US3483748A - Temperature sensing - Google Patents
Temperature sensing Download PDFInfo
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- US3483748A US3483748A US636346A US3483748DA US3483748A US 3483748 A US3483748 A US 3483748A US 636346 A US636346 A US 636346A US 3483748D A US3483748D A US 3483748DA US 3483748 A US3483748 A US 3483748A
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- temperature
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K5/00—Measuring temperature based on the expansion or contraction of a material
- G01K5/48—Measuring temperature based on the expansion or contraction of a material the material being a solid
- G01K5/483—Measuring temperature based on the expansion or contraction of a material the material being a solid using materials with a configuration memory, e.g. Ni-Ti alloys
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- 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
- C22F1/006—Resulting in heat recoverable alloys with a memory effect
Definitions
- Nickel-titanium alloy compositions in the range of 47 atomic percent to 53 atomic percent are known for use as temperature sensors in the range of C. to 160 C.
- An article of such an alloy can be made to change from a first configuration to a second configuration when its temperature reaches a transition temperature dependent on the percentages of nickel and titanium.
- An article is disclosed in which the ratio of nickel to titanium varies as a function of depth into the article, which article would then change its configuration gradually over a range of temperatures.
- the device may be made responsive to a definite selected temperature within this range by heating the article to this selected temperature and then cooling it.
- the invention relates broadly to NiTi alloys and more specifically to NiTi alloys in the range of 47 atomic percent to 53 atomic percent nickel. These alloys are treated and discussed in Patent 3,174,851 and the article on page 3232 of volume 36, No. 10 of the Journal of Applied Physics, published in October 1965.
- the invention comprises a temperature sensing composition of NiTi alloy having a non-homogeneous composition.
- the composition of any active increment of said alloy lies within the limitations of 47 atomic percent to 53 atomic percent.
- Atomic percent is the percentage of atoms of a material present per hundred atoms in an alloy.
- Temperature modifying materials in combination with the NiTi alloys are also used in the practice of the invention.
- the invention also covers the construction of a novel NiTi sensing alloy and a technique for constructing the non-homogeneous composition by diffusing temperature modifying materials into the basic NiTi alloy.
- NiTi alloy compositions in the range of 47 atomic percent to 53 atomic percent have a peculiar and rather singular characteristic property.
- the material acts like a memory device and stores the configuration.
- the transition temperature of the material will vary with the NiTi composition (refer to FIGURE 1). In particular, it will be noted that the transition temperature will vary C. for a half atomic percent variation in the range of 50 to 51 atomic percent NiTi.
- a very ditficult problem is to manufacture an alloy having the exact required composition for a specified transition temperature. This is so for a variety of reasons. It is known that by mixing the desired proportions of nickel and titanium in a molten state and solidifying does not result in the predetermined desired composition. Some of the constituent materials are lost in evaporation, some are oxidized. There is also the problem of homogeneity and contamination, either and both can alter the end composition. In practice, a batch intended to provide a spe cific atomic percent composition rarely ends up anywhere within the range of percents of interest and usually outside due to the very precise composition tolerances that are necessary for exact reproduction of a specific transition temperature response alloy.
- NiTi sensor which avoids the limitations and disadvantages of prior sensors of this type.
- FIGURE 1 is a curve of transition temperatures as a function of the atomic percent of NiTi alloy
- FIGURE 2 is a flow diagram of a process for constructing a temperature sensing NiTi composition and sensors embodying the present invention
- FIGURE 3 is a schematic representation of a cross section of a sensor embodying the present invention.
- FIGURE 4 is a curve useful in describing the operation of the FIGURE 3 sensor.
- FIGURES 5a and 5b are curves useful in explaining the operation of the invention.
- a coated nickeltitanium wire generally designated 15.
- the number 11 symbolically designates a coating of preferably nickel, cobalt, titanium or iron.
- the coating is diffused through the nickel titanium element, in this case, the wire 15, to create or to provide a non-homogeneous distribution composition through the cross section of the wire.
- the radial lines 17 symbolically indicate the diffusion of the coating 11 into the wire.
- the thickness across the lines 17 indicate the relative concentration of coating in relation to the surface of the wire.
- FIGURE 4 of the drawings there is a graphical representation of an assumed non-homogeneous distribution corresponding to the FIGURE 3 representation.
- the wire 15 was assumed to have a 50 atomic percent nickel-titanium formulation. After the coating material was diffused into the wire for a predetermined time, further assumptions were made.
- the circle 16 corresponding to the center of the wire is assumed to have a 50.5 to 51 atomic percent nickel while the outside surface of the wire in contact with the coating 11 is assumed to contain 53 atomic percent nickel.
- a straight line distribution through the wire was also assumed. Accordingly, the composition variation with the annulus 12 is shown to lie between the dotted lines defining the sector 12 in FIGURE 4. Likewise, annulae 13, 14 and 16 correspond With sectors 13', 14 and 16'.
- FIGURE 2 shows that the first step is to plate the basic nickel titanium alloy. Diffusing nickel or iron or cobalt into the nickel titanium structure has the effect of moving the transition temperature to the right as seen in FIGURE 1. The effect of adding titanium is the equivalent of removing nickel from a nickel titanium alloy or moving from right to left on the abscissas in FIGURE 1.
- the wire or the nickel titanium substrate After the wire or the nickel titanium substrate is coated it is heated to diffuse the coating into the alloy. The variables of time and temperature are adjusted to the shape of the wire, its size, etc.
- the coating After the coating has been diffused into the body of the substrate to the desired incident, it is raised in temperature above 700 C. and shaped into a first configuration. At and above approximately 700 C. the first configuration is stored in the material in View of its unique capabilities.
- the material is cooled below the transition temperature. In this case, the material would be cooled below -30 C. since this is required by 53 atomic percent nickel occurring at the surface of the Wire. At or below 30 C. the material is shaped into a second configuration and slowly raised in temperature.
- the material starts at a temperature of T or lower. As it is raised in temperature to T the annulus 12 has reached its transition temperature and thus attempts to revert to its first or stored configuration.
- wire 15 passes through T to T where the transition to the stored first configuration is completed.
- the use of a wire having a non-homogeneous cross sectional composition provides a wide band of transition temperatures. It is possible to accurately adjust the wire or sensing material to a particular transition temperature below which there will be no configuration change and above which a configuration change takes place. The accuracy of the adjustment is determined only by the accuracy of the associated temperature sensing instrumentation.
- a temperature sensing composition comprising nickel titanium wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said different nickel titanium ratios.
- a composition as defined in claim 1 which includes in addition a temperature modifying material in proportion to the nickel and titanium for providing temperature effects equivalent to an alloy consisting of nickel and titanium in the percentage of 47 to 53 atomic percent nickel.
- composition as defined in claim 2 where the temperature modifying material is in the class consisting of iron and cobalt.
- a temperature sensing composition comprising a nickel titanium alloy wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said different nickel titanium ratios, the alloy having a stored first configuration and shaped into a second configuration.
- a sensor as described in claim 7 which includes in addition a temperature modifying material in proportion for providing temperature effects equivalent to that of an alloy consisting of nickel titanium in the range specified.
- composition as defined in claim 8 where the temperature modifying material is in the class consisting of iron, cobalt and titanium.
- a temperature sensing composition comprising a nickel titanium alloy wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said difierent nickel titanium ratios, the alloy having a stored first configuration and shaped into a second configuration, a portion having undergone at least a partial change in con figuration from the second configuration toward the stored first configuration.
- a process for making a nickel titanium sensing composition comprising:
- thermoplastic material is taken from the class consisting of nickel, titanium, iron and cobalt.
- a process for making nickel titanium sensing composition which includes in addition the following steps:
Description
Dec. 16, 1969 TRANSITION TEMPERATURE (CI ATOMIC NI FIG.I
PLATE NiTi ALLOY DIFFUSE PLATING INTO ALLOY SHAPE IsT CONFIGURATION SHAPE ZND CONFIGURATION HEAT TO T WHERE T T T2 COOL AND HOLD FIG.2
N. E. ROGEN ETAL TRANSITION TEMPERATURE (C I -20 I I 5 5 I50 I75 N 01 ATOMIC Ni NEIL E. ROGEN RUSSELL J. HILL INVENTORS MH l6 ATTORNEYS United States Patent 3,483,748 TEMPERATURE SENSING Neil E. Rogen, Newton, and Russell J. Hill, Wilmington, Mass, assignors to Avco Corporation, Cincinnati, Ohio, a corporation of Delaware Filed May 5, 1967, Ser. No. 636,346
Int. Cl. G01k /48 US. Cl. 73339 Claims ABSTRACT OF THE DISCLOSURE Nickel-titanium alloy compositions in the range of 47 atomic percent to 53 atomic percent are known for use as temperature sensors in the range of C. to 160 C. An article of such an alloy can be made to change from a first configuration to a second configuration when its temperature reaches a transition temperature dependent on the percentages of nickel and titanium. An article is disclosed in which the ratio of nickel to titanium varies as a function of depth into the article, which article would then change its configuration gradually over a range of temperatures. The device may be made responsive to a definite selected temperature within this range by heating the article to this selected temperature and then cooling it.
Cross references There is a remote relationship between this application and co-pending application Temperature Indicator Device, Ser. No. 564,372, filed July 11, 1966, and co pending application A Temperature Monitor, Ser. No. 615,232, filed Feb. 10, 1967.
Background of the invention The invention relates broadly to NiTi alloys and more specifically to NiTi alloys in the range of 47 atomic percent to 53 atomic percent nickel. These alloys are treated and discussed in Patent 3,174,851 and the article on page 3232 of volume 36, No. 10 of the Journal of Applied Physics, published in October 1965.
The invention comprises a temperature sensing composition of NiTi alloy having a non-homogeneous composition. The composition of any active increment of said alloy lies within the limitations of 47 atomic percent to 53 atomic percent. Atomic percent is the percentage of atoms of a material present per hundred atoms in an alloy.
Temperature modifying materials in combination with the NiTi alloys are also used in the practice of the invention.
The invention also covers the construction of a novel NiTi sensing alloy and a technique for constructing the non-homogeneous composition by diffusing temperature modifying materials into the basic NiTi alloy.
It is known that NiTi alloy compositions in the range of 47 atomic percent to 53 atomic percent have a peculiar and rather singular characteristic property. When such alloys are formed into a first configuration at or above 700 C. the material acts like a memory device and stores the configuration.
If such heat treated NiTi alloy is now cooled below a transition temperature and its configuration changed to a second configuration, the second configuration will be maintained so long as the temperature of the material does not reach the transition temperature. If the transition temperature is reached the material will change its configuration to the first (stored) configuration.
The transition temperature of the material will vary with the NiTi composition (refer to FIGURE 1). In particular, it will be noted that the transition temperature will vary C. for a half atomic percent variation in the range of 50 to 51 atomic percent NiTi. A very ditficult problem is to manufacture an alloy having the exact required composition for a specified transition temperature. This is so for a variety of reasons. It is known that by mixing the desired proportions of nickel and titanium in a molten state and solidifying does not result in the predetermined desired composition. Some of the constituent materials are lost in evaporation, some are oxidized. There is also the problem of homogeneity and contamination, either and both can alter the end composition. In practice, a batch intended to provide a spe cific atomic percent composition rarely ends up anywhere within the range of percents of interest and usually outside due to the very precise composition tolerances that are necessary for exact reproduction of a specific transition temperature response alloy.
It is an object of the invention to provide a process for constructing a temperature sensing NiTi alloy.
It is another object of the invention to provide a process for constructing a NiTi sensing alloy that contains a non-homogeneous distribution of NiTi.
It is still another object of the invention to provide a NiTi sensor which avoids the limitations and disadvantages of prior sensors of this type.
It is yet another object of the invention to provide a NiTi sensor which will respond to a specific transition temperature in a broad range of transition temperatures.
It is yet another object of the invention to provide a process for taking a NiTi sensing alloy and broadening its temperature response.
The novel features that are considered characteristic of the invention are set forth in the appended claims; the invention itself, however, both as to its organization and method of operation, together with additional objects and advantages thereof, will best be understood from the following description of a specific embodiment when read in conjunction with the accompanying drawings, in which:
FIGURE 1 is a curve of transition temperatures as a function of the atomic percent of NiTi alloy;
FIGURE 2 is a flow diagram of a process for constructing a temperature sensing NiTi composition and sensors embodying the present invention;
FIGURE 3 is a schematic representation of a cross section of a sensor embodying the present invention;
FIGURE 4 is a curve useful in describing the operation of the FIGURE 3 sensor; and
FIGURES 5a and 5b are curves useful in explaining the operation of the invention.
Referring to FIGURE 3 of the drawings, there is shown a coated nickeltitanium wire generally designated 15. The number 11 symbolically designates a coating of preferably nickel, cobalt, titanium or iron. In accordance with the invention the coating is diffused through the nickel titanium element, in this case, the wire 15, to create or to provide a non-homogeneous distribution composition through the cross section of the wire. The radial lines 17 symbolically indicate the diffusion of the coating 11 into the wire. The thickness across the lines 17 indicate the relative concentration of coating in relation to the surface of the wire.
Referring to FIGURE 4 of the drawings, there is a graphical representation of an assumed non-homogeneous distribution corresponding to the FIGURE 3 representation.
Initially, the wire 15 was assumed to have a 50 atomic percent nickel-titanium formulation. After the coating material was diffused into the wire for a predetermined time, further assumptions were made. The circle 16 corresponding to the center of the wire is assumed to have a 50.5 to 51 atomic percent nickel while the outside surface of the wire in contact with the coating 11 is assumed to contain 53 atomic percent nickel. A straight line distribution through the wire was also assumed. Accordingly, the composition variation with the annulus 12 is shown to lie between the dotted lines defining the sector 12 in FIGURE 4. Likewise, annulae 13, 14 and 16 correspond With sectors 13', 14 and 16'.
It is clear from FIGURES 1 and 4 that the transition temperature for each of the annulses 13 through 16 will vary in accordance with composition of each sector. For this discussion averages will be used.
It is now proposed to examine the manner by which the usual structure is constructed and used. The flow diagram in FIGURE 2 shows that the first step is to plate the basic nickel titanium alloy. Diffusing nickel or iron or cobalt into the nickel titanium structure has the effect of moving the transition temperature to the right as seen in FIGURE 1. The effect of adding titanium is the equivalent of removing nickel from a nickel titanium alloy or moving from right to left on the abscissas in FIGURE 1.
After the wire or the nickel titanium substrate is coated it is heated to diffuse the coating into the alloy. The variables of time and temperature are adjusted to the shape of the wire, its size, etc.
After the coating has been diffused into the body of the substrate to the desired incident, it is raised in temperature above 700 C. and shaped into a first configuration. At and above approximately 700 C. the first configuration is stored in the material in View of its unique capabilities.
Following the shaping step, at elevated temperatures the material is cooled below the transition temperature. In this case, the material would be cooled below -30 C. since this is required by 53 atomic percent nickel occurring at the surface of the Wire. At or below 30 C. the material is shaped into a second configuration and slowly raised in temperature.
It is at this point that the material takes on a unique characteristic. Referring to FIGURE a a homogeneous material when raised in temperature through its transition temperature T will undergo a very rapid change in configuration from the second configuration to its first (stored) configuration as depicted by curve 19.
On the other hand, assuming a non-homogeneous composition of the type previously described, the material starts at a temperature of T or lower. As it is raised in temperature to T the annulus 12 has reached its transition temperature and thus attempts to revert to its first or stored configuration.
There does not occur an abrupt transition to the stored configuration as in the case of a homogeneous material since only a portion of the cross section is at its transition temperature.
A. configuration change along curve 21 starts to take place. It continues along curve 21 as the temperature of there can be no transitional configuration change until the temperature T is reached since those portions of the wire,
Suppose now it is desired to provide a temperature sensor which will be activated precisely at T or 20 C. This can be accomplished by forming a homogeneous nickel titanium wire containing 52 atomic percent nickel. As was previously mentioned this is very difficult to do and often impractical.
Instead utilizing the non-homogeneous configuration just described and discussed one need only raise the temperature of the wire from T to T and then immediately cool the wire below T The wire is then held at a temperature below T In going from T to T those portions of the Wire, annulus 12 and annulus 13, exceed their transition temperatures and the wire is at an intermediate transition point 24 on curve 21.
When the wire is cooled below T and then reheated annulus 12 and annulus 13, which would ordinarily undergo a configuration change have done so previously. Thus a configuration change begins to take place only after temperature T is reached. The change now proceeds along curve 22 as the temperature of the wire is increased.
In summary, the use of a wire having a non-homogeneous cross sectional composition provides a wide band of transition temperatures. It is possible to accurately adjust the wire or sensing material to a particular transition temperature below which there will be no configuration change and above which a configuration change takes place. The accuracy of the adjustment is determined only by the accuracy of the associated temperature sensing instrumentation.
The various features and advantages of the invention are thought to be clear from the foregoing description. Various other features and advantages not specifically enumerated will undoubtedly occur to those versed in the art, as likewise will many variations and modifications of the preferred embodiment illustrated, all of which may be achieved without departing from the spirit and scope of the invention.
We claim:
1. A temperature sensing composition comprising nickel titanium wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said different nickel titanium ratios.
2. A composition as defined in claim 1 which includes in addition a temperature modifying material in proportion to the nickel and titanium for providing temperature effects equivalent to an alloy consisting of nickel and titanium in the percentage of 47 to 53 atomic percent nickel.
3. A composition as defined in claim 2 where the temperature modifying material is in the class consisting of iron and cobalt.
4. A composition as defined in claim 2 where the atomic percent of one of the materials making up the alloy decreases with the depth from a surface of the alloy.
5. A composition as defined in claim 2 where the atomic percent of the temperature modifying material making up the alloy decreases with the depth from a surface of the alloy.
6. A composition as defined in claim 1 where the atomic percent of one of the materials making up the alloy decreases with the depth from a surface of the alloy.
7. A temperature sensing composition comprising a nickel titanium alloy wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said different nickel titanium ratios, the alloy having a stored first configuration and shaped into a second configuration.
8. A sensor as described in claim 7 which includes in addition a temperature modifying material in proportion for providing temperature effects equivalent to that of an alloy consisting of nickel titanium in the range specified.
9. A composition as defined in claim 8 where the temperature modifying material is in the class consisting of iron, cobalt and titanium.
10. A composition as defined in claim 8 where the atomic percent of one of the materials making up the alloy decreases with the depth from a surface of the alloy.
11. A composition as defined in claim 8 where the atomic percent of the temperature modifying material making up the alloy decreases with the depth from a surface of the alloy.
12. A composition as defined in claim 7 where the atomic percent of one of the materials making up the alloy decreases with the depth from a surface of the alloy.
13. A temperature sensing composition comprising a nickel titanium alloy wherein the ratio of nickel to titanium is deliberately nonuniform throughout the composition, said ratios lying within the range of 47 to 53 atomic percent nickel whereby said composition has a range of transitional temperatures corresponding to said difierent nickel titanium ratios, the alloy having a stored first configuration and shaped into a second configuration, a portion having undergone at least a partial change in con figuration from the second configuration toward the stored first configuration.
14. A composition as defined in claim 13 where the atomic percent of one of the materials making up the alloy decreases with the depth from a surface of the alloy.
15. A composition as defined in claim 13 where the atomic percent of the temperature modifying material making up the alloy decreases with the depth from a surface of the alloy.
16. A process for making a nickel titanium sensing composition comprising:
(a) providing a shaped homogeneous alloy of nickel titanium in the range of 47 to 53 atomic percent nickel;
(h) diffusing into the alloy a temperature modifying material such that the temperature modifying material is not evenly distributed through the shape, the proposition of temperature modifying material providing temperature effects equivalent to that of nickel and titanium in the range of 47 to 53 atomic percent nickel.
17. A process as described in claim 16 where the temperature modifying material is taken from the class consisting of nickel, titanium, iron and cobalt.
18. A process as described in claim 16 where the proportion of temperature modifying material diifused into the shaped alloy decrease with depth from a surface.
19. A process for making nickel titanium sensing composition which includes in addition the following steps:
(a) providing a shaped homogeneous alloy of nickel titanium in the range of 47 to 53 atomic percent nickel;
(b) diffusing into the alloy a temperature modifying material such that the temperature modifying material is not evenly distributed through the shape, the proposition of temperature modifying material providing temperature effects equivalent to that of nickel and titanium in the range of 47 to 53 atomic percent nickel;
(d) reducing the temperature below a transition temerature of interest;
(e) changing the shape to a second configuration; and
(f) storing said shaped alloy below the transition tem perature.
20. A process as described in claim 19 where the temperature of the second configuration is raised to a transition temperature to cause at least a partial change in configuration from the second configuration toward the stored shape.
References Cited UNITED STATES PATENTS 3,174,851 3/1965 Buehler 75170 3,403,238 9/1968 Buehler 73378.3
LOUIS R. PRINCE, Primary Examiner D. E. CORR, Assistant Examiner UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,483,748 December 16, 1969 Neil E. Rogen et a1.
It is certified that error appears in the above identified patent and that said Letters Patent are hereby corrected as shown below:
Column 5, line 27, "proposition" should read proportion Column 6, line 3, after "making" insert a line 11, "proposition" should read proportion Claim 19, after (b) insert (c) annealing said shaped alloy at about 700 C. store said shape;
Signed and sealed this 23rd day of June 1970.
(SEAL) Attest:
WILLIAM E. SCHUYLER, JR.
Edward M. Fletcher, Jr.
Commissioner of Patents Attesting Officer
Applications Claiming Priority (1)
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US63634667A | 1967-05-05 | 1967-05-05 |
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US3483748A true US3483748A (en) | 1969-12-16 |
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US636346A Expired - Lifetime US3483748A (en) | 1967-05-05 | 1967-05-05 | Temperature sensing |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955418A (en) * | 1972-07-31 | 1976-05-11 | Imperial Chemical Industries Limited | Temperature indicators |
US4018547A (en) * | 1975-08-28 | 1977-04-19 | Rogen Neil E | Pumping by wire elongation |
US4018308A (en) * | 1975-10-23 | 1977-04-19 | Rogen Neil E | Elevating by shape memory induction |
US4064827A (en) * | 1976-08-19 | 1977-12-27 | Telatemp Corporation | Temperature indicating device |
US4114559A (en) * | 1974-09-23 | 1978-09-19 | Nicoa Corporation | Temperature monitoring |
EP0122429A1 (en) * | 1983-03-14 | 1984-10-24 | BBC Brown Boveri AG | Composite material shaped as bars, tubes, strips, sheets or plates with reversible thermomechanical properties, and process for their manufacture |
FR2589167A1 (en) * | 1985-10-28 | 1987-04-30 | Boulanger Catherine | Process for obtaining metal objects whose shape changes on heating, and objects obtained by this process |
EP0391018A1 (en) * | 1989-02-01 | 1990-10-10 | Leybold Aktiengesellschaft | Sensor for measuring- and analysing apparatus |
US5076197A (en) * | 1990-12-06 | 1991-12-31 | Telatemp Corporation | Temperature indicator |
US5188457A (en) * | 1992-03-11 | 1993-02-23 | General Electric Company | Measurement of the maximum temperature attained by an article |
US5366292A (en) * | 1989-02-01 | 1994-11-22 | Leybold Ag | Sensor formed from a deformation heat recoverable material having a predetermined range of temperatures in which recovery occurs and used for measuring a physical characteristic of a system |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174851A (en) * | 1961-12-01 | 1965-03-23 | William J Buehler | Nickel-base alloys |
US3403238A (en) * | 1966-04-05 | 1968-09-24 | Navy Usa | Conversion of heat energy to mechanical energy |
-
1967
- 1967-05-05 US US636346A patent/US3483748A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174851A (en) * | 1961-12-01 | 1965-03-23 | William J Buehler | Nickel-base alloys |
US3403238A (en) * | 1966-04-05 | 1968-09-24 | Navy Usa | Conversion of heat energy to mechanical energy |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955418A (en) * | 1972-07-31 | 1976-05-11 | Imperial Chemical Industries Limited | Temperature indicators |
US4114559A (en) * | 1974-09-23 | 1978-09-19 | Nicoa Corporation | Temperature monitoring |
US4018547A (en) * | 1975-08-28 | 1977-04-19 | Rogen Neil E | Pumping by wire elongation |
US4018308A (en) * | 1975-10-23 | 1977-04-19 | Rogen Neil E | Elevating by shape memory induction |
US4064827A (en) * | 1976-08-19 | 1977-12-27 | Telatemp Corporation | Temperature indicating device |
EP0122429A1 (en) * | 1983-03-14 | 1984-10-24 | BBC Brown Boveri AG | Composite material shaped as bars, tubes, strips, sheets or plates with reversible thermomechanical properties, and process for their manufacture |
FR2589167A1 (en) * | 1985-10-28 | 1987-04-30 | Boulanger Catherine | Process for obtaining metal objects whose shape changes on heating, and objects obtained by this process |
EP0391018A1 (en) * | 1989-02-01 | 1990-10-10 | Leybold Aktiengesellschaft | Sensor for measuring- and analysing apparatus |
US5366292A (en) * | 1989-02-01 | 1994-11-22 | Leybold Ag | Sensor formed from a deformation heat recoverable material having a predetermined range of temperatures in which recovery occurs and used for measuring a physical characteristic of a system |
US5076197A (en) * | 1990-12-06 | 1991-12-31 | Telatemp Corporation | Temperature indicator |
US5188457A (en) * | 1992-03-11 | 1993-02-23 | General Electric Company | Measurement of the maximum temperature attained by an article |
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