US2105114A - Alloy steel tool - Google Patents
Alloy steel tool Download PDFInfo
- Publication number
- US2105114A US2105114A US174487A US17448737A US2105114A US 2105114 A US2105114 A US 2105114A US 174487 A US174487 A US 174487A US 17448737 A US17448737 A US 17448737A US 2105114 A US2105114 A US 2105114A
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- US
- United States
- Prior art keywords
- steel
- temperature
- vanadium
- tools
- carbon
- 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 2
- 229910000831 Steel Inorganic materials 0.000 description 26
- 239000010959 steel Substances 0.000 description 26
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 18
- 229910052799 carbon Inorganic materials 0.000 description 18
- 229910052720 vanadium Inorganic materials 0.000 description 17
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 17
- 229910000997 High-speed steel Inorganic materials 0.000 description 9
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 9
- 238000005520 cutting process Methods 0.000 description 9
- 229910052750 molybdenum Inorganic materials 0.000 description 9
- 239000011733 molybdenum Substances 0.000 description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 239000000463 material Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 238000005496 tempering Methods 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 229910021538 borax Inorganic materials 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 238000005242 forging Methods 0.000 description 4
- 239000004328 sodium tetraborate Substances 0.000 description 4
- 235000010339 sodium tetraborate Nutrition 0.000 description 4
- 238000000137 annealing Methods 0.000 description 3
- 238000004320 controlled atmosphere Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 2
- XFXPMWWXUTWYJX-UHFFFAOYSA-N Cyanide Chemical compound N#[C-] XFXPMWWXUTWYJX-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- 235000011941 Tilia x europaea Nutrition 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 229910001566 austenite Inorganic materials 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 239000004571 lime Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 235000002918 Fraxinus excelsior Nutrition 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 239000002956 ash Substances 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- KXZJHVJKXJLBKO-UHFFFAOYSA-N chembl1408157 Chemical compound N=1C2=CC=CC=C2C(C(=O)O)=CC=1C1=CC=C(O)C=C1 KXZJHVJKXJLBKO-UHFFFAOYSA-N 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000005261 decarburization Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 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 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- -1 num Substances 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- NNFCIKHAZHQZJG-UHFFFAOYSA-N potassium cyanide Chemical compound [K+].N#[C-] NNFCIKHAZHQZJG-UHFFFAOYSA-N 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000010583 slow cooling Methods 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
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
Definitions
- Patented is... ll, 103s g 2.10am
- This invention relates to alloy steels, and more particularly to the typeknown as high speed steels, which may be employed in the making of cutting tools, dies and other tools.
- tools may be formed from steels containing from 370% to 1.50% carbon, from 2.00% to 4.50% of vanadium, from 7.00% to 11.00% of molybdenum, and from 3.00% to 6.00% of chromium, with the vanadium content approximately three times that of thecarbon content, but always within the' limits of in excess of two and one-half to one and less within the range of my invention which prove very satisfactory:
- compositions of my improved steel will preferably fall within the narrower limits which may be defined as follows:
- the material can be freely annealed and has excellent cutting properties.
- the improved steel should be heated slowly and uniformly to a forging temperature of from 1900 to 1950 degreesFahrenheit. It willforge somewhat easier if heated to a temperature of from 1300 to 1400 degrees Fahrenheit and. held at this temperature for several hours before heating to the higher temperature. After forging, it is necessary to cool slowly as the steel is self-hardening like all high speed steels. Slow cooling may be either in a furnace or by burying in'a heat insulating material such as ashes, lime, mica, infusorial earth, etc.
- Annealing To properly anneal, it is best to pack in a container using sand or lime to which a very small amount of charcoal may be added.
- the container in which the material is to be annealed should be of such a size that only a small amount of packing is necessary, otherwise it may insulate the heat from the steel and cause an unnecessary time for heating to the annealing temperature;
- An annealing temperature of approximately 1550 degrees Fahrenheit is best and the steel should be cooled preferably with the furnace and at a temperature not over about 40 or 50 degrees an hour until a temperature of about 1200 Fahrenheit has been reached when'it may be cooled more rapidly.
- HardeningP The entire process of hardening will depend greatly upon the heat treating equipment available. Controlled atmosphere furnaces or salt baths are preferable for hardening but when these are not available a semi-muflle furnace will serve satisfactorily, in which case it is necessary to cover the material with borax to prevent partial decarburization of the surface. If a semi-muffle furnace is used, the pre-heat should be from about 1300 to 1400 degrees Fahrenheit.
- borax As soon as the steel has reached the temperature of the preheat it should be covered with borax.
- semi-muttle furnaces either for the pre-heat or high heat, it is advisable to use a plate in the bottom of the furnace to prevent the borax attacking the furnace bottom.
- a temperature of approximately 2225 degrees Fahrenheit is satisfactory for most types of tools.
- Single point cutting tools may be heated somewhat higher and fine edge tools, such as taps, should be heated to a temperature about 25 degrees lower.
- Tempering The resistance of a high speed steel to loss of hardness resulting from the tempering temperature will depend somewhat upon the amount of alloys that have been dissolved and the amount of austenite present after hardening. This is indicated by the grain size. If the steel is highly overheated then it will resist tempering to a more noticeable degree than if properly heated or underheated. Any table which gives the hardness resulting from the tempering temperature should be based on about the average grain size to be expected from hardening for the general run of tools such as drills, reamers, milling cutters, etc.
- the tools should be heated slowly to the tempering temperature and should be held at this temperature for about one and one-half hours, after which they may be cooled in air.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
Patented is... ll, 103s g 2.10am
at? s'rnm. or.
James P. Gill, Latrobe, Pa, assior to w dium-Alloys Steel Company, Latrobe, Wa a corporation of Pennsylva No Drawing. Application November 13, 1937,. Serial No. 174,407
1 Claim.
This invention relates to alloy steels, and more particularly to the typeknown as high speed steels, which may be employed in the making of cutting tools, dies and other tools. I
There are a number' of high speed steels in commercial use today which usually contain as alloying elements, tungsten, chromium and vanadium; or molybdenum, chromium and vanadium; or tungsten, molybdenum, chromium and vanadium. It is unusual for such steels to contain a carbon content in excess of 370%, since it is generally considered that a higher carbon content makes forging difiicult and increases brittleness to such a degree as toymake the steel generally unsatisfactory.
.In investigating different co loying ingredients, particularly num, chromium and vanadium, Ihave discovered a new balanced composition and a new relationship between the carbon and vanadium contents which can be effectively used to increase materially the cutting efficiency of the steel without material decrease in toughness and yet still have a steel which is readily forgeable and can be readily annealed.
I find for example, that when a high speed steel of the so-called molybdenum type contains approximately 9.00% molybdenum and 4.00% chromium, the vanadium content should be approximately three times that of the carbon contentwhen the latter is in excess of..70%, for best cutting efficiency. Increasing the carbon and vanadium contents in this ratio results in a steel of the molybdenum type which has materially better cutting efiiciency, forgeability and annealibility than previously known steels of this type. Maintaining this relationship in the carbon and vanadium content does not increase the brittleness of the steel to the same extent as where the carbon content increases at a lesser ratio.
Increasing the carbon content in this ratio also results in. a steel which can be readilyforged even when the carbon content is substantially in excess of 370%. P
In the practice of my invention, tools may be formed from steels containing from 370% to 1.50% carbon, from 2.00% to 4.50% of vanadium, from 7.00% to 11.00% of molybdenum, and from 3.00% to 6.00% of chromium, with the vanadium content approximately three times that of thecarbon content, but always within the' limits of in excess of two and one-half to one and less within the range of my invention which prove very satisfactory:
In addition .to the above elements, small amounts of manganese, silicon, sulphur and phosphorus are assumed to be present, with the remainder of the alloy substantially all iron.
Notwithstanding the broader ranges set forth above, the compositions of my improved steel will preferably fall within the narrower limits which may be defined as follows:
Limits Carbon .75- 1.20 Silicon .20- .35 Manganese .10- .30 Sulphur Less than .03 Phosphorus Less than .03 Chromium 3.75- 4.75 Molybdenum 53.25-10.00 Vanadium 2.00- 4.25
Additionally, notwithstanding the narrower limitsset forth above. there will be a desired range within the narrower range which may be defined as follows:
Steels made of the above approximate compositions will be found to have a substantial in crease in wearing ability with increase in the carbon content. As the carbon content increases, while maintaining the proper ratio with the content. of vanadium, it will be found that toughness decreases slowly. While forgeability will decrease slightly with the increase in carbon and vanadium content it does so slowly and the steel will remain forgeable with the carbon content substantially in excessof 310% and with the vanadium content in proper proportion thereto.
Additionally, in 'a composition of that kind the material can be freely annealed and has excellent cutting properties.
.amount to approximately 2%.
In high speed steels of compositions similar to those set forth in the tables given above, and having a ratio of carbon and vanadium as stated, the addition of cobalt from small amounts up to. and including as much as 12% may materially increase the cutting ability of the steel. Also, if nickel is introduced into steels of this type the strength is increased without material decrease in the cutting ability. The nickel content which may be used ranges from an effective Additionally, other well-known alloying ingredients may be added to an extent less than one and one-half percent of the composition in the aggregate.
' Since this improved steel reacts to heat treatment more uniformly than other molybdenum high speed steels, and the same hardness results can be consistently obtained using the same quenching and tempering temperatures, it will be desirable to set forth various methods of heat treating this material.
Forging.-The improved steel should be heated slowly and uniformly to a forging temperature of from 1900 to 1950 degreesFahrenheit. It willforge somewhat easier if heated to a temperature of from 1300 to 1400 degrees Fahrenheit and. held at this temperature for several hours before heating to the higher temperature. After forging, it is necessary to cool slowly as the steel is self-hardening like all high speed steels. Slow cooling may be either in a furnace or by burying in'a heat insulating material such as ashes, lime, mica, infusorial earth, etc.
Annealing To properly anneal, it is best to pack in a container using sand or lime to which a very small amount of charcoal may be added. The container in which the material is to be annealed should be of such a size that only a small amount of packing is necessary, otherwise it may insulate the heat from the steel and cause an unnecessary time for heating to the annealing temperature; An annealing temperature of approximately 1550 degrees Fahrenheit is best and the steel should be cooled preferably with the furnace and at a temperature not over about 40 or 50 degrees an hour until a temperature of about 1200 Fahrenheit has been reached when'it may be cooled more rapidly.
HardeningP-The entire process of hardening will depend greatly upon the heat treating equipment available. Controlled atmosphere furnaces or salt baths are preferable for hardening but when these are not available a semi-muflle furnace will serve satisfactorily, in which case it is necessary to cover the material with borax to prevent partial decarburization of the surface. If a semi-muffle furnace is used, the pre-heat should be from about 1300 to 1400 degrees Fahrenheit.
As soon as the steel has reached the temperature of the preheat it should be covered with borax. When semi-muiile furnaces are used, either for the pre-heat or high heat, it is advisable to use a plate in the bottom of the furnace to prevent the borax attacking the furnace bottom. For maximum hardness a temperature of approximately 2225 degrees Fahrenheit is satisfactory for most types of tools. Single point cutting tools may be heated somewhat higher and fine edge tools, such as taps, should be heated to a temperature about 25 degrees lower. As soon as the steel has reached the temperature of the furnace it should be oil quenched, The same hardening temperatures apply for controlled atmosphere furnaces or for salt baths but when these furnaces are available it is desirable to use a pre-heatin-g temperature in the vicinity of about 1500 degrees Fahrenheit. It is unnecessary to .use a borax covering in controlled atmosphere furnaces. It is difilcult to state the lengt-hof time necessary for holding at the highheat as this depends considerably upon the size of the tools being treated and'upon the type of equipment in use. In general, the same comparable time. should be used as with othertypes of high speed steels.
Tempering.-The resistance of a high speed steel to loss of hardness resulting from the tempering temperature will depend somewhat upon the amount of alloys that have been dissolved and the amount of austenite present after hardening. This is indicated by the grain size. If the steel is highly overheated then it will resist tempering to a more noticeable degree than if properly heated or underheated. Any table which gives the hardness resulting from the tempering temperature should be based on about the average grain size to be expected from hardening for the general run of tools such as drills, reamers, milling cutters, etc. It should not be based on the structure that is oftentimes found in single point cutting tools which may be overheated to produce a comparatively coarse grain and, therefore, have considerable austenite resulting from the higher hardening temperature. The following table of drawing temperatures shows the hardness that can he expected in my improved steel after quenching from a temperature of 2225 degrees Fahrenheit. Tools hardened at this temperature will have a comparatively small grain.
Tampering temperature ggg A qiinnnhpd 66 800 F- 62. 5 900 F 63. 5 950 F. 64. 5 1000 F- 65 1025 F. 66 1050 F. 64. 5 1075 F 63 1100 F 62 1125 61 1150 F 59 1200 F 54- 5 About the same hardness results will be obtained with tools quenched from 2200 degrees Fahrenheit and slightly higher results with tools quenched from a temperature of 2250 degrees Fahrenheit. The tools should be heated slowly to the tempering temperature and should be held at this temperature for about one and one-half hours, after which they may be cooled in air.
Superficial surface hardening.During recent years there has been a tendency for many manufacturers of high speed steel to impart a superficial surface hardness after the tools have been finish ground. Standard nitriding treatments have been used but, in general, this has not been found satisfactory as apparently the concentration of the nitrides is too great at the surface of the steel causing unusual brittleness. By immersing the finished tool in a molten bath composed of about 50% sodium cyanide and 50% potassium cyanide at a temperature of approximately 1025 degrees Fahrenheit a superficial hardness is imparted which is probably not over several thousandths in depth but which for certain classes of tools may even double their life. The time in the cyanide bath may be from ten minutes to one and one-half hours, according to the requirements desired. When this treatment is used the tools shouldfirst be given the regular treatment,. finlsh ground and then slowly heated to the temperature at which they should be immersed in the cyanide bath.
This application may be considered a continuation-in-part of my application Serial No. 38,059, filed August 27, 1935.
Having thus described the invention, what I claim as new and desire to secure by Letters Patent of the United States is:
A tool composed of a readily forgeable and ma chinable high speed alloy steel of the molybdenum type, said steel containing from .75% to 1.20% carbon, from 3.75% to 4.75% chromium, from 8.25% to 10.00% molydenum, andfrom 2.00% to 4.25% vanadium, the ratio of the vanadium to carbon being in excess, of two and one-half to one and below three and one-half to one, with the remainder of the alloy substantially all ir'on.
JAMES P. GILL. 10
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US174487A US2105114A (en) | 1937-11-13 | 1937-11-13 | Alloy steel tool |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US174487A US2105114A (en) | 1937-11-13 | 1937-11-13 | Alloy steel tool |
Publications (1)
Publication Number | Publication Date |
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US2105114A true US2105114A (en) | 1938-01-11 |
Family
ID=22636329
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US174487A Expired - Lifetime US2105114A (en) | 1937-11-13 | 1937-11-13 | Alloy steel tool |
Country Status (1)
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US (1) | US2105114A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE28719E (en) * | 1971-12-22 | 1976-02-24 | United States Steel Corporation | Method of making flat steel files |
US4780139A (en) * | 1985-01-16 | 1988-10-25 | Kloster Speedsteel Ab | Tool steel |
-
1937
- 1937-11-13 US US174487A patent/US2105114A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE28719E (en) * | 1971-12-22 | 1976-02-24 | United States Steel Corporation | Method of making flat steel files |
US4780139A (en) * | 1985-01-16 | 1988-10-25 | Kloster Speedsteel Ab | Tool steel |
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