US3773570A - Construction element having strongly negative temperature coefficients of elasticity moduli - Google Patents
Construction element having strongly negative temperature coefficients of elasticity moduli Download PDFInfo
- Publication number
- US3773570A US3773570A US00084307A US3773570DA US3773570A US 3773570 A US3773570 A US 3773570A US 00084307 A US00084307 A US 00084307A US 3773570D A US3773570D A US 3773570DA US 3773570 A US3773570 A US 3773570A
- Authority
- US
- United States
- Prior art keywords
- alloy
- temperature
- construction element
- elasticity
- elements
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000010276 construction Methods 0.000 title claims abstract description 37
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 33
- 239000000956 alloy Substances 0.000 claims abstract description 33
- 230000005298 paramagnetic effect Effects 0.000 claims abstract description 11
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 8
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 7
- 238000005482 strain hardening Methods 0.000 claims abstract description 7
- 238000000137 annealing Methods 0.000 claims abstract description 6
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 6
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 4
- 238000004881 precipitation hardening Methods 0.000 claims description 11
- 230000000737 periodic effect Effects 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052796 boron Inorganic materials 0.000 claims description 4
- 229910052739 hydrogen Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 3
- 229910052718 tin Inorganic materials 0.000 claims description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- 229910052723 transition metal Inorganic materials 0.000 claims description 2
- 150000003624 transition metals Chemical class 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 abstract description 27
- 239000002184 metal Substances 0.000 abstract description 27
- 239000000463 material Substances 0.000 abstract description 16
- 238000000034 method Methods 0.000 abstract description 7
- 230000008859 change Effects 0.000 abstract description 3
- 238000001556 precipitation Methods 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
- 229910052712 strontium Inorganic materials 0.000 abstract description 3
- 229910052791 calcium Inorganic materials 0.000 abstract description 2
- 239000006185 dispersion Substances 0.000 abstract description 2
- 229910052726 zirconium Inorganic materials 0.000 abstract description 2
- 150000002739 metals Chemical class 0.000 description 12
- 239000013078 crystal Substances 0.000 description 11
- 238000005259 measurement Methods 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 230000035882 stress Effects 0.000 description 4
- 230000009466 transformation Effects 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 150000002500 ions Chemical class 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 238000000844 transformation Methods 0.000 description 3
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000003574 free electron Substances 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 230000005291 magnetic effect Effects 0.000 description 2
- RNAMYOYQYRYFQY-UHFFFAOYSA-N 2-(4,4-difluoropiperidin-1-yl)-6-methoxy-n-(1-propan-2-ylpiperidin-4-yl)-7-(3-pyrrolidin-1-ylpropoxy)quinazolin-4-amine Chemical compound N1=C(N2CCC(F)(F)CC2)N=C2C=C(OCCCN3CCCC3)C(OC)=CC2=C1NC1CCN(C(C)C)CC1 RNAMYOYQYRYFQY-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 229910004349 Ti-Al Inorganic materials 0.000 description 1
- 229910004692 Ti—Al Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000009529 body temperature measurement Methods 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006355 external stress Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000005294 ferromagnetic effect Effects 0.000 description 1
- 230000005307 ferromagnetism Effects 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000011005 laboratory method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 235000013372 meat Nutrition 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000005408 paramagnetism Effects 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052711 selenium Inorganic materials 0.000 description 1
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K11/00—Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00
- G01K11/22—Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00 using measurement of acoustic effects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K7/00—Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
- G01K7/32—Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements using change of resonant frequency of a crystal
Definitions
- 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.
- e l/E dEldT minus 1 to 3 10' per degree
- low that is to say between plus 1 10' degrees "'and minus 1 10' degrees
- 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.
- 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.
- 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.
- 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.
- 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
- 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
- FIG. 3 is a schematic perspective view of a measuring device embodying the invention.
- 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.
- 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.
- 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):
- 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.
- 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.
- Preferred orientations for polycrystalline metals are produced by drawing and/or rolling (hot-rolling or cold-rolling) and/or annealing.
- thermoelastic coefficient 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.
- 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.
- 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 electromechanical transducers
- 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:
- 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.
- tuning fork is 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.
- 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.
- 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
- 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.
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- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Thermal Sciences (AREA)
- Acoustics & Sound (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Materials For Medical Uses (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH1249466A CH461815A (de) | 1966-08-29 | 1966-08-29 | Gegenstand mit stark negativem Temperaturkoeffizienten der Elastizitätsmoduln |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3773570A true US3773570A (en) | 1973-11-20 |
Family
ID=4383509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00084307A Expired - Lifetime US3773570A (en) | 1966-08-29 | 1970-10-27 | Construction element having strongly negative temperature coefficients of elasticity moduli |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3773570A (de) |
| CH (1) | CH461815A (de) |
| DE (2) | DE1558517C2 (de) |
| GB (1) | GB1200192A (de) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3974001A (en) * | 1966-04-22 | 1976-08-10 | Institut Dr. Ing. Reinhard Straumann, A.G. | Paramagnetic alloy |
| US20050196588A1 (en) * | 2003-12-08 | 2005-09-08 | Olympus Corporation | Electronic device |
| US20060225526A1 (en) * | 2002-07-12 | 2006-10-12 | Gideon Levingston | Mechanical oscillator system |
| US20070140065A1 (en) * | 2003-10-20 | 2007-06-21 | Gideon Levingston | Balance wheel, balance spring and other components and assemblies for a mechanical oscillator system and methods of manufacture |
| US20090116343A1 (en) * | 2005-05-14 | 2009-05-07 | Gideon Levingston | Balance spring, regulated balance wheel assembly and methods of manufacture thereof |
| US20100034057A1 (en) * | 2006-09-08 | 2010-02-11 | Gideon Levingston | Thermally compensating balance wheel |
| CN104180919A (zh) * | 2014-08-12 | 2014-12-03 | 南京理工大学 | 基于微谐振器的高精度温度测量系统 |
| WO2014201239A3 (en) * | 2013-06-14 | 2015-03-05 | The Texas A&M University System | Systems and methods for tailoring coefficients of thermal expansion between extreme positive and extreme negative values |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL288063A (de) * | 1962-02-09 | |||
| FR1355568A (fr) * | 1962-12-17 | 1964-03-20 | Snecma | Procédé de soudo-brasage de deux pièces dont l'une au moins est en graphite |
-
1966
- 1966-08-29 CH CH1249466A patent/CH461815A/de unknown
-
1967
- 1967-05-26 DE DE1558517A patent/DE1558517C2/de not_active Expired
- 1967-05-26 DE DE1558518A patent/DE1558518C2/de not_active Expired
- 1967-08-29 GB GB39415/67A patent/GB1200192A/en not_active Expired
-
1970
- 1970-10-27 US US00084307A patent/US3773570A/en not_active Expired - Lifetime
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3974001A (en) * | 1966-04-22 | 1976-08-10 | Institut Dr. Ing. Reinhard Straumann, A.G. | Paramagnetic alloy |
| US20060225526A1 (en) * | 2002-07-12 | 2006-10-12 | Gideon Levingston | Mechanical oscillator system |
| US7641381B2 (en) * | 2002-07-12 | 2010-01-05 | Gideon Levingston | Mechanical oscillator system |
| US7726872B2 (en) | 2003-10-20 | 2010-06-01 | Gideon Levingston | Balance wheel, balance spring and other components and assemblies for a mechanical oscillator system and methods of manufacture |
| US20070140065A1 (en) * | 2003-10-20 | 2007-06-21 | Gideon Levingston | Balance wheel, balance spring and other components and assemblies for a mechanical oscillator system and methods of manufacture |
| US20050196588A1 (en) * | 2003-12-08 | 2005-09-08 | Olympus Corporation | Electronic device |
| US8333501B2 (en) | 2005-05-14 | 2012-12-18 | Carbontime Limited | Balance spring, regulated balance wheel assembly and methods of manufacture thereof |
| US20090116343A1 (en) * | 2005-05-14 | 2009-05-07 | Gideon Levingston | Balance spring, regulated balance wheel assembly and methods of manufacture thereof |
| US20100034057A1 (en) * | 2006-09-08 | 2010-02-11 | Gideon Levingston | Thermally compensating balance wheel |
| US8100579B2 (en) | 2006-09-08 | 2012-01-24 | Gideon Levingston | Thermally compensating balance wheel |
| WO2014201239A3 (en) * | 2013-06-14 | 2015-03-05 | The Texas A&M University System | Systems and methods for tailoring coefficients of thermal expansion between extreme positive and extreme negative values |
| US10557182B2 (en) | 2013-06-14 | 2020-02-11 | The Texas A&M University System | Systems and methods for tailoring coefficients of thermal expansion between extreme positive and extreme negative values |
| CN104180919A (zh) * | 2014-08-12 | 2014-12-03 | 南京理工大学 | 基于微谐振器的高精度温度测量系统 |
| CN104180919B (zh) * | 2014-08-12 | 2017-05-17 | 南京理工大学 | 基于微谐振器的高精度温度测量系统 |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1200192A (en) | 1970-07-29 |
| DE1558517B1 (de) | 1973-08-16 |
| DE1558517C2 (de) | 1974-03-14 |
| CH461815A (de) | 1968-08-31 |
| DE1558518C2 (de) | 1974-03-21 |
| DE1558518B1 (de) | 1973-08-23 |
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