|Publication number||US2482097 A|
|Publication date||Sep 20, 1949|
|Filing date||Jul 27, 1944|
|Priority date||Jul 27, 1944|
|Publication number||US 2482097 A, US 2482097A, US-A-2482097, US2482097 A, US2482097A|
|Inventors||Charles Clarke William|
|Original Assignee||Armco Steel Corp|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (7), Referenced by (10), Classifications (7)|
|External Links: USPTO, USPTO Assignment, Espacenet|
@atented fiept, 20, i949 STATES PATENT OFFICE by mesne assignments,
to Armco Steel Corporation, a corporation of Ohio No Drawing. Application July 27, 1944, Serial No. 546,927
This application is a companion to my copending application, Serial No. 546,926, filed of even date herewith and entitled Alloy and method, and the invention relates to chromium-nickel stainless steels and to a method for conditioning the same for hardening as well as to pre-hardened and precipitation-hardened products or manufactures thereof.
An object of my invention is the provision of chromium-nickel stainless steels that are suited to hardening at low temperature.
Another object is the provision of a commercially practical method for conditioning such steels wherein, by annealing, the alloys are rendered highly suitable for a wide variety of fabricating .operations and, in which method, by subsequent double hardening treatment, the alloys are transformed and precipitation-hardened in a thoroughly effective manner.
A further object of my invention is the provision of chromium-nickel stainless steel products which are precipitation-hardened from soft, formable and machinable condition, and which as hardened possess high tensile and compressive values and have reasonably high ductility together with freedom from substantial directional eflects which characterize the usual cold-rolled chromium-nickel stainless steel sheet and strip.
Other objects of my invention in part will be obvious and in part pointed out hereinafter.
The invention accordingly consists in the combinatlon of elements, composition of materials, and conditions of treatment, and in the various steps, and the relation of each of the same to one or more of the others as described herein, the scope of the application of which is indicated in the following claims. 7
As conducive to a clearer understanding of certain features of my invention, it may be noted at this point that stainless steels are defined as low-carbon steels which comprise 10% to 35% chromium, with or without nickel, and with or without supplemental additions of copper, manganese, silicon, cobalt, molybdenum, tungsten, vanadium, titanium, columbium, sulphur, and the like, for special purposes, and a remainder which is substantially all iron. The carbon content may range from 0.03% to 0.20%, or more where desired.
There are among the stainless alloys certain chromium-nickel stainless steels, particularly those which are classifiable with the more commonly known 18% chromium-8% nickel grades, which remain stably austenitic at room temperatures after quenching, and in no manner are 7 Claims. ($31. 148-2154) hardenable by heat treatment. These steels are work-hardenable, however, which in many instances is not a satisfactory property for the provision of hardened products. Because of other more favorable properties, however, the steels are in widespread demand for fabrication into products by such methods as hot-working, cold-forming, machining, punching, drilling, drawing or spinning. A further difficulty, however, arises as a result of rolling or drawing the metal; troublesome directional effects are notable especially a loss in compression along the direction of rolling or drawing. After fabrication, the steels are put into use either in soft strain-relieved condition, or in the work-hardened condition when feasible.
Some efiort has been made in the prior art to provide stainless steels which are hardenable by heating to a temperature low enough to avoid or minimize oxidation and undue distortion. This effort has been to realize a precipitation, at this relatively low temperature, of a critically disbursed phase. An analogy presents itself in the case of the well-known aluminum alloys.
For example, in the prior art, it has been suggested to use titanium or columbium as hardening agents for chromium-nickel stainless steels. Such precipitation hardenable alloys have been disappointing either because the expected results are not actually obtained, or because of difliculties encountered in obtaining products of consistently uniform and reliable properties. "Moreover, titanium is difiicult to control in amount due to erratic recovery in the steel melting operation, and presents a very serious difficulty in the case of products to be welded because of the loss of titanium during the welding operation.
An outstanding object of my invention accordingly is the provision of chromium-nickel stainless steels which lend themselves to ready fabrication in sheet, strip, bar, wire and other forms into a host of products which subsequently are hardened at low temperature with minimum scaling and discoloration, and without warping, which steels and products fashioned thereof are characterized by other desirable properties in both pre-hardened and hardened condition.
Referring now more particularly to the practice of my invention, I find that by closely correlating the chromium and nickel contents of the steel, and in addition including the ingredient copper in critical amounts, a stainless steel which is susceptible to precipitation-hardening is had. This result is new and surprising. My stainless steel comprises about 16.5% to approximately conditioning treatment 18.5% chromium, nickel in an approximate range of 4.75% to 5.60%, copper'in amounts between about 3.5 and approximately 5.0%, carbon preferably not exceeding about 0.1%, and the remainder substantially all iron. Also I find that certain further benefits are had by including in the composition one or more elements of the group consisting of beryllium from traces up to around 0.25%.
By subjecting my stainless steels to a special the alloys are found to retain a characteristic high temperature coppersoluble austenitic structure down to about room temperature. These alloys then are hardened by transformation and the precipitation of copper from solid solution. I
The special conditioning treatment of my invention includes holding wrought or cast stainless steel of the particular composition just described within a temperature range of aboutl'l00" F. extending up to around 2000 F., a temperature of approximately 1800 F. being preferred. This treatment serves to place the metal in an austenitic copper-soluble condition which is retainable down to at least about room temperature. The period of holding at high temperature is not too critical, a period of about y hour is preferred. Usually for this treatment the metal is adjusted to temperature in a suitable heat-treating furnace and is held therein at temperature for the necessary period. I then quench the metal as in air, oil or water to around room temperature, as at quenching rate of about 400 F. per minute, and thus provide an annealed or pre-hardened copper-soluble alloy which retains an austenitic structure much in a manner as do 18% chromium- 8% nickel austenitic stainless steels after similar treatment. As quenched, the alloys are reasonably ductile, have good directional qualities and hardnesses usually below about Rockwell B100. In addition they are formable and machinable, one or more of which properties contribute in making it possible to fabricate the metal at this point into any of a wide variety of pre-hardened products.
From the quenched or pre-hardened chromiumnickel-copper stainless steels, which now are precipitation hardenable by subsequent treatment to be described, I provide products in such forms as bars, wire, rounds, sheet, strip or plate. Also, I may provide shapes which are more intricate, illustratively trim, structural members or the like as for the aircraft industries, cold-headed bolts and screws requiring hard shanks, shafting, surgical instruments, valves and valve seats. In all of these advantage is taken of excellent workin and forming properties of the pro-hardened metal such as cold-forming, upsetting, drawing, spinning, machining, stamping, punching, cutting, and the like which are consistent with the properties of the metal.
After the pre-hardening treatment and fabricating operation have been achieved, I subject the chromium-nickel-copper stainless steel to either one of two preliminary heat-exchange hardening treatments. As a first and preferred alternative, I reheat the metal, illustratively in the same heat-treating furnace employed in the high temperature treatment, so as to bring the transformation point of the austenitic to the ferritic condition above ordinary room temperature. In this treatment the metal is held at 1250-1600 F., preferably at about 1400 F., from about five minutes up to six hours or more. A three-quarter hour period as an approximate figure is found cipitation of a copper-rich phase.
4 to be most practical and, therefore, is preferred. Followin the reheating stay the metal is cooled as in air or water with the result that transformation does occur 'above room temperature.
The transformation noted produces a chromium-nickel martensitic structure and partial pre- Hardnesses after this transformation vary in or near the range of Rockwell C33 to C37 depending upon the exact composition and the particular conditions of treatment within the limits defined herein.
As an alternative, instead of reheating in the manner described, I employ a preliminary hardening treatment which involves cooling the prehardened metal to effect transformation below usual room temperatures. In the practice of this alternative, I hold the pre-hardened metal, as in fabricated condition, in a suitable cooling compartment, or the like, at cooling temperatures of about 32 F. to F. or lower for such periods of time as to effect transformation. Usually at least hour at cooling temperature, as in dry ice and/ or acetone for the cooling medium, is preferred.
When transformation has been achieved either through reheating and quenching or by low temperature conditioning as described, the alloys then are ready for positive precipitation-hardening which as an operation forms a second step of my hardening treatment. In performing this second step I heat the alloys, as in the form of fabricated products, within a temperature range of about 850 F. to approximately 950 F., preferably at about 900 F., and hold the same at temperature for about V2 hour. The time of treatment, however, may vary from approximately fifteen minutes to two hours without excessive under-aging or over-aging. This treatment serves to give substantially complete precipitation of a copper-rich phase throughout the metal grains. The copperrich precipitate is not visible under an ordinary light microscope, but I find that it can be photographed with the aid of an electron microscope. It is this precipitated copper-rich phase which gives the hardness.
Following the heating at hardening temperature the steels and products thereof are advantageously quenched to room temperature. In the hardened condition, as after quenching, the alloys display high values both in tension and compression, high yield strength, good directional qualities, 9, reasonable degree of ductility, and good hardness, this latter usually falling in or near the range of Rockwell C37 to C44. The alloys and products thereof also are quite resistant to salt spray and to corrosion in ordinary atmosphere, both before and after hardening.
As a further feature of my invention I provide welded joints and welded products from the chromium-nickel-copper stainless steels disclosed herein and treat the metal, including the weld, in accordance with my initial high temperature annealing and subsequent double-hardening treatments. In order to afford a beneficial source of weld addition metal, I also provide weld rods which include as filler or deposit metal the chromium-nickel-copper alloy metal disclosed.
My stainless steels are weldable by are, gas, spot, or otherweldlng methods without substantial loss of copper, which is an important advantage remembering that alloys which contain aluminum, titanium, or the like to promote 76 the precipitation-hardening efiect suffer a loss the hardening material in the welding operation.
iii the broad group of chromium-nickel-copper stainless steels noted hereinbefore I prefer in particular those which include, in approximate percentages, 16.5% to 17.5% chromium, 4.85% to 5.35% nickel, 3.60% to 4.35% copper, and carbon up to 0.08%. To illustrate certain properties which are obtainable with this more specific group of alloys, 9, table is given below. All values given for annealed condition refer to one-half hour treatment at 1800 F. followed by water-quenching, while the values noted for hardened condition refer to this form of annealing treatment followed by three-quarter hour treatment at 1400" F. and water-quenching coupled with one-half hour treatment at 900 F. and water-quenching.
2. In a method of precipitation hardening lowcarbon chrominum-nickel stainless steel, providing a steel containing about 16.5% to 18.5% chromium, about 4.75% to 5.60% nickel, copper between about 3.5% and 5.0%, and the remainder substantially all iron; rendering said alloy in a stable austenitic condition at about room temperature through suitable heating and quenching; then heating said alloy within a temperature range of about 1300 F. to 1500 F. and quenching the same to efiect transformation thereof; and finally heating the transformed alloy within a temperature range of about 850 F. to 950 F. to precipitate copper and obtain an increase in the alloy hardness.
3. In a method of precipitation-hardening lowcarbon chromium-nickel stainless steel, providing a steel containing about 16.5% to 18.5%
Table Rockwell Brinell Ult. Tens. 5a., 0.2% Yield 8tr., 2- g Hardness Hardness p. a. i. p. s. i. 68m g gg 1880-100 150-240 120,000 to 140,000 30,000 to 45,000 mm 40 tom r l fi 030-44 012-410 180,000 to 000,000 100,000 to 1 a to 15 35 to 55 The hardened chromium-nickel-copper stainless steels which include beryllium, as from traces up to around 0.25%. are characterized by higher ultimate tensile strength, greater yield strength and higher flnal hardnesses than the figures given above. Such steels are especially suitable for cutting tools, dies, hard balls, and the like. The beryllium contributes as a second precipitation-hardening agent to the hardening eflect of the copper.
Thus it will be seen that there is provided in this invention a chromium-nickel stainless steel suited for hardening by heat treatment, as well as a method of precipitation-hardening these steels, in which the various objects hereinbefore noted together with many thoroughly practical advantages are successfully achieved. It will be seen that the method makes possible the provision from chromium-nickel stainless steels which can be cast, welded, or wrought, or subjected to a number of forming, machining or fabricating operations, products which are hard yet which are substantially free of directionality and possess a reasonable amount of ductility. In addition the hardened steels and articles or products thereof possess high ultimate tensile and compressive values and high yield strength,
As many possible embodiments may be made at my invention and as many changes may be made in the embodiments hereinbefore set forth,
' it is to be understood that all matter described herein is to be interpreted as illustrative and not as a limitation.
1. In a method of conditioning low-carbon chromium-nickel stainless steel, providing a steel containing about 16.5% to 18.5% chromium.
about 4.75% to 5.60% nickel, and including copper between about 3.5% and 5.0%, and the remainder substantially all iron; treating said steel within a temperature range of about 1700 F. to 2000 F. and quenching the same to provide a copper-soluble austenitic condition stable down to at least room temperature; transforming the alley; and heating the transformed alloy within a temperature range of 850 F. to 950 F. to precipitate copper and obtain an increase in the alloy hardness.
obtain an increase substantially all iron;
chromium; about 4.75%
to 5.607 nickel, 00;: r between about 3.5% 0 De and 5.0%, and the remainder rendering said alloy in a stable austenitic condition at about room temperature with a substantial amount of the copper in solution through suitable heating and quenching; then cooling said alloy to below a temperature of at least 32 F. for transforming the same; and finally heating the transformed alloy within a temperature range of about 850 F. to 950 F. to precipitate copper and obtain an increase in the alloy hardness.
4. A hardened chromium-nickel containing about 16.5% about 4.75% to 5.60%
stainless steel to 18.5% chromium, nickel, copper between about 3.5% and 5.0%, carbon not exceeding about 0.1%, beryllium from traces up to around 0.25 and the remainder substantially all iron, said alloy being characterized by'a precipitated copper-rich and beryllium-rich phase throughout the metal.
5. A hardened chromium-nickel stainless steel comprising about 16.5% to 18.5% about 4.75% to 5.60% nickel, copper between about 3.5% and 5.0%, carbon not exceeding about 0.1% and the remainder substantially all iron, said alloy being characterized by heating between temperatures of about 1700" F. to approximately 2000 F. and quenching to ensure a predominantly austenitic structure down to at least about room temperature, by transformation. and by heating within a temperature range of about 850 F. to approximately 950 F. to precipitate copper and obtain an increase in alloy hardness. I
6. A hardened chromium-nickel stainless steel comprising about 16.5% to 17.5% chromium, about 4.85% to 5.35% nickel, copper between about 3.60% and 4.35%, carbon up to around 0.08%, and the remainder substantially all iron, said steel being characterized by heating at approximately 1800 F. and cooling to ensure a predominantly austen-itic structure down to at least about room temperature, by heating at about 1400 F. and quenching, and by heating at approximately 900 F. to precipitate copper and in hardness.
- 7 R I. Pre-hardened chromium nickel stainless steel in the wrought or cast condition, comprising, about 16.5% to 18.5% chromium, 4.75% to 5.60% nickel, copper between about 3.5% and 5.0%, carbon not exceeding about 0.1%, and the remainder substantially all iron, said product being characterized by heating the metal between temperatures of about 1700 F. to approximately 2000 F. and quenching to ensure a predominantly austenitic structure down to at least about room temperature in which copper is present in solution.
' WILLIAM CHARLES CLARKE.
REFERENCES CITED The following references are of record in the tile oi this patent:
s'rsrms gm'mrrs p ges 100 and 413, by Bullens. Published in 1,939 by John Wiley and Sons. New York. N. Y.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US1945653 *||Jan 31, 1929||Feb 6, 1934||Metal & Thermit Corp||Alloy|
|US2031152 *||Aug 10, 1932||Feb 18, 1936||Rustless Iron And Steel Corp O||Manufacture of alloys of iron, chromium, nickel, and copper|
|US2080368 *||Jun 22, 1934||May 11, 1937||Goodyear Zeppelin Corp||Process for improving the physical properties of austenitic steels|
|US2249417 *||Jul 18, 1938||Jul 15, 1941||Thomas B Chace||Copper clad steel|
|US2319538 *||Aug 6, 1940||May 18, 1943||Everard Tuxford Digby||Heat treatment of copper-chromium alloy steels|
|GB409411A *||Title not available|
|GB437592A *||Title not available|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US2614921 *||Aug 25, 1950||Oct 21, 1952||Armco Steel Corp||Stainless steel and method|
|US2635044 *||Jul 11, 1950||Apr 14, 1953||Cooper Alloy Foundry Co||Hardenable stainless steel alloy|
|US2670528 *||Jun 9, 1951||Mar 2, 1954||Paul E Brunberg||Process of thermal regulation of work and tools|
|US2694626 *||Aug 25, 1950||Nov 16, 1954||Armco Steel Corp||Stainless steels|
|US2967770 *||May 29, 1959||Jan 10, 1961||Republic Steel Corp||Transformable stainless steel|
|US3103454 *||Oct 1, 1957||Sep 10, 1963||Paocsssl|
|US3123468 *||Jun 28, 1960||Mar 3, 1964||Armco Steel Corporation||Alloy steel and method|
|US3619180 *||Dec 6, 1968||Nov 9, 1971||Atomic Energy Commission||Stress-corrosion-resistant alloy|
|US4769213 *||Aug 21, 1986||Sep 6, 1988||Crucible Materials Corporation||Age-hardenable stainless steel having improved machinability|
|US7475478 *||Sep 11, 2006||Jan 13, 2009||Kva, Inc.||Method for manufacturing automotive structural members|
|U.S. Classification||148/578, 148/326, 148/607, 420/60|