US3044872A - Steel alloy composition - Google Patents

Steel alloy composition Download PDF

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Publication number
US3044872A
US3044872A US850117A US85011759A US3044872A US 3044872 A US3044872 A US 3044872A US 850117 A US850117 A US 850117A US 85011759 A US85011759 A US 85011759A US 3044872 A US3044872 A US 3044872A
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United States
Prior art keywords
steel
alloy
weight percent
niobium
chromium
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Expired - Lifetime
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US850117A
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English (en)
Inventor
Walter C Hayes
Robert W Dickinson
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North American Aviation Corp
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North American Aviation Corp
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Publication date
Application filed by North American Aviation Corp filed Critical North American Aviation Corp
Priority to US850117A priority Critical patent/US3044872A/en
Priority to GB36720/60A priority patent/GB921838A/en
Priority to CH1229560A priority patent/CH415068A/fr
Priority to BE596717A priority patent/BE596717A/fr
Application granted granted Critical
Publication of US3044872A publication Critical patent/US3044872A/en
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    • 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
    • C22C38/26Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
    • 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
    • C22C38/22Ferrous alloys, e.g. steel alloys containing chromium 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
    • C22C38/28Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium

Definitions

  • This invention relates to an improved high temperature alloy. More particularly, this invention relates to an improved high temperature steel alloy with low thermal coeflicient of expansion, high thermal conductivity, and good high temperature mechanical properties.
  • Austenitic stainless steels are well known in the art.
  • An example of a stainless steel is AISI type No. 304 which contains from 18% to 20% chromium and 8% to 11% nickel with 2% max. of manganese. It has a low carbon content and has many uses. However, it has some draw-backs, one of which is its relatively high cost because of the high chromium and nickel content. Also, its thermal coeflicient of expansion is a little high for certain applications while its thermal conductivity is too low. On the other hand, ferritic steels have low coetficient of expansion anda high thermal conductivity as well as low cost but they are weak at elevated temperatures.
  • ferritic alloy which would combine the conductivity and expansion properties of ferritic steels with the excellent strength properties of austenitic steels for use at high temperatures.
  • high thermal. conductivity, low thermal coeflicient of expansion and, therefore, low thermal stresses are important.
  • an object of this invention to provide a new steel alloy having high creep and stress rupture properties at elevated temperatures. It is also an object of this invention to provide a steel alloy having a high corrosion resistance in molten metal service. Another object of this invention is to provide a steel alloy having adequate strength and ductility in the heat-affected zone of weldments without costly post weld heat treatments. Another object of this invention is to provide a ferritic steel alloy having high temperature properties equal to or surpassing those of the austenitic steels. Still another object is to provide a steel alloy which is obtainable at a much lower cost than stainless steel. It is also an object to provide a steel alloy which has a low coefficient of expansion, a high thermal conductivity, and a high resistance to thermal, stresses at elevated temperatures. Still other objects of this invention will become apparent from the discussion which follows.
  • a steel alloy having improved high temperature properties containing from about 0.4% to about 10% chromium, from about 0.4% to about 4% molybdenum, from about 0.05% to about 0.4% carbon, from about 0.1% to about 1.5% manganese, from about 0.1% to about 1% niobium, from about 0% to about 1.4% titanium, from about 0% to about 4% nickel, and the remainder substantially iron.
  • the alloy can contain about 0.1% (max.) boron, about 0.02%
  • the steel composition or alloys of this invention contain from about 0.4 to about 10 weight percent chromium in order to give the steel adequate corrosion and oxida tion resistance.
  • the steel alloys of this invention are particularly useful for service above about 1050 F. In order to assure oxidation resistance at temperatures of this magnitude it is preferred to include at least about 1.5 weight percent chromium. This constitutes a preferred minimum chromium concentration.
  • One of the properties of the steel alloy of this invention is good notched impact properties at high temperatures. It is found that these are not enhanced to any appreciable degree by chromium concentrations above about 7.5 weight percent and, therefore, the latter amount constitutes a preferred upper limit to the chromium concentration. Hence, the preferred range of chromium is from about 1.5 weight percent to about 7 weight percent.
  • the molybdenum concentration in the steel alloys of this invention varies from about 0.4 to about 4 weight percent.
  • An amount of molybdenum equivalent to about 0.4 weight percent together with the amount of chromium indicated above is sufiicient to impart a perceptible degree of resistance to oxidation and a fair degree ofstrengthening at elevated temperatures.
  • the 0.4 weight percent therefore, constitutes a preferred lower limit for the molybdenum content. No additional benefit is obtained from amounts of molybdenum above about;4 weight percent and the latter, therefore, constitutes an upper limit of the molybdenum concentration.
  • the carbon is present in the novel steel alloys inamounts ranging from about 0.05 to about 0.4 weight percent in order to impart strengthening characteristics to the steel. At least about 0.05 weight percent carbon is required in order to impart a discernible increase in the strength of the steel. Above about 0.4 weight percent carbon there is a danger of making the steel too brittle.
  • the broad range of carbon concentrations, there fore, varies in the range of from about 0.05 to about 'to about 1 Weight percent niobium to the above described steels containing chromium, molybdenum, and carbon in the amounts indicated, imparts ahigh degree of strength increase at elevated temperatures. 'With the added 'niobium, the resulting steel has a low notch sensitivity in stress rupture tests at elevated temperatures.
  • niobium in the steel alloy of this invention varies from about 0.1 to about 1 weight percent.
  • the alloys of this composition also have the added adpercent in one embodiment of the steel alloy of this in- 5 vantage of low cost, good general corrosion resistance, vention.
  • To the titanium-containing steel alloy can be resistance to chloride stress corrosion, good weldability, added from about 0.1 to about 1 weight percent niobium and good resistance to thermal stresses. to increase the elevated temperature strength of the al- In general, a heat of steel of this ihvehtloh is melted loy as stated hereinabove.
  • poud Cast y Conventional thethodsh cast metal can timum strengthening properties are obtained when the 10 b hot Worked y Convohtloual Praotlces to a ll/ ⁇ ought total amount of the added niobium and titanium varies product.
  • Heat treatment is accomplished by heat ng to from about 0.2 to about 1.5 weight percent and wherein om bout 1300" to about 2200 for a Peflod of the amount of niobium is from about 0.1 weight percent from to about hours- Following thls, the to about 1 weight percent, and this constitutes a preferred metal alloy alt Cooled of quenched to a tempofatufe of b di of hi i i 15 from about 1300 F. to about 0 F.
  • Nickel is added to steel in order to lower the minimum y aging of tomPefing at a tempel'hthro of from about temperature required for solution heat treating, and to 1100 to about a Poflod of h' about improve low temperature ductility and impact strength. to about 24 hours.
  • Th1s treatment results in a steel alloy
  • Amounts of nickel ranging f o about 0 1 to about 4 whrch is more ductile and less notchsensitive than ordiweight percent give satisfactory results in the solution heat y high -o o Steelstreating of the steel alloy compositions of this invention.
  • the f0ll0W1ng non-llmltlng e p r h Illustrate A least about O 1 weight pol-Cont of nickel is required the var1ous steel alloy compositions of this invention. in order to give a significantly perceptible effect, while EXAMPLE amounts above about 4 weight percent of nickel decrease the response to heat treatment.
  • niobium 25 A11 induction heat was air melted and cast into a hot to a nickel-containing steel alloy having chromium, mopp Square tapered iugot- A chemical ahall'sis lybdenum, and carbon in the amounts outlined hereinof the ingot Showed Substantially the following p above, substantially increases the elevated temperature tion in Percentage y g 232% Chromium, 199% strength of the steel.
  • the amount of niobium added in molybdenum, 047% titanium. 013% Carbon, 0.49% this instance is the same as that added to the other g 7b 0.002% P p 10227 sulniobium-containing steel embodiments of this invention.
  • the 1hgot nickel-containing steel as hereinabove specified can conto form a Plato Wlth a Toduotlou Tatlo of P- tain from about 0.1 to about 1 weight percent niobium.
  • p f y T e steel was heated to 2100 F. for This, then, constitutes another embodiment of the instant a Perlod of 1 hour followed y coollhg to a p invention ture of substantially 70 F.
  • Still another embodiment of this invention is a steel Perathre of Substantially 1300 for a Phrtod of 8 alloy composition containing the chromium, molybdenum, hours: and then Cooled to carbon, and nickel in the amounts specified hereinabove XAM together with titanium and niobium in an amount vary- E PLE H ing from about 0.2 to about 1.5 weight percent wherein
  • a heat having the amount of niobium varies from about 0.1 to about 1 fohoWlug oomposltloll Was Processodl 242% chroweight percent.
  • This composition then has the properties 111111111, 194% o yb o of a similar composition minus nickel described herein- 3311656, 012% hloblum, tltahlum, P above as well as the added advantage of having a low- Phofus, Sulfur, Silicon, O-006% nitrogen, ered solution heat treating temperature.
  • the nickel-, aluminum, and the balance Substantially iron. titanium-, and niobium-containing alloy, therefore, con- Still other steel alloys of this invention and their comstitutes still another embodiment of this invention. position are given in the following Table I.
  • the balance Table I Heat No. Or Mo 0 Mn Nb Ti Ni B, N, .41, Si, P, 3,
  • Tables II and III show the various properties of a steel alloy of this invention together with the properties of ferritic steel and 304 stainless steel for comparison purposes.
  • the offset yield strength of the niobium-containing alloy of this invention is 124% higher than that of 2.25 chromium and 1% molybdenum fenritic steel and 150% higher than that of 304 stainless steel at room temperature; 147% higher than that of ferritic steel and 378% higher than that of stainless steel at 1050 F. (565 C.) and 206% higher than ferritic steel and 366% higher than stainless steel at 1200 F. (650 C.).
  • the ultimate tensile strength of the niobium-containing steel is 35% higher than that of ferritic steel and 26% higher than that of stainless steel at room temperature; 41% higher than 6 that of ferritic steel and 29% higher than that of stainless steel at 1050 F.; and 82% higher than that of ferri-tic steel and 25% higher than that of stainless steel at 1200 F.
  • the minimum creep rate of the niobium-containing steel of this invention is from about a factor of 2 to about a factor of 10 lower than for ferritic steel and firom about a factor of 5
  • the steel alloy specimens of this invention used for the tests given in Tables II and III were 4 inches long with a 1.5 inch gauge length and a gauge diameter of 0.375 inch.
  • An alloy having improved high temperature properties consisting essentially offrom about 0.4% to about 7.5% chromium from about 0.4% to about 4.0% molybdenum from about 0.05% to about 0.4% carbon from about 0.1% to about 1.5% manganese from about 0.1 to about 1.0% niobium from about 0.1% to about 1.4% titanium and the remainder essentially iron.
  • An alloy having improved high temperature properties consisting essentially offrom about 2.0% to less than 4.0% chromium from about 1.0% to about 2.0% molybdenum from about 0.05% to about 0.4% carbon from about 0.1% to about 1.5% manganese from about 0.1% to about 1.0% niobium from about 0.11% to about 1.4% titanium and the remainder essentially iron.
  • An alloy having improved high temperature properties consisting essentially ofabout 2.25% chromium about 1.0% molybdenum about 0.15% carbon about 0.5% manganese about 0.4% niobium about 0.4% titanium about 0.1% (max.) boron about 0.02% (max.) nitrogen about 0.2% (max) aluminum about 1.5% (max.) silicon about 0.03% (max.) phosphorus about 0.03% (max.) sulfur and the remainder essentially iron.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)
US850117A 1959-11-02 1959-11-02 Steel alloy composition Expired - Lifetime US3044872A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US850117A US3044872A (en) 1959-11-02 1959-11-02 Steel alloy composition
GB36720/60A GB921838A (en) 1959-11-02 1960-10-26 Steel alloy composition
CH1229560A CH415068A (fr) 1959-11-02 1960-11-02 Alliage d'acier
BE596717A BE596717A (fr) 1959-11-02 1960-11-03 Nouvel alliage.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US850117A US3044872A (en) 1959-11-02 1959-11-02 Steel alloy composition

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BE (1) BE596717A (fr)
CH (1) CH415068A (fr)
GB (1) GB921838A (fr)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3110636A (en) * 1961-12-21 1963-11-12 Gen Electric High temperature turbine rotor shafts and method of heat treating
US3295964A (en) * 1961-12-28 1967-01-03 Fujikoshi Kk Titanium-tantalum high-speed steel
US3476909A (en) * 1965-06-17 1969-11-04 Mitsubishi Heavy Ind Ltd Method of deposit welding chromium steels
US3770394A (en) * 1970-09-14 1973-11-06 Crucible Inc Stainless steel tubing with a maximum titanium to carbon ratio of 6
US3819364A (en) * 1972-09-29 1974-06-25 Deutsche Edelstahlwerke Gmbh Welding hard metal composition
US3847600A (en) * 1969-08-27 1974-11-12 Nippon Kokan Kk High temperature alloy steel
US4058650A (en) * 1975-07-11 1977-11-15 Hitachi Metals, Ltd. Back material of metal band saw high in fatigue strength
US4129442A (en) * 1976-01-14 1978-12-12 Kawasaki Jukogyo Kabushiki Kaisha Wear- and impact-resisting cast steel
DE2907152A1 (de) * 1978-02-24 1979-08-30 Nippon Steel Corp Stahlblech mit hoher nitrat-spannungsrisskorrosionsbestaendigkeit
US4249961A (en) * 1976-03-06 1981-02-10 Harri Nevalainen High strength steel for diffusion chromizing
US4261768A (en) * 1979-06-27 1981-04-14 Voest-Alpine Aktiengesellschaft Low alloyed steel having improved corrosion behavior, in particular relative to sea water
US4353743A (en) * 1979-05-29 1982-10-12 Bethlehem Steel Corporation Steel composition for chipper knife
GB2179674A (en) * 1985-07-25 1987-03-11 Nippon Kokan Kk 9% Chromium heat-resistant steel
EP0461652A1 (fr) * 1990-06-14 1991-12-18 Togo Seisakusyo Corporation Collier de serrage en forme de bande pour tuyaux souples et leur procédé de fabrication
EP0632139A1 (fr) * 1993-06-28 1995-01-04 Thyssen Stahl Aktiengesellschaft Utilisation d'un acier pour travail à chaud
EP0643148A4 (fr) * 1993-03-12 1995-06-14 Nippon Steel Corp Materiau en acier pour partie d'arbre trempee par induction et partie d'arbre ainsi produite.
US5492573A (en) * 1993-04-19 1996-02-20 Hitachi Metals, Ltd. High-strength stainless steel for use as material of fuel injection nozzle or needle for internal combustion engine, fuel injection nozzle made of the stainless steel
US5595614A (en) * 1995-01-24 1997-01-21 Caterpillar Inc. Deep hardening boron steel article having improved fracture toughness and wear characteristics

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5927376B2 (ja) * 1980-08-29 1984-07-05 川崎製鉄株式会社 板厚75mm以上の石油精製装置、石炭液化装置および石炭ガス化装置その他圧力容器に供せられるCr−Mo鋼材
ZA847054B (en) * 1983-09-14 1986-04-30 Chamber Of Mines Services Ltd A new steel
JPS61174322A (ja) * 1985-01-28 1986-08-06 Nippon Steel Corp 機械構造用鋼の圧延材軟質化法
US5310431A (en) * 1992-10-07 1994-05-10 Robert F. Buck Creep resistant, precipitation-dispersion-strengthened, martensitic stainless steel and method thereof
US6890393B2 (en) 2003-02-07 2005-05-10 Advanced Steel Technology, Llc Fine-grained martensitic stainless steel and method thereof
US6899773B2 (en) 2003-02-07 2005-05-31 Advanced Steel Technology, Llc Fine-grained martensitic stainless steel and method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2159723A (en) * 1935-06-18 1939-05-23 Union Carbide & Carbon Corp Apparatus subjected to heat and cold alternately
US2194178A (en) * 1936-06-24 1940-03-19 Electro Metallurg Co Low alloy steel
US2513935A (en) * 1947-12-13 1950-07-04 Jessop William & Sons Ltd Alloy steels
US2590835A (en) * 1948-12-16 1952-04-01 Firth Vickers Stainless Steels Ltd Alloy steels
US2905577A (en) * 1956-01-05 1959-09-22 Birmingham Small Arms Co Ltd Creep resistant chromium steel

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2159723A (en) * 1935-06-18 1939-05-23 Union Carbide & Carbon Corp Apparatus subjected to heat and cold alternately
US2194178A (en) * 1936-06-24 1940-03-19 Electro Metallurg Co Low alloy steel
US2513935A (en) * 1947-12-13 1950-07-04 Jessop William & Sons Ltd Alloy steels
US2590835A (en) * 1948-12-16 1952-04-01 Firth Vickers Stainless Steels Ltd Alloy steels
US2905577A (en) * 1956-01-05 1959-09-22 Birmingham Small Arms Co Ltd Creep resistant chromium steel

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3110636A (en) * 1961-12-21 1963-11-12 Gen Electric High temperature turbine rotor shafts and method of heat treating
US3295964A (en) * 1961-12-28 1967-01-03 Fujikoshi Kk Titanium-tantalum high-speed steel
US3476909A (en) * 1965-06-17 1969-11-04 Mitsubishi Heavy Ind Ltd Method of deposit welding chromium steels
US3847600A (en) * 1969-08-27 1974-11-12 Nippon Kokan Kk High temperature alloy steel
US3770394A (en) * 1970-09-14 1973-11-06 Crucible Inc Stainless steel tubing with a maximum titanium to carbon ratio of 6
US3819364A (en) * 1972-09-29 1974-06-25 Deutsche Edelstahlwerke Gmbh Welding hard metal composition
US4058650A (en) * 1975-07-11 1977-11-15 Hitachi Metals, Ltd. Back material of metal band saw high in fatigue strength
US4129442A (en) * 1976-01-14 1978-12-12 Kawasaki Jukogyo Kabushiki Kaisha Wear- and impact-resisting cast steel
US4249961A (en) * 1976-03-06 1981-02-10 Harri Nevalainen High strength steel for diffusion chromizing
DE2907152A1 (de) * 1978-02-24 1979-08-30 Nippon Steel Corp Stahlblech mit hoher nitrat-spannungsrisskorrosionsbestaendigkeit
US4353743A (en) * 1979-05-29 1982-10-12 Bethlehem Steel Corporation Steel composition for chipper knife
US4261768A (en) * 1979-06-27 1981-04-14 Voest-Alpine Aktiengesellschaft Low alloyed steel having improved corrosion behavior, in particular relative to sea water
GB2179674A (en) * 1985-07-25 1987-03-11 Nippon Kokan Kk 9% Chromium heat-resistant steel
DE3624669A1 (de) * 1985-07-25 1987-03-12 Nippon Kokan Kk Hitzebestaendiger 9%-chromstahl hervorragender zaehigkeit, hoher rissbestaendigkeit und hoher dauerstandfestigkeit bei schweissverbindungen
GB2179674B (en) * 1985-07-25 1989-08-23 Nippon Kokan Kk 9% chromium heat-resistant steel excellent in toughness and having high cracking resistance and high creep strength in welded joint
US5116571A (en) * 1985-07-25 1992-05-26 Nippon Kokan Kabushiki Kaisha Chromoum heat-resistant steel excellent in toughness and having high cracking resistance and high creep strength in welded joint
EP0461652A1 (fr) * 1990-06-14 1991-12-18 Togo Seisakusyo Corporation Collier de serrage en forme de bande pour tuyaux souples et leur procédé de fabrication
EP0643148A4 (fr) * 1993-03-12 1995-06-14 Nippon Steel Corp Materiau en acier pour partie d'arbre trempee par induction et partie d'arbre ainsi produite.
US5545267A (en) * 1993-03-12 1996-08-13 Nippon Steel Corporation Steel product for induction-hardened shaft component and shaft component using the same
US5492573A (en) * 1993-04-19 1996-02-20 Hitachi Metals, Ltd. High-strength stainless steel for use as material of fuel injection nozzle or needle for internal combustion engine, fuel injection nozzle made of the stainless steel
EP0632139A1 (fr) * 1993-06-28 1995-01-04 Thyssen Stahl Aktiengesellschaft Utilisation d'un acier pour travail à chaud
US5595614A (en) * 1995-01-24 1997-01-21 Caterpillar Inc. Deep hardening boron steel article having improved fracture toughness and wear characteristics

Also Published As

Publication number Publication date
BE596717A (fr) 1961-05-03
CH415068A (fr) 1966-06-15
GB921838A (en) 1963-03-27

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