US2757221A - Thermocouple element composition - Google Patents
Thermocouple element composition Download PDFInfo
- Publication number
- US2757221A US2757221A US441670A US44167054A US2757221A US 2757221 A US2757221 A US 2757221A US 441670 A US441670 A US 441670A US 44167054 A US44167054 A US 44167054A US 2757221 A US2757221 A US 2757221A
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- Prior art keywords
- alloy
- thermocouple
- approximately
- silicon
- manganese
- 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
- 239000000203 mixture Substances 0.000 title description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 41
- 229910052759 nickel Inorganic materials 0.000 claims description 20
- 229910052710 silicon Inorganic materials 0.000 claims description 19
- 239000010703 silicon Substances 0.000 claims description 17
- 229910052804 chromium Inorganic materials 0.000 claims description 14
- 239000011651 chromium Substances 0.000 claims description 14
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 13
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 13
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 10
- 239000010955 niobium Substances 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- 229910045601 alloy Inorganic materials 0.000 description 36
- 239000000956 alloy Substances 0.000 description 36
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 15
- 239000000470 constituent Substances 0.000 description 5
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 230000001590 oxidative effect Effects 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- 230000006866 deterioration Effects 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910000599 Cr alloy Inorganic materials 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 239000000788 chromium alloy Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 2
- 150000004763 sulfides Chemical class 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000004678 hydrides Chemical class 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- -1 oxides Chemical class 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
- H10N10/80—Constructional details
- H10N10/85—Thermoelectric active materials
- H10N10/851—Thermoelectric active materials comprising inorganic compositions
- H10N10/854—Thermoelectric active materials comprising inorganic compositions comprising only metals
Definitions
- This invention relates to thermocouples and, moreparticularly, to a combination of alloy composit ons for the two components of a thermocouple which reslst the deteriorative effect of various furnace atmospheres at high temperatures.
- the electromotive force developed by any alloy at any United States Patent given temperature is sensitive to changes in the nature and quantities of the metallic constituents presentin the alloy.
- metallic constituents presentin the alloy There are other constituents too, of a non-metallic nature, which are invariably present in all industrial alloys and which, if varied, have a marked eifect in changing the electromotive force of a given alloy combination.
- non-metallic constituents include oxygen, nitrogen and hydrogen which are adsorbed by the metallic constituents of the alloy, and they further include compounds such as oxides, nitrides, hydrides and sulfides Which are soluble to a significant extent in the matrix of which the alloy is composed.
- thermocouple alloys reach the ultimate consumer with properties conforming to the electromotive force which is desired.
- the consumer uses these thermocouples for temperature control under conditions which frequently tend to alter the composition of the thermocouple alloys. For example, the atmospheres in industrial furnaces are in most cases either oxidizing or reducing.
- thermocouple alloy When these atmospheres produce changes in the composition of the thermocouple alloy, as they invariably do at high temperatures, a corresponding change will occur in the thermal electromotive force of the alloy and the couple will depart from its initial calibration. Further changes due to the formation of oxides, carbides, and sulfides can occur. These metallic compounds, initially formed on the surface of the alloys, can dissolve in the alloys and diffuse in from the surface inasmuch as they tend to precipitate on grain boundaries within the alloy during the cooling cycle and serve as regions for further attack by the heated furnace atmospheres during a subsequent heating cycle. Thus, in addition to changes in the electromotive force of the alloys, a general weakening of the structure results and the alloys develop brittle properties which destroy their usefulness.
- thermocouple Since both elements of any thermocouple contribute to the electromotive force of the combination, it is essential that both of them resist, to a high degree, the destructive changes which have been outlined hereinbefore. None is gained when one element of the thermocouple is highly resistant to attack from furnace atmospheres if the other is easily destroyed. The utility of the thermocouple is strictly limited to the service which can be obtained from the weaker member of the alloy combination.
- the nickel-chromium alloy of 8 to 10% chromium was chosen for the positive leg of the thermocouple because it produced a greater electromotive force than would be produced if alloys of higher or lower chromium content were employed.
- electropositive element may consist of 18 to 22% chromium and thebalance substantially all'nickel
- the alloy may contain up to 2% columbium, up to 2% iron, 'up to 2% manganese, from 0.5 to 2% silicon, and from 0.01 to 0.15% carbon. Presence of columbium and, to a lesser extent, silicon in these alloys is particularly desirous in those atmospheres in which chromium alloys are subject to green rot deterioration, such as furnace atmospheres that are alternately oxidizing and reducing in character.
- the electronegative leg may contain from 2% to 4% manganese, approximately 1% to 3% aluminum, and silicon in amounts not more than 2%, less than 1% cobalt, balance essentially nickel.
- thermocouple consisting of a positive leg of 8 to 10% chromium, balance essentially nickel, and a negative leg of substantially 3% manganese, not over 2% silicon, not over 3% of aluminum, balance essentially nickel; 7.92 mv.
- thermocouple having a positive leg of 18 to 22% chromium, balance essentially nickel, and the negative leg described in the preceding statement, hereinafter referred to as thermocouple, No. 1; +0.11 mv.
- thermocouple No. 1; +0.11 mv.
- the positive leg of this thermocouple may and does contain mmor amounts of other metals.
- the alloy actually used in the tests consisted of C .05%, Mn 0.5%, Si 1.2%, C, 19.5%, balance essentially Ni).
- thermocouple No. II A thermocouple consisting of a positive leg of such an alloy and the negative leg heretofore described, and hereinafter referred to as thermocouple No. II, the deviation was +0.11 mv. (Except for the columbium, the positive leg of the thermocouple was essentially that described in the previous statement. It actually consisted of C .06%, Mn 06%, Si .86%, Cr 19.04%, Cb 1.12%, and balance essentially nickel.)
- thermocouples I and II which are characterized by high resistance to deterioration at high temperatures in conventional furnace atmospheres, develop electromotive forces of sufficient amount to make them useful as
- thermocouples I and II when compared to the prior art thermocouple, in reducing and oxidizing furnace atmospheres, makes. such thermocouples desirous and useful in many situations in which thermocouples are used.
- thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium and the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2% to 4% manganese, approximately 1% to 3% aluminum, approximately 1% silicon, and the balance essentially nickel.
- thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium, up to 2% columbium, and. the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2%;to 14% manganese, approximately 1%to 3% aluminum, approximately 1% silicon, and thebalance essentially nickel.
- thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium, up to 2%. columbium, up;uto;2% manganese, 0.5 to 2% silicon, 0.01 to 0.15% carbon, and the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2%-. t0 4% manganese, approximately 1% to 3% aluminum, approximately 1% silicon, and the balance essentially nickel.
- thermocouple .cornprisingqan electropositive element consisting of substantially ;19.'5% chromium, substantially0.05%. carbon,.s.ubstantially 1.2% silicon, substantially e0.5% .manganese, and the balance essentially nickel, and an electronegative element containing approximately.-2% vto..4% manganese, approximately 1% silicon,.approximately 1% to 3%,.alurninum, and the balance essentially nickel.
- Athermocouple comprising an electropositive element consisting ofsubstantially 19.5% chromium, substantially 0.06% carbon, substantially 0.8% silicon,
- substantially 0.06% manganese substantially 1.1% columbium, .and the balance essentially nickel, and an electronegative element containing. approximately 2% to 4% manganese, approximately 1% silicon, approximately 1% to 3% aluminum, and the balance. essentially nickel.
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- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Description
2,757,221 I I THERMO'COUPLE ELEMENT COMPOSITION Charles Leon Guettel, East Orange, N. J., assignon to Driver-Harris Company, Harrison, N. J., a corporation of New Jersey No Drawing. Application July 6,1954,
Serial No. 441,670
5 Claims. (Cl. 136-5) This invention relates to thermocouples and, moreparticularly, to a combination of alloy composit ons for the two components of a thermocouple which reslst the deteriorative effect of various furnace atmospheres at high temperatures. i
The electromotive force developed by any alloy at any United States Patent given temperature is sensitive to changes in the nature and quantities of the metallic constituents presentin the alloy. There are other constituents too, of a non-metallic nature, which are invariably present in all industrial alloys and which, if varied, have a marked eifect in changing the electromotive force of a given alloy combination. These non-metallic constituents include oxygen, nitrogen and hydrogen which are adsorbed by the metallic constituents of the alloy, and they further include compounds such as oxides, nitrides, hydrides and sulfides Which are soluble to a significant extent in the matrix of which the alloy is composed.
It is quite possible, industrially, to manufacture alloys of definite composition which will produce a definite electromotive force within specified limits at a given temperature. Both metallic and non-metallic constituents can be readily controlled, the former by metal additions and the latter by oxidizing or deoxidizing agents used in themelting operation. As a result, the thermocouple alloys reach the ultimate consumer with properties conforming to the electromotive force which is desired. However, the consumer uses these thermocouples for temperature control under conditions which frequently tend to alter the composition of the thermocouple alloys. For example, the atmospheres in industrial furnaces are in most cases either oxidizing or reducing. When these atmospheres produce changes in the composition of the thermocouple alloy, as they invariably do at high temperatures, a corresponding change will occur in the thermal electromotive force of the alloy and the couple will depart from its initial calibration. Further changes due to the formation of oxides, carbides, and sulfides can occur. These metallic compounds, initially formed on the surface of the alloys, can dissolve in the alloys and diffuse in from the surface inasmuch as they tend to precipitate on grain boundaries within the alloy during the cooling cycle and serve as regions for further attack by the heated furnace atmospheres during a subsequent heating cycle. Thus, in addition to changes in the electromotive force of the alloys, a general weakening of the structure results and the alloys develop brittle properties which destroy their usefulness.
Since both elements of any thermocouple contribute to the electromotive force of the combination, it is essential that both of them resist, to a high degree, the destructive changes which have been outlined hereinbefore. Nothing is gained when one element of the thermocouple is highly resistant to attack from furnace atmospheres if the other is easily destroyed. The utility of the thermocouple is strictly limited to the service which can be obtained from the weaker member of the alloy combination.
A thermocouple which has become popular because of its electromotive force characteristics comprises a combination in which the electropositive element is a nickelchromium alloy containing approximately 8 to 10% of chromium with other metallic additions in minor amounts and the electronegative element is a nickel alloy with a manganese content of approximately 3% and aluminum and silicon in amounts usually not exceeding 2% each. The nickel-chromium alloy of 8 to 10% chromium was chosen for the positive leg of the thermocouple because it produced a greater electromotive force than would be produced if alloys of higher or lower chromium content were employed. But, I have found that alloys containing 18 to 22% chromium used with a nickel alloy conciently high electromotive force to form satisfactory therthan the thermocouple in which the positive leg is formed of the 8 to 10% chromium alloys heretofore used.
'While the electropositive element may consist of 18 to 22% chromium and thebalance substantially all'nickel,
except for-incidental impurities normally associated with nickel and residual amounts of deoxidizers added'to the -melt, the alloy may contain up to 2% columbium, up to 2% iron, 'up to 2% manganese, from 0.5 to 2% silicon, and from 0.01 to 0.15% carbon. Presence of columbium and, to a lesser extent, silicon in these alloys is particularly desirous in those atmospheres in which chromium alloys are subject to green rot deterioration, such as furnace atmospheres that are alternately oxidizing and reducing in character. The electronegative leg, as stated, may contain from 2% to 4% manganese, approximately 1% to 3% aluminum, and silicon in amounts not more than 2%, less than 1% cobalt, balance essentially nickel. Its preferred proportions are carbon .02%, manganese 2.90%, silicon 1.10%, aluminum 1.75%, cobalt.50%, as little iron as possible, balance essentially nickel. An actual analysis of a sample of this alloy showed carbon .01%, manganese 2.98%, silicon .99%, aluminum 1.99%, balance essentially nickel.
In testing alloys of the prior art for use in thermocouples in an atmosphere containing appreciable amounts of carbon monoxide, carbon dioxide and hydrogen, and a lesser amount of methane, I have found that the alloy comprising the positive leg shows great deviation in E. M. F. during operation. These tests were carried out in the reducing atmosphere for a period of 171 hours at a temperature of 1750 F. The changes in E. M. F. in several alloys tested were as follows:
The prior art thermocouple consisting of a positive leg of 8 to 10% chromium, balance essentially nickel, and a negative leg of substantially 3% manganese, not over 2% silicon, not over 3% of aluminum, balance essentially nickel; 7.92 mv.
A thermocouple having a positive leg of 18 to 22% chromium, balance essentially nickel, and the negative leg described in the preceding statement, hereinafter referred to as thermocouple, No. 1; +0.11 mv. (As stated above, the positive leg of this thermocouple may and does contain mmor amounts of other metals. Thus, the alloy actually used in the tests consisted of C .05%, Mn 0.5%, Si 1.2%, C, 19.5%, balance essentially Ni).
Where the atmosphere contains gases in which chromlum alloys are susceptible to green rot deterioration, up to 2% of columbium may be added to the alloy of the positive leg. A thermocouple consisting of a positive leg of such an alloy and the negative leg heretofore described, and hereinafter referred to as thermocouple No. II, the deviation was +0.11 mv. (Except for the columbium, the positive leg of the thermocouple was essentially that described in the previous statement. It actually consisted of C .06%, Mn 06%, Si .86%, Cr 19.04%, Cb 1.12%, and balance essentially nickel.)
Thesetwo thermocouples, which are characterized by high resistance to deterioration at high temperatures in conventional furnace atmospheres, develop electromotive forces of sufficient amount to make them useful as The much greater stability of thermocouples I and II, when compared to the prior art thermocouple, in reducing and oxidizing furnace atmospheres, makes. such thermocouples desirous and useful in many situations in which thermocouples are used.
I claim: I
1. A thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium and the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2% to 4% manganese, approximately 1% to 3% aluminum, approximately 1% silicon, and the balance essentially nickel.
2. A thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium, up to 2% columbium, and. the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2%;to 14% manganese, approximately 1%to 3% aluminum, approximately 1% silicon, and thebalance essentially nickel. i
3. A thermocouple comprising an electropositive element composed of an alloy of from 18 to 22% chromium, up to 2%. columbium, up;uto;2% manganese, 0.5 to 2% silicon, 0.01 to 0.15% carbon, and the balance essentially nickel, and an electronegative element composed of an alloy containing approximately 2%-. t0 4% manganese, approximately 1% to 3% aluminum, approximately 1% silicon, and the balance essentially nickel.
'4. A thermocouple .cornprisingqan: electropositive element consisting of substantially ;19.'5% chromium, substantially0.05%. carbon,.s.ubstantially 1.2% silicon, substantially e0.5% .manganese, and the balance essentially nickel, and an electronegative element containing approximately.-2% vto..4% manganese, approximately 1% silicon,.approximately 1% to 3%,.alurninum, and the balance essentially nickel.
5. Athermocouple comprising an electropositive element consisting ofsubstantially 19.5% chromium, substantially 0.06% carbon, substantially 0.8% silicon,
substantially 0.06% manganese, substantially 1.1% columbium, .and the balance essentially nickel, and an electronegative element containing. approximately 2% to 4% manganese, approximately 1% silicon, approximately 1% to 3% aluminum, and the balance. essentially nickel.
2,691,690 Pochetal. Oct. 12, 1954 Seaver Feb. 26, 1952
Claims (1)
- 3. A THERMOCOUPLE COMPRISING AN ELECTROPOSITIVE ELEMENT COMPOSED OF AN ALLOY OF FROM 18 TO 22% CHROMIUM, UP TO 2% COLUMBIUM, UP TO 2% MANGANESE, 0.5 TO 2% SILICON, 0.01 TO 0.15% CARBON, AND THE BALANCE ESSENTIALLY NICKEL, AND AN ELECTRONEGATIVE ELEMENT COMPOSED OF AN ALLOY CONTAINING APPROXIMATELY 2% TO 4% MANGANESE, APPROXIMATELY 1% TO 3% ALUMINUM, APPROXIMATELY 1% SILICON, AND THE BALANCE ESSENTIALLY NICKEL.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US441670A US2757221A (en) | 1954-07-06 | 1954-07-06 | Thermocouple element composition |
| ES0222810A ES222810A1 (en) | 1954-07-06 | 1955-07-05 | Thermocouple element composition |
| DEB36396A DE1133443B (en) | 1954-07-06 | 1955-07-06 | Nickel alloy thermocouple |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US441670A US2757221A (en) | 1954-07-06 | 1954-07-06 | Thermocouple element composition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2757221A true US2757221A (en) | 1956-07-31 |
Family
ID=23753812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US441670A Expired - Lifetime US2757221A (en) | 1954-07-06 | 1954-07-06 | Thermocouple element composition |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US2757221A (en) |
| DE (1) | DE1133443B (en) |
| ES (1) | ES222810A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3328209A (en) * | 1963-01-07 | 1967-06-27 | Engelhard Ind Inc | Noble metal thermocouple having base metal compensating leads |
| US3329533A (en) * | 1964-06-22 | 1967-07-04 | Engelhard Ind Inc | Noble metal thermocouple having base metal compensating leads |
| US3411956A (en) * | 1963-10-15 | 1968-11-19 | Hoskins Mfg Company | Thermocouple with nickel-containing elements |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01501108A (en) * | 1986-09-08 | 1989-04-13 | コモンウェルス・サイエンティフィック・アンド・インダストリアル・リサーチ・オーガナイゼーション | stable metal sheathed thermocouple cable |
| AU622856B2 (en) * | 1987-10-23 | 1992-04-30 | Nicrobell Pty Limited | Thermocouples of enhanced stability |
| DE19526975C2 (en) * | 1995-07-25 | 1998-02-12 | Heraeus Sensor Nite Gmbh | Temperature measuring device |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2587391A (en) * | 1949-06-10 | 1952-02-26 | Gen Electric | Thermocouple |
| US2691690A (en) * | 1952-08-22 | 1954-10-12 | Driver Harris Co | Thermocouple element composition |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1046219A (en) * | 1950-12-08 | 1953-12-04 | Kanthal Ab | Thermoelectric alloy |
-
1954
- 1954-07-06 US US441670A patent/US2757221A/en not_active Expired - Lifetime
-
1955
- 1955-07-05 ES ES0222810A patent/ES222810A1/en not_active Expired
- 1955-07-06 DE DEB36396A patent/DE1133443B/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2587391A (en) * | 1949-06-10 | 1952-02-26 | Gen Electric | Thermocouple |
| US2691690A (en) * | 1952-08-22 | 1954-10-12 | Driver Harris Co | Thermocouple element composition |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3328209A (en) * | 1963-01-07 | 1967-06-27 | Engelhard Ind Inc | Noble metal thermocouple having base metal compensating leads |
| US3411956A (en) * | 1963-10-15 | 1968-11-19 | Hoskins Mfg Company | Thermocouple with nickel-containing elements |
| US3329533A (en) * | 1964-06-22 | 1967-07-04 | Engelhard Ind Inc | Noble metal thermocouple having base metal compensating leads |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1133443B (en) | 1962-07-19 |
| ES222810A1 (en) | 1956-01-01 |
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