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Publication numberUS2202391 A
Publication typeGrant
Publication dateMay 28, 1940
Filing dateNov 3, 1938
Priority dateNov 3, 1938
Publication numberUS 2202391 A, US 2202391A, US-A-2202391, US2202391 A, US2202391A
InventorsMason Warren P
Original AssigneeBell Telephone Labor Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Piezoelectric apparatus
US 2202391 A
Abstract  available in
Images(1)
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Claims  available in
Description  (OCR text may contain errors)

May 28 1940 w. P. MASON 2,202,391

PIEZOEJECTRIG APPARATUS Filed Nov.` s, 193s TEMPERATURE- c B KM ATTORNEY i Patented May 28, 1940 UNITED STATES ATENT OFFICE PIEZOELECTRIC APPARATUS Application November 3, 1938, Serial No. 238,530

12 Claims.

This invention relates to piezoelectric crystal apparatus and particularly to piezoelectric elements of the sodium potassium tartrate type in which it is desirable to be able to stabilize the 5 resonance frequency with variations in temperature.

An object of the invention is to reduce the temperature coefficient of piezoelectric elements consisting of Rochelle salt.

l A principal object of the invention is to provide a piezoelectric element of the Rochelle salt type that may have a substantially zero temperature coefficient of frequency.

Another' object cf the invention is to provide l a piezoelectric element of the sodium potassium tartrate type that may be employed as a reactance of high stability during changing temperatures in frequency selective and control systems.

A body of piezoelectric material has various resonance frequencies depending upon the mode of vibration, the dimensions of the material and its density. Since the dimensions and the density vary with temperature it is to be expected that the mechanical resonance frequency will likewise vary. However, when a body of piezoelectric material is associated with electrodes and is subjected to an. electric field to excite it into vibration at or near one of the natural resonance frequencies oi' the body the electromechanical system involves an electrical driving circuit coupled electromechanically to the mechanical vibratingA system. Because of their coupling the electrical and mechanical systems are not independent of each other and, accordingly, the effective electrical reactance of the coupled system as presented at the electrodes of the piezoelectric element eX- periences variations in consequence of the changes in the mechanical resonance characteristics of the piezoelectric body With changing temperature. ln addition to this effect upon the reactance, there is,vin the case of sodium potassium tartrate, a still more important effect occasioned b-y the variations in dielectric capacitance, in the piezoelectric constant and in the electro-mechanical coupling especially in the temperature region adjacent the Curie point which lies at approximately 23.6 C. At that point, these electric properties of the sodium potassium tartrrate piezoelectric crystal vary in an extraordinary manner. series resonance frequency of the piezoelectric element and its anti-resonant frequency depart Widely from the mechanical resonance frequency of the piezoelectric body. The change of fre- The result is that both thev quency with temperature, or the temperature coehicient of frequency, as it iscalled, of sodium potassium tartrate is very high in the temperature region about the Curie point and amounts to about 50i) parts per million per degree centi- 5 grade. This requires that piezoelectric elements of such material of the types hitherto generally used as reactances in systems for frequency selection or control must be placed in an environment of regulated temperature wherever stable 10 electrical characteristics are essential.

The temperature coefficient of frequency of sodium potassium tartrate experiences a transition at the Curie point temperature of approximately 23.6 C. Below that temperature thel co- 15 efficient is approximateiy -l2)0; above that teniperature it is approximately 500. It follows that any system or set of conditions for compensating for the temperature coefficient on one side of the Curie point will not suiiice on the 20 other side. Since room temperatures frequently shift from one side of the Curie point to the other it is desirable to so modify the piezoelectric behavior of sodium potassium tartrate that the Curie point Will fall below ordinary room teinperatures in order that in the room temperature range no sudden shift of magnitude of the temperature coefficient of frequency will be experienced.

In accordance with one feature of the inven- 3o tion the Curie point of sodium potassium tartrate is shifted so as to fall outside of the ordinary room temperature range by introducing a certain percentage of an isomorphous substance as, for example, .3 per cent of sodium rubidium tartrate 35 which reduces the Curie point of the resulting crystal to about +7 C.

In accordance with another feature of this invention, the high negative temperature coeiiicient of sodium potassium tartrate and isomor- 40 phous piezoelectric elements is compensated by constructing a composite vibrating or resonating device which includes a tartrate piezoelectric portion and a non-piezoelectric portion mechanically associated with it to vibrate therewith as an integral unit, the non-piezoelectric portion having a temperature coefficient of frequency of opposite sign or positive and of such magnitude as to give the combined unit a substantially zero coeicient. 50

A further feature of the invention relates to a composite bar operating at a triple frequency harmonic and having the junction points of the piezoelectric and non-piezoelectric portions at antinodes of motion to minimize the tendency of 55 the Vibration to cause the different portions of the bar to pull apart.

In the accompanying drawing:

Fig. l illustrates an isomorphous sodium potassium tartrate crystal containing a small percentage of sodium rubidium tartrate;

Fig, 2 illustrates in perspective a combined 'tartrate and metallic alloy piezoelectric vibrator having a Zero temperature coeificient;

Fig. 3 shows a side view of the device of Fig. 2;

Fig. 4 illustrates a modified form of the resonator of Figs. 2 and 3 designed to operate at a triple frequency harmonic mode; y

Fig. 5 illustrates an alternative design of the structure of Fig. 4;

Fig. 6 shows a modification in which the elecu trodes are adjustably spaced from the piezoelectrie portion of the composite vibrator; and

Fig. 7 shows contrasting graphs of the variation in frequency with temperature of a composite device constructed with a piezoelectric element of sodium potassium tartrate and a similar device employing an isomorphous material conM taining sodium rubidiurn tartrate.

Fig. 1 indicates the manner of producing an X cut from an isomorphous crystal of the sodium potassium tartrate type. The Curie point of Rochelle salt (sodium tartrate) occurs at about +236 C. whereas the Curie point of the rubidium isomorphous material mixture of Pig. 1 occurs at about +7 C. It may be remarked that the temperature coefficient of frequency for longitudinal vibration of an X cut bar of Rochelle salt undergoes a marked discontinuity at the Curie point. Above that temperature the coefficient is approximately 500. Below that temperature it is about 1200. With the rub-idium salt mixture of Fig. 1 the temperature co efficient of frequency is relatively constant throughout the entire temperature range above +7" C. It follows that the rubidium salt permits a single compensation to suffice throughout the most useful temperature range; moreover, the compensation required is only about half that required for ordinary Rochelle salt below its Curie point which` is the range usually encoun tered in practical use of piezoelectric apparatus.

Fig. 2 shows a longitudinally vibrating piezoelectric device comprising a central piezoelectric portion 2 preferably consisting of sodium potassium tartrate including about .3 per cent of sodium rubidium tartrate. and end portions 3 and 4 of metal. Portions 3 and d may consist of an alloy as, for example, the sol-called stoic metal which contains about 37 per cent nickel and the remainder iron. Portions 3 and i are of smaller cross-section than portion i? except at their jiuiction planes 5 where the metal is provided with a thin web coextensive in area with the piezoelectric material to facilitate making a strong glued joint. The metal portions 3 and It are glued or otherwise affixed to piezoelectric. portion 2 to cause the ensemble to vibrate longitudinally as a unit when properly excited.

The design of a vibrating device such as is illustrated in Fig. 2 is based upon the fundamental principles developed in the articles entitled An Electromechanical Representation of a Piezoelectric Crystal appearing at pages 1252- 1263 of the Proceedings of the Institute of Radio Engineers, vol. 23, October 1935, and A Dynamic Measurement of the Elastic, Electric and Piezoelectric Constants of Rochelle Salt published in the Physical Review, vol. 55, pages 775-789, April 15, 1939.

wl Zelo p1) 2v v1 (l) In the foregoing equation w represents the. angular frequency (Zoff), Z the length of piezoelectric portion 2, Z1 the length of each of the portions 3 and Il, u the propagation velocity of motion in a longitudinal direction in portion 2, v1 the corresponding velocity in portions 3 and 4, p and p1 the respective densities of the piezoelectric material and the metallic alloy and Ze, lo Isl and lol the respective thicknesses and Widths of portions 2 and 3 as indicated in Fig. 2. It will be understood that portions 3 and. 4 are equal in dimensions and that the Webs 5 are made as thin as possible and may be omitted if desired. In any case their mass is relatively small and may be neglected in the calculations which follow in which the length` Z1 may be taken. as the entire length of the metallic portion including the web 5 if such a web be employed.

As the temperature to which the system is exposed varies, changes will take place in eachof the quantities of Equation 1. If, however, the quantities are so related that with change in temperature t the quantity w which represents frequency remains constant or, in other words, the derivative of frequency with respect to temperature is zero the system possesses what is known as a Zero temperature coeiiicient of frequency. To ascertain the conditions forI this relationship We may differentiate Equation 1 with respect to t Since the derivative of any function with respect to temperature divided by the function is the temperature coeiiicient of that function we may write where T11, T,JJ etc., are respective temperature coefiicients of Z1, w, etc, Hence Equation 3 may be rewritten tan -gwwzl tan wlll wl C052 QQ !)TlTl1'l-Tw-Tvl1`1-COS2 U1 2U uw WML-|- T+ T10-{- Tl- 171,1v Tpl- TD1- TIcl] (el) The mass M of piezoelectric portion 2 is M :Zlglop (5) Which remains constant with changes in temperature. Hence @1 @1 i, dlg e dt O Zleldt l Zzep dt+ll0pt+lelpdt Dividing by ZZeZop T+ Tlo-l-Tzj- Tl=0 (7) In similar fashion it may be shown that Tpli- T101 '1- Tze -1- T11: 0 (8) Substituting the Values shown by Equations 7 and 8 in Equation 4 tan gvwll tan @731 wl 2 wzl lTzfi-Tw-Tvlii--l "2*v1Tz-i- TLD-T111: cos co v1 2v uw [T -Tl-T +T1i 9 Zellolivi v "l 1 Solving for Tw wl -UUPU [T -T -T +T W95- tan "TTT -T 151101111111 l 1 l1 111 all n 1 COS* v l Tco: t in t i wl an U1 il an 2v 2v cos2 -Z U1 cos2 w-Z] tan La?? wl 2 wl Q [Tv-Tl] COS 5;) wz z (lo) tan -1 tan wwl i wl, 211 27) cs2 il U1 cos2 w-l! The frequency fn of a longitudinal vibration in a bar of piezoelectric material of length l and wave propagation velocity v is dv (21) @fida v di (12) d fo a il d =f i f (13) v v Z 2l Tfo=T-T1 (14) Similarly if Tf1 be the frequency of longitudinal Vibration of a bar of material having a length Z1 and propagation velocity in Substituting from (14) and (15) into (10) tan22 angl-1 Zelgp) LdZ1 2?) 01d ZellolplvlTfo TflI-tl 2 2v[Tf0] os 2v Tw: al1 wl tan tan z 1}1 21) 2v O 2 l v1 COS? LZ1 c S 2 v1 (16) t 1 t 1 T il an v1 JV www JFT 011 an 2v zezopv fO 21) C052 Lx-Jl lgllolpllll flL 11| C052 1 ZelllpfIh-I il tan 2v tan 2v 2U 2 2l U1 2 il cos 2v cos U1 (17) Tw becomes zero if [0l-2v Cos2 gil 161101'0101 Ill-Llloi'orv1 Ul C052 .111 U1 Substituting the value of Qlgpv 401101121 from Equation 1,

, al tan mi2-lll wl w11 Pfc wZ-l-tan i?) tan -lcos2 n a 0 1 La 2v TflLtan 2v tan U1 v1 2 (19) Writing tan 7/ Tfu xB-i-tan x tan y tan .t Tf1 tan x tan .zj-y m) (20) Dividing by tan :1: tan y Equation 24 is the criterion for zero temperature coecient of frequency of the composite bar for longitudinal vibration. The equation is independent of the relative cross-sections of p01'- tions 2 and 3. However, since the impedances to 75 longitudinal vibration are different in portions 2 and 3 there will occur in addition to the fundamental longitudinal vibrations, reflections at the junctions of portions 2 and 3 with portion il. Such reflections may be eliminated if the impedances be matched. The characteristic impedance Zo of the piezoelectric portion 2 is and the characteristic impedance Z1 of the nonpiezoelectric member 3 is Z1=Ze1lo1pr1 (26) For the matched impedance condition Zo=Z1 (27) Zelopvzlellolpi'l (28) Assuming as before that portion 2 consists of a bar cut from a crystal of a mixture of sodium rubidium tartrate and sodium potassium tartrate having an X cut, 7;:4200 meters per second and p=l.79. For portions 3 and Il assumed to be of stoic metal, that is, 37 per cent nickel and the remainder iron, the magnitudes are as given in Table VIII by Professor Pierce at page 27 of the Proceedings of American Academy of Arts and Sciences, vol. 63, No. l, April, 1928,

@1:4150 (approx.)

zelo M(8.02) (4150 1.1i. (1.79) (4200) Accordingly the ratio of cross-sectional areas for matched impedances is indicated by Equation 29. It is, however, unnecessary to match impedances to obtain the zero temperature coefficient condition. If instead of the relationship of Equation 28 we were to select a higher ratio of Zelo p1) Zellolilli that is, by making the cross-sectional area of the metal portions relatively smaller the conditions for zero temperature coecient could be met as indicated by Equation 24 and the electromechanical coupling coefcient could be materially raised as may sometimes be desirable.

For the matched impedance case the lengths of the materials in the composite case can be calculated by substituting Equation 28 in Equation l.

From Equation 34 we may calculate the relative lengths of the piezoelectric portion 2 and the metallic portions 3 and 4. Taking the values WO2-500, Tf1=+230 'I'he solution of Equation 36 may be obtained by reference to trigonometric tables from which it is found that The actual length of the parts of the composite bar may be determined by reference to Equation 37 since it is apparent therefrom that The actual dimensions of the composite bar Vibrator for any particular frequency may, therefore, be quite simply computed. As has been eX- plained, a somewhat different result will be obtained if a different relation than that of Equation 28 is selected. However, the basic method of design remains the same although the actual calculations will be somewhat more involved.

Fig. 3 shows how the vibrator of Fig. 2 may be constructed so as to be supported by small wires passing horizontally through holes N at nodal points. Electrodes may be electroplated on the piezoelectric portion 2 or otherwise associated with it in any desired manner.

Where a higher vibration frequency and a lower impedance are desirable resort may be had to a triple frequency mode of vibration. In this case Equation 24 is still valid as the criterion for zero temperature coefficient of frequency as it is perfectly general in character for longitudinal vibration of a composite bar. For matched impedance we may take the condition of Equation 28. Bearing in mind that We are now dealing with a frequency w which is three times as high as that involved in the design of the structure of Eig. 1,

Hence Equation 44 is satisfied by and from Equation 40 nagegaan t, E 2 2v 2 Q and This partition into thirds is a peculiarly advantageous expedient since the dividing line comes at a loop of the motion and hence at a node of tensile stress so that there is no vibrating force tending to pull the constituent bars apart at their terminal junctions. Nodes of motion occur at central points in each constituent bar. It is, therefore, expedient to support the composite bar at nodal points 6 and I shown, for example, in Figs. 4, and 6.

Fig. 4 illustrates a vibrating system in which a piezoelectric element bar 8 is glued at its ends to equal length bars 9 and I0. The bar 8 may consist of the rubidium sodium tartrate material which has been described and bars 9 and I0 of the 37 per cent nickel-iron alloy. The piezoelectric element is provided with platings or coatings I I and I2 of electrically conducting material to which the charging electromotive force may be applied. 'Ihe coatings are carefully spaced from metallic portions 9 and I0. The composite bar 8, 9, I0, is supported at nodal points of motion 6 and 'I by means of supports I3, I4 which may, if desired, be screws extending upwardly from a base member of insulating material.

Fig. 5 illustrates another method of accomplishing the same result as in Fig. 4. In this structure, a small web I5 of metal is left connecting members 9 and I0. The two piezoelectric crystal bars I6 and I1 are glued to the web. I5. These bars may be used as a divided plate crystal as, e. g., in such selective circuits as those of U. S. Patents 2,081,405, May 25, 1937, and 2,094,044 of September 28, 1937.

Fig. 6 shows a top view of a modified apparatus resembling that of Figs. 2 and 3 but in ment through an air-gap electrode arrangement. In this device horizontally mounted supporting members I8 and I9 are provided at opposite sides of the horizontally mounted composite vibrator 20, 2|, 22. Adjusting screws 23, 24 serve to hold the composite bar at its nodal points, and also to enable the members i8 and IS to be spaced closer to or farther from the composite bar. The members I8 and I 9 are supported in any desirable manner as by flexible vertical stems to permit their separation to be thus varied. The conductive coatings or platings 25, 26 which are to serve as electrodes are located on the inner sides of members I3 and I9 closely adjacent the piezoelectric portion 2l. The mechanical design of the composite vibrating bar may be in accordance with that of the structure of Figs. E and 3 which has been described in detail.

Fig. 7 illustrates graphs of the frequency characteristic of a composite vibrating bar with the dimensions indicated in the gure as plotted from measurements of its performance. The frequency deviation with temperature above and below a standard frequency of 50,667 cycles is indicated by the ordinates and the temperatures are abscissae. The upper cm've shows the performance of a sodium 'potassium tartrate-37 per cent iron-nickel combination. The lower curve shows the performance of the same metallic end pieces glued to a piezoelectric element of the sodium potassium tartrate type containing -about .l per cent of sodium rubidium tartrate cut perpendicular to the y or b axis of the crystal with its length and an angle of 45 degrees rom the :c or a axis of the crystal. It will be apparent that the mixture improves the performance of the device by extending the low range temperature coefficient portion to approximately 19 C. as against approximately 24 C. for the sodium potassium tartrate. The result shows that the over-all temperature coefficient has also been reduced from a magnitude of approximately 500 parts per million per degree centigrade for the composite device for sodium potassium tartrate (Rochelle salt) to about .l of that magnitude. Obviously, this temperature coeiiicient may be made as small as is desired by the method of this invention.

Vfhat is claimed is:

1. A composite vibrator comprising a piezoelectric element, a non-piezoelectric loading means xedly attached thereto whereby the device may vibrate as a unit, the temperature coefficients of frequency of the piezoelectric element and of the non-piezoelectric loading means having opposite signs and the density and dimensions of the loading means being so predesigned with respect to that of the piezoelectric element and with respect to the relative magnitudes of the temperature coeiiicients of frequency that in the region of a desired frequency of vibration the device is resonant at a substantially constant frequency irrespective of temperature variations.

2. In combination, a piezoelectric element consisting of sodium potassium tartrate, loading means xedly secured theretoy the temperature coefficients of frequency of the sodium potassium tartrate and the loading means having opposite signs and the dimensions and masses of the tartrate and loading means being so predesigned that together the tartrate element and the loading means constitute a unit having a desired resonance frequency and a subsantially zero temwhich it is desired to drive the piezoelectric ele-perature coefficient of frequency.

3. A composite resonator comprising elements of Rochelle salt and of a metallic alloy xedly secured together whereby they may vibrate as a mechanical unit the temperature coeiiicients of frequency of the elements having opposite signs and the temperature coeliicients, densities and dimensions of the respective elements being so related numerically that the resonator vibrates at a desired frequency at a given temperature and exhibits a substantially zero temperature coeiiicient of frequency over a relatively wide tempera-ture range in the region of the given temperature.

4. A piezoelectric device comprising a sodium potassium tartrate element and means for causing the device to vibrate at a desired resonance frequency with a substantially zero temperature coefficient of frequency consisting of loading elements fixedly secured to the tartrate element to vibrate therewith in unitary manner, the magnitudes of the density, dimensions and temperature coeicients of the elements being so predesigned as to preclude frequency variations from the desired resonance frequency over a relatively wide range of temperatures and the characteristic impedances of the tartrate element and of the loading elements for longitudinal vibration being matched to eliminate reflections whereby the composite structure tends to 'vibrate in longitudinal manner as a unitary structure having a single resonance frequency.

5. A bar adapted for longitudinal vibration at the triple frequency harmonic corresponding to its length comprising three longitudinally aligned portions of substantially equal length the middle portion consisting of piezoelectric material and the other portions of metallic material fixedly attached thereto, the portions being so proportioned in mass as to yield a zero temperature coefficient of frequency for the bar vibrating as a whole.

6. The combination of claim 5, characterized in this that means are provided for mounting the bar at nodal points for the triple frequency harmonic mode of vibration.

7. A piezoelectric resonator comprising an element cut from an isomorphous crystal of sodium potassium tartrate, the material of the crystal including approximately .3 per cent of sodium rubidium tartrate.

8. A composite vibrator comprising a barshaped member of an isomorphous crystal of sodium potassium tartrate including a small percentage of a substance which lowers the effective Curie point and similar bars of an alloy cemented at the ends of the bar of crystalline material to enable the composite bar to vibrate longitudinally as a unit the alloy having a temperature coefficient of frequency of opposite sign to that of the crystalline material and the lengths of the crystalline and alloy portions being such as to render the temperature coefcient of frequency of the composite device substantially equal to zero.

9. A device comprising three longitudinally aligned bars cemented together at their ends to constitute a composite longitudinal vibrator, the central bar comprising piezoelectric material and the other two bars consisting of metal, the relative lengths of the bars being so chosen that the loops of maximum motion occur at the junction points whereby the tensional stress at the joints is a minimum and means for supporting the device at two nodal points which are relatively Widely spaced whereby the damping introduced by the supporting structure is rendered relatively small.

10. A composite vibrator comprising a pair of longitudinally aligned bars connected by an integral web member of relatively small cross-sectional area and a piezoelectric member extending between the bars and cemented thereto at an end of each whereby the longitudinally aligned -iezoelectric member and bars are adapted to vibrate longitudinally as a unit.

1l. A piezoelectric element of sodium potassium tartrate including a small percentage of sodium rubidium tartrate to reduce the Curie point of the element.

l2. A piezoelectric element of the sodium -potasn sium tartrate type including a small percentage of an somorphous substance sufficient to shift the Curie point below the range of ordinary room temperatures and loading means iixedly secured thereto, the density and dimensions of the loading means being so designed and its temperature coei'cient being so chosen that the combined structure vibrates at a desired resonance frequency with a substantially zero temperature coefficient of frequency.

WARREN P. MASON.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2753529 *Jul 28, 1955Jul 3, 1956Rca CorpElectromechanical resonator
US2803803 *Nov 26, 1952Aug 20, 1957by mesne assignmentsElectric
US2978597 *Mar 14, 1956Apr 4, 1961Harris Transducer CorpCircuit element transducer
US3123727 *Jun 15, 1960Mar 3, 1964 Kritz
US3225226 *Aug 15, 1962Dec 21, 1965Toko Radio Coil Kenkyusho KkElectrical vibrator
US4456850 *Feb 9, 1983Jun 26, 1984Nippon Electric Co., Ltd.Piezoelectric composite thin film resonator
US20050151443 *Dec 16, 2004Jul 14, 2005Lockheed Martin CorporationPiezoelectric micro positioner for large temperature range
Classifications
U.S. Classification310/321, 23/293.00R, 310/346, 252/62.90R
International ClassificationH03H9/00, H03H9/17, H03H3/00, H03H9/05, H03H3/04, H03H9/24
Cooperative ClassificationH03H9/08, H03H9/17
European ClassificationH03H9/17, H03H9/08