US2894867A - Method of producing transformation hardenable stainless steel and articles produced therefrom - Google Patents
Method of producing transformation hardenable stainless steel and articles produced therefrom Download PDFInfo
- Publication number
- US2894867A US2894867A US671213A US67121357A US2894867A US 2894867 A US2894867 A US 2894867A US 671213 A US671213 A US 671213A US 67121357 A US67121357 A US 67121357A US 2894867 A US2894867 A US 2894867A
- Authority
- US
- United States
- Prior art keywords
- stainless steel
- nickel
- steel
- chromium
- 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
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
Definitions
- theferrlt formers and austenite formers must be balanced to provide an M, point in the steel which is below room temperature and preferably between about F. and 50 F.
- austenite formers and ferrite formers are balanced to provide an M temperature between about 0 and 50 F. and the chromium, nickel and carbon are within the area ABCD of the drawing, with the balance iron and other elements which do not adversely afiect the properties, annealing said steel at a temperature in the range of 1775 to 1825 F. and quenching it to provide a soft readily formable austenitic structure, and then cooling said annealed steel to below about F. to transform it to a hard martensitic structure.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
Description
% CHROM/UM July 14, 1959 R. SMITH 2,894,867
METHOD OF PRODUCING TRANSFORMATION HABDENABLE STAINLESS STEEL AND ARTICLES PRODUCED THEREFROM Filed July 11, 1957 AN/VEALl/VG' TEMR CHROM/UM 30 x 04,950 NICKEL Ella-. E-
ANNEALl/VG TEMP.
zooo r sum a zb 2 5 ab 8:5 9:0 sla /0:0 I015 //.0 //.5=/z.o
30X CARBON NICKEL INVENTOR RAYMOND sM/m A Home? METHOD OF PRODUCING TRANSFORMATION HARDENABLE STAINLESS STEEL AND ARTI- CLES PRODUCED THEREFROM Raymond Smith, Pittsburgh, Pa., assignor to United States Steel Corporation, a corporation of New Jersey -Applicafion July 11,1957, Serial No. 671,213 12 Claims. (Cl. 148-2155) This invention relates to production of transformation hardenable stainless steel and more particularly to aus- .tenitic stainless steel which is hardenable by low temperature transformation.
' In the construction of modern aircraft, guided missiles and the like, there is needfor steels having good high temperature and, corrosion resistance properties which can be fabricated in the soft austenitic condition and later transformed to the desired minimum hardness of RockwelljC39 or a tensile'strength of 180,000 p.'s.i. Steels which harden by precipitationare unsuitable for prolonged use at temperatures approaching or above the hardening'temperature due-to their tendency to soften. I have found that these desired properties can be'pro- "duced 'by the proper heat treatment of a steel containing about 15 to 18% chromium, about .55 to 1.75% vanadium together with carbon and nickel within certain critical limits as more fully described hereinafter. Such steelhas the following general composition limits:
Percent Carbon .03 to .30 Manganese 5.. .50 to 2.0 "Silic'on a .20 to 1.50 Nickl- 3.0 to 7.5 Chromium 15.0 to 18.0 IVan adium .55 to 1.75
:balance substantially iron and other elements in amounts whichdo not adverselyaftect the properties.
' .Within such limits theferrlt formers and austenite formers must be balanced to provide an M, point in the steel which is below room temperature and preferably between about F. and 50 F. The vanadium content 2,894,867 Patented July 14, 1959 lrange of 700 to 1100 F. and preferably at about 800 F.
to produce a tempered martensitic structure therein.
Figures 1 and 2 of the accompanying drawing which are graphs wherein the ordinates denote the percentage of chromium and the abscissas the sum of the product of 30 times the percentage of carboncontent plus the percentage of nickel. The shaded areas ABCD. and A B C D represent the amounts of chromium and com bined amounts of carbon and nickel which will give the desired results with the particular austenitizing treatment shown. Thus Figure l depicts the best composition for an 1800 F. austenitizing temperature and Figure 2 the composition requiring a 2000 F. austenitizing temperature. Steels having compositions falling to the right of the lines AB, and A 3 do not transform or harden to a satisfactory degree whereas those falling to the left of the lines CD, and C D transform and harden upon cooling to room temperature after annealing.
The following Table I lists the composition of a numher of heats which are illustrative of the steels of my invention: Table 1 Heat 0 M11 P 8 s1 N1 Or V 801.
The eifect of various annealing temperatures on these is shown in the following Table II.
, Table -II V 15 Min. 1,800 F., W.Q.' 15 Min. 1,900 F., W.Q. 15 M1n.2,000 F., W.Q. 15 Min. 2,050 F., W.Q.
Rockwell Hardness Rockwell Hardness Rockwell Hardness Rockwell Hardness 7 Heat Annealed 2 Hr. 1l0 F. Annealed 2 Hr. -1l0 F. Annealed 2 Hr. 1l0 F. Annealed 2 Hr. F. +2 Hr. 800 F. +2 Hr. 800 F. +2 Hr. 800 F. +2 Hr. 800 F.
033. 5 C40. 0 B96. 0 G43. 5 B98. 5 C 39. 6 B94. 0 C45. 0 C38. 5 C44. 0 B96. O 045. 0 B95. 0 044. 0 B95. 0 C43. 0 043. 5 C43. 0 B97. 0 C46. 5 B92. 5 C42. 5 B94. 0 045. 0 C31. 0 G47. 0 B99. 0 C47. 0 B91. 5 C45. 0 B91. 5 047. 0 044. 0 C47. 5 034. 0 046. 0 021. 5 C46. 0 B95. 5 042. 0 038. 5 047. 5 C36. 0 047. 0 B98. 5 C40. 5 B98. 5 036. 5
The following Table 111 lists certain steels which were martensit'ic'as annealed.
Table III Heat Mn P 8 s1 N1 Or V 501.
Typical steels which were austenitic as annealed and *Showed -15% delta ferrite in annealed condition.
A preferred embodiment of the steel of my invention for developing hardness value in excess of C'45 or tensile strengths in excess of 220,000 p.s.i. contains Percent Carbon .15 to .26
Manganese .75 to 1.20 Silicon .35 to .75 Nickel 3.40 to 5.6 Chromium 16.0 to 17.3 Vanadium .60 to 1.20
Steels of this composition should fall within the area A B C D of Figure 2 and annealed in the range of 1975 to 2025 F., i.e. at about 2000 F., transformed by cooling "to about -110 F. Thereafter such steels may be tempered in the range of 700 to 1100" F. and preferably at about 800 F. to produce the maximum properties. As indicated, such steels will have a Rockwell C value in excess of 45 or tensile strengths in excess of 220,000. Moreover, they are soft and ductile in the annealed condition.
If lower strengths and hardnesses are desired with attendant improvement in'ductile properties the following composition having lower carbon and higher nickel contents in conformity with the area ABCD of Figure l of the drawing may be used:
Percent Carbon .04 to .12 Manganese .75 to 1.20 Silicon .35 to .75 Nickel 4.7 to 7.0 Chromium 15. to 17.8 Vanadium .60 to 1.20
these embodiments are merely for the purpose of illustration and description and that various other f m may be devised within the scope of my invention, as defined in the appended claims.
I claim:
1. Stainless steel characterized by being transformable to a hard martensitic structure by sub-zero treatment from a soft austenitic structure in the annealed condition which can be tempered to improve the ductility thereof, said steel containing Percent Carbon .03 to .30 Manganese .50 to 2.00 Silicon .20 to 1.5 Nickel 3.0 to 7.5 Chromium 15.0 to 18.0 Vanadium .55 to 1.75
the ferrite formers being balanced to provide an M temperature between about0 F. and 50 F. with theremainder iron and other elements "in amounts which do not adversely affect the properties.
2. Stainless steel characterized by being transformable to a hard martensitic structure from a soft austenitic structure in the annealed condition which can be tempered to improve the ductility thereof, said steel containing Percent Carbon .15 to .26 Manganese .75 to 1.2 Silicon .35 to .75 Nickel 3.4 to 5i6 Chromium --16.0to 17.3 Vanadium .6 to -1.2
Percent Carbon .04 to .12 Manganese .75 to 1.2 Silicon .35 .to'.75 Nickel 4.7 to 7.0 Chromium .15 .0 to 17-8 Vanadium .6 to "1.2
the ferrite formers and the austenite formers being balanced to provide an M temperature between about 0 and 50 F. with the balance iron and other elements in amounts which do not adversely affect the properties.
4. Thermally hardened articles composed of'stainless steel containing Percent Carbon .03 to .30 Manganese .50 to 2.0 Silicon .20 to 1.5 Nickel 3.0 to 7.5 Chromium 15.0 to 18.0 Vanadium .55 to 1.75
wherein the austenite and ferrite formers are balanced -to provide an M temperaturebetween about 0 and 50 F. with the balance iron and other elements in amounts which do not adversely affect the properties, said steel having been annealed'at a temperature in the range of 1700" to 2100 F. and quenched to provide a soft austenitic readily formable structure and thereafter hardened by cooling it to below about -1 00 F. to transform it to a hard martensitic structure. g
5. Thermally hardened steel articles l'characterizedby a tensile strength inexcess .of 220,000 p.s.i. composed of stainless steel containing Per Carbon I .15 to .26 Manganese .75 to 1.20 Silicon "'.35to.75 Nickel I s I 3.40 to 5.6 Chromium 16.0 to 17.3 Vanadium ,.6.to 1.2
wherein the austenite formers and ferrite formers are balanced to provide an M temperature between about and -50 F. and the chromium, nickel and carbon are within the area A B C D of the drawing, with the balance iron and other elements in amounts which do not adversely afiect the properties, said steel having been annealed at a temperature in the range of 1975 to 2025 F. and quenched to provide a soft austenitic easily formable structure and thereafter hardened by cooling to below about -100 F. to transform it to a hard martensitic structure.
6. Thermally hardened steel articles composed of stainless steel containing wherein the austenite formers and ferrite formers are balanced to provide an M, temperature between about 0 and 50 F. and the chromium, nickel and carbon are within the area ABCD of the drawing with the balance iron and other elements in amounts which will not adversely afiect the properties, said steel having been annealed at a temperature in the range of 1775 to 1825 F. and quenched to provide a soft readily formable austenitic structure and thereafter hardened by cooling to below about -100 F. to transform it to a hard martensitic structure.
7. A method of producing hardened stainless steel comprising making stainless steel containing Percent Carbon .03 to .30 Manganese .50 to 2.0 Silicon .20 to 1.5 Nickel 3.0 to 7.5 Chromium 15.0 to 18.0 Vanadium .55 to 1.75
Percent Carbon .15 to .26 Manganese .75 to 1.2 Silicon .35 to .75 Nickel 3.4 to 5.6 Chromium 16.0 to 17.3 Vanadium .6 to 1.2
wherein the austenite formers and ferrite formers are balancedto provide an M temperature between about ,0 and '--50 F. and the chromium, nickel and carbon are within the area A B C D of the drawing, with thebalance iron and other elements which do not adversely affect-the properties, annealing said steel at a temperature in the range 1975 to 2025 F., quenching it to provide a soft readily formable austenitic structure and then cooling said annealed steel to below about -'-100 F. to transform it to a hard martensitic structure.
9. A method of producing hardened stainless steel comprising making stainless steel containing 'Percent .04 to .12 .75 to 1.20
wherein the austenite formers and ferrite formers are balanced to provide an M temperature between about 0 and 50 F. and the chromium, nickel and carbon are within the area ABCD of the drawing, with the balance iron and other elements which do not adversely afiect the properties, annealing said steel at a temperature in the range of 1775 to 1825 F. and quenching it to provide a soft readily formable austenitic structure, and then cooling said annealed steel to below about F. to transform it to a hard martensitic structure.
10. A method of producing articles of hardened stainless steel comprising making stainless steel containing Percent .03 to .30 .50 to 2.0
the ferrite formers and the austenite formers being balanced to provide an M temperature between about 0 and 50 F., with the balance iron and other elements in amounts which do not adversely affect the properties, annealing said steel at a temperature in the range of 1700 to 2100 F., quenching it to provide a soft austenitic readily formable structure, forming the desired articles therefrom and then cooling said annealed steel articles to below about 100 F. to transform the steel thereof to a hard martensitic structure.
11. A method of producing articles of hardened stainless steel comprising making stainless steel containing Percent .15 to .26 .75 to 1.2 .35 to .75 3.4 to 5.6 16.0 to 17.3 .6 to 1.2
*wherein the austenite formers and ferrite formers are balanced to provide an M temperature between about 0 and -50 F. and the chromium, nickel and carbon are within the area A B C D of the drawing, with the balance iron and other elements which do not adversely affect the properties, annealing said steel at a temperature in the range of 1975 to 2025 F., quenching it to provide a soft readily formable austenitic structure, forming the desired articles therefrom and then cooling said annealed steel articles to below about 100 F. to transform the steel thereof to a hard martensitic structure.
7 -l2r. ,-A method of producing articles of hardened stainless steel comprising making stainless steel containing I "Percent Carbon .04 to-.12 'Manganese 75 to 1.20 'Silicon .35 to .75
Nickel 4.7'to37.0 chromium 15;0 to $17.8 Vanadium -e 56101.2
wherein the austenite formers and ferrite formers are balanced to provide an M temperature betweenabout O and 50 F. and the chromium, nickel and carbon are the range of 177510182 5 and quenching-it to provide a soft "readily formabl'e austenitic structure, forming the desired articles therefrom, andthen cooling said annealed steel articles to below about l00 F. to transform the steel thereof to a hard martensitic stmcture.
iR efei-ences Cited in the file of this patent UNITED STATES PATENTS Binder July 31, 1951 "Lena July 16, 1957
Claims (1)
1. STAINLESS STEEL CHARACTERIZED BY BEING TRANSFORMABLE TO A HARD MARTENSITIC STRUCTURE BY SUB-ZERO TREATMENT FROM A SOFT AUSTENITIC STRUCTURE IN THE ANNEALED CONDITION WHICH CAN BE TEMPERED TO IMPROVE THE DUCTILITY THEREOF, SAID STEEL CONTAINING
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US671213A US2894867A (en) | 1957-07-11 | 1957-07-11 | Method of producing transformation hardenable stainless steel and articles produced therefrom |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US671213A US2894867A (en) | 1957-07-11 | 1957-07-11 | Method of producing transformation hardenable stainless steel and articles produced therefrom |
Publications (1)
Publication Number | Publication Date |
---|---|
US2894867A true US2894867A (en) | 1959-07-14 |
Family
ID=24693578
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US671213A Expired - Lifetime US2894867A (en) | 1957-07-11 | 1957-07-11 | Method of producing transformation hardenable stainless steel and articles produced therefrom |
Country Status (1)
Country | Link |
---|---|
US (1) | US2894867A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2503461A (en) * | 1946-06-17 | 1950-04-11 | Louis J Weber | Constant speed propeller |
US2990275A (en) * | 1958-09-19 | 1961-06-27 | Union Carbide Corp | Hardenable stainless steel alloys |
US3108870A (en) * | 1960-06-21 | 1963-10-29 | United States Steel Corp | High-strength age-hardenable stainless steel |
US3152934A (en) * | 1962-10-03 | 1964-10-13 | Allegheny Ludlum Steel | Process for treating austenite stainless steels |
US3377162A (en) * | 1964-09-10 | 1968-04-09 | Rand Mines Ltd | Stainless steel |
US3819428A (en) * | 1971-04-22 | 1974-06-25 | C Moore | Metal treatment |
FR2698104A1 (en) * | 1992-11-19 | 1994-05-20 | Creusot Loire | Stainless steel with high temp. stability - contg. vanadium@ which replaces some chromium@ |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2562854A (en) * | 1949-04-22 | 1951-07-31 | Union Carbide & Carbon Corp | Method of improving the high-temperature strength of austenitic steels |
US2799602A (en) * | 1956-10-04 | 1957-07-16 | Allegheny Ludlum Steel | Process for producing stainless steel |
-
1957
- 1957-07-11 US US671213A patent/US2894867A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2562854A (en) * | 1949-04-22 | 1951-07-31 | Union Carbide & Carbon Corp | Method of improving the high-temperature strength of austenitic steels |
US2799602A (en) * | 1956-10-04 | 1957-07-16 | Allegheny Ludlum Steel | Process for producing stainless steel |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2503461A (en) * | 1946-06-17 | 1950-04-11 | Louis J Weber | Constant speed propeller |
US2990275A (en) * | 1958-09-19 | 1961-06-27 | Union Carbide Corp | Hardenable stainless steel alloys |
US3108870A (en) * | 1960-06-21 | 1963-10-29 | United States Steel Corp | High-strength age-hardenable stainless steel |
US3152934A (en) * | 1962-10-03 | 1964-10-13 | Allegheny Ludlum Steel | Process for treating austenite stainless steels |
US3377162A (en) * | 1964-09-10 | 1968-04-09 | Rand Mines Ltd | Stainless steel |
US3819428A (en) * | 1971-04-22 | 1974-06-25 | C Moore | Metal treatment |
FR2698104A1 (en) * | 1992-11-19 | 1994-05-20 | Creusot Loire | Stainless steel with high temp. stability - contg. vanadium@ which replaces some chromium@ |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR100767834B1 (en) | Method for producing precipitate hardened martensitic steel products, steel products obtained by this method | |
CN106244918A (en) | A kind of 1500MPa level high strength and ductility automobile steel and manufacture method thereof | |
US2894867A (en) | Method of producing transformation hardenable stainless steel and articles produced therefrom | |
GB1026257A (en) | Stainless steel | |
US3539404A (en) | Method of making a low alloy steel | |
US3093518A (en) | Nickel alloy | |
US3423252A (en) | Thermomechanical treatment of steel | |
US2506558A (en) | Stainless steel and method | |
US3392065A (en) | Age hardenable nickel-molybdenum ferrous alloys | |
US2892702A (en) | Hardenable stainless steel | |
US3795507A (en) | Semi-austenitic cr-ni-al-cu stainless steel | |
US2664369A (en) | Method of softening low-carbon medium-alloy steel | |
US3770426A (en) | Cold formable valve steel | |
KR960705953A (en) | Bainite steel with little scattering and manufacturing method | |
US3385740A (en) | Weldable and hardenable steel and method of producing same | |
US3438822A (en) | Method of making fine-grained steel | |
GB1583786A (en) | Precipitation hardenable stainless steel | |
US3834948A (en) | Ductile,weldable high-strength-steel wire and method for producing same | |
JPS60106952A (en) | Process hardenable stainless steel of substantially austenite and manufacture | |
JPH0448050A (en) | Spring steel strip | |
US3083095A (en) | Alloy steel and method | |
US2854330A (en) | Stainless steel and method | |
GB1022845A (en) | Heat treatment process for ferrous base alloy members | |
JPS5873717A (en) | Production of low temperature steel | |
US2853381A (en) | Steel responsive to austempering |