US2395608A - Treating inherently precipitationhardenable chromium-nickel stainless steel - Google Patents

Treating inherently precipitationhardenable chromium-nickel stainless steel Download PDF

Info

Publication number
US2395608A
US2395608A US513748A US51374843A US2395608A US 2395608 A US2395608 A US 2395608A US 513748 A US513748 A US 513748A US 51374843 A US51374843 A US 51374843A US 2395608 A US2395608 A US 2395608A
Authority
US
United States
Prior art keywords
chromium
steel
treating
inherently
stainless steel
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
US513748A
Inventor
Robert H Aborn
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.)
United States Steel Corp
Original Assignee
United States Steel Corp
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 United States Steel Corp filed Critical United States Steel Corp
Priority to US513748A priority Critical patent/US2395608A/en
Application granted granted Critical
Publication of US2395608A publication Critical patent/US2395608A/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
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni

Definitions

  • This invention is a method of treating chromium-nickel stainless steel containing carbon and at least one of the'elements, such as titanium, columbium, vanadium, etc., which form a carbide more stable than chromium carbide.
  • This type of steel usually contains aluminum, and the amount of those alloying elements which are ferrite formers other than the named carbide formers is proportioned to the amount of those whichare austenite formers so as to 30% titanium and .15% aluminum.
  • the steel was rendered completely austenitic except for some stable delta ferrite by heating it to 2050 F..
  • the steel after which it was cooled in the furnace to 250 F. in forty-two hours, it thereafter being air cooled to room temperature, the steel having been in 18 gage sheet form so that air cooling provided bring about the formation of stress-laden martensite at a relatively low temperature such as room temperature; when the steel cools from a relatively high temperature at which it is austenitic.
  • This stress-laden martensitic structure of the metal is inherently precipitationhardenable and increases in hardness to a level depending on the temperature to which it is reheated and the time at temperature; but prior to this reheating, the structure has suflicient ductility to permit some degree of cold forming of the metal.
  • the present invention is a method of treating steel of this type by converting it to austenite and then cooling it in such a way that it remains temporarily as an austenitic or austenitic-like structure when it reaches room temperature.
  • This temporary structure is more ductile and permits a far greater degree of cold forming than the precipitation-hardenable martensitic-like condition to which "it ultimate transforms, but only after an interval long enough to permit the completion of the desired forming operations.
  • the steel is heated to austenitize it and is then cooled slowly to temperatures slightly above those producing the stress-laden transformation product, whereupon it is cooled more rapidly to room temperature at a rate preventing any substantial amount of transformation, whereby the steel remains austenitic or in an austenitic-like condition for a substantial time at room temperature.
  • the transformation may be hurried by exposure to other temperatures.
  • the treatment has been applied to the steel when it contains 17% chromium,7% nickel, .06% carbon,
  • the austenitizing temperature may range from 1700" to 2000 F., and the temperature to which the ing, or, in the case of sections having such mass as to render this inadequate, by water quenching.
  • the steel is substantially nonmagnetic, since it appears to be essentially austenitic, and at ordinary room temperature it may remain unchanged for a period of several hours.
  • the resulting struc ture may then be mainly austenitic but it will remain in this condition only a few minutes at most. It follows that the slow cooling to a temperature slightly above that at which the austenite would normally transform to the marte nsitic or martensitic-like structure is necessary, the transformation then being prevented by adequately fast cooling to room temperature. 5
  • said method comprising heating the steel to austenitize it, cooling it slowly to temperatures slightly above those producing said martensite or martensitic like structure, and then rapidlycooling the steel' to'room' temperature at a rate preventing any substantial degree of transformation, whereby the steel remains essentially austenitic for a substantial time at room temperature.

Description

- atented Feb. 26, 1946 TREATING INHER-ENTLY PRECIPITATION- HARDENABLE CHROMIUM-N ICKEL STAINr' LESS STEEL Robert H. Aborn, Short mus; N. J.,,assignor to United States Steel Corporation of Delaware, 7
a corporation of Delaware a Na Drawing. Application December 10, 1943,
Serial No. 513,748
.2 Claims. (Cl. 14s-21.55)
This invention is a method of treating chromium-nickel stainless steel containing carbon and at least one of the'elements, such as titanium, columbium, vanadium, etc., which form a carbide more stable than chromium carbide. This type of steel usually contains aluminum, and the amount of those alloying elements which are ferrite formers other than the named carbide formers is proportioned to the amount of those whichare austenite formers so as to 30% titanium and .15% aluminum. The steel was rendered completely austenitic except for some stable delta ferrite by heating it to 2050 F..
after which it was cooled in the furnace to 250 F. in forty-two hours, it thereafter being air cooled to room temperature, the steel having been in 18 gage sheet form so that air cooling provided bring about the formation of stress-laden martensite at a relatively low temperature such as room temperature; when the steel cools from a relatively high temperature at which it is austenitic. This stress-laden martensitic structure of the metal is inherently precipitationhardenable and increases in hardness to a level depending on the temperature to which it is reheated and the time at temperature; but prior to this reheating, the structure has suflicient ductility to permit some degree of cold forming of the metal.
The present invention is a method of treating steel of this type by converting it to austenite and then cooling it in such a way that it remains temporarily as an austenitic or austenitic-like structure when it reaches room temperature. This temporary structure is more ductile and permits a far greater degree of cold forming than the precipitation-hardenable martensitic-like condition to which "it ultimate transforms, but only after an interval long enough to permit the completion of the desired forming operations.
According to this invention the steel is heated to austenitize it and is then cooled slowly to temperatures slightly above those producing the stress-laden transformation product, whereupon it is cooled more rapidly to room temperature at a rate preventing any substantial amount of transformation, whereby the steel remains austenitic or in an austenitic-like condition for a substantial time at room temperature. During perature and the conditions of cooling or if desired, the transformation may be hurried by exposure to other temperatures.
As a specific example of the invention, the treatment has been applied to the steel when it contains 17% chromium,7% nickel, .06% carbon,
an adequately fast 'cooling'method. By such treatment test reports showed that a maximum Olsen value of 0.500" wasreadily obtained,'the normal Olsen value being 0.250" when the steel was austenitized at 1900 F. and air cooled to room temperature.
In making the commercial form of this steel, it will have only approximately the range of alloying elements noted, with the usual balance of iron and impurities, and in such instances the austenitizing temperature may range from 1700" to 2000 F., and the temperature to which the ing, or, in the case of sections having such mass as to render this inadequate, by water quenching. After the treatment the steel is substantially nonmagnetic, since it appears to be essentially austenitic, and at ordinary room temperature it may remain unchanged for a period of several hours. If the steel is water quenched to room temperature from the high temperature where it is'fully austenitic, except for some delta'fer rite which may be present, the resulting struc ture may then be mainly austenitic but it will remain in this condition only a few minutes at most. It follows that the slow cooling to a temperature slightly above that at which the austenite would normally transform to the marte nsitic or martensitic-like structure is necessary, the transformation then being prevented by adequately fast cooling to room temperature. 5
. I claim: I i
1. A method of treating chromium-nickel stainless steel containing carbon and at least one of the stronger-than-chromium carbide formers such as titanium, columbium, vanadium, etc.,
with its components that are ferrite formers other than said carbide formers proportioned to those that are austenite formers to cause the production of an inherently precipitation-hardenablestress-laden martensite or martensitic-like structure at low temperatures when the steel cools to room temperature from high temperatures where it is essentially austenitic, said method comprising heating the steel to austenitize it, cooling it slowly to temperatures slightly above those producing said martensite or martensitic like structure, and then rapidlycooling the steel' to'room' temperature at a rate preventing any substantial degree of transformation, whereby the steel remains essentially austenitic for a substantial time at room temperature.
2. A method of treating chromium-nickel stainless steel approximately containing 17% chromium, 7% nickel, .06% carbon, .8 0 titamum, and .15% aluminum, with its components that are ferrite formers proportioned to those that are austenite formers to causethe production or stress-laden martensite or martensiticaccuses like product,
ROBERT H. ABORN.
US513748A 1943-12-10 1943-12-10 Treating inherently precipitationhardenable chromium-nickel stainless steel Expired - Lifetime US2395608A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US513748A US2395608A (en) 1943-12-10 1943-12-10 Treating inherently precipitationhardenable chromium-nickel stainless steel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US513748A US2395608A (en) 1943-12-10 1943-12-10 Treating inherently precipitationhardenable chromium-nickel stainless steel

Publications (1)

Publication Number Publication Date
US2395608A true US2395608A (en) 1946-02-26

Family

ID=24044530

Family Applications (1)

Application Number Title Priority Date Filing Date
US513748A Expired - Lifetime US2395608A (en) 1943-12-10 1943-12-10 Treating inherently precipitationhardenable chromium-nickel stainless steel

Country Status (1)

Country Link
US (1) US2395608A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2685546A (en) * 1952-01-05 1954-08-03 Atomic Energy Commission Method for reducing the permeability of alloys by hydrogen
US3235415A (en) * 1961-12-28 1966-02-15 Gen Electric Heat treatment and alloy
US3260979A (en) * 1963-12-11 1966-07-12 Lionel E Leavitt Through-wall electromagnetic coupling
US3658514A (en) * 1968-10-08 1972-04-25 Allegheny Ludlum Steel Martensitic steel
US4042423A (en) * 1975-12-03 1977-08-16 Union Carbide Corporation Method for providing strong wire and strip
US4042421A (en) * 1975-12-03 1977-08-16 Union Carbide Corporation Method for providing strong tough metal alloys
US4204885A (en) * 1979-03-21 1980-05-27 Union Carbide Corporation Method for providing strong wire
US6273968B1 (en) 1999-07-12 2001-08-14 Mmfx Steel Corporation Of America Low-carbon steels of superior mechanical and corrosion properties and process of making thereof

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2685546A (en) * 1952-01-05 1954-08-03 Atomic Energy Commission Method for reducing the permeability of alloys by hydrogen
US3235415A (en) * 1961-12-28 1966-02-15 Gen Electric Heat treatment and alloy
US3260979A (en) * 1963-12-11 1966-07-12 Lionel E Leavitt Through-wall electromagnetic coupling
US3658514A (en) * 1968-10-08 1972-04-25 Allegheny Ludlum Steel Martensitic steel
US4042423A (en) * 1975-12-03 1977-08-16 Union Carbide Corporation Method for providing strong wire and strip
US4042421A (en) * 1975-12-03 1977-08-16 Union Carbide Corporation Method for providing strong tough metal alloys
US4204885A (en) * 1979-03-21 1980-05-27 Union Carbide Corporation Method for providing strong wire
US6273968B1 (en) 1999-07-12 2001-08-14 Mmfx Steel Corporation Of America Low-carbon steels of superior mechanical and corrosion properties and process of making thereof

Similar Documents

Publication Publication Date Title
US2905577A (en) Creep resistant chromium steel
GB936872A (en) Improvements in or relating to a process of heat treating austenitic stainless steel and austenitic stainless steels whenever prepared by the aforesaid process
US2395608A (en) Treating inherently precipitationhardenable chromium-nickel stainless steel
US3917492A (en) Method of making stainless steel
US3337376A (en) Method of hardening hypereutectoid steels
US2797993A (en) Stainless steel
US2934463A (en) High strength steel
US3067072A (en) Method of annealing type 430 stainless steel
US3488231A (en) Treatment of steel
US2664369A (en) Method of softening low-carbon medium-alloy steel
US2799602A (en) Process for producing stainless steel
US3278345A (en) Method of producing fine grained steel
US1943595A (en) Hardened alloy steel and process of hardening same
US3730785A (en) Dual strength blade of 17-4ph stainless steel
US3223562A (en) Heat treating process for martensitic transformation alloys
US2024561A (en) Heat treatment of chromium alloy steels
US2390023A (en) Treating inherently aging chromium-nickel stainless steel
GB1070465A (en) Weldable tough steel containing chromium and manganese and method of manufacturing the same
US3266947A (en) Method of heat treating alloy steel rotor forgings
US3708280A (en) High temperature low alloy steel
US3388011A (en) Process for the production of high strength steels
US2381416A (en) Age hardenable chromium-nickel stainless steel
KR830004429A (en) Manufacturing method of spheroidized annealed steel wire
US3235415A (en) Heat treatment and alloy
US2365956A (en) Thermally hardening steel