US3773570A

US3773570A - Construction element having strongly negative temperature coefficients of elasticity moduli

Info

Publication number: US3773570A
Application number: US00084307A
Authority: US
Inventors: S Steinemann; M Peter
Original assignee: STRAUMANN AG R
Current assignee: STRAUMANN AG R; STRAUMANN R AG CH
Priority date: 1966-08-29
Filing date: 1970-10-27
Publication date: 1973-11-20
Anticipated expiration: 1990-11-20
Also published as: GB1200192A; CH461815A; DE1558518C2; DE1558518B1; DE1558517C2; DE1558517B1

Abstract

The disclosure is directed to construction elements having highly negative temperature coefficients of the moduli of elasticity, and which are characterized in that the construction elements consists of, or contain as the predominant phase, a metal having a paramagnetic atomic susceptibility x > OR = 40, 10 6 emu/g-atom at room temperature, and also a positive temperature coefficient of this susceptibility 1/x dx/dT. Furthermore, the construction element is characterized by a preferred orientation of the crystallites of the metal and which preferred orientation has a rigid orientation relationship to the occurring mechanical load. The materials of the construction elements may be, for example, alloys of Sr and Ca, Ti and Al, Zr and Sc, and multicomponent alloys as Ti-Zr-Al, Ti-Sc-Al. The elements may consist of a samarium-base alloy. The construction elements also may be characterized in that the metal contains limited amounts of B, C, N or O, so-called interstitials of low atomic size. The disclosure is also directed to methods of producing the preferred orientations by cold-working, annealing, or both and these processes are also applicable for hardening the metal by dispersion or precipitation. A specific example of an article in the disclosure is a tuning fork useable as a temperature sensor by virtue of its marked change in resonance frequency with changes of temperature.

Description

United States Patent 1 Steinemann et al.

[ CONSTRUCTION ELEMENT HAVING STRONGLY NEGATIVE TEMPERATURE COEFFICIENTS OF ELASTICITY MODULI [75] Inventors: Samuel Steinemann, Liestal; Martin Peter, Vesenaz, both of Switzerland [73] Assignee: Institut Dr. Ing. Reinhard Straumann A.G., Waldenburg, Switzerland [22] Filed: Oct. 27, 1970 [21] Appl. No.: 84,307

Related US. Application Data [63] Continuation-impart of Ser. No. 663,748, Aug. 28, 1967, abandoned, Continuation-in-part of Ser. No. 631,686, April 18, 1967, Pat. No. 3,547,713.

[30] Foreign Application Priority Data Aug. 29, 1966 Switzerland 12494/66 [52] US. Cl 148/32.5, 75/67, 75/134 A, 75/152, 75/177, 148/27, 148/121, 148/158 [51] Int. Cl. C22c 33/00, H011 3/00, C22b 29/00 [58] Field of Search 148/32, 32.5, 158, 148/161, 27, 13; 75/175.5, 177, 152, 134 R,

[56] References Cited UNITED STATES PATENTS 2,703,278 3/1955 Finlay et al. 7S/l75.5 3,540,946 11/1970 Minton et al. 148/32.5 3,341,373 9/1967 Evans et al. 75/177 3,510,295 5/1970 Cox et al. 148/32.5 X 2,786,756 3/1957 Swazy et al. 148/32.5 X

921,607 5/1909 Goldschmidt.. 75/134 A 3,431,808 3/ 1969 Oudet et al. 84/457 3,547,713 12/1970 Steinemann et al. 148/13 3,597,642 8/1971 Kurino 84/409 Nov. 20, 1973 3,636,810 1/1972 Reefman 84/457 Primary Examiner-L. Dewayne Rutledge Assistant Examiner-W. R. Satterfield Attorney-McGlew and Toren [57 ABSTRACT The disclosure is directed to construction elements having highly negative temperature coeflicients of the moduli of elasticity, and which are characterized in that the construction elements consists of, or contain as the predominant phase, a metal having a paramagnetic atomic susceptibility x z 40, 10 emu/gatom at room temperature, and also a positive temperature coefficient of this susceptibility l/x (ix/J1. Furthermore, the construction element is characterized by a preferred orientation of the crystallites of the metal and which preferred orientation has a rigid orientation relationship to the occurring mechanical load.

The materials of the construction elements may be, for example, alloys of Sr and Ca, Ti and Al, Zr and Se, and multicomponent alloys as Ti-Zr-Al, Ti-Sc-Al. The elements may consist of a Samarium-base alloy. The construction elements also may be characterized in that the metal contains limited amounts of B, C, N or O, so-called interstitials of low atomic size.

The disclosure is also directed to methods of producing the preferred orientations by cold-working, annealing, or both and these processes are also applicable for hardening the metal by dispersion or precipitation.

A specific example of an article in the disclosure is a tuning fork useable as a temperature sensor by virtue of its marked change in resonance frequency with changes of temperature.

7 Claims, 5 Drawing Figures Patented Nov. 20, 1973 3,773,570

2 SheetsSheet l X IN 10* emu/g-otom LOO 2 3 4 Eiectrons per Q M IN 10 dtegrec X dT Fig. 1b 5 3 0 5 2 Etectrons per atom Fig. 1c 1,9 2,5 3,7 1,3 M

2 3 1. Eieccrons per citom Fig.2

Torsion Traction Torsion A Bending I l L Traction I J Bending CUEBiC HEXA GONAL l NVENTORS: SRHUEL ST EINEMAN N MARTIN PETER m Mai Tm Anon was Patented Nov. 20, 1973 3,773,570

2 Sheets-s 2 FNVENTORs MARTIN PETER Bi'yflc W RM Eys CONSTRUCTION ELEMENT HAVING STRONGLY NEGATIVE TEMPERATURE COEFFICIENTS OF ELASTICITY MODULI CROSS REFERENCE TO PRIOR APPLICATION This is a continuation-in-part of application Scr. No. 663,748, filed on Aug. 28, 1967, now abandoned, and of application Ser. No. 631,686 of Apr. 18, 1967, now U.S. Pat. No. 3,547,713.

BACKGROUND OF THE INVENTION Normally no particular requirements are imposed on the temperature behavior of constructional parts in respect of dilatation or elastic properties. There are, however, cases where the dilatation of a material should remain constant or small with varying temperature (gauges, standard measures, pendulum, glass-metal connections, etc.) or where the dependence on temperature of the elasticity of the material or of the articles produced therefrom is prescribed, as, for example, for spiral springs in clocks and measuring systems, for tuning forks, for electromechanical oscillators, and so on. In such cases the temperature coefficients of elasticity are always specified as normal (that is to say of the order of magnitude e l/E dEldT= minus 1 to 3 10' per degree) or low (that is to say between plus 1 10' degrees "'and minus 1 10' degrees These special materials come in the class of the invars, elinvars, etc., and the effect utilized is based on ferromagnetic phenomena which can provide the desired behaviour for dilatation and elasticity within limited temperature ranges.

The converse of these requirements, namely a high dependence of elasticity on temperature, can have important application in technology, and these may be of two kinds. Such a structural material can, for example, serve as a thermometer if the propagation of sound or a vibration frequency is measured in a body made of this material. On the other hand, the requirement of high dependence of the elasticity on temperature may also exist for component parts if, for example, it is desired to obtain less stiffness or to suppress high resonance frequencies with rising temperature for rotating components or components which are liable to resonate (for example for turbines,rockets, instrument suspensions etc.). Still other applications will come for materials with such particular elastic properties, hithertoo not available.

There are some pure metals having low melting points, such as cadmium, tin, and indium, which have highly negative temperature coefficients. But their low hardness and the low melting point make them unsuitable for the purposes mentioned.

There is, however, a group of materials having good mechanical properties, insensitivity to magnetic fields, high melting temperatures, resistance to corrosion, good processability and so on, which also have the desired high dependence of elasticity on temperature oyer a large temperature range. This dependence on temperature takes a negative course, that is to say the moduli of elasticity (modulus of shear G, modulus of elasticity E) decline with rising temperature.

SUMMARY OF THE INVENTION Various contributions make up the cohesion energy of a metal. Elasticity is a cohesive property. There are essentially three contributions to this energy to be considered which are caused by the reciprocal action respectively between the ions of the crystal lattice, between ions and free electrons, and between the free electrons themselves. The first two contributions mentioned give determined uniform features of the elastic behavior of the crystal. The last-mentioned contribution, which can be termed the electron gas contribution, governs on the other hand the temperature behavior of elasticity of certain metals and alloys. The large temperature dependence of the elasticity of the metals of this invention is based on such effects.

The present invention is related to metallic construction elements having highly negative temperature coefficients of the moduli of elasticity, and characterized in that they consist of, or contain as a predominant phase, a metal which has at room temperature a paramagnetic atomic susceptibility X larger than 40 1O" emu/g-atom, and also a positive temperature coefficient of the susceptibility l/X dX/JI. As is seen, the selection of these metals is based on new selection principles which can be explained by electron theory. In fact, the conditions for the susceptibility stress in an unique way the condition, that the electron gas makes a contribution to elasticity.

The contribution of the electron gas to elasticity is given by the kinetic energy of this electron gas. A direct measure of this energy is the specific heat at low temperature (also called electron heat) and, like the susceptibility, it measures the density of states. The susceptibility figure of 40 l0 emu/g-atom corresponds to about a specific heat coefficient of 8 l0 cal/g-atom degree. A high susceptibility, or what is equal, a high density of state and high energy of the electron gas will correlate to the distortion of the crystal lattice, that is to elasticity. It has been found by experiment that the especially interesting temperature behaviour is correlated to the temperature variation of the susceptibility by the unique rule: the temperature coefficient of the susceptibility l/X dX/dT must be positive for a strong negative temperature coefficient of elasticity, e.g., l/E dE/zfl or 1/6 dG/dT; this rule applies if X is sufficiently large.

A second basic element of this invention is preferred orientation. The strong negative temperature coefficient of the metal is a single crystal property and anisotropic. It has been found that the strong temperature dependence of elasticity occurs only for certain directions, that is, it is anisotropic, The engineering metals however are polycrystalline and therefore, provisions must be made to produce a minimum amount of preferred orientation of all crystallites and furthermore the load axis of the construction element must be specified relative to this preferred orientation. These conditions then say that the anisotropic crystallites are all oriented in such a way to give the strong temperature dependence of elasticity.

Another object of the invention is to provide metallic construction elements having strong negative temperature coefficients of elasticity and which are of high mechanical strength.

BRIEF DESCRIPTION OF THE DRAWINGS For an understanding of the principles of the invention, reference is made to the following description of typical embodiments thereof as illustrated in the accompanying drawings.

In the drawings:

FIG. 1a graphically represents the paramagnetic susceptibility X;

FIG. lb graphically represents the temperature coefficient l/x dx/JI of the paramagnetic susceptibility as a function of the electron per atom ration e/a for the transition elements of the 4th, 5th and 6th period of the periodic table and their alloys;

FIG. 1c the preferred electron per atom ratios for the metals for construction element; and

FIG. 2 shows a cubic and hexagonal cell of a crystal lattice with the orientation of the loud axis of the construction element giving the highest negative temperature coefficient of elasticity; and

FIG. 3 is a schematic perspective view ofa measuring device embodying the invention.

The values for the graphical illustration in FIGS. la, lb and 1c have been collated from many literature sources, and own data.

DESCRIPTION OF THE PREFERRED EMBODIMENTS Metals utilizable for the construction elements according to the invention must be paramagnetic and have a high magnetic susceptibility x and a positive temperaturecoefficient l/x dx/dT of this susceptibility.

As can further be seen from FIGS. la and lb, the following electron per atom ratios inscribe utilizable paramagnetic metals: 1.9 to 2.5 and.3.7 to 4.3.

The electron per atom ratio e/a completely circumscribes all alloys having two or more components between te elements of different groups and periods of the periodic system. The electron per atom ratio is the mean number of electrons to be counted beyond closed shells. This is the number of electrons which are decisive for bonding, to the number of atoms. In the case of an alloy composed of n elements having the atomic percentages C, and the number V, of electrons excluding closed shells (valences) the atomic percentages are therefore calculated as the sum of the products atomic concentration times outer electrons (or valency or group number in the periodic table):

1 h =m i i ature ranges. This is quite different from the elastic behavior displayed over a narrow temperature range which is due to an anomaly in the traditional sense. Such anomalies occur, for example, with martensitic transformations, order processes, transformations of ferromagnetism into paramagnetism, etc. For a Ti-Al alloy according to the present invention as an example, the strong negative temperature variation is usable from -200 C up to +600 C or even up to the melting point and the change is practically linear. The strong negative temperature coefficients of elasticity of the new materials being a single crystal property, the anisotropy must be taken into account or even-be used for the technical employment of the materials. The anisotropy is always transmitted to the polycrystal when preferred orientations are present (see for example G. Wassermann and Johanna Grewen: Texturen metallischer Werkstoffe Springer Verlag Berlin Gottingen Heidelberg 1962 or C5. Barret: Structure of Metals, chapter XIX, McGraw Hill 1952). Less investigation has been made into the manner in which the temperature coefiicients of a polycrystalline body depend on preferred orientation. A simple manner of describing such orientation influences consists in determining the direction of load or measurement (in which one of the moduli of elasticity indicated is to act) towards the reference axes of the crystallites, as a mean value.

Referring to Barrett (10c. cit), the elasticity behaviour of the single cristal is determined by the single crystal moduli and an orientation function Q; Q defines the orientation of the load or external stress relative to the axis of the crystal lattices. It is now a standard laboratory technique to determine the mean Q of a poly- A crystalline metal relative to some fixed direction or plane of the metallic body or half product (bar, sheet etc.); in this case this fixed direction is the load axis of the construction element. Some special values of the orientation function Q are:

a. cubic lattice case load axis parallel to l00 of crystal, Q 0

load axis parallel to 1 10 of crystal, Q l/4 load axis parallel to 1 I l of crystal, Q US isotropic orientation of crystallites Q US b. hexagonal lattice case load axis parallel to c-axis Q 1 load axis perpendicular to c-axis Q 0 to i renada! fsxxstallit9s9= 4,

The X-ray examination for preferred orientation will give these mean Q values for polycrystalline metals.

It has been found that, because of the anisotropy of elasticity behavior, it must be:

a. cubic lattice case load is traction or bending Q l/5 load is torsion Q l/5 b. hexagonal lattice case load is traction or bending Q l/4 The important example to discuss in relation to these prescriptions is the tuning fork of FIG. 3 as a temperature sensor. The tuning fork is made of Ti-4 percent Al alloy which has hexagonal structure. The melted alloy is hot-rolled to form of a bar, then hot-rolled to strip, this strip is annealed at 750 C and slightly cold-rolled.

The preferred orientation in this shape is described by

Q

0,2 relative to the length direction. The tuning fork, whose movement of the prongs gives bending stresses, is cut lengthwise (if transverse Q would be about 0,4 and not favorable for the strong temperature dependence of resonance frequency). TI-Iis manufacturing includes therefore the steps: produce preferred orientation by working and choose the good orientation for the construction element. Another way is to fix the orientation of the construction element in a semiproduct and apply transformation steps for this semiproduct that give the preferred orientation.

A procedure for imparting the material with the preferred orientation is described in detail in our application Ser. No.-63 l,686, now US. Pat. No..3,547,7l3.

Preferred orientations for polycrystalline metals are produced by drawing and/or rolling (hot-rolling or cold-rolling) and/or annealing.

Since the present invention requires definite preferred orientation conditions, the manner in which 5 these conditions are satisfied is not of primary importance.

The materials and separable phases of which the articles according to the invention consist, and which have a strongly negative thermoelastic coefficient, depend to accordingly on the conditions x large (namely 40 emu/g-atom at room temperature) and dX/dl positive. Their occurrence is not tied to a fixed structure. For e/a 1.9 to 2.5 (about group 2a of the periodic system) the close packed cubic structures are predomil5 nant, for e/a 3.7 to 4.3 predominantly the hexagonal structure exists.

The moduli of elasticity are rather different for the two ranges of electron per atom ratios and thus permit a selection in this respect also; in fact, different rigidi- 5,000 ppm); operations are nearly the same as for the former alloy.

FIG. 3 of the drawing illustrates an example of construction of an article according to the invention. This is a measuring device 1 in the form of a tuning fork, which may, for example, consist of one of the materials listed in the table and which is here used to measure the temperature of the body 2 or of the ambient. For this purpose the measuring body 1 carries electromechanical transducers 3, which may, for example, be piezocrystals, which maintain an oscillation through a feedback circuit 4, the measurement of frequency being effected in the circuit unit 5. V w

Since the modulus of elasticity of the body has great dependence on temperature, its natural frequency is also correspondingly dependent on temperature, and the natural frequency measured in the circuit unit 5 serves as a measure of the temperature. Since the accuracy of indication is independent of the properties and of any variations of the transmission members, a very convenient temperature measurement device is thus obtained, which works reliably even at high temperatures, and in which the indication can be made at a point at a great distance from the point of measurement because frequency measurement suffers few perturb-a:

C X 1a LE omposl ion e E 10 w x E Ele- Wt. At 10 kg./mm. q-at 10" degree" 10' degree- No. meats percent percent 0) Structure and remarks Sr 95.2 1 a 4'8 2.0 ca. 1,500 ca. 60 Positive ca. 4 Cubic. 2 2. 83 10,000 ca. 140 ca. +2. 7 ca. -5 Up to about 1,100 O. hexagonal: over about Zr 95 l,l0O C. cubic body-centred. 3 5 3.95 11,000 ca. ca. +2.5 6 to -8 Hexagonal up to about 800 C.

4.11 10, 000 ca. ca. +3.0 ca. -6 Hexagonal under 900 0.: bodycentred cubic above 900 0.: precipitation hardening by quenching from about 800 C. and ageing at 5 8:? g: 3. 99 10,000 ca. ca. +3.6 ca. 7 Hexagonal up to about 900 0., cubic above. 6 "{B 2 g 3.93 10,000 ca. 150 ca. +3.5 ca. 6 Hexagonal.

Zr 95 97. 5 7 5 5 a. 97 10,000 ca.140 ca. 7 D0. 8 2} 4. 0 10, 000 ca. 140 ca. +3.0 ca. 6 Do. 9 "2? 2.02 ea. 2,000 ca. 50 ca. +1.0 ca. 4 Cubic.

8 '11 3.98 10,000 ca. 160 ca. +3.6 ca. 7 Hexagonal. 2 Ti 78 87.5 1 22 4. 25 10, 500 ca. +2.0 ca. 3 a: phase.

8 Electron per atom ratio. d Temperature coefficient of susceptibility. b Modulus of elasticity. Temperature coefficent of elastic modulus.

a Paramagnetic atomic susceptibilit For technical alloys which have to comply with the conditions of great strength and hardness and also low mechanical losses, resort is generally had to strengthening procedures, such as cold working, precipitation 55 hardening, multi-phase structure, addition of elements having chemical solution strengthening, and phase transformations, either singly or combined with one another. In the metals for the construction elements action. The variation of frequency of an arrangement of this type amounts to about 0.5 per thousand per degree and is largely constant over a temperature range of several hundred degrees. n H

This tuning fork can be produced by cutting or stamping it out of a metal sheet which has the properties according to the invention, and thus, for example, consists of alloy No. 4 in the table. The preferred oriencordingto the present invention, such strengthening 6O tation has been produced by hot-rolling and still reinprocedures are also possible. Example No. 4 is a precipitation-hardening alloy; the metal is quenched from temperatures in the region 800 to l,l0O C and precipitation-annealed at 400 to 600 C and coldworking can be performed between the two operations. Example No. 5 is a dispersion-hardening alloy (alloying. elements are B,C,O,N, the so-called interstitials up to forced by the heat treatment at 800 l,l0O C and cold-rolling. Cutting of the tuning fork ist now done for the condition I 0.25, e.g., in lengthwise direction for a cold-rolled and flattened bar (for other shapes I can 5 call for other orientations).

Any other article in which a highly negative temperature coefficient for the whole'or part of it is desired'or necessary may obviously also be produced from the structural matterial, such as for example parts of machines running at high speed and tending towards undesirable natural vibrations, and wherein the natural frequency of these parts should decrease with rising temperature. The stiffness of such materials decrease with increasing temperature, however, their strength is not markedly affected up to 600 C or even higher. Such conditions for a structural material can also be desirable in aeronautic construction.

While specific embodiments of the invention have been shown and described in detail to illustrate the application of the principles of the invention, it will be understood that the invention may be embodied otherwise without departing from such principles.

What is claimed is:

l. A temperature sensitive metallic construction element comprising an alloy, said alloy consisting essentially of a major portion of strontium and a minor portion of another element selected from Group Ila of the Periodic Table, and further characterized by having a. a highly negative temperature coefficient of the moduli of elasticity, a paramagnetic atomic susceptibility X Z 40 10 emu/mo] and a positive temperature coefficient l/X dX/dT b. said element having a prereferred orientation which generates anisotropy of the temperature coefficients of the moduli of elasticity by cold-working or annealing, said preferred orientation being defined by the mean value of the product sum of the direction cosine taken overall the crystalline orientations with respect to the stress direction, said value being greater than 0.2 for the elastic modulus and smaller than 0.2 for the shear modulus. I

2. A construction element as claimed in claim 1, in which said alloy further comprises an amount of the elements H, B, C, N or 0, said amount not exceeding 5,000 ppm.

3. A construction element as claimed in claim 1, wherein said alloy is hardenable by subjecting it to precipitation hardening or dispersion hardening heattreatment.

4. A construction element as claimed in claim 1, wherein said alloy consists essentially of -99 atomic percent of titanium, the remainder being aluminum.

5. A temperature sensitive metallic construction element comprising an alloy, said alloy consisting essentially of a first element selected from the Group Nb of the Periodic Table and one or more additional elements selected from the transition metal series, tin and aluminum and further characterized by having a. a highly negative temperature coefficient of the moduli of elasticity, a paramagnetic atomic susceptibility X 2 40 10 emu/mol, a positive temperature coefficient l/X dX/a'l, and

b. an electron concentration of between 3.7 to 4.3,

c. said element having a preferred orientation which generates anisotropy of the temperature co efficients of the moduli of elasticity by coldworking or annealing, said preferred orientation being defined by the mean value of the product sum of the direction cosine taken overall the crystalline orientations with respect to the stress direction, said value being smaller than 0.25 for the elastic modulus and greater than 0.25 for the shear modulus.

6. A construction element as claimed in claim 5, in which said alloy further comprises an amount of the elements H, B, C, N or 0, said amount not exceeding 5,000 ppm.

7. A construction element as claimed in claim 5, wherein said alloy is hardenable by subjecting it to precipitation hardening or dispersion hardening heattreatment.

Claims

2. A construction element as claimed in claim 1, in which said alloy further comprises an amount of the elements H, B, C, N or O, said amount not exceeding 5,000 ppm.
3. A construction element as claimed in claim 1, wherein said alloy is hardenable by subjecting it to precipitation hardening or dispersion hardening heat-treatment.
4. A construction element as claimed in claim 1, wherein said alloy consists essentially of 85-99 atomic percent of titanium, the remainder being aluminum.
5. A temperature sensitive metallic construction element comprising an alloy, said alloy consisting essentially of a first element selected from the Group IVb of the Periodic Table and one or more additional elements selected from the transition metal series, tin and aluminum and further characterized by having a. a highly negative temperature coefficient of the moduli of elasticity, a paramagnetic atomic susceptibility X > or = 40 . 106 emu/mol, a positive temperature coefficient 1/X dX/dT, and b. an electron concentration of between 3.7 to 4.3, c. said element having a preferred orientation which generates anisotropy of the temperature coefficients of the moduli of elasticity by cold-working or annealing, said preferred orientation being defined by the mean value of the product sum of the direction cosine taken overall the crystalline orientations with respect to the stress direction, said value being smaller than 0.25 for the elastic modulus and greater than 0.25 for the shear modulus.
6. A construction element as claimed in claim 5, in which said alloy further comprises an amount of the elements H, B, C, N or O, said amount not exceeding 5,000 ppm.
7. A construction element as claimed in claim 5, wherein said alloy is hardenable by subjecting it to precipitation hardening or dispersion hardening heat-treatment.