WO2015050496A1 - Acier à outils pour travail à froid, résistant à la corrosion et à l'usure - Google Patents

Acier à outils pour travail à froid, résistant à la corrosion et à l'usure Download PDF

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WO2015050496A1
WO2015050496A1 PCT/SE2014/051143 SE2014051143W WO2015050496A1 WO 2015050496 A1 WO2015050496 A1 WO 2015050496A1 SE 2014051143 W SE2014051143 W SE 2014051143W WO 2015050496 A1 WO2015050496 A1 WO 2015050496A1
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steel
powder metallurgy
content
steel according
calculated
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PCT/SE2014/051143
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English (en)
Inventor
Sebastian Ejnermark
Thomas Hillskog
Lars Ekman
Rikard Robertsson
Victoria Bergqvist
Jenny Karlsson
Petter Damm
Ulrika Mossfeldt
Roland Edvinsson
Annika Engström Svensson
Berne Högman
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Uddeholms Ab
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Application filed by Uddeholms Ab filed Critical Uddeholms Ab
Priority to CA2924877A priority Critical patent/CA2924877C/fr
Priority to JP2016520067A priority patent/JP6488287B2/ja
Priority to AU2014330080A priority patent/AU2014330080B2/en
Priority to CN201480054689.4A priority patent/CN105705667B/zh
Priority to KR1020167011377A priority patent/KR102256012B1/ko
Priority to RU2016109549A priority patent/RU2675308C2/ru
Priority to US14/917,521 priority patent/US20160214177A1/en
Priority to MX2016004080A priority patent/MX2016004080A/es
Priority to BR112016007332-0A priority patent/BR112016007332B1/pt
Publication of WO2015050496A1 publication Critical patent/WO2015050496A1/fr

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/14Both compacting and sintering simultaneously
    • B22F3/15Hot isostatic pressing
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    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
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    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/06Making metallic powder or suspensions thereof using physical processes starting from liquid material
    • B22F9/08Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
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    • C21D1/18Hardening; Quenching with or without subsequent tempering
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/56General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering characterised by the quenching agents
    • C21D1/613Gases; Liquefied or solidified normally gaseous material
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/002Heat treatment of ferrous alloys containing Cr
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/008Heat treatment of ferrous alloys containing Si
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C33/02Making ferrous alloys by powder metallurgy
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • C22C33/0257Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • C22C33/0285Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
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    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
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    • 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
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    • C22C38/00Ferrous alloys, e.g. steel alloys
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    • C22C38/24Ferrous alloys, e.g. steel alloys containing chromium with vanadium
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    • C22C38/30Ferrous alloys, e.g. steel alloys containing chromium with cobalt
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    • 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
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    • 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
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    • 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
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    • 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
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    • 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
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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    • 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
    • C22C38/52Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
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    • 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
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/24Nitriding
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    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/80After-treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/248Thermal after-treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2201/00Treatment under specific atmosphere
    • B22F2201/02Nitrogen
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2301/00Metallic composition of the powder or its coating
    • B22F2301/35Iron

Definitions

  • the invention relates to corrosion and wear resistant cold work tool steel and a method of making the cold work steel and use of the cold work tool steel.
  • Nitrogen alloyed martensitic tool steels have recently been introduced on the market and attained a considerable interest, because they combine a high wear resistance with an excellent corrosion resistance. These steels have a wide rang of applications such as for moulding of aggressive plastics, for knives and other components in food processing and for reducing corrosion induced contamination in the medical industry.
  • the steels are generally produced by powder metallurgy.
  • the basic steel composition is firstly atomized and subsequently subjected to a nitrogenation treatment in order to introduce the desired amount of nitrogen into the powder. Thereafter the powder is filled into a capsule and subjected to hot isostatic pressing (HIP) in order to produce an isotropic steel.
  • HIP hot isostatic pressing
  • the amount of carbon is generally reduced to a very low level as compared to conventional tool steels.
  • the carbon content has been limited to less than 0.3 %C, preferably less than 0.1 %C in DE 42 31 695 A 1 and to ⁇ 0.12 % C in WO 2005/054531 Al .
  • the general object of the present invention is to provide a powder metallurgy (PM) produced nitrogen alloyed cold work tools steel alloy having improved properties, in particular a good corrosion resistance in combination with a high hardness.
  • a particular object is to provide a nitrogen alloyed martensitic cold work tools steel alloy having improved corrosion resistance at a fixed chromium content.
  • a further object is to provide a method of producing said material.
  • the amount of carbon should be controlled such that the amount of carbides of the type M2 3 C 6 and M7C 3 in the steel is limited to 10 vol. %, preferably the steel is free from said carbides. Nitrogen (1.0 - 2.2%)
  • the nitrogen content should therefore be much higher than the carbon content in order to avoid the precipitation of MjCs-carbides.
  • the nitrogen content is balanced against the contents of the strong carbide formers, in particular vanadium.
  • the nitrogen content is limited to 1.0 - 2.2%, preferably 1.1 - 1.8% or 1.3 - 1.7%. (C+ ) (1.3 - 2.2%)
  • the total amount of carbon and nitrogen is an essential feature of the present invention.
  • the combined amount of (C + N) should be in the range of 1.3 - 2.2%, preferably 1.7 - 2.1% or 1.8 - 2.0%.
  • C/N (0.17 - 0.50)
  • a proper balance of carbon and nitrogen is an essential feature of the present invention.
  • the type and amounts of the hard phases can be controlled.
  • the amount of the hexagonal phase M 2 X will be reduced after hardening.
  • the C N ratio should therefore be 0.17 - 0.50.
  • the lower ratio may be 0.18, 0.19, 0.20, 0.21, 0.22, 0.23, 0.24 or 0.25.
  • the upper ratio may be 0.5, 0.48, 0.46, 0.45, 0.44, 0.42, 0.40, 0.38, 0.36 or 0.34.
  • the upper limit may be freely combined with the lower limit. Preferred ranges are 0.20 - 0.46 and 0. 22 - 0.45.
  • Chromium When it is present in a dissolved amount of at least 1 1%, chromium results in the formation of a passive film on the steel surface.
  • Chromium shall be present in the steel in an amount between 13 and 30 % in order to give the steel a good hardenability and oxidation and corrosion resistance.
  • Cr is present in an amount of more than 16% in order to safeguard a good pitting corrosion resistance.
  • the lower limit is set in accordance to the intended application and may be 17%, 18%, 19%, 20%, 21% or 22% However, Cr is a strong ferrite former and in order to avoid ferrite after hardening the amount need to be controlled. For practical reasons the upper limit may be reduced to 26%, 24% or even 22%. Preferred ranges include 16 - 26%, 18 - 24%, 19 - 21%, 20 - 22% and 21 - 23%. Molybdenum (0.5 - 3.0%)
  • Mo is known to have a very favourable effect on the hardenability. It is also known to improve the pitting corrosion resistance. The minimum content is 0.5%, and may be set to 0.6%, 0.7%, 0.8% or 1.0%. Molybdenum is a strong carbide forming element and also a strong ferrite former. The maximum content of molybdenum is therefore 3.0%. Preferably Mo is limited to 2.0 %, 1.7% or even 1.5%.
  • molybdenum may be replaced by twice as much tungsten.
  • tungsten is expensive and it also complicates the handling of scrap metal. The maximum amount is therefore limited to 1%, preferably 0.2% and most preferably no additions are made.
  • Vanadium (2 0 5.0%)
  • Vanadium forms evenly distributed primary precipitated nitrocarbides of the type M(N,C) in the matrix of the steel.
  • M is mainly vanadium but significant amounts of Cr and Mo may be present. Vanadium shall therefore be present in an amount of 2-5.
  • the upper limit may be set to 4.8%, 4.6%, 4.4%, 4.2% or 4.0%.
  • the lower limit may be 2.2%, 2.4%, 2.5%, 2.6%, 2.7%, 2,8%, 2.8% and 2.9%.
  • the upper and lower limits may be freely combined within the limits set out in claim 1. Preferred ranges includes 2 - 4%.
  • Niobium is similar to vanadium in that it forms nitrocabides of the type M(N,C) and may in principle be used to replace vanadium but that requires the double amount of niobium as compared to vanadium.
  • the maximum addition of Nb is 2.0%.
  • the combined amount of (V + Nb/2) should be 2.0 - 5.0%.
  • Nb results in a more angular shape of the M(N,C). The preferred maximum amount is therefore 0.5%.
  • no niobium is added.
  • Si is used for deoxidation. Si is present in the steel in a dissolved form. Si is a strong ferrite former and should therefore be limited to ⁇ 1.0%. Manganese (0.2 - 2.0%)
  • Manganese contributes to improving the hardenability of the steel and together with sulphur manganese contributes to improving the machinability by forming manganese sulphides.
  • Manganese shall therefore be present in a minimum content of 0.2%, preferably at least 0.3%. At higher sulphur contents, manganese prevents red brittleness in the steel.
  • the steel shall contain max.2.0%, preferably max. 1.0 %Mn. Preferred ranges are 0.2 - 0.5%, 0.2 - 0.4%, 0.3 - 0.5% and 0.3 - 0.4%.
  • Nickel is optional and may be present in an amount of up to 5%. It gives the steel a good hardenability and toughness. Because of the expense, the nickel content of the steel should be limited as far as possible. Accordingly, the Ni content is limited to 1%, preferably 0.25%.
  • Cu is an optional element, which may contribute to increasing the hardness and the corrosion resistance of the steel. If used, a preferred range is 0.02 - 2% and a most preferred range is 0.04 - 1.6%. However, it is not possible to extract copper from the steel once it has been added. This drastically makes the scrap handling more difficult. For this reason, copper is normally not deliberately added.
  • Co is an optional element. It contributes to increase the hardness of the martensite.
  • the maximum amount is 10 % and, if added, an effective amount is about 4 to 6 %.
  • a preferred maximum content is 0.2%.
  • the steel shall therefore contain ⁇ 0.5 %, preferably ⁇ 0.035%.
  • B may be used in order to further increase the hardness of the steel.
  • the amount is limited to 0.01%, preferably ⁇ 0.004%.
  • These elements are carbide formers and may be present in the alloy in the claimed ranges for altering the composition of the hard phases. However, normally none of these elements are added.
  • the total content of the hard phases MX, M 2 X, M23C6 and M7C3 shall not exceed 50 vol. %, wherein M is one or more of the above specified metals, in particular V, Mo and/or Cr and X is C, N and/or B and wherein the contents of said hard phases fulfil the following requirements (in vol. %):
  • the content of MX is 5 -15 vol. %
  • the content of M2X is ⁇ vol. 3%
  • the content of M23C6 + M7C3 is ⁇ 3 vol. %.
  • the steel is free from the component M7C3.
  • the pitting resistance equivalent (PRE) is often used to quantify pitting corrosion resistance of stainless steels. A higher value indicates a higher resistance to pitting corrosion.
  • PRE pitting resistance equivalent
  • %Cr +3.3 %Mo + 30 %N wherein %Cr, %Mo and %N are the calculated equilibrium contents dissolved in the matrix at the austenitising temperature (TA), wherein the chromium content dissolved in the austenite is at least 13 %..
  • the dissolved contents can be calculated with
  • Thermo-Calc for the actual austenitising temperature (TA) and/or measured in the steel after quenching is in the range of 950 - 1200 °C, typically 1080- 1 150 °C.
  • the lower limit for the calculated PRE-value may be 25, 26, 27, 28, 29, 30, 31, 32 or 33.
  • High nitrogen stainless steels are based on a replacement of carbon with nitrogen. By substituting most of the carbon with nitrogen it is possible to substitute the chromium rich carbides of the type M7C 3 and M2 3 C 6 with very stable hard particles of the type MN-nitrides.
  • the amount of Cr, Mo and N in solid solution at the hardening temperature is therefore very much increased, because less chromium is bound in the hard phase and because the carbides of the type M23C6 and M7C3 do not have any solubility for nitrogen. Thereby, more chromium is left in solid solution and the thin passive chromium rich surface film is strengthened, which leads to an increased resistance to general corrosion and pitting corrosion. Accordingly, it is to be expected that the pitting corrosion resistance would decrease if carbon replaces part of the nitrogen.
  • High nitrogen stainless steels known in the art therefore have a low carbon content.
  • the tool steel having the claimed chemical composition can be produced by conventional gas atomizing followed by nitrogenation of the powder before HIP-ing.
  • the nitrogen content in the steel after gas atomizing is normally less than 0.2%. The remaining nitrogen is thus added during the nitrogenation treatment of the powder.
  • the steel After consolidation the steel may be used in the as HIP-ed form or formed into a desired shape. Normally the steel is subjected to hardening and tempering before being used. Austenitising may be performed by annealing at an austenitising temperature (TA) in the range of 950 - 1200 °C, typically 1080- 1 150 °C. A typical treatment is annealing at 1080 °C for 30 minutes. The steel may be hardened by quenching in a vacuum furnace by deep cooling in liquid nitrogen, and then tempered at 200 °C for 2 times at 2 hours (2x2h).
  • TA austenitising temperature
  • a steel according to the invention is compared to a steel having lower carbon content and a different balance between carbon and nitrogen. Both steels were produced by powder metallurgy.
  • the basic steel compositions were melted and subjected to gas atomization.
  • the obtained powders were subjected to a nitrogenation treatment in order to introduce the desired amount of nitrogen into the powders.
  • the nitrogen content was increased from about 0.1% to the respective content.
  • the steels thus obtained had the following compositions (in wt. %):
  • the steels were austenitised at 1080 °C for 30 minutes and hardened by quenching by deep cooling in liquid nitrogen in a vacuum furnace followed by tempering at 200 °C for 2 times at 2 hours (2x2h).
  • the inventive steel had a hardness of 60 HRC and the comparative steel a hardness of 58 HRC.
  • the alloy micro structure consisted of tempered martensite and hard phases. Two distinct hard phases were identified in the micro structure of both steels: MX and M 2 X. In the comparative steel the hexagonal M2X was the majority phase and the face centred cubic MX-phase was the minority phase. However, in the inventive steel MX was the majority phase and M 2 X was the minority phase.
  • the materials susceptibility for pitting corrosion was experimentally examined by anodic polarisation sweep. An electrochemical cell with a saturated Ag/AgCl reference electrode and a carbon mesh counter electrode, were used for cyclic polarization measurements. The 500 mesh grounded sample was first open circuit potential (OCP) recorded with a 0.1 M NaCl solution to ensure a stable potential was reached.
  • OCP open circuit potential
  • Fig. 1 discloses a schematic anodic polarization curve and the information that can be obtained from the curve.
  • the forward scan gives information about the initiation of pitting and the reverse scan provides information about the alloys repassivation behavior.
  • Eb is the value of the potential for pitting breakdown above which new pits will initiate and existing pits will propagate. As the potential is decreased on the reverse scan , there is a decrease in current density.
  • the alloy is repassivated where the reverse scan crosses the forward scan.
  • Ep is the repassivation potential, or protection potential i.e. the potential below which no pitting occur.
  • the difference between Eb and Ep is related to the susceptibility to pitting and crevice corrosion. The greater the difference the greater the susceptibility.
  • Table 1 discloses that the inventive steel with the increased carbon content has the less tendency to suffer localised corrosion and also that the inventive steel also repassivate more easily than the comparative steel. Accordingly, the inventive steel is much less sensitive to pitting and crevice corrosion.
  • Thermo-Calc The influence of the relative amounts of carbon and nitrogen on the formation of the different hard phases in the steel was calculated in Thermo-Calc for a steel having variable C and N contents and the following basic composition in weight %: Cr: 19.8, Mo: 2.5, V: 2.75; Si: 0.3, Mn: 0.3, Fe balance.
  • Fig. 2 discloses the amount of hard phases as a function of the ratio C/N and it can be seen that amount of M 2 X decreases rapidly with increasing ratio C/N. However, M2 3 C 6 starts to form already at a C/N ratio of about 0.25.
  • Fig. 3 discloses calculated PRE-values as a function of the ratio C/N and it can be seen that the highest values are obtained for the steels according to the invention.
  • Fig. 4 discloses the amount of hard phases as a function of the ratio C/N and it can be seen that amount of M 2 X decreases very rapidly with increasing ratio C/N. It can also be seen that M2 3 C 6 starts to form at a C/N ratio of about 0.3.
  • Fig. 5 discloses calculated PRE-values as a function of the ratio C N and again it can be seen that the highest values are obtained for the steels according to the invention.
  • the present invention provides a to provide a powder metallurgy (PM) produced nitrogen alloyed cold work tools steel having an improved corrosion resistance in combination with a high hardness.
  • the cold work tool steel of the present invention is particular useful

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Powder Metallurgy (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Heat Treatment Of Steel (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

L'invention concerne un acier à outils pour travail à froid, résistant à la corrosion et à l'usure. L'acier comprend les constituants principaux suivants (en % en poids) : C 0,3–0,8 N 1,0–2,2 (C+N) 1,3–2,2 C/N 0,17–0,50 Si ≤ 1,0 Mn 0,2–2.0 Cr 13-30 Mo 0,5–3,0 V 2,0–5,0, le complément étant constitué d'éventuels éléments, du fer et d'impuretés.
PCT/SE2014/051143 2013-10-02 2014-10-02 Acier à outils pour travail à froid, résistant à la corrosion et à l'usure WO2015050496A1 (fr)

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CA2924877A CA2924877C (fr) 2013-10-02 2014-10-02 Acier a outils pour travail a froid, resistant a la corrosion et a l'usure
JP2016520067A JP6488287B2 (ja) 2013-10-02 2014-10-02 耐食耐摩耗冷間加工工具鋼
AU2014330080A AU2014330080B2 (en) 2013-10-02 2014-10-02 Corrosion and wear resistant cold work tool steel
CN201480054689.4A CN105705667B (zh) 2013-10-02 2014-10-02 耐腐蚀和磨损的冷作工具钢
KR1020167011377A KR102256012B1 (ko) 2013-10-02 2014-10-02 내부식 및 내마모성 냉간 공구강
RU2016109549A RU2675308C2 (ru) 2013-10-02 2014-10-02 Коррозионно-стойкая и износостойкая инструментальная сталь для холодной обработки
US14/917,521 US20160214177A1 (en) 2013-10-02 2014-10-02 Corrosion and wear resistant cold work tool steel
MX2016004080A MX2016004080A (es) 2013-10-02 2014-10-02 Acero para herramientas de trabajo en frio resistente a la corrosion y desgaste.
BR112016007332-0A BR112016007332B1 (pt) 2013-10-02 2014-10-02 Aço fabricado por metalurgia do pó e método para fabricar o mesmo

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US11179778B2 (en) * 2013-12-20 2021-11-23 Höganäs Ab (Publ) Method for producing a sintered component and a sintered component
CN105177437A (zh) * 2015-09-24 2015-12-23 安庆市灵宝机械有限责任公司 一种耐磨损耐腐蚀合金钢
JP7167428B2 (ja) * 2017-11-10 2022-11-09 昭和電工マテリアルズ株式会社 鉄基焼結合金材及びその製造方法
RU2651071C1 (ru) * 2017-11-27 2018-04-18 Юлия Алексеевна Щепочкина Сплав на основе железа
CN108893673A (zh) * 2018-06-04 2018-11-27 江苏新华合金电器有限公司 蒸发器拉杆和拉杆螺母用12Cr13棒材及其制备方法
KR102146354B1 (ko) * 2019-11-19 2020-08-20 주식회사 첼링 내마모성과 내식성이 우수한 주방용 칼 및 그 제조방법
CN113215482B (zh) * 2021-03-22 2022-05-20 武汉钜能科技有限责任公司 耐磨冷作工具钢
CN114318164B (zh) * 2021-03-22 2023-01-20 武汉钜能科技有限责任公司 耐磨耐蚀工具钢
CN114318131B (zh) * 2021-03-22 2023-01-20 武汉钜能科技有限责任公司 耐磨合金
CN113416831A (zh) * 2021-05-27 2021-09-21 中钢集团邢台机械轧辊有限公司 一种宽幅铝冷轧工作辊热处理工艺方法
CN114150130B (zh) * 2021-12-01 2023-09-08 宁波江丰热等静压技术有限公司 一种热等静压吊具用板材的热处理方法及应用
WO2023141206A1 (fr) * 2022-01-19 2023-07-27 Maclean-Fogg Company Matrice d'outil métallique imprimé en 3d
CN114774643A (zh) * 2022-05-10 2022-07-22 无锡亿宝机械设备有限公司 一种m42材质的全硬化工作辊的改进型热处理方法

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US20160214177A1 (en) 2016-07-28
ES2588539T3 (es) 2016-11-03
BR112016007332A2 (pt) 2017-08-01
PT2857126T (pt) 2016-08-18
AU2014330080A1 (en) 2016-03-24
HUE030403T2 (en) 2017-05-29
EP2857126A3 (fr) 2015-08-05
PL2857126T3 (pl) 2016-11-30
BR112016007332B1 (pt) 2020-03-10
CN105705667A (zh) 2016-06-22
RU2675308C2 (ru) 2018-12-18
RU2016109549A3 (fr) 2018-06-29
CN105705667B (zh) 2017-11-21
TW201522664A (zh) 2015-06-16
CA2924877A1 (fr) 2015-04-09
RU2016109549A (ru) 2017-11-10
EP2857126A2 (fr) 2015-04-08
CA2924877C (fr) 2022-04-26
MX2016004080A (es) 2016-10-13
TWI638054B (zh) 2018-10-11
DK2857126T3 (en) 2016-07-04
AU2014330080B2 (en) 2017-11-23
KR102256012B1 (ko) 2021-05-24
KR20160065165A (ko) 2016-06-08

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