US1986024A - Method for increasing the strength of alloys - Google Patents

Method for increasing the strength of alloys Download PDF

Info

Publication number
US1986024A
US1986024A US664449A US66444933A US1986024A US 1986024 A US1986024 A US 1986024A US 664449 A US664449 A US 664449A US 66444933 A US66444933 A US 66444933A US 1986024 A US1986024 A US 1986024A
Authority
US
United States
Prior art keywords
alloy
temperature
alloys
strength
room temperature
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
US664449A
Inventor
Wesley P Sykes
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to US664449A priority Critical patent/US1986024A/en
Application granted granted Critical
Publication of US1986024A publication Critical patent/US1986024A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/007Heat treatment of ferrous alloys containing Co

Definitions

  • the present invention relates to a method for increasing the strength of alloys which are capable of being age hardened and consist substantially of iron, cobalt and metal from the 6th group' of Mendelejefis periodic table of elements.
  • Such alloys may contain relatively small 7 percentages of additional elements such as vanadium, manganese and carbon. Alloys of this character are well known and generally are em- 10 ployed as metal cutting tools such tools being par ticularly adapted for use in cutting steel.
  • Alloys of the above composition may be produced by casting the mixed ingredients into an alloy ingot which may be forged, rolled, pressed or otherwise treated as required in a manner similar to the treatment of high speed steels.
  • the alloy is heated to a temperature between 1000 C. and 1500 C.
  • An alloy consisting for example of about 29.8% cobalt, 18.7% tungsten, 3.32 molybdenum,
  • I employ an arrested quench. For example after the alloy.
  • the resulting product has a Rockwell C hardness of about 45 to 4'7 and 45 a transverse breaking strength of about 450,000
  • the temperature of the alloy 50 is reduced to the temperature of'the bath in a very short time, probably less than a minute since at the end of that time the alloy has substantially the same color as the lead bath.
  • the transverse breaking strength of the alloy after quench- I 56 ing in the lead bath and cooling to approximately room temperature is about 100,000 lbs. greater than the strength of-a similar alloyquenched from a temperature of about 1200 C. to room temperature. Quenching the alloy from the heat treating temperature above 1000 C. to a tempera- 5 ture of about 600 C. prevents precipitation in the alloy of an excess hard compound between these temperatures while the slow cooling from 600 C. eifects an increase in strength of the alloy.
  • the alloy When the alloy has been cooled to room temw perature or to a temperature between room temperature and about 300 C., it may be aged at temperatures varying from about 250 to 700 C. The aging process increases the hardness of the alloy to about 63 to 69 on the Rockwell C scale 15 but at the same time efiects a slight reduction in the strength of the alloy. If the lower range of aging temperature is employed the increase in hardness of the alloy takes place very slowly, so that it is generally preferable to harden the alloy 20 at temperatures varying from about 500 to 650 C.
  • alloys having the specific composition given above were quenched from 1275 C. into a salt bath at 600 0., held in the bath for about 1 minutes and then cooled 25 from 600 C. to room temperature in air or in lime in a period of time varying from about 15 minutes to' 3 hours. These alloys were then "age hardened by placing-them in a furnace heated to about 70 C. and the furnace temperature was 30 then increased to about 525 C. in aboutv 40 minutes. This temperature was maintained for approximately 15 minutes after which the alloys were removed and cooled to room temperature either in lime or in still air, the cooling period in lime being about three hours and the, cooling period in still air being about 15 minutes. These latter cooling rates are not important but should not be too rapid.
  • the alloys so treated had a hardness of about 66 on the Rockwell C scale and a transverse breaking strength of about 340,000 lbs. per square inch which indicates that although the primary strength of such alloys is reduced during the age hardening process the secondary strength is still far above that obtained in alloys in which an arrested quench has not been employed.
  • an alloy consisting substantially of about 15% to 35% cobalt, about 12% to 30% of metal from the 6th group of Mendelejefis periodic table of elements, an appreciable amount up to about 3% vanadium, an appreciable amount up to about 0.6% manganese and the remainder iron.
  • the invention-however is not limited to this com-- consist substantially of iron, cobalt and tungsten,
  • quenching the alloy to a temperature between about 500 C. and about 700 C., cooling the alloy at a relatively slow rate to a temperature between comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature: of about 500 C. to 700 C., slowly cooling the alloy in aperiod of time varying from about fifteen minutes to six. hours ,to, a temperature between room temperature and 300 C., and then aging the alloy at a temperature between 250 C. and 700 C.
  • the remainder of the composition consisting subv stantially of iron which comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature of about 500 C. to 700 C. and slowly cooling the alloy to room temperature in a period of time varying from about fifteen minutes to about six hours.

Description

UNITED STATES PATENT OFFICE rmrnon roa mcamsmc rm: s'mnncrn OF ALLOYS New York No Drawing. Application Apr-I14, 1933, I Serial No. 664,449
a Claim' (01. 148-215) The present invention relates to a method for increasing the strength of alloys which are capable of being age hardened and consist substantially of iron, cobalt and metal from the 6th group' of Mendelejefis periodic table of elements. Such alloys, if desired, may contain relatively small 7 percentages of additional elements such as vanadium, manganese and carbon. Alloys of this character are well known and generally are em- 10 ployed as metal cutting tools such tools being par ticularly adapted for use in cutting steel.
Alloys of the above composition may be produced by casting the mixed ingredients into an alloy ingot which may be forged, rolled, pressed or otherwise treated as required in a manner similar to the treatment of high speed steels.
After this treatment the alloy is heated to a temperature between 1000 C. and 1500 C.,
quenched to about room temperature and then aged at a temperature between about 250 C. and
700 C. An alloy consisting for example of about 29.8% cobalt, 18.7% tungsten, 3.32 molybdenum,
1.85% vanadium, 0.16% manganese, 0.1% carbon, 0.1% chromium and the remainder iron after the above heat treatment has a Rockwell C hardness which may vary from about 63 to 69 and a transverse breaking strength varying from about 175,000 to 250,000 lbs. per square inch.
In carrying out the present invention, I employ an arrested quench. For example after the alloy.
has been heated at a temperature of about 1000 C. to 1500 C. for a relatively short period of time varying from a few minutes to about fifteen minutes, instead of quenching the alloy to room temperature as heretofore suggested, I quench it in a molten lead, salt or equivalent bath to a temperature between about 500 C. and 700 C.,
i. e. about 600 C. and then transfer'the alloy to a muille furnace heated to about 600 C. and
40 cool the alloy to a temperature below 300 C.,
which if desired may be room temperature, in
a period of time which may vary from about 111- teen minutes to six hours. The resulting product has a Rockwell C hardness of about 45 to 4'7 and 45 a transverse breaking strength of about 450,000
to about 520,000 lbs. per square inch.
When the alloy is quenched from a temperature of about 1200 C. in a lead bath having a temperatime of about 600 C., the temperature of the alloy 50 is reduced to the temperature of'the bath in a very short time, probably less than a minute since at the end of that time the alloy has substantially the same color as the lead bath. The transverse breaking strength of the alloy after quench- I 56 ing in the lead bath and cooling to approximately room temperature is about 100,000 lbs. greater than the strength of-a similar alloyquenched from a temperature of about 1200 C. to room temperature. Quenching the alloy from the heat treating temperature above 1000 C. to a tempera- 5 ture of about 600 C. prevents precipitation in the alloy of an excess hard compound between these temperatures while the slow cooling from 600 C. eifects an increase in strength of the alloy.
When the alloy has been cooled to room temw perature or to a temperature between room temperature and about 300 C., it may be aged at temperatures varying from about 250 to 700 C. The aging process increases the hardness of the alloy to about 63 to 69 on the Rockwell C scale 15 but at the same time efiects a slight reduction in the strength of the alloy. If the lower range of aging temperature is employed the increase in hardness of the alloy takes place very slowly, so that it is generally preferable to harden the alloy 20 at temperatures varying from about 500 to 650 C.
In carrying out my invention, alloys having the specific composition given above were quenched from 1275 C. into a salt bath at 600 0., held in the bath for about 1 minutes and then cooled 25 from 600 C. to room temperature in air or in lime in a period of time varying from about 15 minutes to' 3 hours. These alloys were then "age hardened by placing-them in a furnace heated to about 70 C. and the furnace temperature was 30 then increased to about 525 C. in aboutv 40 minutes. This temperature was maintained for approximately 15 minutes after which the alloys were removed and cooled to room temperature either in lime or in still air, the cooling period in lime being about three hours and the, cooling period in still air being about 15 minutes. These latter cooling rates are not important but should not be too rapid. The alloys so treated had a hardness of about 66 on the Rockwell C scale and a transverse breaking strength of about 340,000 lbs. per square inch which indicates that although the primary strength of such alloys is reduced during the age hardening process the secondary strength is still far above that obtained in alloys in which an arrested quench has not been employed.
Asa metal cutting tool material, I prefer to employ an alloy consisting substantially of about 15% to 35% cobalt, about 12% to 30% of metal from the 6th group of Mendelejefis periodic table of elements, an appreciable amount up to about 3% vanadium, an appreciable amount up to about 0.6% manganese and the remainder iron. The invention-however is not limited to this com-- consist substantially of iron, cobalt and tungsten,
or substantially of iron, cobalt. tungsten and vanadium within the limits indicated above and which are made either by casting or sintering the ingredients of the alloy. Although I prefer to employ my process with alloys which are substantially carbon free the presence of relatively small quantities of carbon does not interfere with the operation of the process.
What I claim as new and desire to secure by Letters Patent of the United States, is:
1. The method of producing a strong alloy containing about 15% to 35% cobalt; about 12% to of metal of the sixth group of Men'delejefis periodic table of elements, the remainder consisting substantially of iron, which comprises heating the alloy to a temperature above 1000.
C. but not materially higher than 1500 C. quenching the alloy to a temperature between about 500 C. and about 700 C. and cooling the alloy at a relatively slow rate to room temperature.
2. The method of producing a strong alloy containing about 15% to cobalt, about 12% to 30% of metal of the sixth group of Mendele- Jeff's periodic table of elements, the remainder consisting substantially of iron, which comprises heating the alloy to a temperature above 1000 .C. but not materially higher than 1500 C.,
quenching the alloy to a temperature between about 500 C. and about 700 C., cooling the alloy at a relatively slow rate to a temperature between comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature: of about 500 C. to 700 C., slowly cooling the alloy in aperiod of time varying from about fifteen minutes to six. hours ,to, a temperature between room temperature and 300 C., and then aging the alloy at a temperature between 250 C. and 700 C.
4. The method of producinga strong alloy consisting substantially of about 15% to 35% cobalt, about 12% to 30% of metal of the sixth group of Mendelejeifs periodic table of elements, a fractional quantity up to about 3% vanadium,
the remainder of the composition consisting subv stantially of iron, which comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature of about 500 C. to 700 C. and slowly cooling the alloy to room temperature in a period of time varying from about fifteen minutes to about six hours.
5. ,The method of producing a strong alloy consisting substantially of about 15% to 35% cobalt, about 12% to 30% of metal of the sixth group of Mendelejefis periodic tableoi. elements, a fractional quantity up to about 3% vanadium, the remainder ofv the composition consisting substantially of iron, which, comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature of about 500" C; to 700. C., cooling the alloy to room temperature in a period of time varying from about fifteen minutes to about six hours, and age hardening the alloy ,at a temperature between 250 C. and I00" C. l
6. The method of producing a strong alloy consisting substantially of about 15% to 35% cobalt, about 12% to 30% of metal from a group consisting of tungsten, molybdenum and chromium, a fractional quantity up to about 3% vanadium, a fractional quantity and up to about .6%' manganese, the remainder of the composition consistingsubstantially of iron, which comprises heating the alloy to a temperature above 1000 C. but not materially higher than 1500 C., quenching the alloy in a bath having a temperature of about 500 C. to 700 C., cooling the'alloy to room temperature in a period of time varying from about fifteen minutes to about six hours, and
age hardening the alloy at a temperature between 250 C. and 700 C.
- WESLEY P. SYKES.
US664449A 1933-04-04 1933-04-04 Method for increasing the strength of alloys Expired - Lifetime US1986024A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US664449A US1986024A (en) 1933-04-04 1933-04-04 Method for increasing the strength of alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US664449A US1986024A (en) 1933-04-04 1933-04-04 Method for increasing the strength of alloys

Publications (1)

Publication Number Publication Date
US1986024A true US1986024A (en) 1935-01-01

Family

ID=24666012

Family Applications (1)

Application Number Title Priority Date Filing Date
US664449A Expired - Lifetime US1986024A (en) 1933-04-04 1933-04-04 Method for increasing the strength of alloys

Country Status (1)

Country Link
US (1) US1986024A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3052954A (en) * 1959-05-25 1962-09-11 Clevite Corp Method of using a material as a rolling contact bearing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3052954A (en) * 1959-05-25 1962-09-11 Clevite Corp Method of using a material as a rolling contact bearing

Similar Documents

Publication Publication Date Title
US2237434A (en) Heat treatment bath
US1986024A (en) Method for increasing the strength of alloys
US3271206A (en) Short-time heat-treating process for steels
US1943595A (en) Hardened alloy steel and process of hardening same
US2501059A (en) Manufacture of black-heart malleable cast iron
US2614921A (en) Stainless steel and method
US1894836A (en) Metal working alloy
US3116180A (en) Method of producing articles having a cutting edge portion and consisting of stainless chromium steel
US1972241A (en) Steel and method of treating the same
US2201555A (en) Copper and copper base alloys
US2400511A (en) Heat-treatment baths
US2426773A (en) Tempering process for steel objects
US1464174A (en) Air-hardening steel alloy
US2901384A (en) Method for treating cast iron castings
US3219442A (en) Alloy steels and articles thereof
DE671071C (en) Process for improving the ductility of alloys based on iron-cobalt
US2011976A (en) Cobalt-tungsten-iron alloy
JPH0576522B2 (en)
US2486283A (en) Heat-treatment for high carbon high chromium steel
US2105114A (en) Alloy steel tool
DE651164C (en) Process for the production of hard and tough workpieces
US2288999A (en) Gear production
US2195402A (en) Process of making cast tool steel
JPS6244522A (en) Manufacture of high strength ductile cast iron
US2646375A (en) Process for hardening alloy gray cast iron