Nothing Special   »   [go: up one dir, main page]

US2126749A - Alloy - Google Patents

Alloy Download PDF

Info

Publication number
US2126749A
US2126749A US143469A US14346937A US2126749A US 2126749 A US2126749 A US 2126749A US 143469 A US143469 A US 143469A US 14346937 A US14346937 A US 14346937A US 2126749 A US2126749 A US 2126749A
Authority
US
United States
Prior art keywords
alloy
thermal treatment
hardness
boron
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
US143469A
Inventor
Golyer Anthony G De
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.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Priority to US143469A priority Critical patent/US2126749A/en
Application granted granted Critical
Publication of US2126749A publication Critical patent/US2126749A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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 present invention relates to a new and useful alloy containing boron, zirconium, chromium and cobalt, which is characterized by being responsive to thermal treatment for the 5' improvement of physical properties.
  • An object of the present invention is to provide an alloy especially adapted for use as metal cutting tools, the cutting efficiency of which is superior to that of heretofore known high speed Y tools and other alloys.
  • a further object is to provide analloy which is free from, or substanlo tially free from, carbon, and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency and other physical properties and characteristics can be accurately controlled over a comparatively wide range.
  • Alloys of this invention may be used in the cast condition for certain purposes, but approximatemaximum values of hardness, resistance to impact and certain other important physical properties can be developed only through thermal treatment, or through mechanical working and thermal treatment. Bodies of the alloy which have been subjected to such treatment are particularly valuable for use as tools, dies,
  • cast bodies of this alloy may have a hardness of from 52 to 58 on the Rockwell C scale and by subjecting the material to suitable thermal treatment, such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C.
  • suitable thermal treatment such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C.
  • the alloy can subsequently be subjected to a second thermal treatment, such 15 as heating to a temperature lower than 1000 C. for a period of one hour or more, followed by cooling at a normal rate, by which the hardness can be increased to from approximately 58 to 66 Rockwell C. valuable for many industrial uses.
  • compositions within the 40 scope of the present invention which I have found well adapted for numerous industrial applications are of the following: boron 1.75%, zlrconium 4.75%, chromium.7.50 cobalt substantially the balance; boron 1.95%, zirconium 45 0.75%, chromium 15%, cobalt substantially the balance;. boron 2.30%, zirconium 2%, chromium 12%, cobalt substantially the balance.
  • An objective of the present invention is to provide an alloy having high hardness, advanta- 60 geous metal cutting properties, etc., which is free from, or substantially free from, carbon, and thus eliminate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc.
  • the alloy is 20 though I prefer to have the alloys entirely free from carbon, in many instances I have found carbon present in the nature of an impurity incidental to manufacture. It' is important, however. to restrict the carbon content to a maximum 0! about 0.15%, as I have found that the presence of higher percentages of this element not only embrittle the alloy, but also inhibit or retard the desired or necessary reactions during thermal treatment. The presence of appreciable amounts of carbon decreases the red hardness of the alloy; 1-. e., hardness at temperatures oi approximately 550 C. and higher.
  • the preferred structure of a body of the present alloy comprises at least two-principal constituents; one, a relatively hard lntermetallicj compound of boron with one or more of the other essential components; and,
  • the ratio of the constituents as well as the ratio oi particle size in any particular body or the alloy may be accurately controlled and fixed over a wide range I by means of thermal treatment or mechanical working and thermal treatment.
  • the alloy of the present invention comprises boron, zirconium,

Landscapes

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

Description

Patented Aug. 16, 1938 PATENT OFFICE ALLOY Anthony de Golyer, New York, N. Y.
No Drawing. Application May 19, 1937, Serial No. 143,469 v 1 Claim.
The present invention relates to a new and useful alloy containing boron, zirconium, chromium and cobalt, which is characterized by being responsive to thermal treatment for the 5' improvement of physical properties. This application is a continuation in part of my copending application Serial No. 721,771 filed April 21, 1934.
An object of the present invention is to provide an alloy especially adapted for use as metal cutting tools, the cutting efficiency of which is superior to that of heretofore known high speed Y tools and other alloys. A further object is to provide analloy which is free from, or substanlo tially free from, carbon, and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency and other physical properties and characteristics can be accurately controlled over a comparatively wide range.
I have found through experiment that by alloying or otherwise intimately combining boron, zirconium, chromium and cobalt within the range of boron 0.50% to 4%, zirconium 0.25% to 5%, chromium 1% to 17% and cobalt substantially the balance, that I obtain metallic compositions which are readily responsive to thermal treatment by means of which the physical properties and characteristics can be developed and controlled.
Alloys of this invention may be used in the cast condition for certain purposes, but approximatemaximum values of hardness, resistance to impact and certain other important physical properties can be developed only through thermal treatment, or through mechanical working and thermal treatment. Bodies of the alloy which have been subjected to such treatment are particularly valuable for use as tools, dies,
40 and the like for the-cutting .or mechanical working of metals, as well as for many other industrial uses.
Numerous metallic compositions have heretofore been proposed as improvements on the known types of high speed tool steel, but all of such proposed compositions have disadvantages which render them unsuitable for general application as metal cutting or forming tools. One
disadvantage of such compositions is that nonev treatment for the development of precipitation hardening, often referred to as age hardening.
I prefer to subject the alloy to thermal treatment before using it for metal cutting tools,'dies, etc. 7 I have found that both the cast and forged mate- 5 rials are responsive to thermal treatment. As an illustration, cast bodies of this alloy may have a hardness of from 52 to 58 on the Rockwell C scale and by subjecting the material to suitable thermal treatment, such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C. The alloy can subsequently be subjected to a second thermal treatment, such 15 as heating to a temperature lower than 1000 C. for a period of one hour or more, followed by cooling at a normal rate, by which the hardness can be increased to from approximately 58 to 66 Rockwell C. valuable for many industrial uses.
An important property of the alloy is that virtually all of the maximum hardness, developed by thermal treatment, is retained when the alloy is subjected to temperatures between 500 and 2a The more important distinctive advantages 5 are apparently due to the presence. of appreciable amounts of boron in the composition, in conjunction with the other components, within the percentages specified herein.
Specific examples of composition within the 40 scope of the present invention which I have found well adapted for numerous industrial applications are of the following: boron 1.75%, zlrconium 4.75%, chromium.7.50 cobalt substantially the balance; boron 1.95%, zirconium 45 0.75%, chromium 15%, cobalt substantially the balance;. boron 2.30%, zirconium 2%, chromium 12%, cobalt substantially the balance.
An objective of the present invention is to provide an alloy having high hardness, advanta- 60 geous metal cutting properties, etc., which is free from, or substantially free from, carbon, and thus eliminate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc. Al-
'In the latter condition the alloy is 20 though I prefer to have the alloys entirely free from carbon, in many instances I have found carbon present in the nature of an impurity incidental to manufacture. It' is important, however. to restrict the carbon content to a maximum 0! about 0.15%, as I have found that the presence of higher percentages of this element not only embrittle the alloy, but also inhibit or retard the desired or necessary reactions during thermal treatment. The presence of appreciable amounts of carbon decreases the red hardness of the alloy; 1-. e., hardness at temperatures oi approximately 550 C. and higher.
My investigations indicate that the preferred structure of a body of the present alloy, particularly after thermal treatment, comprises at least two-principal constituents; one, a relatively hard lntermetallicj compound of boron with one or more of the other essential components; and,
two, a solid solution of two or more or the essentlal components which has a lower degree of hardness and functions as a matrix. The ratio of the constituents as well as the ratio oi particle size in any particular body or the alloy may be accurately controlled and fixed over a wide range I by means of thermal treatment or mechanical working and thermal treatment.
By reason of the combined advantageous physical properties and-characteristics'possessed by the alloy 01' the present invention, tools and other articles composed oi! this alloy may be operated eiliciently and economically under conditions which are impossible or uneconomical with tools, etc., composed of heretofore ,khow'n alloys or metallic compositions.
By the term the balance substantially cobalt" or the "balance cobalt" in the foregoing and in the following claim, I intend that the alloy of the present invention comprises boron, zirconium,
and chromium within the percentaae limits specified, with the remainder cobalt, except for inei'iectual amounts of impurities which may be present incidental to manufacture.
I claim:
' A precipitation hardened. alloy containing boron 0.50% .to 4%, zirconium-0.25% to--5%, chromium 1% to 17%, the balance cobalt.
ANTHONY G. or GOLYER.
US143469A 1937-05-19 1937-05-19 Alloy Expired - Lifetime US2126749A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US143469A US2126749A (en) 1937-05-19 1937-05-19 Alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US143469A US2126749A (en) 1937-05-19 1937-05-19 Alloy

Publications (1)

Publication Number Publication Date
US2126749A true US2126749A (en) 1938-08-16

Family

ID=22504223

Family Applications (1)

Application Number Title Priority Date Filing Date
US143469A Expired - Lifetime US2126749A (en) 1937-05-19 1937-05-19 Alloy

Country Status (1)

Country Link
US (1) US2126749A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2983602A (en) * 1957-09-24 1961-05-09 Armour Res Found Cobalt alloys
US3362816A (en) * 1963-06-22 1968-01-09 Fed Republic Of Germany Cobalt alloy

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2983602A (en) * 1957-09-24 1961-05-09 Armour Res Found Cobalt alloys
US3362816A (en) * 1963-06-22 1968-01-09 Fed Republic Of Germany Cobalt alloy

Similar Documents

Publication Publication Date Title
AU2023282167A1 (en) Creep Resistant Titanium Alloys
US3839022A (en) Hot work tools and alloys therefor
US3128175A (en) Low alloy, high hardness, temper resistant steel
US2126749A (en) Alloy
US2097177A (en) Alloy
US2126750A (en) Alloy
US2097176A (en) Alloy
US2147637A (en) Alloy
JP2020169378A (en) Aluminum alloy for compressor slide components and compressor slide component forging
US2147636A (en) Alloy
US2244517A (en) Alloy
US2126748A (en) Alloy
US2097178A (en) Alloy
US2102869A (en) Zinc alloys
US2126746A (en) Alloy
US2126743A (en) Boron alloy
US2126742A (en) Alloy
US2126745A (en) Alloy
JPH01316442A (en) Hot processing aluminum base alloy
US2126744A (en) Alloy
US2097179A (en) Alloy
US2290025A (en) Aluminum alloy
US2097181A (en) Alloy
US2849310A (en) Copper-base alloy
US2097180A (en) Alloy