US2187525A - Article of welded construction - Google Patents

Article of welded construction Download PDF

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Publication number
US2187525A
US2187525A US276230A US27623039A US2187525A US 2187525 A US2187525 A US 2187525A US 276230 A US276230 A US 276230A US 27623039 A US27623039 A US 27623039A US 2187525 A US2187525 A US 2187525A
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US
United States
Prior art keywords
vanadium
chromium
carbon
article
austenitic
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
US276230A
Inventor
Schafmeister Paul
Houdremont Eduard
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.)
KRUPP NIROSTA Co Inc
KRUPP NIROSTA COMPANY Inc
Original Assignee
KRUPP NIROSTA Co Inc
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
Priority claimed from US393835A external-priority patent/US2186710A/en
Application filed by KRUPP NIROSTA Co Inc filed Critical KRUPP NIROSTA Co Inc
Priority to US276230A priority Critical patent/US2187525A/en
Application granted granted Critical
Publication of US2187525A publication Critical patent/US2187525A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/939Molten or fused coating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12639Adjacent, identical composition, components
    • Y10T428/12646Group VIII or IB metal-base
    • Y10T428/12653Fe, containing 0.01-1.7% carbon [i.e., steel]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12972Containing 0.01-1.7% carbon [i.e., steel]
    • Y10T428/12979Containing more than 10% nonferrous elements [e.g., high alloy, stainless]

Definitions

  • Our invention relates to corrosion-proof articles composed of austenitic chromium nickel steel alloys containing vanadium.
  • austcnitic chromium nickel steel alloys hitherto employed as chemically neutral, become brittle, and are no longer resistant, for instance, to the attack of acid or salt solutions, when they have experienced a heating up to about 500-800 C., which can be compared to a drawing treatment, as occurs, for instance, in welding constructional parts. It has already been proposed, with satisfying results, to employ for the manufacture of objects of austenitic chromium nickel steel alloys, which, either in their manufacture or during service, are exposed to a heating equivalent to a drawing treatment, and cannot subsequently be given a high heat treatment, to restore the pure austenitic condition, austenitic chromium nickel steel alloys, the carbon content of which is less than 07%.
  • This invention has for its object to afford ,another solution of this problem by which the tech- .nical difficulty of lowering the carbon content to very slight values is avoided.
  • This object is obtained, according to the invention, by adding to the austenitic chromium nickel steel alloys, for instance, to thosecontaining from 18-25% of chromium and '7-12% of nickel, to prevent them from becoming brittle-short when heated up to the chromium carbide precipitation range of about 500-800" C., an alloy constituent, to wit, vanadium. Vanadium forms a stable chemical compound with a portion of the carbon dissolved in the austenitic base structure. The proportion of vanadium to the carbon is so determined that practically all of the carbon is bound to this alloy constituent.
  • vanadium has the effect of binding to itself almost the entire carbon, in a manner not jeopardizing the chemical stability of the alloy, so that the base structure, which, as to the rest, is austenitic, is practically free of dissolved carbon, which therefore cannot assume another form, and thus cause the alloy to become brittle when the alloy is heated to about 500- 800 C.
  • Our invention is'of particular value in connection with articles of welded construction, for use in the chemical and metallurgical fields, which, without being annealed after welding, stubbornly resist intergranular corrosion within the zone tempered by the welding operation when subjected to corroding media, because substantially the whole Within this range, the range usually preferred for commercial construction'is approximately 18% chromium, about 8 or 9% nickel, carbon from .2%, and vanadium irom sists intergranular corrosion within the zone tempered by the welding operaticn-whensubjected to corroding media, and which is made.
  • oi a stable austenitic alloy composed oi approximately 18 to.

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)
  • Arc Welding In General (AREA)

Description

Patented Jan. 16, 1940 UNITED STATES PATENT OFFICE,
ARTICLE OF WELDED CONSTRUCTION No Drawing. Original application September 19,
1929, Serial No. 393,835. Divided and this appiication May 27, 1939, Serial No. 276,230. In
Germany June 26, 1929 4 Claims.
Our invention relates to corrosion-proof articles composed of austenitic chromium nickel steel alloys containing vanadium.
This application is a division of our application Serial No. 393,835, filed September 19, 1929.
Experience has shown that austcnitic chromium nickel steel alloys, hitherto employed as chemically neutral, become brittle, and are no longer resistant, for instance, to the attack of acid or salt solutions, when they have experienced a heating up to about 500-800 C., which can be compared to a drawing treatment, as occurs, for instance, in welding constructional parts. It has already been proposed, with satisfying results, to employ for the manufacture of objects of austenitic chromium nickel steel alloys, which, either in their manufacture or during service, are exposed to a heating equivalent to a drawing treatment, and cannot subsequently be given a high heat treatment, to restore the pure austenitic condition, austenitic chromium nickel steel alloys, the carbon content of which is less than 07%. This invention has for its object to afford ,another solution of this problem by which the tech- .nical difficulty of lowering the carbon content to very slight values is avoided. This object is obtained, according to the invention, by adding to the austenitic chromium nickel steel alloys, for instance, to thosecontaining from 18-25% of chromium and '7-12% of nickel, to prevent them from becoming brittle-short when heated up to the chromium carbide precipitation range of about 500-800" C., an alloy constituent, to wit, vanadium. Vanadium forms a stable chemical compound with a portion of the carbon dissolved in the austenitic base structure. The proportion of vanadium to the carbon is so determined that practically all of the carbon is bound to this alloy constituent. Tests made with two chromium nickel steel alloys that contained about 18% of chromium, 9% of nickel,,.12% of carbon, and, respectively, and 2% of vanadium, have shown that steel alloys of this type are fully resistant to active chemical attacks even when in a condition resulting from exposure to a heat-. ing up to about 500-800" C. without a subsequent high heat treatment. Measurements of the magnetic saturation made to investigate the structure have shown that the values of magnetic saturation of the material, when quenched and drawn, are not substantially higher than those of the magnetic saturation of the same material when merely quenched. For comparison purposes, it may be noted that the'corresponding values of a vanadiumless austenitic chromium nickel steel alloy are far higher in the temperature range oi 500800 C. than in a cool state; The fact that the values of saturation are practically equal in the re-heated and in the quenched state in contradlstinction to vanadiumless chromium nickel steels proves that in the vanadium chromium nickel steel alloys, the drawing operation is much less capable of altering the nature of the base structure than in the corresponding vanadiumless chromium nickel steel alloys. In the inventors opinion the reason for this phenomenon resides in the following:
The presence of vanadium has the effect of binding to itself almost the entire carbon, in a manner not jeopardizing the chemical stability of the alloy, so that the base structure, which, as to the rest, is austenitic, is practically free of dissolved carbon, which therefore cannot assume another form, and thus cause the alloy to become brittle when the alloy is heated to about 500- 800 C.
Potential tests, made with the above two vanadium chromium nickel steel alloys, have shown that these alloys, even after having been drawn to'about 500-800 C., and tested in a solution of sulfuric acid of 5%, at room temperature, and practically freed from oxygen by evacuation, possess a potential that is above the potential of hydrogen, while corresponding austenitic chromium nickel steel alloys that do not contain vanadium, after re-heating and under equal conditions, show a potential which is below that of hydrogen. The addition of vanadium therefore causes an increase of the potential beyond that of hydrogen, and thus an increase of the chemical stability, whereby these alloys are made resistant to very severe attacks by chemical agents, and, more particularly, are protected from becoming brittle under the action of a drawing treatment.
Our invention is'of particular value in connection with articles of welded construction, for use in the chemical and metallurgical fields, which, without being annealed after welding, stubbornly resist intergranular corrosion within the zone tempered by the welding operation when subjected to corroding media, because substantially the whole Within this range, the range usually preferred for commercial construction'is approximately 18% chromium, about 8 or 9% nickel, carbon from .2%, and vanadium irom sists intergranular corrosion within the zone tempered by the welding operaticn-whensubjected to corroding media, and which is made. oi a stable austenitic alloy composed oi approximately 18 to. 25% chromium, approximately 7 to 12% nickel, a small proportion of carbon, and vanadium, the vanadium and the carbon being present in the a'l-= loy in such proportions and relation to each other, that practically the whole of said carbon in said alloy appears therein in stable combination with the vanadium, iron constituting substantially the entire balance.
2. An article of welded construction for use in the chemical and metallurgical fields which, without being annealed after welding, stubbornly re sists intergranular corrosion within the zone tempered by the welding operation when subjected to corroding media, and which is made of a stable austenitic alloy composed of approximately 18 to 25% chromium, approximately 7 to 12% nickel,
carbon less than 1%, vanadium up to approximately 6%, iron constituting substantially the" entire balance.
3. An article of welded construction for use in the chemical and metallurgical fields which, without being annealed after welding, stubbornly resists intergranular corrosion within the zone ternpered by the weldingoperatioh when subjected to corrodingmedia, and which is made of a stable austeniticalloy composed of about 18% chromium, about 9% nickel, about .12% carbon, and about .5 to 2% vanadium, iron constituting substantially theentire balance. l
PAUL scnamms'ma.
,EDUARD HOUDREMONT.
US276230A 1929-09-19 1939-05-27 Article of welded construction Expired - Lifetime US2187525A (en)

Priority Applications (1)

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US276230A US2187525A (en) 1929-09-19 1939-05-27 Article of welded construction

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US393835A US2186710A (en) 1929-06-26 1929-09-19 Steel alloy
US276230A US2187525A (en) 1929-09-19 1939-05-27 Article of welded construction

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2495835A (en) * 1945-10-15 1950-01-31 George N Hibben Light-colored enameled steel article
US2759249A (en) * 1950-06-20 1956-08-21 Babcock & Wilcox Co Welding dissimilar metal members with welded joint, including stabilized ferritic metal zone
US2770030A (en) * 1950-06-15 1956-11-13 Babcock & Wilcox Co Welded joint between dissimilar metals
US3377162A (en) * 1964-09-10 1968-04-09 Rand Mines Ltd Stainless steel
US20160279739A1 (en) * 2013-11-29 2016-09-29 Mitsubishi Heavy Industries, Ltd. Method for determining characteristic stress of welding structure, method for designing welded structure, and method for manufacturing welded structure

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2495835A (en) * 1945-10-15 1950-01-31 George N Hibben Light-colored enameled steel article
US2770030A (en) * 1950-06-15 1956-11-13 Babcock & Wilcox Co Welded joint between dissimilar metals
US2759249A (en) * 1950-06-20 1956-08-21 Babcock & Wilcox Co Welding dissimilar metal members with welded joint, including stabilized ferritic metal zone
US3377162A (en) * 1964-09-10 1968-04-09 Rand Mines Ltd Stainless steel
US20160279739A1 (en) * 2013-11-29 2016-09-29 Mitsubishi Heavy Industries, Ltd. Method for determining characteristic stress of welding structure, method for designing welded structure, and method for manufacturing welded structure
US9931715B2 (en) * 2013-11-29 2018-04-03 Mitsubishi Heavy Industries, Ltd. Method for determining characteristic stress of welding structure, method for designing welded structure, and method for manufacturing welded structure

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