US2201425A - Alloy steel - Google Patents
Alloy steel Download PDFInfo
- Publication number
- US2201425A US2201425A US204754A US20475438A US2201425A US 2201425 A US2201425 A US 2201425A US 204754 A US204754 A US 204754A US 20475438 A US20475438 A US 20475438A US 2201425 A US2201425 A US 2201425A
- Authority
- US
- United States
- Prior art keywords
- steel
- chromium
- alloy
- carbide
- carbides
- 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
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- 229910000851 Alloy steel Inorganic materials 0.000 title description 6
- 229910000831 Steel Inorganic materials 0.000 description 18
- 239000011651 chromium Substances 0.000 description 18
- 239000010959 steel Substances 0.000 description 18
- 229910045601 alloy Inorganic materials 0.000 description 16
- 239000000956 alloy Substances 0.000 description 16
- 229910052804 chromium Inorganic materials 0.000 description 15
- 150000001247 metal acetylides Chemical class 0.000 description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 14
- 229910052799 carbon Inorganic materials 0.000 description 14
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 13
- 229910052750 molybdenum Inorganic materials 0.000 description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 10
- 229910052802 copper Inorganic materials 0.000 description 10
- 239000010949 copper Substances 0.000 description 10
- 239000011733 molybdenum Substances 0.000 description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 9
- 229910052742 iron Inorganic materials 0.000 description 9
- 229910017052 cobalt Inorganic materials 0.000 description 8
- 239000010941 cobalt Substances 0.000 description 8
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 7
- 238000005260 corrosion Methods 0.000 description 7
- 229910001220 stainless steel Inorganic materials 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 239000002131 composite material Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 3
- ICPIKPGERJWARK-UHFFFAOYSA-N cobalt copper molybdenum Chemical compound [Co][Cu][Mo] ICPIKPGERJWARK-UHFFFAOYSA-N 0.000 description 3
- 229910052698 phosphorus Inorganic materials 0.000 description 3
- 239000011574 phosphorus Substances 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- ZBHWCYGNOTVMJB-UHFFFAOYSA-N [C].[Cr].[Fe] Chemical compound [C].[Cr].[Fe] ZBHWCYGNOTVMJB-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 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 description 2
- 229910000734 martensite Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-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
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052785 arsenic Inorganic materials 0.000 description 1
- RQNWIZPPADIBDY-UHFFFAOYSA-N arsenic atom Chemical compound [As] RQNWIZPPADIBDY-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 229910052711 selenium Inorganic materials 0.000 description 1
- 239000011669 selenium Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/30—Ferrous alloys, e.g. steel alloys containing chromium with cobalt
Definitions
- bides can exist within the range of concentration Patented May '21, 1940 UNITED STATES PATENT OFFICE ALLOY STEEL Karl Torkel Berglund, Sandviken, Sweden, as-
- loy base the composition of which lies within the following approximate limits:
- the carbon content that is most suitable for difierent fields of use is determined, in the main, by the maximum hardness that it is sought to attain by hardening, and also by the desired qualities of the edge of the tool.
- the maximum hardness that it is possible to obtain by hardening increases with increasing carbon content, but simultaneously, the difficulties connected with shaping and working the steel in hot and cold state also increase.
- a carbon content of at least 0.50%, and preferably not lower than 0.70% is required.
- An increased carbon content gives as a rule a better edge, but having regard to the possibility of working the steel by cold rolling and cold drawing and to the difficulties of rendering the carbides in a sufficiently finely divided state, a higher carbon content than about 1.35% can hardly be considered for this purpose.
- the improved edge obtained through an increased carbon content is explained by the increased quantity of hard and wear-resistant carbides.
- An increased carbide content impairs as a rule the resistancy to corrosionof the steel, due to the chromium content of the carbides being so high that the chromium content of the ground mass is reduced.
- the conclusion may be drawn that for one and. the same carbon content the amount by weight of carbides when in the cubic phase should be 1.5 to 1.8 times the amount obtained if the carbides are in the trigonal phase.
- the cubic carbide may occasion that, for a certain chromium content of the steel, the ground mass becomes poorer in chromium, with the resultant risk of inferior resistancy to corrosion.
- the carbides or at least the greater portion of the same may be obtained in the cubic phase by incorporating with a chromium steel containing 0.20 to 1.35% carbon and 8 to 22% chromium, a further alloy component of molybdenum, cobalt and copper.
- the steel according to the present invention is thus mainly characterized by that, in addition to an alloy base of the composition above set forth, and normal amounts of manganese, silicon, phosphorus, and sulphur present in commercial iron and steel, it also contains the combined alloy component molybdenum-cobalt-copper, the content of these elements being each at least 0.20% and together at least 0.60% and at the most of the weight of the steel thus alloyed.
- Molybdenum may be wholly or partially replaced by tungsten.
- a further addition of moderate quantities of manganese, cobalt or copper does not noticeably change the quantity of the carbides.
- a certain increase of the quantity of carbides is obtained by an addition of tungsten or molybdenum. If, however, in accordance with the present invention, a composite addition of molybdenum, cobalt and copper is made, for instance, about 1% of each substance, the carbide content of the steel is increased to 18 or 19%. This increase of the carbide content is quite surprising in view of the fact that cobalt and copper each by itself does notincrease the carbide content.
- the manganese content it may be mentioned that in a steel according to the present invention the manganese content should be less than 0.65%, since with the composite alloy component here contemplated a greater optimum hardness can be obtained below this limit than at a higher manganese content.
- An alloy steel according to the present invention which is particularly suitable for the manufacture of fine hardened edge tools, such as razor blades and surgical instruments, contains:
- the steel according to the present invention may contain percentages exceeding 0.05% of one or more of the alloy elements: Beryllium, boron, aluminium, titanium, vanadium, arsenic, selenium, zirconium, niobium, tin, antimony, tantalum, uranium.
- molybdenum may be replaced wholly or partially by tungsten, the term molybdenum in the following claims should be construed as covering tungsten also.
- An alloy steel of the martensitic type which is stainless in the hardened condition, characterized by containing when in hardened condition,
- substantially all of the carbides in the cubic phase and possessing great hardness and wearing strength comprising as its principal alloying ingredients carbon in the proportion of 0.20 to 1.35%, chromium in the proportion of to 22%, nickel less than 0.20%, phosphorus less than 0.05%, molybdenum in the proportion of 0.20 to 5%, cobalt in the proportion'of 0.20 to 5%, copper in the proportion of 0.20 to 5%, the remainder being iron with impurities in an amount which will not alter the properties of the alloy.
- An alloy steel of the martensitic type which is stainless in the hardened condition, charac-- terized by containing when in hardened condition substantially all of the carbides in the cubic phase and possessing great hardness and wearing strength, comprising as its principal alloying ingredients carbon in the proportion of 0.70 to 1.35%, chromium in the proportion of 10 to 18%, nickel less than 0.20%, phosphorus less than 0.05%, molybdenum in the proportion of 0.20 to 2%, cobalt in the proportion of 0.20 to 2%, copper in the proportion of 0.20 to 2%, the remainder being iron with impurities in an amount which will not alter the properties of the alloy.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
Description
. bides can exist within the range of concentration Patented May '21, 1940 UNITED STATES PATENT OFFICE ALLOY STEEL Karl Torkel Berglund, Sandviken, Sweden, as-
signor to Sandvikens Jcrnverks Aktiebolag, Sandviken, Sweden, a company of Sweden No Drawing. Application April 28, 1938, Serial No. 204,754. In Sweden May 3, 1937 2 Claims.
loy base the composition of which lies within the following approximate limits:
' Per cent Carbon 0. 20- 2. 50 Chromium 8 -22 Iron, maximum about 90 Having regard to the resistancy to corrosion the lower limit of the chromium content of all of these steels maybe placed at about 2%- With less exacting requirements as to resistancy'to corrosion, somewhat lower chromium contents may also be used. The upper limit of the chromium content is at about 20%, having regard to the hardenability of the steels.
The carbon content that is most suitable for difierent fields of use is determined, in the main, by the maximum hardness that it is sought to attain by hardening, and also by the desired qualities of the edge of the tool. The maximum hardness that it is possible to obtain by hardening, increases with increasing carbon content, but simultaneously, the difficulties connected with shaping and working the steel in hot and cold state also increase.
If the steel is to be used for articles having a thin cutting edge of a suificient durability for practical purposes, a carbon content of at least 0.50%, and preferably not lower than 0.70%, is required. An increased carbon content gives as a rule a better edge, but having regard to the possibility of working the steel by cold rolling and cold drawing and to the difficulties of rendering the carbides in a sufficiently finely divided state, a higher carbon content than about 1.35% can hardly be considered for this purpose. The improved edge obtained through an increased carbon content is explained by the increased quantity of hard and wear-resistant carbides. An increased carbide content, however, impairs as a rule the resistancy to corrosionof the steel, due to the chromium content of the carbides being so high that the chromium content of the ground mass is reduced.
According to existing equilibrium diagrams of the alloy system iron-chromium-carbon, two carhere contemplated, namely, a trigonal carbide (Cr,Fe)1Cs and a cubic carbide (Cr,Fe) 4C or, probably more correctly, (Cr,Fe)2aCs. At temperatures above about 800 C. only the trigonal carbide can exist when equilibrium is attained, whereas at temperatures below about 800 C. also the cubic carbide appears together with the trigonal one.
Generically speaking the conclusion may be drawn that for one and. the same carbon content the amount by weight of carbides when in the cubic phase should be 1.5 to 1.8 times the amount obtained if the carbides are in the trigonal phase.
On the other hand, owing to its greater quantity the cubic carbide may occasion that, for a certain chromium content of the steel, the ground mass becomes poorer in chromium, with the resultant risk of inferior resistancy to corrosion.
According to the present invention the carbides or at least the greater portion of the same may be obtained in the cubic phase by incorporating with a chromium steel containing 0.20 to 1.35% carbon and 8 to 22% chromium, a further alloy component of molybdenum, cobalt and copper. The steel according to the present invention is thus mainly characterized by that, in addition to an alloy base of the composition above set forth, and normal amounts of manganese, silicon, phosphorus, and sulphur present in commercial iron and steel, it also contains the combined alloy component molybdenum-cobalt-copper, the content of these elements being each at least 0.20% and together at least 0.60% and at the most of the weight of the steel thus alloyed. Molybdenum may be wholly or partially replaced by tungsten.
It has been proved by tests that the resistancy to corrosion of an alloy steel according to'this invention is not impaired but, on the contrary, is improved both in the annealed state and, above all, in the hardened state.
This twofold effect of a combined alloy component of molybdenum, cobalt and copper was not to be expected in view of the fact that a moderate addition of one of these elements alone does not result in any noticeable deviation from the equilibrium diagram for iron-chromium-carbon alone.
In addition to the gain of an improved resistancy to corrosion due to the said combined addition of alloy components, the advantage of a larger quantity of carbides for a. given carbon content is also gained, and thus greater hardness and increased wearing strength in the hardened state, and it has also been found that the complex cubic carbide that is formed under these conditions, can more easily be obtained in a finely dispersed state in connection with the shapmosphere of carbon dioxide so as to eliminate the risk of the carbides being oxidized by the oxygen of the air. A great number of tests have ven the result that in the case of a chromium steel containing about 1% carbon and from 13 to 14% chromium but having no other intentional alloy components, the quantity of the carbides amount to from 7 to 8 per cent ofthe weight of the steel.
A further addition of moderate quantities of manganese, cobalt or copper does not noticeably change the quantity of the carbides. On the other hand, a certain increase of the quantity of carbides is obtained by an addition of tungsten or molybdenum. If, however, in accordance with the present invention, a composite addition of molybdenum, cobalt and copper is made, for instance, about 1% of each substance, the carbide content of the steel is increased to 18 or 19%. This increase of the carbide content is quite surprising in view of the fact that cobalt and copper each by itself does notincrease the carbide content.
A roentgenographic examination of carbide residues has given the following results: In a chromium steel of this type without extra alloy com- .ponents the carbides consisted of approximately equal parts trigonal carbide and cubic carbide, and thus conformed with the requirements of the equilibrium diagram. On the other hand, the carbide residue of a chromium steel to which the composite component molybdenum-cobalt-copper had been added, proved to consist practically completely of cubic carbide, in spite of the fact that the said steel had been heated during a long period of time at about 860 C. that is to say, at a temperature range at which, accordinging to available equilibrium diagrams, the trigonal carbide only should be present.
The great resistancy to corrosion shown by a steel of the said type containing molybdenumcobalt-copper will be explained in part, it is believed, by the following analyses shown by the carbide residues:
Percent Percent Percent Fe Cr Cal-hides of a chromium steel with Mo-Co-Gu-addition. 5. 64 40. 7 47. 3 carbides of a chromium steel without extra alloy elements 8. 20 26. 63. 4
Per cent Carbon 1.02 Manganese 0.41 Silicon 0.19 Chromium 12.9 Molybdenum 0.95 Cobalt 1.49 Copper 1.00
The analysis of the carbide residue of this steel corresponds to the formula (Cr, Fe, Mn, Mo, C0)22.44Cs.oo
a value which, having regard to the possible accuracy of analysis, corresponds exceedingly well to the theoretical formula (Cr, Fe) 2308, and whichis also in keeping with the results of the roentgenographie examination.
It may be pointed out that the addition of copper appears to be of essential importance to the marked increase in resistancy to corrosion as well as to the formation of the desired cubic carbide.
As regards the manganese content it may be mentioned that in a steel according to the present invention the manganese content should be less than 0.65%, since with the composite alloy component here contemplated a greater optimum hardness can be obtained below this limit than at a higher manganese content.
An alloy steel according to the present invention which is particularly suitable for the manufacture of fine hardened edge tools, such as razor blades and surgical instruments, contains:
For special fields of use it may be desirable slightly to modify the mechanical and other properties of the alloy steels by an addition of further alloy elements, over and above the composite alloy component molybdenum-cobalt-copper. Thus, the steel according to the present invention may contain percentages exceeding 0.05% of one or more of the alloy elements: Beryllium, boron, aluminium, titanium, vanadium, arsenic, selenium, zirconium, niobium, tin, antimony, tantalum, uranium.
Since, as previously stated, molybdenum may be replaced wholly or partially by tungsten, the term molybdenum in the following claims should be construed as covering tungsten also.
I claim:
1. An alloy steel of the martensitic type, which is stainless in the hardened condition, characterized by containing when in hardened condition,
substantially all of the carbides in the cubic phase and possessing great hardness and wearing strength, comprising as its principal alloying ingredients carbon in the proportion of 0.20 to 1.35%, chromium in the proportion of to 22%, nickel less than 0.20%, phosphorus less than 0.05%, molybdenum in the proportion of 0.20 to 5%, cobalt in the proportion'of 0.20 to 5%, copper in the proportion of 0.20 to 5%, the remainder being iron with impurities in an amount which will not alter the properties of the alloy.
2. An alloy steel of the martensitic type, which is stainless in the hardened condition, charac-- terized by containing when in hardened condition substantially all of the carbides in the cubic phase and possessing great hardness and wearing strength, comprising as its principal alloying ingredients carbon in the proportion of 0.70 to 1.35%, chromium in the proportion of 10 to 18%, nickel less than 0.20%, phosphorus less than 0.05%, molybdenum in the proportion of 0.20 to 2%, cobalt in the proportion of 0.20 to 2%, copper in the proportion of 0.20 to 2%, the remainder being iron with impurities in an amount which will not alter the properties of the alloy.
KARL TORKEL BERGLUND.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE2201425X | 1937-05-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2201425A true US2201425A (en) | 1940-05-21 |
Family
ID=20424951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US204754A Expired - Lifetime US2201425A (en) | 1937-05-03 | 1938-04-28 | Alloy steel |
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US (1) | US2201425A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2932568A (en) * | 1958-05-13 | 1960-04-12 | Carpenter Steel Co | High temperature alloy steel with improved room temperature properties |
US3645724A (en) * | 1969-02-10 | 1972-02-29 | Robert L Goldberg | Stainless steel |
US3794445A (en) * | 1969-10-31 | 1974-02-26 | Hitachi Ltd | Water turbine runner |
US4043842A (en) * | 1972-07-12 | 1977-08-23 | Joiret Victor L J | Grinding members |
US4043844A (en) * | 1970-09-01 | 1977-08-23 | Feltz Michel J | Heat-treated cast grinding members |
EP0295111A2 (en) * | 1987-06-11 | 1988-12-14 | Aichi Steel Works, Ltd. | A steel having good wear resistance |
US4985092A (en) * | 1987-06-11 | 1991-01-15 | Aichi Steel Works, Limited | Steel having good wear resistance |
US20090071313A1 (en) * | 2005-12-07 | 2009-03-19 | Sandvik Intellectual Property Ab | Music string |
US10487429B2 (en) * | 2013-12-19 | 2019-11-26 | Groz-Beckert Kg | Tool for textiles and production method for same |
US20220002896A1 (en) * | 2018-10-26 | 2022-01-06 | Aesculap Ag | Method for the surface treatment of a metal or alloy product, and metal or alloy product |
-
1938
- 1938-04-28 US US204754A patent/US2201425A/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2932568A (en) * | 1958-05-13 | 1960-04-12 | Carpenter Steel Co | High temperature alloy steel with improved room temperature properties |
US3645724A (en) * | 1969-02-10 | 1972-02-29 | Robert L Goldberg | Stainless steel |
US3794445A (en) * | 1969-10-31 | 1974-02-26 | Hitachi Ltd | Water turbine runner |
US4043844A (en) * | 1970-09-01 | 1977-08-23 | Feltz Michel J | Heat-treated cast grinding members |
US4043842A (en) * | 1972-07-12 | 1977-08-23 | Joiret Victor L J | Grinding members |
EP0295111A2 (en) * | 1987-06-11 | 1988-12-14 | Aichi Steel Works, Ltd. | A steel having good wear resistance |
EP0295111A3 (en) * | 1987-06-11 | 1989-11-23 | Aichi Steel Works, Limited | A steel having good wear resistance |
US4985092A (en) * | 1987-06-11 | 1991-01-15 | Aichi Steel Works, Limited | Steel having good wear resistance |
US20090071313A1 (en) * | 2005-12-07 | 2009-03-19 | Sandvik Intellectual Property Ab | Music string |
US7777108B2 (en) * | 2005-12-07 | 2010-08-17 | Sandvik Intellectual Property Ab | Music string |
US10487429B2 (en) * | 2013-12-19 | 2019-11-26 | Groz-Beckert Kg | Tool for textiles and production method for same |
US20220002896A1 (en) * | 2018-10-26 | 2022-01-06 | Aesculap Ag | Method for the surface treatment of a metal or alloy product, and metal or alloy product |
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