US2297687A - Alloy and cutting tool - Google Patents

Alloy and cutting tool Download PDF

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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
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United States
Prior art keywords
alloy
cutting tool
chromium
iron
alloys
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Expired - Lifetime
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US348445A
Inventor
Charles O Burgess
William D Forgeng
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HAYNES STELLITE Co
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HAYNES STELLITE CO
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Priority to US348445A priority Critical patent/US2297687A/en
Priority to US419287A priority patent/US2334245A/en
Priority to US419289A priority patent/US2334246A/en
Application granted granted Critical
Publication of US2297687A publication Critical patent/US2297687A/en
Anticipated expiration legal-status Critical
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/06Alloys based on chromium
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T407/00Cutters, for shaping
    • Y10T407/27Cutters, 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.

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.
US348445A 1940-07-30 1940-07-30 Alloy and cutting tool Expired - Lifetime US2297687A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US348445A US2297687A (en) 1940-07-30 1940-07-30 Alloy and cutting tool
US419287A US2334245A (en) 1940-07-30 1941-11-15 Cutting tool
US419289A US2334246A (en) 1940-07-30 1941-11-15 Cutting tool

Applications Claiming Priority (1)

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US348445A US2297687A (en) 1940-07-30 1940-07-30 Alloy and cutting tool

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US2297687A true US2297687A (en) 1942-10-06

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Cited By (4)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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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