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EP0292061B1 - Alliage résistant à la corrosion - Google Patents

Alliage résistant à la corrosion Download PDF

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Publication number
EP0292061B1
EP0292061B1 EP88200969A EP88200969A EP0292061B1 EP 0292061 B1 EP0292061 B1 EP 0292061B1 EP 88200969 A EP88200969 A EP 88200969A EP 88200969 A EP88200969 A EP 88200969A EP 0292061 B1 EP0292061 B1 EP 0292061B1
Authority
EP
European Patent Office
Prior art keywords
alloy according
corrosion
structural components
alloy
making structural
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
EP88200969A
Other languages
German (de)
English (en)
Other versions
EP0292061A1 (fr
Inventor
Manfred Dr. Rockel
Ernst Wallis
Michael Dr. Köhler
Ulrich Dr. Heubner
Rolf Kirchheiner
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.)
VDM Nickel Technologie AG
Original Assignee
VDM Nickel Technologie AG
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 VDM Nickel Technologie AG filed Critical VDM Nickel Technologie AG
Priority to AT88200969T priority Critical patent/ATE61420T1/de
Publication of EP0292061A1 publication Critical patent/EP0292061A1/fr
Application granted granted Critical
Publication of EP0292061B1 publication Critical patent/EP0292061B1/fr
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
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • 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
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • 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

  • the invention relates to a modified alloy according to material no. 1.4563 and its use.
  • This known alloy has the following composition:
  • This alloy was developed in order to be able to provide a material that is particularly corrosion-resistant to technical phosphoric acids.
  • the invention has for its object to further improve this known alloy in its corrosion properties without other properties being adversely affected.
  • this goal could be achieved by increasing the molybdenum content to 6 to 7% and also ensuring a nitrogen addition of 0.10 to 0.25%. Due to the increased molybdenum content, the resistance to pitting and crevice corrosion in chloride-containing media is significantly improved during the Nitrogen content stabilizes the austenitic structure and reduces its tendency to excrete TCP phases.
  • the nitrogen content is in the range 0.14 to 0.22%, preferably 0.16 to 0.20% or 0.18%.
  • Table 1 contains information on the chemical composition of 5 by 2 samples which have been subjected to the tests described below. Samples 11 and 12 are examples of the alloy according to the invention, while samples 21 and 22 relate to the starting alloy, which contains less molybdenum and no nitrogen. The table also shows 2 samples from 3 other test alloys. In the following, only the first digit of the sample number is used to identify the 5 different alloys.
  • Table 2 contains information on various properties of the 5 alloys tested for comparison.
  • the alloys are labeled 1 to 5.
  • Column 2 refers to the critical crevice corrosion temperature
  • column 3 to the critical pitting temperature, each in 6% FeCl3 solution.
  • Column 4 contains values for the Corrosion rates in technical phosphoric acid (H3PO4, 72%).
  • Column 5 shows the removal rates under conditions according to ASTM G 28, Practice B.
  • column 6 contains information on the sensitization time with regard to the resistance to intergranular corrosion , ranges being given in each case, because strong fluctuations must be expected.
  • the critical crevice corrosion and pitting temperatures are significantly higher in the alloy according to the invention than in the starting alloy. Temperatures are reached that have previously only been achieved with material 5, which is much higher alloyed.
  • the corrosion rates in technical phosphoric acid are in the range of the comparative alloy No. 2 designed for this purpose. The goal set here, namely to create a material in which the improvement of some properties is not at the expense of other properties.
  • the removal rate according to column 5 is smaller by more than a power of ten for the material according to the invention than for the comparison materials. This is particularly noteworthy because it has previously been assumed that molybdenum only improves the resistance of a material to corrosion in reducing acids. Apparently, the significant improvement now found in oxidizing acids is due to the combined effect of molybdenum and chromium.
  • the removal rates in monochloroacetic acid for three different materials are compared in FIG. 2, namely once for the base material and once for welded material.
  • the material 1 according to the invention performs better in all cases than the comparison materials 2 and 3.
  • test according to ASTM G 28, Practice A is used to examine materials for their resistance to intergranular corrosion. It is carried out in a boiling solution with 50% H2SO4 and 3.7% Fe2 (SO4) 3. Such conditions occur in practice, for example, when handling contaminated sulfuric acids.
  • the test according to ASTM G 28, Practice B, is used to determine the corrosion behavior of materials in strongly oxidizing acids containing metal ions.
  • a boiling solution with 23% H2SO4, 1.2% HCl, 1% FeCl3 and 1% CuCl2 is used. This simulates conditions such as those that occur in pickling plants.
  • Sour gas test tests have been developed to test the resistance to stress corrosion cracking under conditions such as can occur in deep boreholes when searching for natural gas and crude oil.
  • the material according to the invention showed no damage from stress corrosion cracking and no pitting corrosion.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Chemically Coating (AREA)
  • Powder Metallurgy (AREA)
  • Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Materials For Medical Uses (AREA)
  • Secondary Cells (AREA)
  • Prostheses (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)

Claims (11)

1. Alliage avec 30 à 32% de nickel, 26 à 28% de chrome, 0,5 à 1,5% de cuivre au maximum 2% de manganèse, 6 à 7% de molybdène et 0,10 à 0,25% d'azote au maximum 1,0% de silicium, au maximum 2,0% d'aluminium, au maximum 0,03% de carbone, le reste du fer y compris les impuretés inévitables.
2. Alliage selon la revendication 1, caractérisé en ce que la teneur en azote est égale à 0,14 à 0,22%
3. Alliage selon la revendication 1, caractérisé en ce que la teneur en azote est égale à 0,16 à 0,20%
4. Alliage selon la revendication 1, caractérisé en ce que la teneur en azote est égale à environ 0,18%.
5. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent présenter une bonne résistance à la corrosion, en particulier à la corrosion locale et/ou en fissures, dans des milieux aqueux, neutres ou acides, avec une concentration élevée en ions chlorure.
6. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent présenter un taux de dénudation de moins que 0,20 mm/a dans l'acide phosphorique technique avec une concentration en ions chlorure allant jusqu'à 1000 ppm à 100°C.
7. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent présenter un potentiel de corrosion locale d'au moins 1000 mVH à 75°C et d'au moins 800 mVH à 90°C dans des milieux aqueux neutres avec une concentration en ions chlorure d'un ordre de grandeur de 20.000 ppm.
8. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent présenter une température critique de corrosion locale d'au moins 80°C et une température critique de corrosion en fissures d'au moins 50°C, dans les milieux acides avec une concentration en ions chlorure de 50.000 ppm et plus, comme par exemple dans une solution de FeCl₃.
9. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent résister à la corrosion intercristalline dans les conditions selon ASTM G28, practice A.
10. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées qui doivent présenter dans les conditions selon ASTM G28, practice B, à l'état recuit en solution, un taux de dénudation inférieur à 0,5 mm/a.
11. Utilisation de l'alliage selon les revendications 1 à 4 comme matériau pour fabriquer des pièces détachées gui doivent être exemptes de corrosion fissurante due à la contrainte et locale, dans les conditions d'essai agressif au gaz acide.
EP88200969A 1987-05-19 1988-05-14 Alliage résistant à la corrosion Expired - Lifetime EP0292061B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT88200969T ATE61420T1 (de) 1987-05-19 1988-05-14 Korrosionsbestaendige legierung.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3716665 1987-05-19
DE19873716665 DE3716665A1 (de) 1987-05-19 1987-05-19 Korrosionsbestaendige legierung

Publications (2)

Publication Number Publication Date
EP0292061A1 EP0292061A1 (fr) 1988-11-23
EP0292061B1 true EP0292061B1 (fr) 1991-03-06

Family

ID=6327824

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88200969A Expired - Lifetime EP0292061B1 (fr) 1987-05-19 1988-05-14 Alliage résistant à la corrosion

Country Status (12)

Country Link
US (1) US4876065A (fr)
EP (1) EP0292061B1 (fr)
JP (1) JPS6425936A (fr)
KR (1) KR960010598B1 (fr)
AT (1) ATE61420T1 (fr)
AU (1) AU596745B2 (fr)
BR (1) BR8802449A (fr)
CA (1) CA1334801C (fr)
DE (2) DE3716665A1 (fr)
ES (1) ES2021822B3 (fr)
NO (1) NO168313C (fr)
ZA (1) ZA883561B (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4784830A (en) * 1986-07-03 1988-11-15 Inco Alloys International, Inc. High nickel chromium alloy
FR2705689B1 (fr) * 1993-05-28 1995-08-25 Creusot Loire Acier inoxydable austénitique à haute résistance à la corrosion par les milieux chlorurés et sulfuriques et utilisations.
DE4342188C2 (de) * 1993-12-10 1998-06-04 Bayer Ag Austenitische Legierungen und deren Verwendung
WO1997048830A1 (fr) * 1996-06-17 1997-12-24 Sumitomo Metal Industries, Ltd. Alliage possedant une forte teneur en chrome et en nickel et resistant a la corrosion par sulfure d'hydrogene
EP0851037B1 (fr) * 1996-06-17 2002-09-04 Sumitomo Metal Industries, Ltd. Alliage possedant une forte teneur en chrome et en nickel et resistant a la corrosion par sulfure d'hydrogene
US6918967B2 (en) * 2000-03-15 2005-07-19 Huntington Alloys Corporation Corrosion resistant austenitic alloy
SE520027C2 (sv) * 2000-05-22 2003-05-13 Sandvik Ab Austenitisk legering
AT408889B (de) * 2000-06-30 2002-03-25 Schoeller Bleckmann Oilfield T Korrosionsbeständiger werkstoff
US6709528B1 (en) * 2000-08-07 2004-03-23 Ati Properties, Inc. Surface treatments to improve corrosion resistance of austenitic stainless steels
SE527177C2 (sv) * 2001-09-25 2006-01-17 Sandvik Intellectual Property Användning av ett austenitiskt rostfritt stål
MY136087A (en) * 2001-10-22 2008-08-29 Shell Int Research Process to reduce the temperature of a hydrogen and carbon monoxide containing gas and heat exchanger for use in said process
US6740291B2 (en) 2002-05-15 2004-05-25 Haynes International, Inc. Ni-Cr-Mo alloys resistant to wet process phosphoric acid and chloride-induced localized attack
US6764646B2 (en) 2002-06-13 2004-07-20 Haynes International, Inc. Ni-Cr-Mo-Cu alloys resistant to sulfuric acid and wet process phosphoric acid
DE10233961A1 (de) * 2002-07-25 2004-02-12 Schmidt + Clemens Gmbh + Co. Edelstahlwerk Kaiserau Verfahren zum thermischen Spalten von Kohlenwasserstoffen
US20050131263A1 (en) * 2002-07-25 2005-06-16 Schmidt + Clemens Gmbh + Co. Kg, Process and finned tube for the thermal cracking of hydrocarbons
JP5053321B2 (ja) * 2009-04-07 2012-10-17 本田技研工業株式会社 車両用内装部材
DE102009061021B4 (de) * 2009-05-20 2015-05-07 VDM Metals GmbH Verfahren zur Herstellung einer Metallfolie
DE102010049781A1 (de) 2010-10-29 2012-05-03 Thyssenkrupp Vdm Gmbh Ni-Fe-Cr-Mo-Legierung
ES2543046T3 (es) * 2012-01-18 2015-08-14 Sandvik Intellectual Property Ab Aleación austenítica
US10174397B2 (en) * 2014-02-13 2019-01-08 Vdm Metals International Gmbh Titanium-free alloy

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044871A (en) * 1960-04-13 1962-07-17 Cooper Alloy Corp Hardenable corrosion resistant stainless steel
BE757048A (fr) * 1969-10-09 1971-03-16 Boehler & Co Ag Geb Applications d'un acier entierement austenique dans des conditions corrodantes
SE411130C (sv) * 1976-02-02 1985-09-09 Avesta Jernverks Ab Austenitiskt rostfritt stal med hog mo-halt
US4201575A (en) * 1979-05-18 1980-05-06 Carpenter Technology Corporation Austenitic stainless corrosion-resistant alloy
JPS5811736A (ja) * 1981-07-13 1983-01-22 Sumitomo Metal Ind Ltd 耐応力腐食割れ性に優れた高強度油井管の製造法
US4487744A (en) * 1982-07-28 1984-12-11 Carpenter Technology Corporation Corrosion resistant austenitic alloy
AU580758B2 (en) * 1984-03-16 1989-02-02 Inco Alloys International Inc. High-strength alloy for industrial vessels

Also Published As

Publication number Publication date
KR880014124A (ko) 1988-12-22
JPS6425936A (en) 1989-01-27
NO168313B (no) 1991-10-28
NO168313C (no) 1992-02-05
NO882157L (no) 1988-11-21
US4876065A (en) 1989-10-24
CA1334801C (fr) 1995-03-21
EP0292061A1 (fr) 1988-11-23
AU596745B2 (en) 1990-05-10
AU1637688A (en) 1988-11-24
NO882157D0 (no) 1988-05-18
KR960010598B1 (ko) 1996-08-06
DE3716665A1 (de) 1988-12-08
BR8802449A (pt) 1988-12-20
DE3861905D1 (de) 1991-04-11
ZA883561B (en) 1990-01-31
ES2021822B3 (es) 1991-11-16
ATE61420T1 (de) 1991-03-15

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