US3561953A - Austenitic heat-resisting steel containing nickel, chromium and manganese - Google Patents

Austenitic heat-resisting steel containing nickel, chromium and manganese Download PDF

Info

Publication number
US3561953A
US3561953A US714213A US3561953DA US3561953A US 3561953 A US3561953 A US 3561953A US 714213 A US714213 A US 714213A US 3561953D A US3561953D A US 3561953DA US 3561953 A US3561953 A US 3561953A
Authority
US
United States
Prior art keywords
steel
present
chromium
manganese
calcium
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
US714213A
Inventor
Itaru Niimi
Hideyo Yagasaki
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Application granted granted Critical
Publication of US3561953A publication Critical patent/US3561953A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum

Definitions

  • the present invention relates to austenitic heat-resisting steels containing nickel, chromium and manganese for engine valves and similar products requiring hardness, high temperature strength and toughness when used in modern high performance engines.
  • One method for improving hot-workability is to add boron or other elements.
  • the present inventors succeeded to improve hot-workability and some other characteristics by minimizing the oxygen content and by addition of calcium in the steel.
  • composition of the austenitic heat-resisting steel according to the present invention is by weight as follows: carbon 0.l-0.6%; silicon 0.l'-2.0%; manganese 3.0-l5.0%; nickel lll-15.0%; chromium l5.0-28.0%; tungsten G01-2.0%; molybdenum U01-1.5%; columbium Q01-1.5%; vanadium 0.0l-l.5%; nitrogen 0.2-0.6%; calcium 00m-0.020%; oxygen less than 0.008%; balance of iron and unavoidable incidental impurities.
  • a primary object of the present invention is to provide a steel characterized by improved age-hardenability, high temperature strength and toughness which can better withstand conditions encountered in modern high performance engines.
  • Another important object of the invention is to provide an improved steel composition by inclusion of tungsten, molybdenum, columbium and vanadium.
  • Still another important object of the invention is to provide an improved steel composition, having the above described characteristics, wherein hot-workability is also improved, a preferred treatment including the minimizing of oxygen content and addition of calcium to the steel.
  • FIG. 1 is a diagram showing the relationship between testing temperature and elongation of test specimens of steels of the present invention and conventional steels obtained by tensile tests in the hot-working temperature range;
  • FIG. 2 is a diagram showing hardness change in aging after solution treatment of the steels of the present invention and that of the conventional steels;
  • FIG. 3 is a diagram showing machinability of the steels of the present invention compared to that of conventional steels
  • FIG. 4 is a diagram showing fatigue strength of the steels of the present invention compared with that of conventional steels obtained by fatigue tests at elevated temperature;
  • FIG. 5 is an elevation of a test specimen partially broken away to reveal sections before tensile test at elevated temperature
  • FIGS. 5a and 5b illustrate the appearance of similar test specimens of conventional steel and steel according to the present invention, respectively, after tensile test;
  • FIG. 6 is a microphotograph of non-metallic inclusions in a conventional steel.
  • FIG. 7 is a microphotograph of non-metallic inclusions of the steel according to the present invention.
  • the improved steel is made by adding to a conventional stainless steel melt appropriate quantities, as above indicated, of tungsten, molybdenum, columbium and vanadium either as pure elements or in combination with other elements.
  • the age-hardenability and the high temperature strength are increased by precipitation of complex compounds of chromium, tungsten and molybdenum [(Cr, W, Mo)23(C, N)e] and complex compounds of columbium and vanadium [(Cb, V) (C, N
  • the refining practice of the improved steel is generally carried out in the following way.
  • the material is rened in a basic furnace either by use of lime rich White slag of basicity more than 2, or, at the last stage of the same basic process, by electrolyzing the white slag by applying direct current to reduce oxygen content to less than 0.008% and sulfur to less than 0.01%.
  • the steel is tapped out of the furnace, at which time 0.1-0.25% calcium is added by using the rare earth calcium silicon alloy or the ferrosilicon calcium alloy for reducing oxygen to less than 0.008% and leaving 0.001 to 0.020% of calcium in the steel.
  • non-metallic inclusions in the steel of the present invention is extremely small and particularly their appearances rarely involve silicates and sulphides elongated along the liber flow as seen in conventional steels, but only involve inclusions dispersed in fine particles. Appearances of these non-metallic inclusions are shown in FIGS. 6 and 7.
  • FIG. 6 shows the non-metallic inclusions in the conventional steel products. As seen in the figure, the amount of non-metallic inclusions in the 'conventional steel is rather large and they appear as elongations along the fiber flow.
  • FIG. 7 shows the non-metallic inclusions in the steel of the present invention. By contrast, the amount of non-metallic inclusions is extremely small and they appear as a dispersion of fine particles. By presence of calcium under oxygen minimization, the non-metallic inclusions were reduced and the appearance of them was improved. Grain refining of the matrix by a carbonitride of columbium and vanadium, and calcium improved hot toughness, hot-workability and machinability. Y
  • Table 2 shows chemical analyses of specimens in the test.
  • the specimen (a) is a typical heatresisting steel containing 21% Cr-4% Ni-9% Mn-0.4% N obtained by conventional process.
  • Specimens (b) and (c) are steels according to the present invention.
  • FIG. 4 shows results of .fatigue tests of specimens (a) and (b). They were tested at the temperature of 700 C. under revolution of 3600 r.p.m. The abcissa shows number of revolution to rupture (N) and the ordinate shows stress amplitude (fr, kg./mm.2).
  • both steels containing the same materials were refined in a basic Heroult arc furnace of 1.5 ton in capacity.
  • the tests were made on two heats of 21% Cr-4% Ni-9% Mn-0.4% N steel and five heats of the steel of the present invention. Seven pieces of 200 kg. ingots were cast from each heat. Refining of the steel of this invention was carried carefully with consideration of deoxidation and desulfurization.
  • the processing diagram is as follows:
  • FIG. 2 shows the hardness change when all specimens were heated at 1150 C. and 1200 C. for one hour, water cooled and aged at 700 C. and 750 C., respectively.
  • the aging time (hr.) was taken as an abscissa and the Rockwell C-scale Hardness (HRC) as an ordinate.
  • HRC Rockwell C-scale Hardness
  • FIG. 3 shows the results of machining test of each specimen.
  • round bars of 35 mm. in diameter were employed.
  • the hardness of specimen (a) was HRC 27.7- 28.9; that of specimen (b) was HRC 28A-29.6 and that of specimen (c) was HRC 29.2-3l.0.
  • the cutting tools were a straight tool manufactured from high speed steel with chemical composition of 0.8% C4% Cr-l8% W-l% V, and hardened to HRC 64.3-64.9.
  • the cutting conditions were fixed as follows; the depth of cut was 1.0 mm.; feed 0.15 mm./rev.; and cutting speed was varied between 24- 112 m./min. Cutting length causing a definite wear in the tool edge was determined at each cutting speed.
  • the machinability of the steel of the present invention is much improved compared with conventional steels.
  • FIG. 4 shows results of fatigue tests of specimens (a) and (b). They were tested at the temperature of 7000 C. under revolution of 3600 r.p.m.
  • the abcissa shows number of revolutions to rupture (N) and the ordinate shows stress amplitude (a, kg./mm.2).
  • the lowest limit of carbon content was determined to be 0.1% which is essential to form, with nitrogen, the complex compounds of chromium, tungsten, molybdenum, columbium and vanadium, and for age-hardenability and strengthening of matrix in relation to the amount of other elements.
  • the upper limit was set at 0.6% considering decrease of hot-workability and machinability.
  • the amount of silicon is better to be low in order to improve the corrosion resistance, but, as it is a deoxidizing element, its limit was set at (ll-2.0%.
  • the upper limit of 2.0% in this case is due to the fact that it is a maximum amount to secure hot toughness as well as corrosion resistance.
  • the minimum amount of manganese was set at 3.0% for maintaining the steel of the present invention to austenitic structure. Manganese in excess of 15.0% lowers the oxidation resistance of the steel. The range of content was thus determined to be 3.0- .0%.
  • the minimum amount of nickel required is 1.0% in order to stabilize the austenitic structure and to improve its corrosion resistance. With increase of nickel content, these characteristics are improved but the content in excess of 15.0% does not improve them and hence, is not economic.
  • the range of nickel content was set at 1.0-15.0%.
  • Chromium is an indispensable element for providing heat resistance and is also an important carbide former.
  • the amount of this element should be 15.0% at minimum for the purpose of dissolving a large quantity of nitrogen characterizing the present steel.
  • the steel contains more than 28.0% of chromium, the heat resistance is rarely improved and the steel becomes brittle because of delta phase and, further, sigma phase produced.
  • the range of chromium content was fixed at 15.0-28.0%, but it is more desirable to utilize between 18.0 and 23.0% for improving various characteristics of the present steel.
  • Tungsten and molybdenum are effective for improving age-hardenability and high temperature strength and the effect is more apparent when both elements are present.
  • the ranges of contents of these elements were determined to be 0.01-2.0% and G01-1.5%, respectively, because hot workability decreases with the increase of the content. More desirable ranges of contents of tungsten and molybdenum are 0.03-l.0% and 0.02-0.5% respectively, for improving various characteristics of the steel.
  • Vanadium is eiective for improving age-hardenability, high temperature strength, and toughness, but corresponding to its content, it tends to harm the hot workability so that the range of contents was limited to G01-1.5%.
  • a more desirable range for exhibiting the characteristic features of the improved steel is 0.02-0.5
  • Columbium is effective for improving hot workability and hot toughness, while the columbium compound prevents the grain growth of matrix.
  • These eects of columbium are particularly noted in the steel of the present invention which is oxygen-minimized and calcium restricted. Containing more than 0.01% of columbium,V these effects are remarkable, 'but excess of 1.5% decreases the hot workability, and sometimes it makes austenitic matrix unstable and brittle.
  • the range of content was, therefore, fixed at 0.01-1.5%.
  • a more desirable range of columbium content is 0.02-0.5% for exhibiting the characteristic features of the present steel.
  • the described contents of tungsten, molybdenum and vanadium are required 0.2-3.5% in total, to retain characteristics of the present steel.
  • a more desirable range of contents is 0.5-2.0% in order to exhibit the most proper characteristics.
  • Nitrogen along with carbon, is of supreme importance for precipitation hardening by carbonitrides as described before and for stabilizing and strengthening the austenitic matrix of the steel.
  • the required content of nitrogen was determined to be at least 0.2% and desirably more than 0.3%.
  • the upper limit of nitrogen content of 0.6% is set to prevent occurrence of blow holes and other defects in the ingot.
  • the steel of the present invention must contain 0.001-0.020% of calcium by addition of 0.10.25% of calcium alloy as described. In either case of calcium content being less than 0.001% or more than 0.020%, the eifect of improvement of said characteristics is reduced. A more desirable range of calcium content for raising the characteristics of the present steel is 0.003-0.012%.
  • the oxygen content at less than 0.008% improves agehardenability, hot workability and toughness, and in addition, in combination with calcium, improves the characteristics of the steel produced by the addition of proper amount of tungsten, molybdenum, Columbium and vanadium as described.
  • the oxygen content in excess of 0.008% is less effective.
  • the impurities which are unavoidably mixed in the course of melting process of the present invention are small amounts of copper, titanium, boron, lead, tin and arsenic.
  • titanium and boron can be added positively to improve hot workability as described. Addition of boron is described in U.S. Pat. No. 2,839,391. Aiccording to the present invention, these elements are not positively added but boron ordinarily comes into steel to the extent of about 0.001% at maxi mum from ferro-alloys or furnace linings, and titanium also enters the mix as an impurity at about 0.05% at maximum; both impurities remain in the steel. In general, the above-named impurities are desired to be substantially small in the present steel, but inclusion of small amounts in the mixture cannot be avoided.
  • the steel according to the present invention is an excellent and practical heat resisting steel suitable for use as engine valve material and in other high temperature applications. It is to be understood that, besides engine valves, the invention covers all types of steel products obtained by hot forging and rolling and manufactured by the described refining process and made of the described components.
  • An austenitic heat-resisting steel consisting essentially of:
  • An austenitic heat-resisting steel consisting essentially of:

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)

Abstract

AN AUSTENITIC HEAT-RESISTING STEEL, FOR ENGINE VALVES AND SIMILAR APPLICATIONS, CAPABLE OF WITHSTANDING CONDITIONS ENCOUNTERED IN MODERN HIGH PERFORMANCE ENGINES REQUIRING HARDNESS, HIGH TEMPERATURE STRENGTH AND TOUGHNESS, CONSISTING ESSENTIALLY OF 0.1-0.6% CARBON, 0.1-2.0% SILICON, 3.0-15.0% MANGANESE, 1.0-15% NICKEL, 15.0-28.0% CHROMIUM, 0.01-2.0% TUNGSTEN, 0.01-1.5% MOLYBDENUM, 0.01-1.5% VANADIUM, 0.01-1.5% COLUMBIUM, 0.2-0.6% NITROGEN, 0.001-0.020% CALCIUM, LESS THAN 0.008% OXYGEN, AND THE BALANCE OF IRON WITH INCIDENTAL IMPURITIES.

Description

Feb.
ITARU NllMl ET AL AUSTENITIC HEAT-RESISTING STEEL CONTAINING NICKEL, CHROMIUM AND MANGANESE BYMM) Y I A rroe/vf Ys..
Feb. 9, 1971 v |TARU NUM; ETAL 3,561,953
AUSTENITIC HEAT-RESISTING STEEL CONTAINING NICKEL, CHROMIUM AND MANGANESE Filed March 19, 1968 2 Sheets-Sheet 2 INVENTORS. A/HM /l YA Q A 5415/, QQ]
wm f
f''Q/VEVS.
H/lf YO FIG.
/meu
Mwst-e or @Evo/ awww To @Um-02E FIG. 6;
United States Patent O AUSTENITI'C HEAT-RESISTING STEEL CONTAIN- ING NICKEL, CHROMIUM AND MANGANESE Itaru Niimi, Toyota-shi, and Hideyo Yagasaki, Sendai-shi,
Japan, assignors to Toyota Jidosha Kogyo Kabushiki Kaisha, Aichi-ken, Japan Filed Mar. 19, 1968, Ser. No. 714,213 Int. Cl. C22c 39/20 U.S. Cl. 75-128 2 Claims ABSTRACT OF THE DISCLOSURE An austenitic heat-resisting steel, for engine valves and similar applications, capable of withstanding conditions encountered in modern high performance engines requiring hardness, high temperature strength and toughness, consisting essentially of OLI-0.6% carbon, 0.l-2.0% silicon, 3.0-l5.0% manganese, 1 0-15% nickel, l5.0-28.0% chromium, 0.0l-2.0% tungsten, 0.l-l.5% molybdenum, 0.0l-l.5% vanadium, 0.0l-l.5% columbium, 0.2-0.6% nitrogen, 0.00l-0.020% calcium, less than 0.008% oxygen, and the balance of iron with incidental impurities.
The present invention relates to austenitic heat-resisting steels containing nickel, chromium and manganese for engine valves and similar products requiring hardness, high temperature strength and toughness when used in modern high performance engines.
Hitherto extensively used heat-resisting steels have been presented as for example in U.S. Pat. Nos. 2,602,738, 2,657,130, 2,671,726 and 2,698,785.
Applicants have discovered that the age-hardenability, high temperature strength and toughness of a steel such as proposed in the above-named patents, and containing 21% Cr-4% Ni-9% Mn0.4% can be improved by addition of tungsten, molybdenum, columbium and vanadium so as to produce a valve steel which can stand the heavy conditions of modern high performance engines. While by mere addition of these elements, the agehardenability and high temperature strength of the steel is considerably bettered, it was also found that the steel turned poor in hot-Workability and lost practical value.
One method for improving hot-workability is to add boron or other elements. The present inventors, however, succeeded to improve hot-workability and some other characteristics by minimizing the oxygen content and by addition of calcium in the steel.
Chemical composition of the austenitic heat-resisting steel according to the present invention is by weight as follows: carbon 0.l-0.6%; silicon 0.l'-2.0%; manganese 3.0-l5.0%; nickel lll-15.0%; chromium l5.0-28.0%; tungsten G01-2.0%; molybdenum U01-1.5%; columbium Q01-1.5%; vanadium 0.0l-l.5%; nitrogen 0.2-0.6%; calcium 00m-0.020%; oxygen less than 0.008%; balance of iron and unavoidable incidental impurities.
From the above it will be apparent that a primary object of the present invention is to provide a steel characterized by improved age-hardenability, high temperature strength and toughness which can better withstand conditions encountered in modern high performance engines.
Another important object of the invention is to provide an improved steel composition by inclusion of tungsten, molybdenum, columbium and vanadium.
Still another important object of the invention is to provide an improved steel composition, having the above described characteristics, wherein hot-workability is also improved, a preferred treatment including the minimizing of oxygen content and addition of calcium to the steel.
The novel features that are considered characteristic 3,561,953 Patented Feb. 9, 1971 of the invention are set forth with particularity in the appended claims. The invention, itself, however, both as to its organization and its method of operation, together with additional objects and advantages thereof, will best be understood from the following description of specific embodiments when read in connection With the accompanying drawings, wherein like reference characters indicate like parts throughout the several gures and in which:
FIG. 1 is a diagram showing the relationship between testing temperature and elongation of test specimens of steels of the present invention and conventional steels obtained by tensile tests in the hot-working temperature range;
FIG. 2 is a diagram showing hardness change in aging after solution treatment of the steels of the present invention and that of the conventional steels;
FIG. 3 is a diagram showing machinability of the steels of the present invention compared to that of conventional steels;
FIG. 4 is a diagram showing fatigue strength of the steels of the present invention compared with that of conventional steels obtained by fatigue tests at elevated temperature;
FIG. 5 is an elevation of a test specimen partially broken away to reveal sections before tensile test at elevated temperature;
FIGS. 5a and 5b illustrate the appearance of similar test specimens of conventional steel and steel according to the present invention, respectively, after tensile test;
FIG. 6 is a microphotograph of non-metallic inclusions in a conventional steel; and
FIG. 7 is a microphotograph of non-metallic inclusions of the steel according to the present invention.
Referring more particularly to the drawings wherein the characteristics of improved high temperature heatresisting steels according to the invention are compared under various tests to conventional steels, it is first stated that the improved steel is made by adding to a conventional stainless steel melt appropriate quantities, as above indicated, of tungsten, molybdenum, columbium and vanadium either as pure elements or in combination with other elements. The age-hardenability and the high temperature strength are increased by precipitation of complex compounds of chromium, tungsten and molybdenum [(Cr, W, Mo)23(C, N)e] and complex compounds of columbium and vanadium [(Cb, V) (C, N
The refining practice of the improved steel is generally carried out in the following way. The material is rened in a basic furnace either by use of lime rich White slag of basicity more than 2, or, at the last stage of the same basic process, by electrolyzing the white slag by applying direct current to reduce oxygen content to less than 0.008% and sulfur to less than 0.01%.
Concerning deoxidation by slag-electrolyzing, U.S. Pat. No. 3,203,883 shows that deoxidation and desulfurization of 13% chromium stainless steel, for instance, may be carried out electrochemically by applying direct current at the last stage of refining using lime rich slag, and oxygen and sulfur content in the steel is reduced to 0.0045 to 0.0029% and 0.004% respectively. This patented method for deoxidation and desulfurization may be followed to make the present steel easily and with certainty. In case of refining only by the white slag, however, much skill is required because slag control is fairly diicult.
Subsequent to said refining, the steel is tapped out of the furnace, at which time 0.1-0.25% calcium is added by using the rare earth calcium silicon alloy or the ferrosilicon calcium alloy for reducing oxygen to less than 0.008% and leaving 0.001 to 0.020% of calcium in the steel.
The amount of non-metallic inclusions in the steel of the present invention is extremely small and particularly their appearances rarely involve silicates and sulphides elongated along the liber flow as seen in conventional steels, but only involve inclusions dispersed in fine particles. Appearances of these non-metallic inclusions are shown in FIGS. 6 and 7.
FIG. 6 shows the non-metallic inclusions in the conventional steel products. As seen in the figure, the amount of non-metallic inclusions in the 'conventional steel is rather large and they appear as elongations along the fiber flow. FIG. 7 shows the non-metallic inclusions in the steel of the present invention. By contrast, the amount of non-metallic inclusions is extremely small and they appear as a dispersion of fine particles. By presence of calcium under oxygen minimization, the non-metallic inclusions were reduced and the appearance of them was improved. Grain refining of the matrix by a carbonitride of columbium and vanadium, and calcium improved hot toughness, hot-workability and machinability. Y
In the present invention, these excellent characteristics can be attained only when deoxidation and desulfurization refining are made as above described and thereafter said calcium alloy has been additionally applied.
Characteristic features of the steel of the present invention are illustrated below referring to some test examples. Table 2 shows chemical analyses of specimens in the test. In the table, the specimen (a) is a typical heatresisting steel containing 21% Cr-4% Ni-9% Mn-0.4% N obtained by conventional process. Specimens (b) and (c) are steels according to the present invention.
TABLE 2.-CHEMICAL ANALYSES (by WEIGHT PERCENT) Specimen (a) (b) (C) Conventional Present Present steel e steel 0. 48 0. 43 0. 41 0. 23 0. 28 0. 35 8. 55 7. 95 8. 50 0. 022 0. 021 0. 023 0. 004 0. 003 3. 98 4. 08 20. 08 22. 06 W... 0. 35 0. 30 M0.. 0. 12 0. 22 Cb 0. 152 0. 315 V 0. 3l 0. 45 Ca-- 0. 0098 0. 0065 0. 47 0.43 O 0. 0099 0. 0058 0. 0042 Varied characteristic features of these specimens are shown by comparison in Table 3 and in FIGS. 1 to 5b.
TABLE 3.-ME CHANICAL PROPERTIES AT THE ELEVATED TEMPERATURE (TESTED AT 700 C.)
NOTE: Heat treatment; 1,200 C. 1 hr. W.C. and 850 0.)(5 hrs. A C.
The results shown in Table 3 indicate that the steel ofthe present invention is fairly high in tensile strength and creep rupture strength so that the steel excels conventional steels in high temperature strength, and from its high elongation, reduction of area, and Charpy impact value, its excellent toughness is clearly shown.
Also the results of fatigue tests at elevated temperature show that the steel of the invention is higher in hot fatigue strength than conventional steels, and that the former is practically valuable for engine valves. FIG. 4 shows results of .fatigue tests of specimens (a) and (b). They were tested at the temperature of 700 C. under revolution of 3600 r.p.m. The abcissa shows number of revolution to rupture (N) and the ordinate shows stress amplitude (fr, kg./mm.2).
The relationship of testing temperature and elongation of the specimens of the present steels and conventional one, obtained by tensile tests in hot-working temperature range, is shown in FIG. l.
In FIG. l, thev testing'temperature C.) was taken -as'an abcissa and the elongation (percent) as an ordinate.
As seen in FIG. 1, the elongation of the steels of the present invention as compared with conventional steel at 1100"v C. is apparently very high showing excellent hot workability The typical appearance of the specimens after the test is-shoWn in FIGS. 5a and 5b in comparison with that of before the test, shown in FIG. 5. The elongation in the course of heating of the specimen (b) was much larger than the specimen (a) which shows large hot ductilityand excellent hot workability of the present steel.
Comparison of steels by other methods also indicated that the steel ofthe present invention is higher n the hot workability than the conventional steels.
It is particularly noted that the yield of end product in processing ofthe steel of the present invention which is oxygen-minimized and calcium-restricted greatly increased as compared with the conventional steel of 21% Cr4% Ni-9% Mn0.4% N. The comparison of the yield of both steels in the processing from 200 kg. ingots to 9.3 mm. round bars was carried out in the following way. In the test, both steels containing the same materials were refined in a basic Heroult arc furnace of 1.5 ton in capacity. The tests were made on two heats of 21% Cr-4% Ni-9% Mn-0.4% N steel and five heats of the steel of the present invention. Seven pieces of 200 kg. ingots were cast from each heat. Refining of the steel of this invention was carried carefully with consideration of deoxidation and desulfurization.
The processing diagram is as follows:
heat to 1150 C. 200 kg. ingot -i heat 00 1200 C. 40 mm. x 40 mm. rough rolling 9.3 mm. round bar final rolling The yield in the above process is shown in Table 4.
TABLE 4.-YIELDS OF CONVENTIONAL 21% Cr4% N19%Mn-0.4% N STEEL AND PRESENT STEEL mm. x 40 mm. x 200 kg. 110 mln. 40 mm. 9.3 mm: ingots billets billets round bars Conventional steel:
Weight (kg.) 2, 704. 8 1, 306. 4 1, 154. 9 1, 098. 1 Yield from ingot (percent) 48. 3 42. 7 40. 6 Present steel:
Weight (kg.) 6, 786. 5 5, 620. 0 5, 347. 8 5, 157. 7 Yield from ingot (percent) 82. 9 78. 8 76. 0
In the conventional steel, cracks often occurred in the course of rough forging from ingots to billets. These cracks appeared also in the course of rough rolling of billets. The yield of the conventional steel from the ingots to 9.3 mm. round bars was 40.6%, as shown in Table 4. In contrast, no crack appeared in the present invention steel through the Whole processing and the yield was 76.0%.
A good yield was also obtained in manufacturing engine valves from the steel of the present invention.
FIG. 2 shows the hardness change when all specimens were heated at 1150 C. and 1200 C. for one hour, water cooled and aged at 700 C. and 750 C., respectively. In FIG. 2, the aging time (hr.) was taken as an abscissa and the Rockwell C-scale Hardness (HRC) as an ordinate. As shown in the gure, the hardness of the steel of the present invention, specimens ('b) and (c), after 100 hours aging was HRC 39-41, while that of the conventional steel, specimen (a), was HRC 32-34, whereby it is evident that the age-hardenability of the steel of the present invention is much improved over that of the conventional steel.
FIG. 3 shows the results of machining test of each specimen. In the tests, round bars of 35 mm. in diameter were employed. The hardness of specimen (a) was HRC 27.7- 28.9; that of specimen (b) was HRC 28A-29.6 and that of specimen (c) was HRC 29.2-3l.0. The cutting tools were a straight tool manufactured from high speed steel with chemical composition of 0.8% C4% Cr-l8% W-l% V, and hardened to HRC 64.3-64.9. The cutting conditions were fixed as follows; the depth of cut was 1.0 mm.; feed 0.15 mm./rev.; and cutting speed was varied between 24- 112 m./min. Cutting length causing a definite wear in the tool edge was determined at each cutting speed.
The cutting length of each specimen at the cutting speed of 62 m./min., for example, was 200G-4000 mm. for the specimen (a); 33,000-36,000 mm. for the specimen (b), and 21,000-26,000 mm. for the specimen (c) as shown in FIG. 3. The machinability of the steel of the present invention is much improved compared with conventional steels.
FIG. 4 shows results of fatigue tests of specimens (a) and (b). They were tested at the temperature of 7000 C. under revolution of 3600 r.p.m. The abcissa shows number of revolutions to rupture (N) and the ordinate shows stress amplitude (a, kg./mm.2).
Detailed description of the chemical analyses of steel according to the present invention to obtain improved characteristics is given below.
The lowest limit of carbon content was determined to be 0.1% which is essential to form, with nitrogen, the complex compounds of chromium, tungsten, molybdenum, columbium and vanadium, and for age-hardenability and strengthening of matrix in relation to the amount of other elements. The upper limit was set at 0.6% considering decrease of hot-workability and machinability.
The amount of silicon is better to be low in order to improve the corrosion resistance, but, as it is a deoxidizing element, its limit was set at (ll-2.0%. The upper limit of 2.0% in this case is due to the fact that it is a maximum amount to secure hot toughness as well as corrosion resistance.
The minimum amount of manganese was set at 3.0% for maintaining the steel of the present invention to austenitic structure. Manganese in excess of 15.0% lowers the oxidation resistance of the steel. The range of content was thus determined to be 3.0- .0%.
The minimum amount of nickel required is 1.0% in order to stabilize the austenitic structure and to improve its corrosion resistance. With increase of nickel content, these characteristics are improved but the content in excess of 15.0% does not improve them and hence, is not economic. The range of nickel content was set at 1.0-15.0%.
Content of manganese and nickel together were, for retaining proper characteristic of the steel of the present invention, 8.0-30.0% in sum of twice the content of manganese and the content of nickel. At below 8.0%, there precipitates a free ferric which is harmful for toughness, and excess of 30.0% is uneconomic, or sometimes is accompanied by poor oxidation resistance.
Chromium is an indispensable element for providing heat resistance and is also an important carbide former. The amount of this element should be 15.0% at minimum for the purpose of dissolving a large quantity of nitrogen characterizing the present steel. When the steel contains more than 28.0% of chromium, the heat resistance is rarely improved and the steel becomes brittle because of delta phase and, further, sigma phase produced. Thus the range of chromium content was fixed at 15.0-28.0%, but it is more desirable to utilize between 18.0 and 23.0% for improving various characteristics of the present steel.
Tungsten and molybdenum are effective for improving age-hardenability and high temperature strength and the effect is more apparent when both elements are present. The ranges of contents of these elements were determined to be 0.01-2.0% and G01-1.5%, respectively, because hot workability decreases with the increase of the content. More desirable ranges of contents of tungsten and molybdenum are 0.03-l.0% and 0.02-0.5% respectively, for improving various characteristics of the steel.
Vanadium is eiective for improving age-hardenability, high temperature strength, and toughness, but corresponding to its content, it tends to harm the hot workability so that the range of contents was limited to G01-1.5%. A more desirable range for exhibiting the characteristic features of the improved steel is 0.02-0.5
Columbium is effective for improving hot workability and hot toughness, while the columbium compound prevents the grain growth of matrix. These eects of columbium are particularly noted in the steel of the present invention which is oxygen-minimized and calcium restricted. Containing more than 0.01% of columbium,V these effects are remarkable, 'but excess of 1.5% decreases the hot workability, and sometimes it makes austenitic matrix unstable and brittle. The range of content was, therefore, fixed at 0.01-1.5%. A more desirable range of columbium content is 0.02-0.5% for exhibiting the characteristic features of the present steel.
The described contents of tungsten, molybdenum and vanadium are required 0.2-3.5% in total, to retain characteristics of the present steel. A more desirable range of contents is 0.5-2.0% in order to exhibit the most proper characteristics.
Nitrogen, along with carbon, is of supreme importance for precipitation hardening by carbonitrides as described before and for stabilizing and strengthening the austenitic matrix of the steel. The required content of nitrogen was determined to be at least 0.2% and desirably more than 0.3%. The upper limit of nitrogen content of 0.6% is set to prevent occurrence of blow holes and other defects in the ingot.
Calcium greatly contributes to improvement of hot workability, toughness and machinability by grain refining, and reducing and improving the appearance of nonmetallic inclusions. Therefore, the steel of the present invention must contain 0.001-0.020% of calcium by addition of 0.10.25% of calcium alloy as described. In either case of calcium content being less than 0.001% or more than 0.020%, the eifect of improvement of said characteristics is reduced. A more desirable range of calcium content for raising the characteristics of the present steel is 0.003-0.012%.
The oxygen content at less than 0.008% improves agehardenability, hot workability and toughness, and in addition, in combination with calcium, improves the characteristics of the steel produced by the addition of proper amount of tungsten, molybdenum, Columbium and vanadium as described. The oxygen content in excess of 0.008% is less effective.
The impurities which are unavoidably mixed in the course of melting process of the present invention, are small amounts of copper, titanium, boron, lead, tin and arsenic. Among these elements, titanium and boron can be added positively to improve hot workability as described. Addition of boron is described in U.S. Pat. No. 2,839,391. Aiccording to the present invention, these elements are not positively added but boron ordinarily comes into steel to the extent of about 0.001% at maxi mum from ferro-alloys or furnace linings, and titanium also enters the mix as an impurity at about 0.05% at maximum; both impurities remain in the steel. In general, the above-named impurities are desired to be substantially small in the present steel, but inclusion of small amounts in the mixture cannot be avoided.
As above described, the steel according to the present invention is an excellent and practical heat resisting steel suitable for use as engine valve material and in other high temperature applications. It is to be understood that, besides engine valves, the invention covers all types of steel products obtained by hot forging and rolling and manufactured by the described refining process and made of the described components.
Although certain specic embodiments of the invention have been shown and described, it is obvious that many modifications thereof are possible. The invention, therefore, is not to be restricted except insofar as is necessitated by the prior art and by the spirit of the appended claims.
What is claimed is:
1. An austenitic heat-resisting steel consisting essentially of:
Percent Carbon l 0.l-0.6 Silicon 0.l-2.0 Manganese 3.0-15.0
Nitrogen 0.2-0.6 Nickel 1.0-15.0 Chromium 15.0-28.0 Tungsten 0.0l-2.0 Molybdenum 0.01-1.5 Vanadium 0.01-1.5 Columbium 0.0l-1.5 Calcium 0.001-0020 Oxygen-less than 0.008% by Weight, and
the balance of iron with incidental impurities.
2. An austenitic heat-resisting steel consisting essentially of:
Percent Carbon 0.1-0.6 silicon o.1-2.0 Manganese 3.0-15.0 Nitrogen 0.3-0.6 Nickel 1.0-l5.0 Chromium 18.0-23.0 Tungsten 0.03-l.0 Molybdenum 0.02-05 Vanadium 0.02-0.5 Columbium 0.02-0.5 Calcium 0.003-0.012 Oxygen-less than 0.008% by weight, and
the balance of iron with incidental impurities.
References Cited UNITED STATES PATENTS 2,793,113 5/1957 Rait 75-1285 2,848,323 8/1958 Harris 75--128.5 2,853,410 9/1958 Lula 75-128.5 3,151,979 10/1964 Carney 75-128.6
HYLAND BIZOT, Primary Examiner UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,561,953 Dated February 9, 1971 Inventor(s) ItaTU Nllml et al.
It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
In the heading to the printed specification, after lin 8, insert Claims priority, application Japan, March 24, 1967, 18413/67 Signed and sealed this 17th day of August 1971.
(SEAL) Attest:
EDWARD M.FLETCHER,JR. WILLIAM E. SCHUYLER, JI Attestlng Officer Commissioner of Patenti FORM PO-1050(1D-69)
US714213A 1968-03-19 1968-03-19 Austenitic heat-resisting steel containing nickel, chromium and manganese Expired - Lifetime US3561953A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US71421368A 1968-03-19 1968-03-19

Publications (1)

Publication Number Publication Date
US3561953A true US3561953A (en) 1971-02-09

Family

ID=24869165

Family Applications (1)

Application Number Title Priority Date Filing Date
US714213A Expired - Lifetime US3561953A (en) 1968-03-19 1968-03-19 Austenitic heat-resisting steel containing nickel, chromium and manganese

Country Status (1)

Country Link
US (1) US3561953A (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3778255A (en) * 1972-04-05 1973-12-11 Res Inst Metals Of Tohoku Univ Corrosion resistant low carbon chromium alloy steel
US3839022A (en) * 1971-01-28 1974-10-01 Dunford Hadfields Ltd Hot work tools and alloys therefor
DE2421604A1 (en) * 1973-05-04 1974-11-14 Nippon Steel Corp STAINLESS STEEL
US3904401A (en) * 1974-03-21 1975-09-09 Carpenter Technology Corp Corrosion resistant austenitic stainless steel
US4099966A (en) * 1976-12-02 1978-07-11 Allegheny Ludlum Industries, Inc. Austenitic stainless steel
FR2527636A1 (en) * 1982-05-26 1983-12-02 Ugine Aciers REFRACTORY REFRACTORY STEEL FOR ABRASION AND DEFORMATION RESISTANT MOLDING AT VERY HIGH TEMPERATURE IN ATMOSPHERE CONTAINING SULFUR OXIDES
EP0231492A1 (en) * 1985-12-20 1987-08-12 Fried. Krupp Gesellschaft mit beschränkter Haftung Austenitic, nitrogen-containing chromium-nickel-molybdenum-manganese steel; process for manufacturing this steel and uses thereof
FR2595717A1 (en) * 1986-03-17 1987-09-18 Sviluppo Materiali Spa AUSTENITIC STEEL HAVING IMPROVED HIGH TEMPERATURE AGGRESSIVE AGGRESSIVE AGENTS
EP0296439A2 (en) * 1987-06-23 1988-12-28 TRW Thompson GmbH & Co. KG Austenitic steel for valves of internal combustion engines
US4853185A (en) * 1988-02-10 1989-08-01 Haynes International, Imc. Nitrogen strengthened Fe-Ni-Cr alloy
US4929419A (en) * 1988-03-16 1990-05-29 Carpenter Technology Corporation Heat, corrosion, and wear resistant steel alloy and article
EP0411569A1 (en) * 1989-08-02 1991-02-06 Hitachi Metals, Ltd. Heat resistant steel for use as material of engine valve
EP0467756A1 (en) * 1990-07-18 1992-01-22 AUBERT & DUVAL Austenitic steel having improved strength properties at high temperature, process for its manufacturing and the fabrication of mechanical parts, more particularly of valves
EP2765214A3 (en) * 2013-02-12 2014-09-03 Honeywell International Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
WO2016055430A1 (en) * 2014-10-08 2016-04-14 Swep International Ab A brazing material for brazing articles of austenitic stainless steel and method therefore
RU2581321C1 (en) * 2015-06-01 2016-04-20 Байдуганов Александр Меркурьевич High-temperature alloy
US9534281B2 (en) 2014-07-31 2017-01-03 Honeywell International Inc. Turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US9896752B2 (en) 2014-07-31 2018-02-20 Honeywell International Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US10316694B2 (en) 2014-07-31 2019-06-11 Garrett Transportation I Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
EP3636792A1 (en) * 2018-10-12 2020-04-15 Borgwarner Inc. Novel austenitic alloys for turbochargers

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3839022A (en) * 1971-01-28 1974-10-01 Dunford Hadfields Ltd Hot work tools and alloys therefor
US3778255A (en) * 1972-04-05 1973-12-11 Res Inst Metals Of Tohoku Univ Corrosion resistant low carbon chromium alloy steel
DE2421604A1 (en) * 1973-05-04 1974-11-14 Nippon Steel Corp STAINLESS STEEL
US3904401A (en) * 1974-03-21 1975-09-09 Carpenter Technology Corp Corrosion resistant austenitic stainless steel
US4099966A (en) * 1976-12-02 1978-07-11 Allegheny Ludlum Industries, Inc. Austenitic stainless steel
EP0097106A1 (en) * 1982-05-26 1983-12-28 Ugine Savoie Heat resisting cast steel, abrasion-proof and able to withstand strain at very high temperatures in atmospheres containing sulfur oxides
FR2527636A1 (en) * 1982-05-26 1983-12-02 Ugine Aciers REFRACTORY REFRACTORY STEEL FOR ABRASION AND DEFORMATION RESISTANT MOLDING AT VERY HIGH TEMPERATURE IN ATMOSPHERE CONTAINING SULFUR OXIDES
EP0231492A1 (en) * 1985-12-20 1987-08-12 Fried. Krupp Gesellschaft mit beschränkter Haftung Austenitic, nitrogen-containing chromium-nickel-molybdenum-manganese steel; process for manufacturing this steel and uses thereof
FR2595717A1 (en) * 1986-03-17 1987-09-18 Sviluppo Materiali Spa AUSTENITIC STEEL HAVING IMPROVED HIGH TEMPERATURE AGGRESSIVE AGGRESSIVE AGENTS
USRE33753E (en) * 1986-03-17 1991-11-26 Centro Sviluppo Materiali S.P.A. Austenitic steel with improved high-temperature strength and corrosion resistance
EP0296439A2 (en) * 1987-06-23 1988-12-28 TRW Thompson GmbH & Co. KG Austenitic steel for valves of internal combustion engines
EP0296439A3 (en) * 1987-06-23 1989-07-12 Trw Thompson Gmbh Austenitic steel for valves of internal combustion engines
US4853185A (en) * 1988-02-10 1989-08-01 Haynes International, Imc. Nitrogen strengthened Fe-Ni-Cr alloy
US4929419A (en) * 1988-03-16 1990-05-29 Carpenter Technology Corporation Heat, corrosion, and wear resistant steel alloy and article
US5064610A (en) * 1989-08-02 1991-11-12 Hitachi Metals, Ltd. Heat resistant steel for use as material of engine valve
EP0411569A1 (en) * 1989-08-02 1991-02-06 Hitachi Metals, Ltd. Heat resistant steel for use as material of engine valve
EP0467756A1 (en) * 1990-07-18 1992-01-22 AUBERT & DUVAL Austenitic steel having improved strength properties at high temperature, process for its manufacturing and the fabrication of mechanical parts, more particularly of valves
FR2664909A1 (en) * 1990-07-18 1992-01-24 Aubert & Duval Acieries AUSTENITIC STEEL HAVING IMPROVED RESISTANCE AT HIGH TEMPERATURE AND PROCESS FOR OBTAINING SAME AND PRODUCING MECHANICAL PARTS, ESPECIALLY VALVES.
EP2765214A3 (en) * 2013-02-12 2014-09-03 Honeywell International Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US10975718B2 (en) 2013-02-12 2021-04-13 Garrett Transportation I Inc Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US9534281B2 (en) 2014-07-31 2017-01-03 Honeywell International Inc. Turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US9896752B2 (en) 2014-07-31 2018-02-20 Honeywell International Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
US10316694B2 (en) 2014-07-31 2019-06-11 Garrett Transportation I Inc. Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same
WO2016055430A1 (en) * 2014-10-08 2016-04-14 Swep International Ab A brazing material for brazing articles of austenitic stainless steel and method therefore
RU2581321C1 (en) * 2015-06-01 2016-04-20 Байдуганов Александр Меркурьевич High-temperature alloy
EP3636792A1 (en) * 2018-10-12 2020-04-15 Borgwarner Inc. Novel austenitic alloys for turbochargers
CN111041386A (en) * 2018-10-12 2020-04-21 博格华纳公司 Novel austenitic alloy for turbocharger
US11434556B2 (en) 2018-10-12 2022-09-06 Borgwarner Inc. Austenitic alloys for turbochargers

Similar Documents

Publication Publication Date Title
US3561953A (en) Austenitic heat-resisting steel containing nickel, chromium and manganese
US2793113A (en) Creep resistant steel
US7014812B2 (en) Sulfur-containing free-cutting steel for machine structural use
US2990275A (en) Hardenable stainless steel alloys
US5032356A (en) High fatigue strength metal band saw backing material
US2291842A (en) Production of steel
US4391635A (en) High Cr low Ni two-phased cast stainless steel
US5013524A (en) Martensite-hardenable steel
US3366473A (en) High temperature alloy
EP0526467B1 (en) Air hardening steel
JPS5946300B2 (en) Steel for cold forging with excellent machinability and its manufacturing method
JPS6318038A (en) Low-alloy steel excellent in creep resistance and hydrogen attack-resisting characteristic
US2602028A (en) Austenitic steels
US5223214A (en) Heat treating furnace alloys
US3113862A (en) High speed steel
US4049430A (en) Precipitation hardenable stainless steel
US3948649A (en) Free cutting steel
US2334870A (en) Austenitic chromium-nickel and/or manganese steels
US2949355A (en) High temperature alloy
CA1073708A (en) Oxidation resistant iron base alloys
US5102479A (en) High strength non-heat refining free cutting steels
Needham et al. The effect of residuals on the elevated temperature properties of some creep resistant steels
JPS58171558A (en) Tough nitriding steel
JPH07179988A (en) Hot tool steel excellent in high temperature strength
RU2318900C2 (en) Complex modifier for steel