US1988568A - Temperature compensator - Google Patents
Temperature compensator Download PDFInfo
- Publication number
- US1988568A US1988568A US611235A US61123532A US1988568A US 1988568 A US1988568 A US 1988568A US 611235 A US611235 A US 611235A US 61123532 A US61123532 A US 61123532A US 1988568 A US1988568 A US 1988568A
- Authority
- US
- United States
- Prior art keywords
- alloy
- temperature
- permeability
- magnetic
- maximum
- 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
- 229910045601 alloy Inorganic materials 0.000 description 22
- 239000000956 alloy Substances 0.000 description 22
- 230000035699 permeability Effects 0.000 description 18
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- 239000000203 mixture Substances 0.000 description 7
- 239000011572 manganese Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 238000000137 annealing Methods 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 230000004907 flux Effects 0.000 description 3
- 238000005098 hot rolling Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000010791 quenching Methods 0.000 description 3
- 230000000171 quenching effect Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000010583 slow cooling Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- YOCUPQPZWBBYIX-UHFFFAOYSA-N copper nickel Chemical compound [Ni].[Cu] YOCUPQPZWBBYIX-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R11/00—Electromechanical arrangements for measuring time integral of electric power or current, e.g. of consumption
- G01R11/02—Constructional details
- G01R11/17—Compensating for errors; Adjusting or regulating means therefor
- G01R11/18—Compensating for variations in ambient conditions
- G01R11/185—Temperature compensation
Definitions
- the alloy we propose to use has the following composition:
- the percentage of carbon does not afiect permeability nor the slope of the temperature permeability curve if kept below 25%. Carbon above .25% causes the permeability curve to become less regular.
- the presence of manganese appears to have the efiect of decreasing both the permeability and theslope of the temperature permeability curve. The curve also becomes more irregular with increasing percentages of manganese. .50% is the maximum allowable manganese content.
- Silicon, sulphur, of phosphorus in'the usual small amounts appear to have little or no effect upon the permeability of the alloy. They are added as necessary deoxidizers in the preparation of the alloy, following customary furnace procedure.
- the compensating articles are then formed by hot rolling and cold stamping as may be necessary. Since the processes of rolling and stamping affect the magnetic characteristics as explained above, the compensators are then heat treated.
- the invention therefore involves a new composition which is of particular use in correcting" inaccuracies in magnetic measuring instruments due to temperature changes. It also involves a heat treatment subsequent to such forming operations as hot rolling and cold stamping in order to produce uniform magnetic properties in the magnetic permeability and the relation of the variation of this permeability to temperature.
- a temperature-responsive compensator for magnetic measuring instruments formed from an alloy having the followingcomposition:
- a temperature-responsive compensator for magnetic measuring instruments formed from an alloy containing between 29.75% and 30.5% nickel, carbon not in excess of 25%, manganese not in excess of 50% and the balance substantially all iron.
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Soft Magnetic Materials (AREA)
Description
Patented Jan. 22, 1935 UNITED STATES TEMPERATURE COMPENSATOR Donald w. Randolph and Ralph E. Mitchel, Flint,
Mich., assignors,by mesne assignments, to General Motors Corporation, Detroit, Mich., a corporation of Delaware No Drawing. Application May 13, 1932,
Serial No. 611.235
2 Claims.
ployed permanent magnets, the magnetic linesv of force of which are partly effective to influence the rotation of speed-indicating members, and partly passed through a shunt, the latter portion of the flux beingineflective upon the rotation of the speed-indicating member. The active lines of force have a lesser influence at higher tem- Q peratures because of the increasing electrical resistance of the speed-indicating member. It
has therefore been proposed to increase the pro.-
portion of the magnetic flux which influences the speed-indicating member at high temperatures by introducing into the shunt an alloy which is less permeable at higher temperatures. Such devices are shown in patents to Wedin 1,848,068 and Davey 1,848,057. In this way the magnet is more eifective upon the speed-indieating member with increasing temperature, as a larger proportion of its flux becomes available for the active field. An alloy of nickel and copper has been used for this purpose.
Such an alloy of nickeland copper has been frequently found somewhat unsatisfactory because of a lack of uniformity in its corrective influence throughout the range of temperature to which the instrument is subjected. It has been proposed also to use in addition to the nickel-copper alloy some other alloy, the two alloys, acting together, being intended to have a resultant compensation effect which shall render the readings accurate at all temperatures.
We have found if an alloy having the specified composition set forth below is employed and if the temperature-compensating devices are prepared as set forth herein, the desired correction to secure accurate readings may be had Without resort to an additional alloy.
The alloy we propose to use has the following composition:
Ni 29.75 to 30.5%
C .25 maximum Mn .50 maximum S 025% maximum P .025% maximum Si .25 maximum Fe balance In this alloy the nickel content is very important. Increasing the proportion of nickel increases the permeability and the slope of the temperature permeability curve. Small variations in the nickel content make great diflerences in the temperature-responsive characteristics. It is important that the percentages be kept within the specified limits. If the percentage rises above 30.5% the alloy has too high a permeability and too steep a slope for practical purposes. To insure the necessary permeability the nickel content should-notbe below 29.75%. Below 9. percentage somewhat less than 29.75% the alloy becomes very ineflicient, and with percentages not much below the minimum limit specified the alloy has magnetic transformation points within the'operating range (ll- F.)
The percentage of carbon does not afiect permeability nor the slope of the temperature permeability curve if kept below 25%. Carbon above .25% causes the permeability curve to become less regular.
The presence of manganese appears to have the efiect of decreasing both the permeability and theslope of the temperature permeability curve. The curve also becomes more irregular with increasing percentages of manganese. .50% is the maximum allowable manganese content.
Silicon, sulphur, of phosphorus in'the usual small amounts appear to have little or no effect upon the permeability of the alloy. They are added as necessary deoxidizers in the preparation of the alloy, following customary furnace procedure.
It is very difiicult to make successive lots of metal having exactly the same composition, and the subsequent processes of rolling hot metal into strip form cannot be very accurately controlled. The resultant magnetic properties of the metal are greatly affected by slight variations in composition and by the rolling treatment. Even if the composition is held within much closer limits than is commercially practicable, the magnetic variation in the resultant material is so great that it would be necessary to change the size of the piece of metal used for the magnetic compensator with every new lot of metal that was used. Since the magnetic proportions are greatly affected by the rolling treatment which the metal receives and also by cold stamping and bending operations, it would not be practical to use material of this type for temperature compensation where thousands of instruments have to be built to the same standards of performance. In order to eliminate the variations due to chemical composition, hot rolling, and cold working, it has been discovered that a heat treatment may be employed which can be so adjusted as to eliminate these variables, and it becomes possible to pro duce temperature compensators of such uniform magnetic properties that they may be applied Without correction as to size or location in the magnetic field. to any number of similar instruments with uniform results.
To that end, after holding the analysis within the above limits and obtaining an alloy with a permeability of between 30 and at F. having a permeability-temperature curve with a slope varying between 59% and .72%, the compensating articles are then formed by hot rolling and cold stamping as may be necessary. Since the processes of rolling and stamping affect the magnetic characteristics as explained above, the compensators are then heat treated.
In this subsequent heat treating the following facts are made use of 1. Quenching the alloy in water from annealing temperatures between 850 F. and 1500 F. has a marked effect on the permeability. The permeability is decreased as the annealing temperature is increased. Above the temperature of 1500 F. there is no further efiect on the permeability of the alloy.
2. Up to 1400 F. quenching from annealing temperatures has little or no effect upon the permeability-temperature curve of the alloy. Over 1400 F. causes the temperature permeability curve to become less regular and to lose its linear characteristics.
3. Slow cooling of the alloy from the annealing temperature must be avoided. With slow cooling as in air, the permeability prior to heat treatment is restored. The alloy must be quickly cooled as by quenching in water for example.
4. .The time of annealing is not an important factor in the heat treatment of this alloy.
The invention therefore involves a new composition which is of particular use in correcting" inaccuracies in magnetic measuring instruments due to temperature changes. It also involves a heat treatment subsequent to such forming operations as hot rolling and cold stamping in order to produce uniform magnetic properties in the magnetic permeability and the relation of the variation of this permeability to temperature.
We claim:
1. A temperature-responsive compensator for magnetic measuring instruments formed from an alloy having the followingcomposition:
Ni 29.75 to 30.5%
C .25 maximum Mn .50 maximum S .025% maximum P .025 maximum Si .25 maximum Fe balance 2. A temperature-responsive compensator for magnetic measuring instruments formed from an alloy containing between 29.75% and 30.5% nickel, carbon not in excess of 25%, manganese not in excess of 50% and the balance substantially all iron.
DONALD W. RANDOLPH. RALPH H. MITCHEL
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US611235A US1988568A (en) | 1932-05-13 | 1932-05-13 | Temperature compensator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US611235A US1988568A (en) | 1932-05-13 | 1932-05-13 | Temperature compensator |
Publications (1)
Publication Number | Publication Date |
---|---|
US1988568A true US1988568A (en) | 1935-01-22 |
Family
ID=24448188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US611235A Expired - Lifetime US1988568A (en) | 1932-05-13 | 1932-05-13 | Temperature compensator |
Country Status (1)
Country | Link |
---|---|
US (1) | US1988568A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2648019A (en) * | 1949-11-15 | 1953-08-04 | Jaeger Ets Ed | Magnetically acting speedometer |
US2649559A (en) * | 1949-12-01 | 1953-08-18 | Stewart Warner Corp | Electric tachmometer |
US2720603A (en) * | 1951-12-28 | 1955-10-11 | Gen Motors Corp | Speedometer temperature compensation |
US2720604A (en) * | 1951-12-28 | 1955-10-11 | Gen Motors Corp | Low-temperature compensating alloy for magnetic instruments |
US2725493A (en) * | 1951-07-14 | 1955-11-29 | Gen Motors Corp | Temperature compensation for a magnetic speedometer drive |
US2930725A (en) * | 1957-03-13 | 1960-03-29 | Int Nickel Co | Nickel-iron alloys |
-
1932
- 1932-05-13 US US611235A patent/US1988568A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2648019A (en) * | 1949-11-15 | 1953-08-04 | Jaeger Ets Ed | Magnetically acting speedometer |
US2649559A (en) * | 1949-12-01 | 1953-08-18 | Stewart Warner Corp | Electric tachmometer |
US2725493A (en) * | 1951-07-14 | 1955-11-29 | Gen Motors Corp | Temperature compensation for a magnetic speedometer drive |
US2720603A (en) * | 1951-12-28 | 1955-10-11 | Gen Motors Corp | Speedometer temperature compensation |
US2720604A (en) * | 1951-12-28 | 1955-10-11 | Gen Motors Corp | Low-temperature compensating alloy for magnetic instruments |
US2930725A (en) * | 1957-03-13 | 1960-03-29 | Int Nickel Co | Nickel-iron alloys |
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