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US2090044A - Alloys - Google Patents

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Publication number
US2090044A
US2090044A US29674A US2967435A US2090044A US 2090044 A US2090044 A US 2090044A US 29674 A US29674 A US 29674A US 2967435 A US2967435 A US 2967435A US 2090044 A US2090044 A US 2090044A
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US
United States
Prior art keywords
alloys
alloy
beryllium
titanium
cobalt
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
Application number
US29674A
Inventor
Hessenbruch Werner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vacuumschmelze GmbH and Co KG
Original Assignee
Heraeus Vacuumschmelze AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
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Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt

Definitions

  • the prior stellite type of alloy (cobalt-chromi- 20 um basis) also incorporated one or more of additional ingredients such, for example, as tungsten and molybdenum, and sometimes nickel.
  • the present invention is concerned with alloys of the cobalt chromium type, which alloysare capable of heat treatment and have material- 30 1y improved properties, such as cutting emciency. strength and toughness, although they are not brittle.
  • metals such as beryllium 35 or titanium or both. I prefer also to melt and pour my improved alloys in vacuo.
  • the present invention contemplates an alloy containing from about 30% to about 60.0% cobalt and from about 20% to 10 about 40% chromium. While some improvement may be effected by the beryllium or titanium even when substantial amounts of carbon are present, I prefer to reduce or even eliminate the carbon, and I have further found that the properties may very readily be appreciably improved by heat treatment. ably quenched in oil or some equivalent quenching medium, from a high temperature, and then' For example, the alloys are desir-' subsequently annealed at a temperature of from about 500 to 900 C.
  • the brittleness of stellites and similar cutting alloys heretofore employed is at least in large part produced by the content of carbon, and the invention contemplates the ad- 5,
  • the total amount of titanium or beryllium or both should be in the 10' neighborhood of from about .3% to about 4%]
  • chromium and beryllium or titanium I also contemplate the use of tungsten, molybdenum or tantalum either individually or in combinations.
  • the total content l5 of this constituent should be less than 25% of the,alloy, and it is preferable where only molybdenum and/or tantalum are employed, to keep the totalbelow about 15%.
  • Nickel may also be added to the alloy, although preferably not in excess of about 10%.
  • Thepreferred range of beryllium or titanium (or both combined) is from about 1% to about 2%.
  • a cutting tool composed of an alloy consisting 40 of from about .3% to about 4% beryllium, molyb denum up to about 15%, and the balance a basic ingredient composed of cobalt and chromium, the former of which comprises from about 30% to about 60% of the entire alloy and the latter of which comprises from about 20% to about 40% of the entire alloy.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Materials For Medical Uses (AREA)

Description

Patented Aug. 17, 1937 UNITED STATES PATENT OFFICE 2,090,044 annoys Werner Hessenbruch, Hanau-on-the-Maln, Germany, assignor to Heraeus-Vacuumschmelze, A. G., Hanau-on-the-Main, Germany No Drawing. Application July 3, 1935, Serial No. 29,674. In Germany July 14, 1934 1 Claim. (01. 75-171) Recently there have been some sintered alloysv introduced for machining hard materials and ordinary steels. While these alloys represent an improvement over some of the former materials employed in high-speed tools, as well as an improvement over heretofore known alloys similar to the so-called stellite (built up on a cobaltchromium basis), still these prior sintered alloys have been subject to a number of disadvantages. For example, the prior alloys have been very brittle. Other types of alloys employed for cut- 5 ting tools heretofore, for example, stellites, have been open to the objection that their hardness,
especially at higher temperatures, was not sumcient.
The prior stellite type of alloy (cobalt-chromi- 20 um basis) also incorporated one or more of additional ingredients such, for example, as tungsten and molybdenum, and sometimes nickel.
These prior alloys, furthermore, had an average content of carbon from about 2% to about 4%,
5 and they were ordinarily cast and were not capable of being improved by heat treatment.
The present invention is concerned with alloys of the cobalt chromium type, which alloysare capable of heat treatment and have material- 30 1y improved properties, such as cutting emciency. strength and toughness, although they are not brittle.
An important factor in producing the improvement is the addition of metals such as beryllium 35 or titanium or both. I prefer also to melt and pour my improved alloys in vacuo.
More specifically, the present invention contemplates an alloy containing from about 30% to about 60.0% cobalt and from about 20% to 10 about 40% chromium. While some improvement may be effected by the beryllium or titanium even when substantial amounts of carbon are present, I prefer to reduce or even eliminate the carbon, and I have further found that the properties may very readily be appreciably improved by heat treatment. ably quenched in oil or some equivalent quenching medium, from a high temperature, and then' For example, the alloys are desir-' subsequently annealed at a temperature of from about 500 to 900 C. The brittleness of stellites and similar cutting alloys heretofore employed is at least in large part produced by the content of carbon, and the invention contemplates the ad- 5,
dition of titanium or beryllium and elimination of or at least reduction in the carbon content,
' in instances where it is desired to materially diminish the brittleness. The total amount of titanium or beryllium or both should be in the 10' neighborhood of from about .3% to about 4%] In addition to the cobalt, chromium and beryllium or titanium, I also contemplate the use of tungsten, molybdenum or tantalum either individually or in combinations. The total content l5 of this constituent should be less than 25% of the,alloy, and it is preferable where only molybdenum and/or tantalum are employed, to keep the totalbelow about 15%.
Nickel may also be added to the alloy, although preferably not in excess of about 10%.' v
Thepreferred range of beryllium or titanium (or both combined) is from about 1% to about 2%.
As a specific example of an alloy of the type contemplated by this invention, which alloy is tough, hard, and strong, even when heated to high temperature, I mention one containing the following ingredients in about the proportions indicated:
' Per cent Cobalt 40 Chromium 25 Tungsten- 18 Nickel 10 Molybdenum 5 I Beryllium from 1% to 2 I claim:-
A cutting tool composed of an alloy consisting 40 of from about .3% to about 4% beryllium, molyb denum up to about 15%, and the balance a basic ingredient composed of cobalt and chromium, the former of which comprises from about 30% to about 60% of the entire alloy and the latter of which comprises from about 20% to about 40% of the entire alloy.
WERNER HESSENBRUCH.
US29674A 1934-07-14 1935-07-03 Alloys Expired - Lifetime US2090044A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2090044X 1934-07-14

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US2090044A true US2090044A (en) 1937-08-17

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2469718A (en) * 1945-01-13 1949-05-10 Vanadium Corp Of America Alloys
US2805945A (en) * 1949-01-28 1957-09-10 Straumann Reinhard Mainspring composed of nickel base alloys
US2841511A (en) * 1952-09-16 1958-07-01 Onera (Off Nat Aerospatiale) Metal alloy and its manufacturing process
US3524775A (en) * 1967-12-06 1970-08-18 Cabot Corp High strength cobalt-beryllium alloy and method of producing the same

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2469718A (en) * 1945-01-13 1949-05-10 Vanadium Corp Of America Alloys
US2805945A (en) * 1949-01-28 1957-09-10 Straumann Reinhard Mainspring composed of nickel base alloys
US2841511A (en) * 1952-09-16 1958-07-01 Onera (Off Nat Aerospatiale) Metal alloy and its manufacturing process
US3524775A (en) * 1967-12-06 1970-08-18 Cabot Corp High strength cobalt-beryllium alloy and method of producing the same

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