by coils Nzl, provides the transforming action and it may thus be seen that if the system is to satisfy our needs, the mechanical or output terminals should work into a low impedance since its load (air) has a low impedance, while the input or electrical impedance is fixed by the characteristics of the transducer at some higher level.
We have found that we can effectively lower the impedance of commercially available transducers by providing circular, disc type fiexural mode transducers with mass loading means extending beyond the edge of the transducer and providing both the active material and the mass loading means with a common pressure or loading chamber. The transducer assembly with its lowered impedance presents a noticeably better acoustic match to the surrounding or ambient medium. With the better match and efficiencies we are able to achieve a higher sonic output level for a given input power level.
It is therefore, a principal object of the subject invention to provide an improved sonic transducer device capable of being more efliciently coupled to its surrounding medium.
Another principal object of the subject invention is to provide an improved sonic transducer device noted by the fact that it has an impedance that is more readily matched to the surrounding atmosphere than heretofore possible.
A further object of the present invention is to provide an improved sonic transducer device capable of being readily mass produced because of its particular configuration.
A still further object of the present invention is to provide an improved sonic transducer device that is noted by the fact that it may be mass produced at a relatively low cost.
The present invention is a composite structure consisting of a thin layer of piezoelectric material element mounted in a housing. The associated circuitry together with the housing form an acoustical loading chamber that significantly reduces the impedance of the transducer element and thereby achieves better impedance match between the transducer element and the ambient atmosphere. The active piezoelectric material is mounted on a thin metallic diaphragm approximately thev same thickness as the piezoelectric material with the diaphragm having an extension or loading ring attached thereto whereby when the metallic diaphragm flexes, the rarefications and compressions of the atmosphere produced by the vibrating extension or loading ring, compliments or reinforces those compressions and rarefactions that appear adjacent the active transducer portion. In addition, we also provide mounting means which allows the diaphragm to move freely while controlling the trans fer of change of pressure from the outer ends to the inner portion of the diaphragm assembly.
The features of our invention which we believe to be novel are set forth with particularity in the appended claims. Our invention itself, however, both as to its organization and method of operation, together with further objects and advantages thereof, may best be understood by reference to the following description taken Patented July 18, 1967 in conjunction with the accompanying drawings in which:
FIG. 1 is an exploded view, one part thereof in partial section, indicating the relative order of the parts of our transducer assembly;
FIG. 2 is a sectional view of our transducer assembly, taken along lines 22 of FIG. 1;
FIG. 3 represents another transducer mounting arrangement;
FIG. 4 is a cross sectional view of our assembled device utilizing the mounting arrangement of FIG. 3; and
FIG. 5 is a schematic representation of the transducer operation.
Referring now to FIG. 1 there is shown an oscillator circuit assembly consisting of circuit elements 12 mounted on a printed circuit board 14. In a device of this sort, transducer assembly 22 represents the frequency determining element of the oscillator in much the same manner as a crystal in a crystal controlled oscillator. Terminals 16, mounted on terminal board 14 and screw clamping means 18 associated with terminals 16 are utilized as terminal means to which an appropriate source of power may be applied (not shown), so that the oscillator will have an appropriate source of operating potential. Leads 20.1 and 20.2 provide the means for electrically connecting the transducer assembly 22 into the oscillator circuit. The active elements of the assembly 22 are comprised, in part, of a thin layer of piezoelectric material 22.2 and a thin metallic disc or diaphragm 21.1 having a thickness that very closely approximates the thickness of the piezoelectric material 22.2.
The oscillator circuit assembly 10 and the transducer assembly 22 are placed within the confines of housing 24, with the diaphragm plate 22.1 resting on the castellated members 26 and the oscillator circuit assembly 10 resting on lip 24.2. Sound diffuser or grille 28 is contained within aperture 26.2, while cover 30 may be utilized to protect the outer portion of the sound chamber end of the housing 24 and to provide a convenient means for mounting housing 24 in a panel.
Referring now to FIG. 2, there is shown a sectional view of the completed assembly taken along lines 2-2 of FIG. 1. It should be noted that similar elements are similarly numbered. In this View, the printed circuit board 14 having circuit element 12 mounted thereon, is shown in position on lip 24.2 of housing 24 while the transducer assembly 22 is affixed to the upper edges of castellated members 26 by means of either cement or any other appropriate fastening means. A typical cement or adhesive that may be used is Silastic.
It should be noted that elements 12 and a portion of terminals 16 have been potted into housing 24 by means of potting material 34. This forms an open area above the potting material allowing clamping screws 18 to accept leads (not shown) connected to a suitable source of power to operate the oscillator. Further, when transducer assembly 22 is properly mounted in the housing, the upper edges of castellated members 26 contact the diaphragm element 22.1 in the region just at or within an area corresponding to the outer perimeter of piezoelectric material 22.2.
When all of the elements forming the novel device are assembled into housing 24 and thereby assume their indicated positions, it will be seen that transducer assembly 22 is located at one end of the resonant tube or cavity 26.2. At the same time, the use of the indicated arrangement permits the formation of an acoustic loading or pressure chamber 26.1 and a vent chamber 26.3, both of which are common to the transducer assembly 22. It is the interaction of these three chambers with assembly 22 that causes the acoustic impedance of transducer assembly 22 to be significantly lowered.
Let us assume, for purposes of illustration that, when transducer assembly 22 is first pulsed, the radiation pressures developed in the assembly 22 will cause the whole assembly to assume a convex, curved or domed configuration. That is, the ends or loading means will extend down into chamber 26.3, while the center of the piezoelectric material 22.2 (FIG. 1) has an upward bow (convex) towards circuit board 14. The dimensions of chambers 26.1 and 26.3 are chosen so that when the domed configuration exists there is a net pressure change (either positive or negative) in chamber 26.1.
The loading means as herein referred to, denotes that area of transducer assembly 22 that extend beyond the edges of castellated members 26 to thereby form the dividing means between chambers 26.1 and 26.3.
The next position to be assumed by transducer assembly 22 is one in which the piezoelectric material 22.2 assumes a concave position with respect to circuit board 14 and wherein the loading means now extends into chamber 26.1. As in the situation of the prior domed or convex configuration, there is again a net pressure change (now either negative or positive) in chamber 26.1 immediately above the piezoelectric material 22.2. In this manner, the central area of transducer assembly 22 (the area located immediately above resonant tube 26.2) is caused to vibrate at its design frequency to produce sound. With our novel design, only this central area of transducer assembly 22 is coupled to the ambient air, and then, only by reason of resonant tube 26.2. Thus, the flexing action of the loading means or peripheral portion (that portion of the transducer assembly 22 extending beyond members 26) cooperating with the central portion of the transducer cause the pressures developed by both the central portion and the peripheral portion of transducer assembly 22 to reinforce each other due to the presence of chamber 26.1 thereby effectively lowering the impedance of transducer assembly 22. With a lowered transducer impedance at its input, resonant tube 26.2 is now able to provide a better output impedance match to the ambient air.
It must be realized that a small but significant space must be provided between the outermost edge of the loading means and the inside wall of housing 24 so that there is only a minimum transfer of change of pressure from chamber 26.1 to chamber 26.3. The area of chamber 26.3 must be sufl-iciently large and preferably vented, to prevent any net pressure from being developed therein due to transducer flexing. Thus, by providing the common loading chamber 26.1 to enhance the interaction between the loading means or peripheral portion and the central portion of transducer assembly 22, the effective transformer ratio N21 (FIG. 5) is significantly changed o thereby provide a better impedance match between the transducer assembly 22 and the ambient air.
Referring now to FIGS. 3 and 4 there is shown another transducer mounting arrangement that has particular utility in our device. It should be noted that those elements in FIGS. 3 and 4 that have similar counterparts in FIGS. 1 and 2, are similarly numbered. In this mounting arrangement, the transducer assembly 22 has piezoelectric material 22.2 mounted on a metallic diaphragm 22.1 and, as described in FIG. 2, the thickness of the piezoelectric material and the metallic disc are approximately equal. In this embodiment, four clips 32 are arranged about the periphery of transducer assembly 22. While in this embodiment only four clips are shown, it will be obvious to those skilled in the art that addition clips may, in some instances, be necessary. However, at least two or three clips may be required to provide a stable mounting for the transducer assembly 22. As shown in FIG. 4, mounting means 32 comprises an outer retainer clip 32.2 and a C shaped transducer mounting clip 32.1. When utilizing this latter mounting arrangement, the castellated members 26 (FIGS. 1 and 2) are removed or cut off and instead, appropriate radial grooves may be either milled into or integrally molded into housing 24 so that the outer retaining clip 32.2 may be firmly seated to prevent movement of transducer assembly 22.
While we have described what is presently considered a preferred embodiment of a sonic transducer device as well as an alternate mounting arrangement for the transducer assembly, it will now 'be obvious to those skilled in the art that various other changes and modifications may be made without departing from the inventive concept contained therein and, it is therefore aimed in the appended claims to cover all such other changes and modifications that fall within the true spirit and scope of our invention.
What is claimed is:
1. In a sonic transducer device the combination comprising:
a piezoelectric disc element having a given thickness and a first diameter;
a metallic disc element having substantially the same thickness as the given thickness and a second diameter larger than the first diameter;
the piezoelectric disc element mounted on the metallic disc element to define a transducer assembly;
the transducer assembly consisting of a central portion of both elements and a peripheral portion of essentially the metallic disc element; and
acoustic loading means acoustically coupling the peripheral portion to the central portion to lower the acoustic impedance of the transducer assembly.
2. The combination of claim 1 further comprising support means, within the housing, fixedly supporting the transducer assembly to form a chamber between the housing and the transducer assembly; the chamber providing the acoustic coupling between the peripheral portion and the central portion.
3. The combination of claim 2 wherein the support means comprises a plurality of castellated members formed integrally with the housing.
4. The combination of claim 3 further comprising a resonator tube formed integrally with the housing, having a length approximately one quarter wavelength at the operating frequency of the transducer assembly acoustically coupling only the central portion to the ambient air.
5. The combination of claim 2 wherein the support means comprises a plurality of C shaped clips affixed to the housing.
6. The combination of claim 5 further comprising a resonator tube formed integrally with the housing, having a length approximately one quarter wavelength at the operating frequency of the transducer assembly acoustically coupling only the central portion to the ambient air.
7. In a sonic transducer device the combination comprising:
a piezoelectric disc element having a given thickness and a first diameter;
a metallic disc element having substantially the same thickness as the piezoelectric disc and a second diameter larger than the first diameter;
the piezoelectric disc element and the metallic disc element being concentrically fastened together to form a flexural mode vibrator transducer assembly having a central portion of both elements and a peripheral portion made essentially of the portion of the metallic disc element which extends beyond the piezoelectric disc element;
housing means supportingly enclosing the transducer assembly;
means in the housing means supporting the transducer assembly within but substantially close to the junction of the central portion and the peripheral portion; and
acoustic loading means in the housing means including a chamber surrounding the peripheral portion and a chamber on one side of the central portion to reduce the acoustic impedance of the transducer assembly.
8. A combination according to claim 7 including a chamber on the other side of said central portion being in the form of a tube which is resonant at the operating frequency of the device for coupling said transducer assembly to ambient air.
9. A combination according to claim 7 in which the two chambers are acoustically coupled together.
References Cited UNITED STATES PATENTS 2,167,254 7/1939 Skellett 310-8 2,506,608 5/1950 McLoad 340-10 2,911,484 11/ 1959 Spitzer 340-10 3,025,359 3/1962 Schilling 179-110 3,058,539 10/1962 Adler 310-83 3,187,300 6/1965 Brate 340-10 MILTON O. HIRSHFIELD, Primary Examiner. J. D. MILLER, Assistant Examiner.

Claims (1)

1. IN A SONIC TRANSDUCER DEVICE THE COMBINATION COMPRISING: A PIEZOELECTRIC DISC ELEMENT HAVING A GIVEN THICKNESS AND A FIRST DIAMETER; A METALLIC DISC ELEMENT HAVING SUBSTANTIALLY THE SAME THICKNESS AS THE GIVEN THICKNESS AND A SECOND DIAMETER LARGER THAN THE FIRST DIAMETER; THE PIEZOELECTRIC DISC ELEMENT MOUNTED ON THE METALLIC DISC ELEMENT TO DEFINE A TRANSDUCER ASSEMBLY; THE TRANSDUCER ASSEMBLY CONSISTING OF A CENTRAL PORTION OF BOTH ELEMENTS AND A PERIPHERAL PORTION OF ESSENTIALLY THE METALLIC DISC ELEMENT; AND ACOUSTIC LOADING MEANS ACOUSTICALLY COUPLING THE PERIPHERAL PORTION TO THE CENTRAL PORTION TO LOWER THE ACOUSTIC IMPEDANCE OF THE TRANSDUCER ASSEMBLY.
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Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3566164A (en) * 1967-06-05 1971-02-23 Centre Electron Horloger System for resiliently supporting an oscillation quartz in a casing
US3578995A (en) * 1969-09-22 1971-05-18 Dynamics Corp Massa Div Electroacoustic transducers of the bilaminar flexural vibrating type
US3638052A (en) * 1969-09-22 1972-01-25 Dynamics Corp America Electroacoustic transducers of the bilaminar flexural vibrating type
US3694674A (en) * 1969-09-29 1972-09-26 Denki Onkyo Co Ltd High voltage generating apparatus
US3704385A (en) * 1971-03-02 1972-11-28 Delta Products Inc Piezoelectric transducer assembly with phase shifting accoustical parts
US3708702A (en) * 1970-12-02 1973-01-02 Siemens Ag Electroacoustic transducer
US3761956A (en) * 1970-10-01 1973-09-25 Nittan Co Ltd Sound generating device
US3879726A (en) * 1972-03-20 1975-04-22 Mallory & Co Inc P R Audible alarm unit
US3921016A (en) * 1973-12-12 1975-11-18 Proctor & Assoc Co Sonic signal generator and housing
US3970879A (en) * 1971-12-29 1976-07-20 Sumitomo Electric Industries, Ltd. Piezoelectric acoustic device
US4006371A (en) * 1973-03-19 1977-02-01 Whitewater Electronics, Inc. Electroacoustical transducer comprising piezoelectric element
US4013992A (en) * 1976-01-28 1977-03-22 The United States Of America As Represented By The Secretary Of The Navy Diver's piezoelectric microphone with integral agc preamplifier
US4042845A (en) * 1976-03-25 1977-08-16 Sontrix Division Of Pittway Corporation Transducer assembly and method for radiating and detecting energy over controlled beam width
US4056741A (en) * 1973-04-18 1977-11-01 Airco, Inc. Audible signal generating apparatus having selectively controlled audible output
US4122365A (en) * 1976-01-26 1978-10-24 Projects Unlimited, Inc. Piezoelectric buzzer device
US4131874A (en) * 1977-05-12 1978-12-26 Westinghouse Electric Corp. Inertial balanced dipole hydrophone
US4172253A (en) * 1972-04-19 1979-10-23 Hermans Albert L Controlled wave pattern ultrasonic burglar alarm
US4190784A (en) * 1978-07-25 1980-02-26 The Stoneleigh Trust, Fred M. Dellorfano, Jr. & Donald P. Massa, Trustees Piezoelectric electroacoustic transducers of the bi-laminar flexural vibrating type
DE2951396A1 (en) * 1979-01-15 1980-07-24 Molex Inc CONNECTING DEVICE FOR A CONVERTER
US4220831A (en) * 1978-07-17 1980-09-02 Zink Henry R Intrusion sensing device
US4253095A (en) * 1978-06-07 1981-02-24 Freund Precision, Inc. Alarm apparatus for detecting disturbance or other change of condition
US4273399A (en) * 1979-11-05 1981-06-16 Amp Incorporated Transducer supporting and contacting means
US4325060A (en) * 1979-12-17 1982-04-13 Purtell Jack L Floating water detector
US4399432A (en) * 1981-02-20 1983-08-16 Lunn David J Audio signaling device and method
US4630342A (en) * 1984-12-21 1986-12-23 Motorola, Inc. Method of mounting a piezoelectric helmholtz transducer on a printed circuit board
US4674161A (en) * 1984-04-11 1987-06-23 Siemens Aktiengesellschaft Connection method for piezo-electric acoustic transducers in electro-acoustic capsules
WO1990004318A1 (en) * 1988-10-05 1990-04-19 Microsonics, Inc. Air-gap hydrophone
US5053671A (en) * 1987-11-16 1991-10-01 Nissan Motor Company, Limited Piezoelectric sensor for monitoring kinetic momentum
US5118981A (en) * 1988-09-09 1992-06-02 Nissan Motor Company, Limited Piezoelectric sensor for monitoring kinetic momentum
US6307300B1 (en) * 1998-06-11 2001-10-23 Murata Manufacturing Co., Ltd Piezoelectric acoustic component
US20070216257A1 (en) * 2004-07-22 2007-09-20 Takanao Fujimura Ultrasonic wave oscillator
US20080097216A1 (en) * 2006-09-18 2008-04-24 Liposonix, Inc. Transducer with shield
US20100123595A1 (en) * 2008-11-20 2010-05-20 Floyd Bell Inc. Audible, piezoelectric signal with integral visual signal
US20110140573A1 (en) * 2006-09-18 2011-06-16 Medicis Technologies Corporation Transducer with shield
USD879749S1 (en) * 2018-11-01 2020-03-31 Shenzhen Zhiyuan Tongtai Technology Co., Ltd. Home speaker mount
USD887397S1 (en) * 2020-02-24 2020-06-16 Qin Wang Speaker wall mount
BE1026880B1 (en) * 2018-12-18 2020-07-22 Sonitron Nv PROCEDURE FOR PRODUCING A PIEZO-ELECTRIC BUZZER AND A PIEZO-ELECTRIC BUZZER

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US2167254A (en) * 1938-04-23 1939-07-25 Bell Telephone Labor Inc Piezoelectric vibrator oscillator
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US3058539A (en) * 1958-05-15 1962-10-16 Zenith Radio Corp Transducer with impedance-matching bridge
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US2167254A (en) * 1938-04-23 1939-07-25 Bell Telephone Labor Inc Piezoelectric vibrator oscillator
US2506608A (en) * 1947-07-23 1950-05-09 Kenneth W Mcload Piezoelectric transducer
US2911484A (en) * 1954-06-28 1959-11-03 Gen Electric Electro-acoustic transducer
US3058539A (en) * 1958-05-15 1962-10-16 Zenith Radio Corp Transducer with impedance-matching bridge
US3025359A (en) * 1960-02-25 1962-03-13 Gulton Ind Inc Vibration-compensated pressure sensitive microphone
US3187300A (en) * 1963-01-29 1965-06-01 Chesapeake Instr Corp Pressure-compensated transducer

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3566164A (en) * 1967-06-05 1971-02-23 Centre Electron Horloger System for resiliently supporting an oscillation quartz in a casing
US3578995A (en) * 1969-09-22 1971-05-18 Dynamics Corp Massa Div Electroacoustic transducers of the bilaminar flexural vibrating type
US3638052A (en) * 1969-09-22 1972-01-25 Dynamics Corp America Electroacoustic transducers of the bilaminar flexural vibrating type
US3694674A (en) * 1969-09-29 1972-09-26 Denki Onkyo Co Ltd High voltage generating apparatus
US3761956A (en) * 1970-10-01 1973-09-25 Nittan Co Ltd Sound generating device
US3708702A (en) * 1970-12-02 1973-01-02 Siemens Ag Electroacoustic transducer
US3704385A (en) * 1971-03-02 1972-11-28 Delta Products Inc Piezoelectric transducer assembly with phase shifting accoustical parts
US3970879A (en) * 1971-12-29 1976-07-20 Sumitomo Electric Industries, Ltd. Piezoelectric acoustic device
US3879726A (en) * 1972-03-20 1975-04-22 Mallory & Co Inc P R Audible alarm unit
US4172253A (en) * 1972-04-19 1979-10-23 Hermans Albert L Controlled wave pattern ultrasonic burglar alarm
US4006371A (en) * 1973-03-19 1977-02-01 Whitewater Electronics, Inc. Electroacoustical transducer comprising piezoelectric element
US4056741A (en) * 1973-04-18 1977-11-01 Airco, Inc. Audible signal generating apparatus having selectively controlled audible output
US3921016A (en) * 1973-12-12 1975-11-18 Proctor & Assoc Co Sonic signal generator and housing
US4122365A (en) * 1976-01-26 1978-10-24 Projects Unlimited, Inc. Piezoelectric buzzer device
US4013992A (en) * 1976-01-28 1977-03-22 The United States Of America As Represented By The Secretary Of The Navy Diver's piezoelectric microphone with integral agc preamplifier
US4042845A (en) * 1976-03-25 1977-08-16 Sontrix Division Of Pittway Corporation Transducer assembly and method for radiating and detecting energy over controlled beam width
US4131874A (en) * 1977-05-12 1978-12-26 Westinghouse Electric Corp. Inertial balanced dipole hydrophone
US4253095A (en) * 1978-06-07 1981-02-24 Freund Precision, Inc. Alarm apparatus for detecting disturbance or other change of condition
US4220831A (en) * 1978-07-17 1980-09-02 Zink Henry R Intrusion sensing device
US4190784A (en) * 1978-07-25 1980-02-26 The Stoneleigh Trust, Fred M. Dellorfano, Jr. & Donald P. Massa, Trustees Piezoelectric electroacoustic transducers of the bi-laminar flexural vibrating type
DE2951396A1 (en) * 1979-01-15 1980-07-24 Molex Inc CONNECTING DEVICE FOR A CONVERTER
US4273399A (en) * 1979-11-05 1981-06-16 Amp Incorporated Transducer supporting and contacting means
US4325060A (en) * 1979-12-17 1982-04-13 Purtell Jack L Floating water detector
US4399432A (en) * 1981-02-20 1983-08-16 Lunn David J Audio signaling device and method
US4674161A (en) * 1984-04-11 1987-06-23 Siemens Aktiengesellschaft Connection method for piezo-electric acoustic transducers in electro-acoustic capsules
US4630342A (en) * 1984-12-21 1986-12-23 Motorola, Inc. Method of mounting a piezoelectric helmholtz transducer on a printed circuit board
US5053671A (en) * 1987-11-16 1991-10-01 Nissan Motor Company, Limited Piezoelectric sensor for monitoring kinetic momentum
US5118981A (en) * 1988-09-09 1992-06-02 Nissan Motor Company, Limited Piezoelectric sensor for monitoring kinetic momentum
WO1990004318A1 (en) * 1988-10-05 1990-04-19 Microsonics, Inc. Air-gap hydrophone
US5033032A (en) * 1988-10-05 1991-07-16 Microsonics, Inc. Air-gap hydrophone
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