US2297687A - Alloy and cutting tool - Google Patents
Alloy and cutting tool Download PDFInfo
- Publication number
- US2297687A US2297687A US348445A US34844540A US2297687A US 2297687 A US2297687 A US 2297687A US 348445 A US348445 A US 348445A US 34844540 A US34844540 A US 34844540A US 2297687 A US2297687 A US 2297687A
- Authority
- US
- United States
- Prior art keywords
- alloy
- cutting tool
- chromium
- iron
- alloys
- 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 title description 19
- 239000000956 alloy Substances 0.000 title description 19
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 239000000203 mixture Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000011651 chromium Substances 0.000 description 5
- 229910017052 cobalt Inorganic materials 0.000 description 5
- 239000010941 cobalt Substances 0.000 description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000005299 abrasion Methods 0.000 description 4
- UPHIPHFJVNKLMR-UHFFFAOYSA-N chromium iron Chemical compound [Cr].[Fe] UPHIPHFJVNKLMR-UHFFFAOYSA-N 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910000997 High-speed steel Inorganic materials 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- 229910052720 vanadium Inorganic materials 0.000 description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- AHIVCQLQCIBVOS-UHFFFAOYSA-N [Fe].[W] Chemical compound [Fe].[W] AHIVCQLQCIBVOS-UHFFFAOYSA-N 0.000 description 1
- 238000005552 hardfacing Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- SNICXCGAKADSCV-UHFFFAOYSA-N nicotine Chemical compound CN1CCCC1C1=CC=CN=C1 SNICXCGAKADSCV-UHFFFAOYSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 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
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/06—Alloys based on chromium
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T407/00—Cutters, for shaping
- Y10T407/27—Cutters, for shaping comprising tool of specific chemical composition
Definitions
- Patented Oct. 6, 1942 ALLOY AND CUTTING TOOL Charles 0. Burgess and William D. l 'orgeng, Niagara Falls, N. Y., assignmto Haynes Stcllite Company, a corporation of Indiana No Drawing. Application July so, 1940, Serial No. 3415445 4 Claims. (01. 148-31) f tools made therefrom.
- Chromium-iron alloys have been used to resist wear and abrasion.
- the composition, and in some instances the heat treatment it has been possible to vary the hardness, toughness, and strength of the alloys over wide ranges.
- hardness of a very high degree such as is required of a metal-cutting tool has heretofore been accompanied by an. undue degree of brittleness.
- Cutting tool "high speed.
- steels have been basically tungsten-iron compositions rather than chromium-iron, and have typically contained 18% tungsten, 4% chromium, and 1% vanadium (so-called 18-4-1) sometimes modifled by the addition of one or more of the metals cobalt, nickel, and molybdenum.
- a hard chromiumiron alloy containing between 45% and 65% chromium is considerably toughened by the addition of carbon, preferably in a percentage between l% and 3%.
- carbon preferably in a percentage between l% and 3%.
- the carbon content may be somewhat above or below that range.
- cobalt nickel; boron; silicon; manganese; tungsten; molybdenum; columbium tantalum; and vanadium.
- a cutting tool alloy has a composition in the neighborhood of 53% chromium, 12% cobalt, 7% nickel, 2% carbon, remainder iron. These percentages may be varied somewhat, but should ordinarily be within the limits:
- the iron being usually more than 15% and preferably at least On occasion it will be desirable to add one or more of the elements silicon, tungsten, molybdenum, titanium, zirconium, columbium, tantalum, and vanadium, in individual percentages not exceeding 5% and in a total aggregate percentage under 10% and manganese up to about 10%; the iron however being maintained above 15%. It is sometimes desirable-to add boron in a percentage not over about 5%: in a proportion between 0.2% and 1.5% this element considerably enhances the cutting qualities and toughness of the alloy.
- the normal impurities of steels, such as phosphorus, sulfur, and nitrogen, may be present in small fractional percentages without departing from the invention.
- the alloys of this invention may be used in the as-cast condition (after casting in sand or carbon molds for instance) or when heat treated.
- a suitable heat treatment consists in holding the alloy at a temperature between about 550 C. and about 850 C. for a time between about five minutes at the higher temperatures to about twenty hours at the lower temperatures.
- the alloys are hot forgeable to a limited extent. If the alloys are to be forged, it is best to begin that operation before they have cooled from the casting step to below 900 C. Some cold deformation of the forged alloy can be effected, preferably after quenching from above 900 C.
- the hardness of the alloy of the invention varies between the approximate limits of to '70 Rockwell C.”
- the best cutting tool quality is usually attained in tools having a hardness in the neighborhood of Rockwell C.'
- the transverse strength of the as-cast alloys is upwards of 1000 pounds (loading applied centrally to a section 0.5 inch by 0.5 inch square, supported in a 4 inch span) and in the preferred range of compositions attains 3000 to 4000 pounds and sometimes more.
- Cutting tests indicate that the alloy tool of the invention compares favorably with standard high speed steel tools of the 18-4-1 type.
- cutting steel billets and semi-steel billets, and using surface speeds, feeds, and cuts considerably greater than normal, tools of this invention cut from two to eight times as far as standard Rex AAA, a widelyused high speed steel of high quality.
- the alloy of this invention is capable of many other uses which are within the invention, for instance as a hard-facing material for tool and machinery wear-resisting parts.
- Alloy, resistant to wear and abrasion and suitable for use as a cutting tool having substantially the composition: between 45% and 65% chromium, between 5% and 20% cobalt, between 4% and 20% nickel, carbon between 1% and 3% to impart toughness, remainder iron.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
Patented Oct. 6, 1942 ALLOY AND CUTTING TOOL Charles 0. Burgess and William D. l 'orgeng, Niagara Falls, N. Y., assignmto Haynes Stcllite Company, a corporation of Indiana No Drawing. Application July so, 1940, Serial No. 3415445 4 Claims. (01. 148-31) f tools made therefrom.
Chromium-iron alloys, often modified by the addition of other elements, have been used to resist wear and abrasion. By varying the composition, and in some instances the heat treatment, it has been possible to vary the hardness, toughness, and strength of the alloys over wide ranges. But hardness of a very high degree such as is required of a metal-cutting tool has heretofore been accompanied by an. undue degree of brittleness. Cutting tool "high speed. steels have been basically tungsten-iron compositions rather than chromium-iron, and have typically contained 18% tungsten, 4% chromium, and 1% vanadium (so-called 18-4-1) sometimes modifled by the addition of one or more of the metals cobalt, nickel, and molybdenum.
It is a primary object of the invention to provide an abrasion resistant chromium iron alloy which, in the form of a cutting tool, will cut metals at high speeds at least as well as 1844 high speed steel.
We have discovered that a hard chromiumiron alloy containing between 45% and 65% chromium is considerably toughened by the addition of carbon, preferably in a percentage between l% and 3%. For some purposes the carbon content may be somewhat above or below that range. We have further found that the general suitability of such an alloy for use as a cutting tool and other abrasion-resisting articles is enhanced by the addition of One or more of the following elements: cobalt; nickel; boron; silicon; manganese; tungsten; molybdenum; columbium tantalum; and vanadium.
According to this invention, a cutting tool alloy has a composition in the neighborhood of 53% chromium, 12% cobalt, 7% nickel, 2% carbon, remainder iron. These percentages may be varied somewhat, but should ordinarily be within the limits:
the iron being usually more than 15% and preferably at least On occasion it will be desirable to add one or more of the elements silicon, tungsten, molybdenum, titanium, zirconium, columbium, tantalum, and vanadium, in individual percentages not exceeding 5% and in a total aggregate percentage under 10% and manganese up to about 10%; the iron however being maintained above 15%. It is sometimes desirable-to add boron in a percentage not over about 5%: in a proportion between 0.2% and 1.5% this element considerably enhances the cutting qualities and toughness of the alloy. The normal impurities of steels, such as phosphorus, sulfur, and nitrogen, may be present in small fractional percentages without departing from the invention.
The alloys of this invention may be used in the as-cast condition (after casting in sand or carbon molds for instance) or when heat treated. A suitable heat treatment consists in holding the alloy at a temperature between about 550 C. and about 850 C. for a time between about five minutes at the higher temperatures to about twenty hours at the lower temperatures. The alloys are hot forgeable to a limited extent. If the alloys are to be forged, it is best to begin that operation before they have cooled from the casting step to below 900 C. Some cold deformation of the forged alloy can be effected, preferably after quenching from above 900 C.
Depending chiefly upon the composition and heat treatment, the hardness of the alloy of the invention varies between the approximate limits of to '70 Rockwell C." The best cutting tool quality is usually attained in tools having a hardness in the neighborhood of Rockwell C.' The transverse strength of the as-cast alloys is upwards of 1000 pounds (loading applied centrally to a section 0.5 inch by 0.5 inch square, supported in a 4 inch span) and in the preferred range of compositions attains 3000 to 4000 pounds and sometimes more.
Cutting tests indicate that the alloy tool of the invention compares favorably with standard high speed steel tools of the 18-4-1 type. In accelerated life tests, cutting steel billets and semi-steel billets, and using surface speeds, feeds, and cuts considerably greater than normal, tools of this invention cut from two to eight times as far as standard Rex AAA, a widelyused high speed steel of high quality.
Although the use of the alloy of this invention as a cutting tool has been emphasized in the foregoing description, the alloy is capable of many other uses which are within the invention, for instance as a hard-facing material for tool and machinery wear-resisting parts.
We claim:
1. Alloy, resistant to wear and abrasion and suitable for use as a cutting tool, having substantially the composition: between 45% and 65% chromium, between 5% and 20% cobalt, between 4% and 20% nickel, carbon between 1% and 3% to impart toughness, remainder iron.
2. Alloy, resistant to wear and abrasion and suitable for use in the as-cast condition as a cutting tool, having substantially the composition: 50% to 56% chromium, 7% to 15% cobalt, 6% to 15% nickel, 1.5% to 2.25% carbon, re-
CHARLES O. BURGESS. WILLIAM D. FORGENG.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US348445A US2297687A (en) | 1940-07-30 | 1940-07-30 | Alloy and cutting tool |
| US419289A US2334246A (en) | 1940-07-30 | 1941-11-15 | Cutting tool |
| US419287A US2334245A (en) | 1940-07-30 | 1941-11-15 | Cutting tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US348445A US2297687A (en) | 1940-07-30 | 1940-07-30 | Alloy and cutting tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2297687A true US2297687A (en) | 1942-10-06 |
Family
ID=23368082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US348445A Expired - Lifetime US2297687A (en) | 1940-07-30 | 1940-07-30 | Alloy and cutting tool |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2297687A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2551170A (en) * | 1947-09-30 | 1951-05-01 | Crucible Steel Co America | Cobalt base alloy and articles thereof |
| US2714760A (en) * | 1951-07-02 | 1955-08-09 | Curtiss Wright Corp | Method of brazing and joint produced thereby |
| US2780545A (en) * | 1954-02-03 | 1957-02-05 | Battelle Development Corp | High-temperature alloy |
| US2809139A (en) * | 1952-10-24 | 1957-10-08 | Research Corp | Method for heat treating chromium base alloy |
-
1940
- 1940-07-30 US US348445A patent/US2297687A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2551170A (en) * | 1947-09-30 | 1951-05-01 | Crucible Steel Co America | Cobalt base alloy and articles thereof |
| US2714760A (en) * | 1951-07-02 | 1955-08-09 | Curtiss Wright Corp | Method of brazing and joint produced thereby |
| US2809139A (en) * | 1952-10-24 | 1957-10-08 | Research Corp | Method for heat treating chromium base alloy |
| US2780545A (en) * | 1954-02-03 | 1957-02-05 | Battelle Development Corp | High-temperature alloy |
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