US3110586A - High strength normalized steel - Google Patents

High strength normalized steel Download PDF

Info

Publication number
US3110586A
US3110586A US125345A US12534561A US3110586A US 3110586 A US3110586 A US 3110586A US 125345 A US125345 A US 125345A US 12534561 A US12534561 A US 12534561A US 3110586 A US3110586 A US 3110586A
Authority
US
United States
Prior art keywords
steel
high strength
normalized
alloy
toughness
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
US125345A
Inventor
John A Gulya
Jr Roy Hetherington
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.)
Lukens Steel Co
Original Assignee
Lukens Steel Co
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 Lukens Steel Co filed Critical Lukens Steel Co
Priority to US125345A priority Critical patent/US3110586A/en
Application granted granted Critical
Publication of US3110586A publication Critical patent/US3110586A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten

Definitions

  • Structural and pressure vessel applications frequently require a steel to be used in a broad range of section thicknesses.
  • available steels are particularly sensitive to section thickness in that they generally exhibit a marked reduction of properties in heavier gauges.
  • Several methods are used to oifset this characteristic property decrease. In some cases, a number of steels are employed together and thereby problems such as inventory, identification, and joining, are multiplied. in other cases, a premium steel is used in lighter sections to provide the required properties in the heavier sections. In still other cases, a steel that is adequate only in the lighter sections will be used, but the heavier sections Will be subjected to rapid cooling from austenitizing temperatures to achieve nearly equivalent properties. This procedure also increases the manufacturing costs and generally provides a material of reduced weldability.
  • Steels used in structural and pressure vessel applications should exhibit weldability, uniform high strength and notch toughness throughout a wide range of section thicknesses.
  • the amount of carbon should below and the tensile strength and notch toughness of the steel increased with low amounts of selected alloying elements.
  • the problem of selecting the proper balance of alloying elements for a steel useful in structural and pressure vessel applications is a difficult one, especially if substantially uniform strengths over a broad range of section thicknesses are to be obtained. This is evidenced in the available steels which exhibit decreased strength accompanied by a marked reduction in notch toughness in the heavier sections.
  • ,It is another object of the present invention to provide a low-carbon, low-alloy steel that is particularly useful in structural and pressure vessel applications having high section thicknesses.
  • the preferred alloy will contain the alloying elements in the following ranges.
  • Element Percent by weight Carbon 0.12 to 0.20 Manganese"; 0.95 to 1.45 Phosphorus Up to 0.035 Sulphur Up to 0.040 'Silicon 0.11 to 0.30 Nickel 0.70 to 1.00 Chromium 0.40 to 0.65 Molybdenum 0.25 to 0.45 Vanadium 0.03 to 0.08
  • Sections of plate approximately one inch and six inches gage were normalized at 1700 -F., allowed to cool to air temperatureand tempered at 1100" F. Treatment times were two and four hours for the one and six inch sections respectively. Analysis of the alloy fol-lows.
  • Element 7 Percentage by weight, Carbon 0.14 Manganese 1.22 Phosphorus 0.020 Sulphur 0.024 Silicon 0.17 Nickel g 0.84 Chromium 0. 60 Molybdenum 0.38 Vanadium 0.04- Copper 0.2!5 Balance iron and incidental steel-making residuals.
  • the amount of carbon should be at the maximum of the permissible ranges if abrasion resistance is desired.
  • An improved weldable normalized steel consisting of Element: Percent by weight Carbon 0.1 to 0.2 8 Manganese 0.9 to 1.45 Phosphorus Up to 0.04 Sulphur Up to 0.05 lSilicon 0.11 to 0.4 0 Nickel 0.5 to 1.00 Chromium 0.35 to 0.70 Molybdenum 0.25 to 0.50 Vanadium 0.02 to 0.10
  • said steel being characterized in having high uniform strength and toughness through a wide range of thicknesses.
  • An improved weldable normalized steel consisting of Element: Percent by weight Carbon 0.12 to 0.20 Manganese 0.95 to 1.45 Phosphorus Up to 0.035 Sulphur Up to 0.040
  • said steel being characterized in having high uniform strength and toughness through a wide range of thicknesses.
  • An improved weldable normalized steel consisting of said steel being characterized in having high uniform strength and toughness through a Wide range of thicknesses.
  • An improved weldable normalized steel consisting of Element: l Percent by weight said steel being characterized in having high uniform Carbon 0.12 to 0.20 strength and toughness through a wide range of thick- Manganese 0.95 to 1.45 nesses. Phosphorus Up to 0.035 Sulphur Up to 0.040 References Cited in the file of this patent 33 3 8-28 5 UNITED STATES PATENTS m 0 70 Gaspali at al A g 28, ch.0m;I.gjjjjjjjjjjjjjjjjjjjjjjjj: 0140 to 0165 2,798,805 Hodge m1 July 9,1957 Molybdenum 0.25 to 0.45 Vanadium 0.03 to 0.08 10 Copper 0.25 to 0.45

Landscapes

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

Description

United States Patent 3,110,586 HIGH STRENGTH NORMALIZED STEEL John A. Gulya, Lancaster, and Roy Hetherington, In, West Chester, Pa., assignors to Lukens Steel Company, Coatesville, Pa., a corporation of Pennsylvania No Drawing. Filed July 20, 1961, Ser. No. 125,345 4 Claims. (Cl. 75-128) The present invention relates to a normalized and tempered alloy steel providing uniform strength combined with good notch toughness and Weldability through a wide range of section thicknesses without resorting to chemistry changes or accelerated cooling rates from austenitizing temperatures for the larger sections of metal.
Structural and pressure vessel applications frequently require a steel to be used in a broad range of section thicknesses. Unfortunately, available steels are particularly sensitive to section thickness in that they generally exhibit a marked reduction of properties in heavier gauges. Several methods are used to oifset this characteristic property decrease. In some cases, a number of steels are employed together and thereby problems such as inventory, identification, and joining, are multiplied. in other cases, a premium steel is used in lighter sections to provide the required properties in the heavier sections. In still other cases, a steel that is adequate only in the lighter sections will be used, but the heavier sections Will be subjected to rapid cooling from austenitizing temperatures to achieve nearly equivalent properties. This procedure also increases the manufacturing costs and generally provides a material of reduced weldability.
Steels used in structural and pressure vessel applications should exhibit weldability, uniform high strength and notch toughness throughout a wide range of section thicknesses. In order to insure excellent weldability, the amount of carbon should below and the tensile strength and notch toughness of the steel increased with low amounts of selected alloying elements. But, the problem of selecting the proper balance of alloying elements for a steel useful in structural and pressure vessel applications is a difficult one, especially if substantially uniform strengths over a broad range of section thicknesses are to be obtained. This is evidenced in the available steels which exhibit decreased strength accompanied by a marked reduction in notch toughness in the heavier sections.
It is an object of the present invention to provide an improved weldable normalized steel that is characterized by high strength and excellent notch toughness over a broad range of thicknesses ithout resorting to chemistry changes or quenching from austenitizing temperatures for heavier sections.
,It is another object of the present invention to provide a low-carbon, low-alloy steel that is particularly useful in structural and pressure vessel applications having high section thicknesses.
It is still another object of the present invention to provide an economical combination of alloying elements that Will have the above desirable characteristics.
The foregoing problems are avoided to a large extent, and the above objects are achieved in the present invention by the provision of a new, useful, economical combination of alloying elements. In both the normalized, and the normalized and tempered condition, high strength,
3,110,586 Patented Nov. 12, 1963 ice toughness, and weldability are maintained throughout a wide range of section thicknesses by an alloy steel within the following compositional range.
Balance iron and incidental steel-making residuals.
Itwill be apparent that other additives such as 0.25- 0.45% copper for resistance to atmospheric corrosion can be used, replacing a like amount of the iron content. Similarly 0.020.l0% aluminum, other deoxidizers or other commonly used additives to produce fine-grained steels can be included. The preferred alloy will contain the alloying elements in the following ranges.
Element: Percent by weight Carbon 0.12 to 0.20 Manganese"; 0.95 to 1.45 Phosphorus Up to 0.035 Sulphur Up to 0.040 'Silicon 0.11 to 0.30 Nickel 0.70 to 1.00 Chromium 0.40 to 0.65 Molybdenum 0.25 to 0.45 Vanadium 0.03 to 0.08
Balance iron and incidental steel-making residuals.
Sections of plate, approximately one inch and six inches gage were normalized at 1700 -F., allowed to cool to air temperatureand tempered at 1100" F. Treatment times were two and four hours for the one and six inch sections respectively. Analysis of the alloy fol-lows.
Element: 7 Percentage by weight, Carbon 0.14 Manganese 1.22 Phosphorus 0.020 Sulphur 0.024 Silicon 0.17 Nickel g 0.84 Chromium 0. 60 Molybdenum 0.38 Vanadium 0.04- Copper 0.2!5 Balance iron and incidental steel-making residuals.
The test results were as follows:
Yield Tensile Elonga- Reduction Impact, (1,000 (1,000 tion, of Area, tt.-lbs., at p.s.i.) p.s.i.) Percent, Percent 40 Sample 1 (1") 105. 5 120. 9 18. 5 60. 6 20 Sample 2 (6) 99. 5 120. 2 20. 0 56. 3 14 Inorder to demonstrate that the high level of mechanical properties characterizing the alloy can be effectively used in the fabrication and welding of structures, the following test results on welded specimens are cited:
In the standard underbead crack test using E 6010 electrodes, cracking amounting to only 15%. These tests were carried out at 70 F. on 2 X 3" pieces of 1" plate which was split in one-half inch thick samples. In the same tests it is not unusual for the available steels having comparable strengths to exhibit 30 to 50% cracking.
In the foregoing welding test, susceptibility to hydrogen effects appears to be the controlling factor. When welding [with low-hydrogen electrodes, however, hydrogen effects are minimized and joint restraint appears to be the dominant factor. In order to assess alloy steels under such conditions, a test developing greater restraint, such as the standard cruciform test, was used. The results of this test' may be expressed quantitatively by determining the percentage underbead cracking in the third pass. Conducting this test on the subject steel using A diameter 12016 electrodes to deposit a /8" fillet at room temperature resulted in only 20% cracking.
Another important measure of the wel -dability of a steel is the ductility of the heat-aifected-zone of welded joints. While this zone is frequently brittle in the available steels in either or both the as-welded and stressrelieved conditions, the heat-alfected-zone Olf the steel of the present invention is more ductile in either condition than the parent metal. For example, butt Welds were made in /3" plate (machined from the above 1 plate) using the above described 12016 electrodes, half of which were stress-relieved at 1100 F. Standard V- notch Charpy specimens were machined from these samples and tested at -80 F. The following table shows the improved ductility obtained:
Parent metal 11 As-lwelded HAZ 2'8 Stress-relieved HAZ 26 Additional 6" thick samples having the following alloy contents were tested:
The following table indicates the excellent characteristics of these alloys:
Yleld Tensile Elonga- Reduction Impact (1,000 (1,000 tion, of Area, at 40 p.s.i.) p.s.i.) Percent, Percent F. ft.-lbs. in 2' Sample 3 (6") 105. 5 116.3 19 51.0 19 Sample 4 (6) 116. 7, 133. 6 16 50. 5 12 Thus the above .data demonstrate that the low-alloy low-carbon steels of the present invention develop uniformly high strength, toughness and weldability throughout a wide range of section thicknesses Without resorting to drastic changes in alloy content or quenching from austenitizing temperatures for the heavier sections.
In all OLf the above alloys the amount of carbon should be at the maximum of the permissible ranges if abrasion resistance is desired.
Throughout the specification and in the claims, percentages are by 'weight. The specific embodiments are intended to be illustrative but not limiting. All modifications and variations that fall within the meaning and purview of equivalency of the claims are therefore intended to be embraced thereby. It will thus be understood that no limitations of the scope of the invention are contemplated by the employment of specific language and that various alterations and modifications may be made such as would occur to one skilled in the art to which the invention relates.
We claim:
1. An improved weldable normalized steel consisting of Element: Percent by weight Carbon 0.1 to 0.2 8 Manganese 0.9 to 1.45 Phosphorus Up to 0.04 Sulphur Up to 0.05 lSilicon 0.11 to 0.4 0 Nickel 0.5 to 1.00 Chromium 0.35 to 0.70 Molybdenum 0.25 to 0.50 Vanadium 0.02 to 0.10
Balance iron and incidental steel-making residuals.
said steel being characterized in having high uniform strength and toughness through a wide range of thicknesses.
2. An improved weldable normalized steel consisting of Element: Percent by weight Carbon 0.12 to 0.20 Manganese 0.95 to 1.45 Phosphorus Up to 0.035 Sulphur Up to 0.040
v Silicon 0.11 to 0. 30 Nickel 0.70 to 1.00 Chromium 0.40 to 0.6 5 Molybdenum 0.25 to 0.45 Vanadium 0.03 to 0.08
Balance iron and incidental steel-making residuals,
said steel being characterized in having high uniform strength and toughness through a wide range of thicknesses.
3. An improved weldable normalized steel consisting of said steel being characterized in having high uniform strength and toughness through a Wide range of thicknesses.
4. An improved weldable normalized steel consisting of Element: l Percent by weight said steel being characterized in having high uniform Carbon 0.12 to 0.20 strength and toughness through a wide range of thick- Manganese 0.95 to 1.45 nesses. Phosphorus Up to 0.035 Sulphur Up to 0.040 References Cited in the file of this patent 33 3 8-28 5 UNITED STATES PATENTS m 0 70 Gaspali at al A g 28, ch.0m;I.gjjjjjjjjjjjjjjjjjjjjj: 0140 to 0165 2,798,805 Hodge m1 July 9,1957 Molybdenum 0.25 to 0.45 Vanadium 0.03 to 0.08 10 Copper 0.25 to 0.45
Balance iron and incidental steel-making residuals,
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,110 586 November 12, 1963 John A, Gulya et a1,
It is hereby certified that error appears in the above numbered patent requiring correction and that the said Letters Patent should read as correc ted below Column 2 line 14 v for "020 to 0. 10" read 0.02 to 0.10 same column 2 in the table at the bottom of the column, the third heading should appear as shown below instead of as in the patent:
Elongation Per-cent in 2 Signed and sealed this 21st day of April 1964.
(SEAL) Attest:
ERNEST W. SWIDER EDWARD J. BRENNER Attesting Officer Commissioner of Patents

Claims (1)

1. AN IMPROVED WELDABLE NORMALIZED STEEL CONSISTING OF ELEMENT PERCENT BY WEIGHT CARBON 0.1 TO 0.28 MANGANESE 0.9 TO 1.45 PHOSPHORUS UP TO 0.04 SULPHUR UP TO 0.05 SILICON 0.11 TO 0.40 NICKEL 0.5 TO 1.00 CHROMIUM 0.35 TO 0.70 MOLYBDENUM 0.25 TO 0.50 VANADIUM 0.02 TO 0.10 BALANCE IRON AND INCIDENTAL STEEL-MAKINE RESIDUALS.
US125345A 1961-07-20 1961-07-20 High strength normalized steel Expired - Lifetime US3110586A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US125345A US3110586A (en) 1961-07-20 1961-07-20 High strength normalized steel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US125345A US3110586A (en) 1961-07-20 1961-07-20 High strength normalized steel

Publications (1)

Publication Number Publication Date
US3110586A true US3110586A (en) 1963-11-12

Family

ID=22419310

Family Applications (1)

Application Number Title Priority Date Filing Date
US125345A Expired - Lifetime US3110586A (en) 1961-07-20 1961-07-20 High strength normalized steel

Country Status (1)

Country Link
US (1) US3110586A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258372A (en) * 1963-01-21 1966-06-28 Int Nickel Co Martensitic low alloy plate steel
US3403060A (en) * 1964-06-18 1968-09-24 Yawata Iron & Steel Co Weldable high tensile strength steel capable of giving weld heat-affected zone having high toughness and joint strength
US3418110A (en) * 1964-01-22 1968-12-24 Goda Susumu Hardenable steel material containing aluminum
US3955971A (en) * 1974-12-11 1976-05-11 United States Steel Corporation Alloy steel for arctic service
US4175987A (en) * 1977-08-04 1979-11-27 Otis Engineering Corporation Low alloy tempered martensitic steel
US4185998A (en) * 1978-12-07 1980-01-29 United States Steel Corporation Steel with improved low temperature toughness
US4251273A (en) * 1979-03-02 1981-02-17 Smith David T Method of forming valve lifters
US4318739A (en) * 1979-06-05 1982-03-09 A. Finkl & Sons Co. Steel having improved surface and reduction of area transverse properties, and method of manufacture thereof
EP0974678A1 (en) * 1998-07-21 2000-01-26 Creusot-Loire Industrie Process and steel for the manufacturing of welded vessels, intended for use in the presence of hydrogen sulphide

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2565953A (en) * 1948-04-08 1951-08-28 Terni Ind Elettr Low alloy steel of high mechanical strength, little sensitive to quenching, weldable, etc.
US2798805A (en) * 1954-09-03 1957-07-09 United States Steel Corp Wrought railroad wheels made of alloy steels

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2565953A (en) * 1948-04-08 1951-08-28 Terni Ind Elettr Low alloy steel of high mechanical strength, little sensitive to quenching, weldable, etc.
US2798805A (en) * 1954-09-03 1957-07-09 United States Steel Corp Wrought railroad wheels made of alloy steels

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258372A (en) * 1963-01-21 1966-06-28 Int Nickel Co Martensitic low alloy plate steel
US3418110A (en) * 1964-01-22 1968-12-24 Goda Susumu Hardenable steel material containing aluminum
US3403060A (en) * 1964-06-18 1968-09-24 Yawata Iron & Steel Co Weldable high tensile strength steel capable of giving weld heat-affected zone having high toughness and joint strength
US3955971A (en) * 1974-12-11 1976-05-11 United States Steel Corporation Alloy steel for arctic service
US4175987A (en) * 1977-08-04 1979-11-27 Otis Engineering Corporation Low alloy tempered martensitic steel
US4185998A (en) * 1978-12-07 1980-01-29 United States Steel Corporation Steel with improved low temperature toughness
US4251273A (en) * 1979-03-02 1981-02-17 Smith David T Method of forming valve lifters
US4318739A (en) * 1979-06-05 1982-03-09 A. Finkl & Sons Co. Steel having improved surface and reduction of area transverse properties, and method of manufacture thereof
EP0974678A1 (en) * 1998-07-21 2000-01-26 Creusot-Loire Industrie Process and steel for the manufacturing of welded vessels, intended for use in the presence of hydrogen sulphide
FR2781506A1 (en) * 1998-07-21 2000-01-28 Creusot Loire PROCESS AND STEEL FOR THE MANUFACTURE OF A HOT WATER ENCLOSURE WORKING IN THE PRESENCE OF HYDROGEN SULPHIDE
US6322642B1 (en) 1998-07-21 2001-11-27 Creusot Loire Industrie Process and steel for the manufacture of a pressure vessel working in the presence hydrogen sulfide

Similar Documents

Publication Publication Date Title
US3201233A (en) Crack resistant stainless steel alloys
US3097294A (en) Electric arc welding and wire therefor
US3110586A (en) High strength normalized steel
KR910006030B1 (en) Austenitic stainless steel for low temperature serivece
US3288600A (en) Low carbon, high strength alloy steel
US2432615A (en) Iron-base alloys
US3216823A (en) Low alloy steel
US3118761A (en) Crack resistant austenitic stainless steel alloys
US2894833A (en) Stainless steel for weld
US3649252A (en) Steels resistant to stress corrosion cracking
US2586042A (en) Low-alloy high-yield strength weldable steel
US3660080A (en) Austenitic alloy and weld
US2432616A (en) Ferrous alloys for use at high temperatures
US2949355A (en) High temperature alloy
US3537846A (en) Welding wire and welding strip for cladding stainless layers on unalloyed and low-alloyed structural steels and for other purposes where a stainless filler material with high chromium and nickel contents is required
US2513395A (en) Boron-treated molybdenum steel
US2474766A (en) Alloy steel
Sehsah et al. Dissimilar Welding of Ductile Cast Iron to 304 Stainless Steel
JPH07100688A (en) Tig welding wire for high-strength cr-mo steel
du Toit Filler metal selection for welding a high nitrogen stainless steel
US3258372A (en) Martensitic low alloy plate steel
US3635698A (en) High-strength, high-toughness (iron-carbon-nickel-molybdenum) steel weld metal
US3527920A (en) Welding of alloy steels
US2513467A (en) Alloy article for use at elevated temperatures
US2871118A (en) Resistance to hot-cracking of chromiumnickel steel welds