US 3219969 A
Description (OCR text may contain errors)
Nov. 23, 1965 B. SNAVELY ELECTROACOUSTIC TRANSDUCER AND DRIVING CIRCUIT THEREFOR 3 Sheets-Sheet 1 Filed Sept. 19 1960 FIG.3.
SHIFTER IVIBRATOR j? MULT CLIPPER AMP.
'l'DlI-FERENTIATOR -2 CLIPPER MULTIVIBRATOR CLIPPER INVENTOR.
B. L. SNAVELY HIIHHIHH Nov. 23, 1965 B. L. SNAVELY 3,219,969
ELECTROACOUSTIC TRANSDUCER AND DRIVING CIRCUIT THEREFOR Filed Sept. 19, 1960 v 5 Sheets-Sheet 2 INVEN TOR. B. L. SNAVELY viz/5 ATTYS Nov. 23, 1965 B. L. SNAVELY 3,219,969
ELECTROACOUSTIC TRANSDUCER AND DRIVING CIRCUIT THEREFOR Filed Sept. 19, 1960 5 Sheets-Sheet 3 FICA.
INVENTOR. B. L. SNAVELY BY 2 (9% WW Y United States Patent 3,219,969 ELECTROACOUSTIC TRANSDUCER AND DRIVING CIRCUIT THEREFOR Benjamin L. Snavely, Silver Spring, Md., assignor to the United States of America as represented by the Secretary of the Navy Filed Sept. 19, 1960, Ser. No. 57,085 Claims. (Cl. 3408) (Granted under Title 35, U.S. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
This invention relates to acoustic transducers and more particularly to electroacoustic transducers that are to be used for underwater purposes.
This invention also relates to control systems for such transducers and more particularly to a control system for insuring substantially constant frequency operation of electroacoustic transducers.
In previous transducers special means are used for acoustically insulating the several parts of the transducer from the structure on which the transducer is supported. Unless these insulating means are used, the supporting structure absorbs some of the acoustic energy from the transducer and either converts this energy into heat or radiates it as acoustic energy. In the latter case, the energy radiated from the structure nearly always alfects the directional radiation pattern adversely. In the former case, the efiiciency of conversion of electrical to mechanical energy is reduced.
For trandsucers operating at fairly great depths in the water, i.e., between and 2,000 fathoms, the reduced efficiency of the transducer will have damaging effects on operation. At these depths it is essential that maximum efficiency of electric to acoustic energy be obtained in order to generate high volume signals into the surrounding water medium.
Accordingly, it is an object of this invention to provide a new and improved electroacoustic transducer capable of operating under the surface of the water at high efficiencies and for emitting large amounts of power into the surrounding sea particularly at great depths.
It is another object of this invention to provide a new and improved electromechanical transducer that is highly efiicient.
It is a further object of this invention to provide a new and improved circuit that requires small amounts of power for controlling the movement of an oscillating armature.
It is still another object of this invention to provide a new and improved circuit for elfecting maximum energy transfer between a pair of electromagnetic members.
A further object of this invention is to provide a new and improved underwater electroacoustic transducer and transducer control system that is very reliable; will operate at great depths in the water; that will emit high power, frequency stabilized signals into the ocean at maximum efliciency; and which is relatively inexpensive.
Various other objects and advantages will appear from the following description of several embodiments of this invention, and the novel features will be particularly .pointed out hereinafter in connection with the appended claims.
The manner in which this invention achieves these objects can best be understood by reference to the accompanying drawings in which:
FIG. 1 is a sectional view of a preferred embodiment of the actual transducer apparatus;
FIG. 2 is a schematic illustration of one form of a transducer control apparatus;
3,219,969 Patented Nov. 23, 1965 FIG. 3 is a schematic diagram of another embodiment of a transducer control apparatus; and
FIG. 4 is a sectional view of another embodiment of the transducer.
Of course it is to be understood that like reference numerals will be used throughout the several drawings to designate like or similar parts.
Referring now to FIG. 1 of the drawings, a sectional view of the electroacoustic transducer is shown, which comprises a rigid, hollow, cylindrical container 11 having a pair of oppositely positioned open ends. A pair of movable elements such as the pistons 12 and 13 illustrated, are each located at a respective end of the cylindrical container 11 and are slideable in proximity to the interior wall of the container. A compressible springlike medium 14, preferably consisting essentially of liquid silicone is filled within the volume of cylinder 11 between pistons 12 and 13. The fluid spring 14 is retained within the cylindrical container by means of the O ring 15 contained on piston 13 and the O ring 16 contained on piston 12.
0 rings 17 and 18 mounted on pistons 13 and 12, respectively, contact the interior walls of cylindrical member 11 and prevent sea water from intermixing with the silicone liquid 14 which is used as a spring-like member. It is essential that the spring-like medium be of sufficient stiffness to balance hydrostatic pressures which are exerted against the pistons 12 and 13 when the device is lowered to great depths in the ocean. It is also necessary that the liquid spring be of sufiicient compliance or softness so as to permit it to be com-pressed when the pistons are actuated by forces associated with acoustic radiation thereof, i.e., when the electromotive means contained within each piston synchronously and reciprocally translates the pistons in opposite directions with respect to each other.
The pistons 12 and 13 are maintained within case 11 in such a manner as to prevent them from falling out of the case by springs 81 and 82 to which they are respectively secured by any suitable means. Springs 81 and 82 are also secured to block 83 which is formed on the interior wall of case 11.
Each of the substantially cylindrical pistons 12 and 13 contains its own electromotive apparatus. A sectional view of the electromotive apparatus associated with piston 12 has been disclosed, the moving means of piston 13 being essentially the same as that of piston 12; therefore it is not believed necessary to specifically disclose the construction of the means to move piston 13 up and down. Armature 21 is centrally located within the hollow portion of piston 12 and is supported by springs, such as 22 and 23, which contact the interior face of the piston and one side of the armature. Cores 24 and 25 mounted on the upper face of piston 12, and cores 26 and 27 mounted on the lower face of the piston have a plurality of coils wound thereon which serve as the electromotive means for driving armature 21. Coils 28 and 29, wound on core 26, are series connected to each other and to the coils 31 and 32, wound on core 27; the series circuit formed by these coils being connected to lead 33. The coils wound on cores 24 and 25 are series connected to each other and are connected to lead 34. Leads 33 and 34 are maintained in place by housing 35, which is located on the lower face of piston 12. A return lead (not shown) is connected from the other end of each of these series circuits back to housing 35. A small cable 36 carrying leads 33 and 34 and the return leads associated therewith is connected between housing 35 and the larger cable 37.
Shaft 41, mounted on armature 21, contains a soft iron disc 42 mounted at the end thereof. Disc 42 is. contained within housing 43 which contains a bar-like structure 45 and a coil 46. Both ends of coil 46 are coupled to the large cable 37 by means of a pair of leads contained in cable 47. Bar-like structure 45 comprises a pair of soft iron members disposed on the upper and lower portions thereof and a pair of permanent magnets forming the vertical walls thereof. A soft iron core (not shown) is disposed within coil 46, thus establishing a magnetic circuit through the coil. Of course, it is to be understood that any other conventional position indicating means may be employed.
The amplitude of the signal appearing across the leads in cable 47 is indicative of the instantaneous velocity of armature 21 with respect to piston 12. As the armature 21 and the shaft 41 carried thereby are moved up and down, the motion of the disc 42 relative to member 45 causes a change in the magnetic flux, from the permanent magnets in structure 45, passing through the soft iron core disposed within coil 46. This changing flux generates a voltage within coil 46.
The operation of the electroacoustic transducer illustrated in FIG. 1 will now be described in detail. Once in every interval of time a current pulse is supplied to coils 28, 29, 31 and 32 by way of lead 33. This current produces a flux in the cores 26 and 27 which are coupled to armature 21 composed of ferromagnetic material thereby imparting electromagnetic forces to the armature causing it to be attracted towards the cores. Movement of armature 21 towards cores 26 and 27 in response to the current pulse causes the springs 23 mounted on the lower interior face of piston 12 to be compressed while the springs 22 mounted on the upper interior face of the piston will expand. When the pulse is removed from the windings 28, 29, 31 and 32, springs 23 will expand and springs 22 will compress causing armature 21 to oscillate from a position in proximity to cores 26 and 27 to a position in proximity in cores 24 and 25. When the armature 21 is in proximity to cores 24 and 25, springs 22 will again expand causing the armature to be returned towards cores 26 and 27. As the armature 21 moves toward cores 26 and 27 and away from cores 24 and 25, another current pulse is supplied to the coils wound on the cores 26 and 27.
As the armature 21 oscillates back and forth between cores 24 and 25 and cores 26 and 27, the disc 41 oscillates within housing 43 producing an alternating voltage on lead 47 indicative of the armature position. In order to insure equal variations with respect to the upper and lower faces of armature 21, a pulse is supplied to the coils wound on cores 24 and 25 by way of lead 34 180 out of phase with the pulse supplied to the lead 33. Application of two pulses per cycle increases the power output to the electromotive apparatus but satisfactory operation can be. achieved by applying pulses only to the coils on cores 26 and 27. Control pulses are supplied to piston 13 by way of lead 48 which is coupled to cable 37 in such a manner as to insure synchronous operation of pistons 12 and 13. These pulses occur in such a manner as to simultaneously insure inward movement of the pistons 12 and 13, i.e. towards the center of the cylinder, and to simultaneously insure outward movement of these pistons, so as to efiect volume displacements in opposite directions from each of the radiating pistons.
This type of operation causes any forces which may be produced by pistons 12 and 13 on the cylindrical container 11 to be cancelled.
In this maner, maximum efficiency is obtained with the electroacoustic transducer because no net forces are applied to the hollow container in which the moving pistons are contained.
Referring now to FIG. 2 of the drawings illustrating one embodiment of the control element for the armature 21 of FIG. 1, which comprises the position indicating mechanism of a control circuit for applying current pulses to the coils of the electromotive element in the core 26 of one of these elements. It is to be understood that this is a schematic representation and that the electromotive means comprises a pair of cores and the associated coils. In this embodiment, only one pulse is applied to the electromotive structure during each cycle and accordingly either the cores 26 and 27 mounted on the lower face of the piston 12 may be removed or those cores mounted on the upper face and their associated circuitry may be removed, i.e. it is only necessary to include a single electromagnetic circuit for moving armature 21.
When the armature 21 oscillates back and forth with respect to core 26, an alternating voltage, the amplitude of which is indicative of the instantaneous position of armature 21, is generated in coil 46 due to the movement of member 42 coupled to the armature by way of shaft 41. The alternating voltage generated in coil 46 is coupled to a conventional A.C. amplifier 51 by way of leads 47. The amplified position signal obtained from amplifier 51 is coupled to phase shifter 52, the output of which is fed to a conventional clipper amplifier 53. The output voltage of the clipper amplifier 53, a square wave of the same frequency and phase as the output of phase shifter 52, is fed to a conventional difierentiator circuit 54 that supplies a positive and negative spike once for each cycle of oscillation of armature 21. The differentiator circuit 54 is coupled to conventional clipper circuit 55 that removes one of the spikes generated by differentiator 54, thus feeding one spike per cycle of armature 21 movement into a conventional multivibrator circuit 56. Multivibrator 56 is of the type that normally produces one pulse in any predetermined period of time, the predetermined period of time being slightly greater than the frequency with which armature 21 is expected to oscillate. When a spike is supplied to multivibrator 56 from clipper circuit 55, it changes state producing an output pulse of predetermined width which is supplied from the multivibrator to the base of transistor 57.
Transistor 57 is normally maintained beyond cutoff, i.e., in a non-conducting state, because of the positive voltage applied to the base thereof from multivibrator 56. When the multivibrator produces a negative impulse of predetermined width, transistor 57 is suddenly rendered conductive and a current path is established from battery 58 through coil 28, lead 36 and the emitter and collector of transistor 57 The current through coil 28 changes the flux of core 26 thereby causing an electromagnetic force to be exerted on armature 21 by core 26. Thus, periodic movement of armature 21 is insured by the mechanical forces imparted thereto by the springs 22 and 23 and the electromotive forces applied thereto by means of the winding 28 and core 26.
In order to effectively reduce the flux level in core 26, rectifier 59 is connected in parallel with the winding 28. This causes the current which is flowing in coil 28 to flow through the rectifier when the transistor 57 is again placed in the non-conducting region in response to the termination of the predetermined width pulse produced by multivibrator 56. The diode 59 also insures complete cutoff of transistor 57 when the pulse supplied thereto from multivibrator 56 -is terminated. It should thus be apparent that transistor 57 and the circuitry associated therewith is a means for providing current impulses to the electromotive apparatus comprising core 26, coil 28 and armature 21 only during a portion of each cycle of the alternating signal generated across winding 46 by the movement of armature 21. Phase shifter circuit 52 shifts the phase of the signal supplied to dilferentiator 54 so that the impulse provided by multivibrator 56 to transistor 57 occurs at the correct time to move armature 21 with respect to core 26.
Referring now to FIG. 3 of the drawings, there is disclosed another embodiment of the control element for imparting synchronized motion to armature 21, comprising an clectromotive apparatus utilizing both cores 24 and 26. Apparatus for generating a signal indicative of the instantaneous portion of armature 21 of FIG. 3 is substantially the same as that disclosed for the similar apparatus of FIG. 2. A positive and a negative spike are obtained from differentiator 54 once each cycle, the spikes being 180 out of phase. One of the pulses, for example the negative pulse, is coupled from the differentiator 54 to the multivibrator 63 by Way of clipper 62, the clipper 62 eliminating the other spike, in this case the positive spike. The negative spike voltage applied to multivibrator 63 causes the multivibrator to change state and provide a negative pulse to base of transistor 64 thereby suddenly rendering this transistor into the conducting state. The transistor 64 is normally maintained beyond cutoff because of the positive voltage supplied thereto by multivibrator 63 prior to the time a negative pulse is fed thereto from clipper 62.
The output of differentiator circuit 54 is also coupled to multivibrator 65 by way of clipped circuit 66 and phase inverting amplifier 67. The clipper circuit 66 removes the negative spike produced by dillerentiator 54 and feeds the positive spike to phase inverting circuit 67 so that a negative pulse is supplied to the input of multivibrator 65 once each cycle and 180 out of phase with the negative spike supplied to multivibrator 63. The negative pulse fed into multivibrator 65 causes a negative pulse of predetermined width to be coupled to the base of transistor thereby rendering that transistor in a conducting state while multivibrator 65 is producing the negative pulse.
Multivibrators 63 and 65 are of the type having a certain natural period of oscillation which is slightly greater than the period of oscillation of armature 21 under normal operating conditions. This is to insure oscillation of the armature 21 if it is in a non-oscillating or steady position. Once the armature 21 is started into oscillation it will be maintained in such a state by the control circuit.
When the negative impulse is supplied to the PNP transistor 64 from the multivibrator 63, the transistor is suddenly rendered in a conducting state and current flows from battery or power supply 68 through the emitter and collector of transistor 64 and the coil 28 wound on core 26. When the current impulse from battery 68 is coupled through transistor 64 to winding 28, the flux on core 26 is driven in one direction, for example a positive direction, inducing a voltage in the secondary winding 69 of core 26. The voltage induced in Win-ding 69 in response to the positive flux change of core 26 will have no effect on the flux level of core 24. This is because rectifiers 71 and 72 serve to block any current that would normally flow from coil 69 to coil 74 as a result of the negative voltage fed to the anode of diode 71 in response to the positive flux change in core 26.
When the transistor switch is rendered non-conducting in response to the positive output voltage or" multivibrator 63, which occurs when the predetermined width pulse terminates, the flux in core 26 changes in a direction opposite to that which occurs when a current pulse is applied through winding 28, i.e., a negative flux change. When the flux level in core 26 is changing in the negative direction, a voltage is induced in winding 69 causing a positive voltage to be produced at the anode of diode 71. This positive voltage cause a current flow through capacito-r 73 and back to the other terminal of secondary Winding 69 when the flux rate of change is initially changed because the condenser 73 appears substantially as a short circuit to an initially changing voltage. As current continues to flow through the diode 71, a charge is built up on capacitor 73 raising the impedance thereof and current then flows from one end of secondary winding 69 through diode 71, coil 74 wound on core 24, and diode 72 back to the other end of coil 69. This efiects an energy transfer from core 26 to core 24 after transistor 64 has been again rendered in the non-conducting state. This arrangement permits most of the magnetic energy which is contained in core 26 when current flow through 6 transistor 64 is terminated to be transferred to core 24, thus removing almost all of the residual magnetic field existing in core 26.
The negative output impulse from multivibrator 65 is coupled to the base of normally non-conducting transistor 75 at a different time than the time that the negative impulse is supplied to transistor 64. Thus current is supplied to Winding 61 at a difierent time than it is supplied to winding 28 and these times are 180 out of phase with respect to movement of armature 21. When current is supplied to coil 61 from battery 76 through transistor 75, the change in flux of core 24 exerts sulficient force on armature 21 so as to attract the armature in the same manner that it is attracted by the fiux change of core 26. When transistor 75 is again placed in the cutoff region, a similar change of energy between core 24 and 26 occurs as when transistor 64 is rendered in the cutoff position. Thus, the positive voltage appearing at the anode of diode 72 when the flux level in core 24 is changing after transistor 75 has cut off will remove the charge which was built up across condenser 73 due to the previous half cycle current conduction through coil 69, diode 71 and condenser 73. Current from coil 74 and diode 72 through condenser 73 and back to the other terminal of coil 74 will tend to charge condenser 73 in the opposite direction to which it has previously been charged. When the charge across condenser 73 has again been built up suficiently, current will flow through diode 72, coil 69, diode 71 and back again to coil 74.
In this manner a complete energy transfer between the cores 24 and 26 is effected by applying, pulses to transistors 64 and 75 at different times in alternate succession. This results in maximum efliciency energy transfer between the two cores, reducing the residual magnetism of each to the flux value which it had under initial operating conditions.
Referring now more particularly to FIG. 4 of the drawings, which illustrates a cross-sectional view of another embodiment of the invention comprising transducer 101. The transducer case is a closed, hollow shell, preferably of circular cross-section, having a pair of oppositely positioned, partially curved surfaces or diaphragms 102 and 103 and a wall 84 having pleated portions 85 and 86. The entire shell is preferably rnade out of steel that is thick enough to be of sufficient tiffness to balance expected hydrostatic pressures exerted thereon when it is 1n use.
The elements or diaphragm-s 102 and 103 are concave with respect to the interior of the transducer in order to increase the strength of the shell, particularly at the corners. Pleated sections 85 and 86 each comprise a plurality of alternately arranged exterior and interior indentations in the wall 84. Only two exterior and one interior indentations being shown for purposes of illustration; the interior indentation being between the exterior ones. These sections are designed to compress against each other when diaphragms 102 and 103 are drawn towards each other and to expand when the diaphragms are both expanding into the surrounding medium.
Apparatus for synchronously moving elements 102 and 103 in opposite directions at the same time is employed. This actuating means is quite similar to the electromotive inertia system employed in the transducer of FIG. 1. Motivating means 87 is coupled to movable portion 102 of shell 84 while motivating means 88 is coupled to movable portion 103. Since the motivating elements are identical, it is deemed necessary to describe only one of them.
Armature 89 made of a ferromagnetic material similar to armature 21 of FIG. 1 is secured to the interior face of element 102. Plate 91 having a soft iron core 92 mounted thereon is coupled to the same face of shell 84 as is armature 89 by springs 93 and 94, fixed thereto, thus forming an inertial system. Coil 95 is connected to leads 96 and 97 forming part of cable 37 and which supply control signals to the motivating means.
The operation of this embodiment will now be described in detail. Control pulses are simultaneously applied to motivating elements 87 and 88, causing movable elements 102 and 103 to be drawn towards the center portion of the shell. The shell must be of sufiicient compliance or softness to cause the indentations of pleated sections 85 and 86 to compress together when electromagnetic energy is applied to the armature. Thus, the wall 84 of the transducer may be considered as a springlike, compliant medium.
After the pulse has terminated, springs 92 and 93 push the interior wall of element 102 away from platform 91. At the same time, similar forces in an opposite direction are exerted by the inertial system associated with motivating element 88 against the interior wall of element 103. In this manner, the indented portions of pleated sections 85 and 86 expand and both surfaces 102 and 103 are forced apart causing expansion of the surrounding medium. Elements 102 and 103 are again drawn together when the next periodic pulse is applied to the electromotive apparatus. In this manner elements 102 and 103 are synchronously moved in opposite directions causing acoustic or pressure energy to be radiated into the medium surrounding transducer 101. The frequency of the generated energy depends on the period of the input pulses supplied to the motivating system which is in turn dependent on the natural frequency of the inertial system.
Periodic input pulses may be applied to the apparatus of FIG. 1 or FIG. 4 from a fixed frequency source, or a feedback arrangement such as disclosed in FIG. 2 may be utilized for transducer 101 of FIG. 4. Of course it is to be understood that any suitable position pickup may be utilized with the system of FIG. 4 if a feedback arrangement is employed.
The transducers of FIGS. 1 and 4 employ spring mass inertial driving systems rather than a fixed motivating means because in the latter type device the air gap between the electromagnetically actuated core and armature is varied as the transducer depth in the water changes. Thus, the air gap would have an optimum value for conversion of electrical to mechanical energy only over a limited range of water depth. In order to obtain efficient transducer operation for great variations in water depth and pressure, it is essential that the overall gap between the core and armature remain fixed as these exterior conditions are altered. Such as independence of hydrostatic water pressure is secured by the employed inertial driving unit.
It should now be apparent that there has been herein disclosed an electroacoustic underwater transducer that transfers electric energy to mechanical energy with a high degree of efficiency. This transducer is capable of emitting high amounts of power to the adjacent underwater medium in which it is located at great depths with great reliability.
It will be understood that various changes in the details, materials and arrangements of parts, which have herein been described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims.
What is claimed is:
1. An underwater electroacoustic transducer comprising a substantially cylindrical, rigid, hollow member having a pair of oppositely positioned open ends, a pair of movable substantially cylindrical pistons, each piston being located at a respective end of the cylindrical member and slideable in proximity to the interior wall thereof,
.a control element, electromotive means contained within each of said pistons and coupled to said control element for synchronously moving said pistons in opposite directions, a fluid spring consisting essentially of liquid silicone filling the volume within the member lbetween said pistons, and means carried by each of said pistons for retaining the liquid silicone Within the member.
2. The transducer of claim 1 wherein each of said pistons includes a plurality of springs contained therein and an armature supported by said springs and mounted in proximity to said electromotive means.
3. The transducer of claim 2 wherein said control element comprises means coupled to the armature of one of said pistons for genera-ting alternating electrical signals indicative of armature movement, and a control circuit coupled between said electromotive means and said generating means, said control circuit including means for applying current impulses to said electromotive means only during a portion of each cycle of the generated alternating Signals.
4. The apparatus of claim 3 wherein said electromotive means comprises a core having a coil wound thereon; and said control circuit comprises a normally nonconducting transistor, a power supply series connected to said coil, the collector and emitter of said transistor being connected between said coil and said power supply, and a rectifier connected across said coil.
5. The apparatus of claim 3 wherein said electromotive means comprises a pair of cores, each respectively mounted on opposite sides of said armature and each respectively having first and second coils wound thereon; and said control circuit comprises a pair of normally nonconducting transistors, each coupled to said first coil of a respectivecore, a pair of impulse producing networks each respeeitvely coupled to one of said transistors for rendering said transistors alternately conducting during different portions of the generated alternating electrical signals, and a network coupled between said second coils for effecting energy transfer between said cores.
6. The apparatus of claim 5 wherein said network for effecting energy transfer between said cores comprises a pair of rectifiers, each coupled between one end of said second coil on one of said cores and the other end of the second coil on the other core, and a condenser coupled between said rectifiers.
7. The apparatus of claim 3 wherein said control circuit further includes a phase shifting network coupled to said generating means, a clipper amplifier connected to said phase shifting network, a ditferentiator network connected to said clipper amplifier, a clipper network connected to said differentiator network, and a multivibrator connected to said clipper network and to said means for applying current impulses.
8. The apparatus of claim 3 wherein said electromotive means comprises a pair of cores, each respectively mounted on opposite sides of said armature and each respectively having coils wound thereon; and said control circuit comprises a pair of normally nonconducting transistors, each coupled to said coil of a respective core, a pair of impulse producing networks each respectively coupled to one of said transistors for rendering said transistors alternately conducting during different portions of the generated alternating electrical signals.
9. A circuit for controlling the movement of an oscillating armature mechanically maintained in motion comprising means coupled to the armature for generating continuously alternating electrical signals indicative of the movement thereof, electromotive means mounted in proximity to the armature for imparting motion thereto, a control circuit coupled between said electromotive means and said generating means, said control circuit including means for applying current impulses to said electromotive means only during a portion of each cycle of the generated continuously alternating signals, said electromotive means having a pair of cores, each respectively mounted on opposite sides of said armature and each respectively having first and second coils wound thereon; and said control circuit having a pair of normally non-conducting transistors, each coupled to said first coil of a respective core, a pair of impulse producing networks each respectively coupled to one of said transistors for rendering said transistors alternately conducting during different portions of the generated alternating electrical signals, and a network coupled between said second coils for effecting energy transfer between said cores.
10. The circuit of claim 9 wherein said network for effecting energy transfer between said cores comprises a pair of rectifiers, each coupled between one end of said second coil on one of said cores and the other end of the second coil on the other core, and a condenser coupled between said rectifiers.
11. A circuit for effecting energy transfer between a first and second core comprising first electromagnetic means coupled to said first core for changing the flux of said first core in a first direction, second electromagnetic means coupled to said second core for changing the flux of said second core in a second direction at a different time than when the flux of said first core is changed in the first direction, a first coil wound on said first core and a second coil wound on said second core, a first rectifying means coupled between one end of said first coil and one end of said second coil for permitting current flow from said first coil to said second coil only when the flux in said first core is changing in a direction opposite to the first direction and a second rectifyingmeans coupled between the other end of said first coil and the other end of said second coil for permitting current flow from said second coil to said first coil only when the flux of said second core is changing in a direction opposite to the second direction, and a capacitor connected between said first and second rectifying means.
12. A circuit for effecting energy transfer between a first and second core comprising first, second, third and fourth coils, said first and second coils being wound on said first core in opposite directions, said third and fourth coils being wound on said second core in opposite directions, a pair of current sources, one of said sources coupled to said first coil and the other of said sources coupled to said third coil, each of said current sources sequentially applying current impulses to the respective coil, a first rectifying means coupled between one end of said second coil and one end of said fourth coil for permitting current flow from said second coil to said fourth coil only when the flux is decreasing in the first core, a second rectifying means coupled between the other end of said second coil and the other end of said fourth coil for permitting current flow from said fourth coil to said second coil only when the flux is decreasing in the second core and a condenser connected between said first and second rectifying means.
13. A circuit for controlling the movement of an oscillating armature mechanically maintained in motion comprising means coupled to the armature for generating continuously alternating electrical signals indicative of the movement there l c ro no i e mea s mo nted in proximity to the armature for imparting motion thereto, a control circuit coupled between said electromotive means and said generating means, said control circuit including means for applying current impulses to said electromotive means only during a portion of each cycle of the generated continuously alternating signals, said control circuit further having a phase shifting network coupled to said generating means, a clipper amplifier connected to said phase shifting network, a differentiator network connected to said clipper amplifier, a clipper network connected to said differentiator network, and a multivibrator connected to said clipper network and to said means for applying current impulses.
14. An underwater acoustic transducer comprising a rigid, hollow member having a pair of oppositely positioned open ends, a pair of pistons, said pistons being synchronously movable in opposite directions with respect to each other, each located at a respective end of said member and slideable in proximity to the interior wall thereof, a compressible spring-like medium retained within said member between said pistons, said medium being a fluid spring of sufiicient stiffness .to balance hydrostatic pressure exerted on said pistons and of sufficient softness to compress when said pistons are actuated by the forces associated with acoustic radiation therefrom, sealing means between each piston and the hollow member for retaining the fluid within said member, and electromechanical vibration generating means positioned within each of said pistons for synchronously and reciprocally moving said pistons in opposite directions with respect to each other.
15. The transducer of claim 14 wherein the fluid spring consists essentially of liquid silicone.
References Cited by the Examiner UNITED STATES PATENTS 2,081,619 5/1937 Ebert.
2,375,158 5/1945 Wills 318l32 X 2,405,575 8/1946 Hayes et a1 340-16 2,519,916 8/1950 Martin 34012 X 2,623,738 12/1952 Davidson 318-l27 2,769,946 11/ 1956 Brailsford 318128 2,843,742 7/ 1958 Cluwen 318127 2,895,095 7/1959 Guyton 318132 2,903,673 9/1959 Harris 3408 2,945,168 7/1960 Steinke 3 l8-128 2,958,078 10/1960 Hickman et a1 340-8 3,004,178 10/ 1961 Efromson 3408 X 3,056,104 9/1962 Kanski et a1 3405 3,118,098 1/1964 Reich 318-132 X 3,124,730 3/1964 Thoma 318128 CHESTER L. JUSTUS, Primary Examiner.