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EP3034211A1 - A wear resistant tool steel produced by HIP - Google Patents

A wear resistant tool steel produced by HIP Download PDF

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Publication number
EP3034211A1
EP3034211A1 EP14198569.7A EP14198569A EP3034211A1 EP 3034211 A1 EP3034211 A1 EP 3034211A1 EP 14198569 A EP14198569 A EP 14198569A EP 3034211 A1 EP3034211 A1 EP 3034211A1
Authority
EP
European Patent Office
Prior art keywords
steel
fulfils
following conditions
steel according
hard phase
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.)
Pending
Application number
EP14198569.7A
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German (de)
French (fr)
Inventor
Tidesten Magnus
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.)
Uddeholms AB
Original Assignee
Uddeholms AB
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 Uddeholms AB filed Critical Uddeholms AB
Priority to EP14198569.7A priority Critical patent/EP3034211A1/en
Priority to JP2017529842A priority patent/JP7038547B2/en
Priority to US15/527,233 priority patent/US11242581B2/en
Priority to UAA201707445A priority patent/UA120710C2/en
Priority to CN201911003552.7A priority patent/CN110699613B/en
Priority to BR112017009295-6A priority patent/BR112017009295B1/en
Priority to KR1020207014647A priority patent/KR20200060533A/en
Priority to MX2017006100A priority patent/MX2017006100A/en
Priority to CN201580060666.9A priority patent/CN107109593B/en
Priority to AU2015363754A priority patent/AU2015363754B2/en
Priority to RU2017120907A priority patent/RU2702517C2/en
Priority to CA2966145A priority patent/CA2966145C/en
Priority to PCT/SE2015/051352 priority patent/WO2016099390A1/en
Priority to KR1020177015784A priority patent/KR20170095219A/en
Priority to SG11201702840YA priority patent/SG11201702840YA/en
Priority to EP15870463.5A priority patent/EP3247815A4/en
Priority to TW104142470A priority patent/TWI675923B/en
Publication of EP3034211A1 publication Critical patent/EP3034211A1/en
Priority to JP2020097227A priority patent/JP2020143380A/en
Priority to US17/645,856 priority patent/US20220119927A1/en
Pending legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • 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%
    • 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
    • CCHEMISTRY; METALLURGY
    • 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
    • C21D6/02Hardening by precipitation
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • 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
    • C22C38/24Ferrous alloys, e.g. steel alloys containing chromium with vanadium
    • 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
    • C22C38/32Ferrous alloys, e.g. steel alloys containing chromium with boron
    • CCHEMISTRY; METALLURGY
    • 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/004Dispersions; Precipitations

Definitions

  • the invention relates to a wear resistant tool steel produced by HIP.
  • the tool steel is alloyed with boron.
  • the present invention relates to a HIPed tool steel comprising a hard phase consisting mainly of multiple borides containing Fe in a hardenable matrix.
  • the double boride is of the type M 2 M'B 2 , where M and M' stand for metals of the multiple boride.
  • Said boride forming elements are generally selected from Cr, Mo, W, Ti, V, Nb, Ta, Hf and Co.
  • M is Mo
  • M' is Fe
  • the boride may contain substantial amounts of one ore more of the other boride forming elements.
  • the double boride will simply be referred to as Mo 2 FeB 2 although the boride also may contain Ni and one or more of the above mentioned boride forming elements.
  • Carbon is to be present in a minimum content of 0.2 %, preferably 0.3 % or 0.35 %.
  • the upper limit for carbon is 1.5 %.
  • Carbon is important for the formation of carbides and for the hardening
  • the carbon content is adjusted in order to obtain 0.4-0.6 % C dissolved in the matrix at the austenitizing temperature.
  • the amount of carbon should be controlled such that the amount of carbides of the type M 23 C 6 , M 7 C 3 , M 6 C and MC in the steel is limited.
  • the upper limit may therefore be set to 0.8, 0.6, 0.5 or 0.45 %
  • Chromium is an optional component. However, Cr is for most applications present in contents of at least 2.5 % in order to provide a sufficient hardenability. Cr is preferably higher for providing a good hardenability in large cross sections during heat treatment. If the chromium content is too high, this may lead to the formation of undesired carbides, such as M 7 C 3 . In addition, this may also increase the propensity of retained austenite in the microstructure.
  • the lower limit may be 2.8 %, 3.4 % or 4.2
  • the upper limit may be 6.0, 5.4 %, or 4,6 %.
  • Chromium contents of mare then 10 %, preferably more than 12 % are used for stainless applications.
  • Mo is the main element forming the hard boride.
  • a high amount of Molybdenum is used in order to obtain a desired precipitation of the boride Mo 2 FeB 2 in an amount of 5-35 vol. %.
  • Preferred ranges include 12-30 % and 15-25%.
  • Mo is also known to have a very favourable effect on the hardenability is essential for attaining a good secondary hardening response. For this reason it is preferred that the amount of Mo remaining in the matrix after quenching form 1100°C is 1.5-2.5 %.
  • Boron which is the main hard phase-forming element, should be at least 0.5 % so as to provide the minimum amount of 5 % hard phase Mo 2 FeB 2 .
  • the amount of B is limited to 3 % for not making the alloy to brittle.
  • tungsten is similar to that of Mo. However, for attaining the same effect it is necessary to add twice as much W as Mo on a weight % basis. Tungsten is expensive and it also complicates the handling of scrap metal. The maximum amount is therefore limited to 3 %, preferably 1%, more preferably 0.3 % and most preferably W is not deliberately added at all.
  • Vanadium forms evenly distributed primary and secondary precipitated carbides of the type MC.
  • M is mainly vanadium but Cr and Mo may be present to some extent.
  • the maximum addition of V is restricted to 15 % and the preferred maximum amount is 5 %.
  • V is mainly added for obtaining a desired composition of the steel matrix before hardening. The addition may therefore be limited to 2.0 % or even to 0.5 %. A preferred range is 0.1-0.5 % V.
  • Niobium is similar to vanadium in that it forms MC. However, for attaining the same effect it is necessary to add twice as much Nb as V on a weight % basis. Nb also results in a more angular shape of the MC. Hence, the maximum addition of Nb is restricted to 15 % and the preferred maximum amount is 5 %. Preferably, no niobium is added.
  • Silicon is used for deoxidation. Si also increases the carbon activity and is beneficial for the machinability. Si is therefore present in an amount of 0.1 - 2.5 %. For a good deoxidation, it is preferred to adjust the Si content to at least 0.2 %.
  • the lower limit may be set to 0.3 %, 0.35 % or 0.4 %. However, Si is a strong ferrite former and should be limited to 2.5 %.
  • the upper limit may be set to 1.5%, 1 %, 0.8 %, 0.7 % or 0.6 %. A preferred range is 0.2 - 0.8 %.
  • 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 0.1 %, preferably at least 0.2 %. At higher sulphur contents manganese prevents red brittleness in the steel.
  • the steel shall contain maximum 2.5 % Mn. The upper limit may be set to 1.5 %, 1.2 %, 1.0 %, 0.8 % or 0.6%. However, preferred ranges are 0.2 - 0.8 % and 0.2 - 0.6 %.
  • Nickel is optional and may be present in an amount of not more than 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 preferably limited to 2%, more preferably to 1.0% or 0.3%.
  • Cu is an optional element, which may contribute to increasing the hardness and the corrosion resistance of the steel. If used, the preferred range is 0.02 - 2% and the 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, which may be present in an amount of not more than 10 %. Co dissolves in iron (ferrite and austenite) and strengthens it whilst at the same time imparting high temperature strength. Co increases the M s temperature. Co can substitute mainly Fe in the Mo 2 FeB 2 boride. A preferred maximum content is 2 %. However, scrap handling will be more difficult. For this reason, Co is not deliberately added
  • These elements are boride and 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.
  • P is an impurity element and a solid solution strengthening element. However, P tends to segregate to the grain boundaries, reduces the cohesion and thereby the toughness. P is therefore normally limited to ⁇ 0.05 %.
  • the steel contributes to improving the machinability of the steel. At higher sulphur contents there is a risk for red brittleness. Moreover, a high sulphur content may have a negative effect on the fatigue properties of the steel.
  • the steel shall therefore contain ⁇ 0.5 %, preferably ⁇ 0.03 %.
  • the powder was sieved to ⁇ 500 ⁇ m, filled in steel capsules having a diameter of 63 mm and a height of 150 mm. HIPing was performed at a temperature of 1150 °C, the holding time was 2 hours and the pressure 110 MPa. The cooling rate was ⁇ 1 °C/s. The material thus obtained was forged at 1130 °C to the dimension 20x30 mm. Soft annealing was performed at 900 °C with a cooling rate of 10 °C/h down to 750 °C and thereafter cooling freely in air. Hardening was performed by austenitizing at 1100 °C for 30 minutes followed by quenching in water followed by tempering. The result of the hardness testing after tempering is given in Table 1.
  • the amount of the hard phase was found to be 24 vol. % and the borides were found to have a small size.
  • the area fraction of borides in different size classes is given in Table 2 below. Table. 1. Hardness as a function of the tempering temperature after hardening from 1100°C. Tempering temperature (°C) Hardness HRC 200 60 300 56 400 54 500 53 525 53 550 54 600 49 Table. 2. Size distribution of the borides. Size range ( ⁇ m) Area fraction (%) 0-1 6.3 1-2 13.5 2-3 4.0 3-4 0.2
  • the microstructure is shown in Fig. 1 .
  • the high area fraction and the uniform distribution of the Mo 2 FeB 2 borides results in a material having excellent anti-galling properties such that it would be possible to dispense with surface treatments like PVD, CVD and TD.
  • the tool steel of the present invention is particular useful in applications requiring very high galling resistance.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention relates tool steel produced by powder metallurgy and hot isostatic pressing resulting in that the steel is isotropic has a non-amorphous microstructure and has a theoretical density (TD) of > 98 %, the steel consists of in weight % (wt.%):
C 0.2 - 1.5
Si 0.1 - 2.5
Mn 0.1 - 2.5
Mo 10-35
B 0.5-3
balance optional elements, iron and impurities.

Description

    TECHNICAL FIELD
  • The invention relates to a wear resistant tool steel produced by HIP. The tool steel is alloyed with boron.
  • BACKGROUND OF THE INVENTION
  • Nitrogen and vanadium alloyed powder metallurgy (PM) tool steels attained a considerable interest because of their unique combination of high hardness, high wear resistance and excellent galling resistance. These steels have a wide rang of applications where the predominant failure mechanisms are adhesive wear or galling. Typical areas of application include blanking and forming, fine blanking, cold extrusion, deep drawing and powder pressing. The basic steel composition is atomized, subjected to nitrogenation and thereafter the powder is filled into a capsule and subjected to hot isostatic pressing (HIP) in order to produce an isotropic steel. A high performance steel produced in this way is described in WO 00/79015 A1 .
  • Although the known steel has a very attractive property profile there is a continuous strive for improvements of the tool material in order to further improve the surface quality of the products produced as well as to extend the tool life, in particular under severe working conditions, where galling is the main problem.
  • DISCLOSURE OF THE INVENTION
  • The object of the present invention is to provide powder metallurgy (PM) produced tool steel having an improved property profile for advanced cold working like fine blanking. Another object of the present invention is to provide a powder metallurgy (PM) produced tool steel having a composition and microstructure leading to improvements in the surface quality of the produced parts.
  • The foregoing objects, as well as additional advantages are achieved to a significant measure by providing a tool steel having a composition as set out in the claims.
  • The invention is defined in the claims.
  • DETAILED DESCRIPTION
  • The present invention relates to a HIPed tool steel comprising a hard phase consisting mainly of multiple borides containing Fe in a hardenable matrix. The double boride is of the type M2M'B2, where M and M' stand for metals of the multiple boride. Said boride forming elements are generally selected from Cr, Mo, W, Ti, V, Nb, Ta, Hf and Co. In the present case M is Mo and M' is Fe. However, the boride may contain substantial amounts of one ore more of the other boride forming elements. However, in the following the double boride will simply be referred to as Mo2FeB2 although the boride also may contain Ni and one or more of the above mentioned boride forming elements.
  • The importance of the separate elements and their interaction with each other as well as the limitations of the chemical ingredients of the claimed alloy are briefly explained in the following. All percentages for the chemical composition of the steel are given in weight % (wt. %) throughout the description. The upper and lower limits of the individual elements may be freely combined within the limits set out in claim 1.
  • Carbon (0.2 - 1.5 %)
  • Carbon is to be present in a minimum content of 0.2 %, preferably 0.3 % or 0.35 %. The upper limit for carbon is 1.5 %. Carbon is important for the formation of carbides and for the hardening Preferably, the carbon content is adjusted in order to obtain 0.4-0.6 % C dissolved in the matrix at the austenitizing temperature. In any case, the amount of carbon should be controlled such that the amount of carbides of the type M23C6, M7C3, M6C and MC in the steel is limited. The upper limit may therefore be set to 0.8, 0.6, 0.5 or 0.45 %
  • Chromium (≤ 25 %)
  • Chromium is an optional component. However, Cr is for most applications present in contents of at least 2.5 % in order to provide a sufficient hardenability. Cr is preferably higher for providing a good hardenability in large cross sections during heat treatment. If the chromium content is too high, this may lead to the formation of undesired carbides, such as M7C3. In addition, this may also increase the propensity of retained austenite in the microstructure. The lower limit may be 2.8 %, 3.4 % or 4.2 The upper limit may be 6.0, 5.4 %, or 4,6 %. On the other hand, Chromium contents of mare then 10 %, preferably more than 12 % are used for stainless applications.
  • Molybdenum (10 - 35 %)
  • Mo is the main element forming the hard boride. In the present invention, a high amount of Molybdenum is used in order to obtain a desired precipitation of the boride Mo2FeB2 in an amount of 5-35 vol. %. Preferred ranges include 12-30 % and 15-25%. Mo is also known to have a very favourable effect on the hardenability is essential for attaining a good secondary hardening response. For this reason it is preferred that the amount of Mo remaining in the matrix after quenching form 1100°C is 1.5-2.5 %.
  • Boron (0.5 - 3 %)
  • Boron, which is the main hard phase-forming element, should be at least 0.5 % so as to provide the minimum amount of 5 % hard phase Mo2FeB2. The amount of B is limited to 3 % for not making the alloy to brittle.
  • Tungsten (≤ 3 %)
  • The effect of tungsten is similar to that of Mo. However, for attaining the same effect it is necessary to add twice as much W as Mo on a weight % basis. Tungsten is expensive and it also complicates the handling of scrap metal. The maximum amount is therefore limited to 3 %, preferably 1%, more preferably 0.3 % and most preferably W is not deliberately added at all.
  • Vanadium (≤ 15 %)
  • Vanadium forms evenly distributed primary and secondary precipitated carbides of the type MC. In the inventive steel M is mainly vanadium but Cr and Mo may be present to some extent. The maximum addition of V is restricted to 15 % and the preferred maximum amount is 5 %. However, in the present case V is mainly added for obtaining a desired composition of the steel matrix before hardening. The addition may therefore be limited to 2.0 % or even to 0.5 %. A preferred range is 0.1-0.5 % V.
  • Niobium (≤ 15 %)
  • Niobium is similar to vanadium in that it forms MC. However, for attaining the same effect it is necessary to add twice as much Nb as V on a weight % basis. Nb also results in a more angular shape of the MC. Hence, the maximum addition of Nb is restricted to 15 % and the preferred maximum amount is 5 %. Preferably, no niobium is added.
  • Silicon (0.1 - 2.5 %)
  • Silicon is used for deoxidation. Si also increases the carbon activity and is beneficial for the machinability. Si is therefore present in an amount of 0.1 - 2.5 %. For a good deoxidation, it is preferred to adjust the Si content to at least 0.2 %. The lower limit may be set to 0.3 %, 0.35 % or 0.4 %. However, Si is a strong ferrite former and should be limited to 2.5 %. The upper limit may be set to 1.5%, 1 %, 0.8 %, 0.7 % or 0.6 %. A preferred range is 0.2 - 0.8 %.
  • Manganese (0.1 - 2.5 %)
  • 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 0.1 %, preferably at least 0.2 %. At higher sulphur contents manganese prevents red brittleness in the steel. The steel shall contain maximum 2.5 % Mn. The upper limit may be set to 1.5 %, 1.2 %, 1.0 %, 0.8 % or 0.6%. However, preferred ranges are 0.2 - 0.8 % and 0.2 - 0.6 %.
  • Nickel (≤ 5%)
  • Nickel is optional and may be present in an amount of not more than 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 preferably limited to 2%, more preferably to 1.0% or 0.3%.
  • Copper (≤ 3.0%)
  • Cu is an optional element, which may contribute to increasing the hardness and the corrosion resistance of the steel. If used, the preferred range is 0.02 - 2% and the 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.
  • Cobalt (≤ 10 %)
  • Co is an optional element, which may be present in an amount of not more than 10 %. Co dissolves in iron (ferrite and austenite) and strengthens it whilst at the same time imparting high temperature strength. Co increases the Ms temperature. Co can substitute mainly Fe in the Mo2FeB2 boride. A preferred maximum content is 2 %. However, scrap handling will be more difficult. For this reason, Co is not deliberately added
  • Ti, Ta, Zr and Hf
  • These elements are boride and 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.
  • Phosphorous
  • P is an impurity element and a solid solution strengthening element. However, P tends to segregate to the grain boundaries, reduces the cohesion and thereby the toughness. P is therefore normally limited to ≤ 0.05 %.
  • Sulphur (≤ 0.5%)
  • S contributes to improving the machinability of the steel. At higher sulphur contents there is a risk for red brittleness. Moreover, a high sulphur content may have a negative effect on the fatigue properties of the steel. The steel shall therefore contain ≤ 0.5 %, preferably ≤ 0.03 %.
  • EXAMPLE
  • 10 kg of an alloy having the composition given below was melted in a laboratory furnace and subjected to Ar-gas atomizing.
    C 0.3
    Si 0.3
    Mn 0.3
    Mo 19
    B 2.1
    Fe balance.
  • The powder was sieved to < 500 µm, filled in steel capsules having a diameter of 63 mm and a height of 150 mm. HIPing was performed at a temperature of 1150 °C, the holding time was 2 hours and the pressure 110 MPa. The cooling rate was < 1 °C/s. The material thus obtained was forged at 1130 °C to the dimension 20x30 mm. Soft annealing was performed at 900 °C with a cooling rate of 10 °C/h down to 750 °C and thereafter cooling freely in air. Hardening was performed by austenitizing at 1100 °C for 30 minutes followed by quenching in water followed by tempering. The result of the hardness testing after tempering is given in Table 1.
  • The amount of the hard phase was found to be 24 vol. % and the borides were found to have a small size. The area fraction of borides in different size classes is given in Table 2 below. Table. 1. Hardness as a function of the tempering temperature after hardening from 1100°C.
    Tempering temperature (°C) Hardness HRC
    200 60
    300 56
    400 54
    500 53
    525 53
    550 54
    600 49
    Table. 2. Size distribution of the borides.
    Size range (µm) Area fraction (%)
    0-1 6.3
    1-2 13.5
    2-3 4.0
    3-4 0.2
  • The microstructure is shown in Fig. 1. The high area fraction and the uniform distribution of the Mo2FeB2 borides results in a material having excellent anti-galling properties such that it would be possible to dispense with surface treatments like PVD, CVD and TD.
  • INDUSTRIAL APPLICABILITY
  • The tool steel of the present invention is particular useful in applications requiring very high galling resistance.

Claims (11)

  1. A tool steel produced by powder metallurgy and hot isostatic pressing resulting in that the steel is isotropic has a non-amorphous microstructure and has a theoretical density (TD) of > 98 %, the steel consists of in weight % (wt.%): C 0.2 - 1.5 Si 0.1 - 2.5 Mn 0.1 - 2.5 Mo 10 - 35 B 0.5 - 3 Cr ≤ 25 V ≤ 15 Nb ≤ 15 Ti ≤ 5 Ta ≤ 5 Zr ≤ 5 Hf ≤ 5 Ni ≤ 5 Co ≤ 10 Cu ≤ 3 W ≤ 3 S ≤ 0.5
    Fe and impurities balance.
  2. A steel according to claim 1, wherein the steel fulfils at least one of the following conditions, C 0.3 - 0.6 Si 0.2 - 1.5 Mn 0.2 - 1.5 Mo 12 - 30 B 0.7 - 2.5
  3. A steel according to claim 1 or 2, wherein the steel fulfils at least one of the following conditions Cr ≤ 20 V ≤ 5 Nb ≤ 5 Ti ≤ 1 Ta ≤ 1 Zr ≤ 1 Hf ≤ 1 Ni ≤ 2 Co ≤ 2 Cu ≤ 1 W ≤ 1 S ≤ 0.03
  4. A steel according to any of the preceding claims, wherein the steel fulfils at least one of the following conditions C 0.3 - 0.5 Si 0.2 - 0.8 Mn 0.2 - 0.8 Mo 15 - 25 B 1.8 - 2.2 Cr 3.0 - 16 V 0.1 - 2.0
  5. A steel according to any of the preceding claims, wherein the steel fulfils at least one of the following conditions C 0.35 - 0.45 Si 0.2 - 0.6 Mn 0.2 - 0.6 Cr 3.0 - 6.0 V 0.1 - 0.5
  6. A steel according to any of claims 1-4, wherein the steel fulfils at least one of the following conditions C 0.35 - 0.45 Si 0.2 -0.6 Mn 0.2 - 0.6 Cr 10.0 - 15.0 V 0.1 - 0.5
  7. A steel according to any of the preceding claims, wherein the steel fulfils at least one of the following conditions V 0.2 - 0.4 P < 0.05 S < 0.003 O < 0.005
  8. A steel according to any of claims 1-4, wherein the metallic matrix fulfils the following requirements after quenching from 1100 °C C 0.4 - 0.5 Si 0.3 - 0.5 Mn 0.3 - 0.5 Mo 1.5 - 2.5 Cr 4.0 - 5-0 V 0.3 - 0.4
  9. A steel according to any of the preceding claims, wherein the steel comprises 5 - 35 volume % hard phase, wherein the hard phase comprises at least one of borides, nitrides, carbides and/or combinations thereof.
  10. A steel according to any of the preceding claims, wherein the maximal Equivalent Circle Diameter of the hard phase is less than 5 µm, preferably less than 3 µm.
  11. A steel according to any of the preceding claims, wherein the steel comprises 15 - 25 volume % hard phase and wherein the maximal Equivalent Circle Diameter of the hard phase is less than 3 µm.
EP14198569.7A 2014-12-17 2014-12-17 A wear resistant tool steel produced by HIP Pending EP3034211A1 (en)

Priority Applications (19)

Application Number Priority Date Filing Date Title
EP14198569.7A EP3034211A1 (en) 2014-12-17 2014-12-17 A wear resistant tool steel produced by HIP
AU2015363754A AU2015363754B2 (en) 2014-12-17 2015-12-15 A wear resistant alloy
RU2017120907A RU2702517C2 (en) 2014-12-17 2015-12-15 Wear-resistant alloy
UAA201707445A UA120710C2 (en) 2014-12-17 2015-12-15 A wear resistant alloy
CN201911003552.7A CN110699613B (en) 2014-12-17 2015-12-15 Wear-resistant alloy
BR112017009295-6A BR112017009295B1 (en) 2014-12-17 2015-12-15 WEAR RESISTANT ALLOY
KR1020207014647A KR20200060533A (en) 2014-12-17 2015-12-15 Wear resistant alloy
MX2017006100A MX2017006100A (en) 2014-12-17 2015-12-15 A wear resistant alloy.
CN201580060666.9A CN107109593B (en) 2014-12-17 2015-12-15 Wear-resistant alloy
JP2017529842A JP7038547B2 (en) 2014-12-17 2015-12-15 Abrasion resistant alloy
US15/527,233 US11242581B2 (en) 2014-12-17 2015-12-15 Wear resistant alloy
CA2966145A CA2966145C (en) 2014-12-17 2015-12-15 A wear resistant alloy
PCT/SE2015/051352 WO2016099390A1 (en) 2014-12-17 2015-12-15 A wear resistant alloy
KR1020177015784A KR20170095219A (en) 2014-12-17 2015-12-15 Wear resistant alloy
SG11201702840YA SG11201702840YA (en) 2014-12-17 2015-12-15 A wear resistant alloy
EP15870463.5A EP3247815A4 (en) 2014-12-17 2015-12-15 A wear resistant alloy
TW104142470A TWI675923B (en) 2014-12-17 2015-12-17 A wear resistant alloy
JP2020097227A JP2020143380A (en) 2014-12-17 2020-06-03 Abrasion resistant alloy
US17/645,856 US20220119927A1 (en) 2014-12-17 2021-12-23 Wear resistant alloy

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WO2017040775A1 (en) 2015-09-04 2017-03-09 Scoperta, Inc. Chromium free and low-chromium wear resistant alloys
CN107604257A (en) * 2016-08-25 2018-01-19 机械科学研究总院先进制造技术研究中心 A kind of HM3 powder steels and its preparation technology
CN109023061A (en) * 2018-08-30 2018-12-18 宁波帅特龙集团有限公司 A kind of sunshade torque arm
CN110042322A (en) * 2019-04-23 2019-07-23 浙江德得贸易有限公司 A kind of pre- hard mold steel and preparation method thereof substituting 45 mould steel
US11939646B2 (en) 2018-10-26 2024-03-26 Oerlikon Metco (Us) Inc. Corrosion and wear resistant nickel based alloys
US12076788B2 (en) 2019-05-03 2024-09-03 Oerlikon Metco (Us) Inc. Powder feedstock for wear resistant bulk welding configured to optimize manufacturability
EP4426872A4 (en) * 2021-11-05 2025-01-22 Uddeholms AB WEAR RESISTANT ALLOY
US12227853B2 (en) 2019-03-28 2025-02-18 Oerlikon Metco (Us) Inc. Thermal spray iron-based alloys for coating engine cylinder bores
US12378647B2 (en) 2018-03-29 2025-08-05 Oerlikon Metco (Us) Inc. Reduced carbides ferrous alloys

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Publication number Priority date Publication date Assignee Title
WO2017040775A1 (en) 2015-09-04 2017-03-09 Scoperta, Inc. Chromium free and low-chromium wear resistant alloys
US11253957B2 (en) 2015-09-04 2022-02-22 Oerlikon Metco (Us) Inc. Chromium free and low-chromium wear resistant alloys
EP3344789A4 (en) * 2015-09-04 2019-07-31 Scoperta, Inc. WEAR RESISTANT ALLOYS WITHOUT CHROME AND LOW CHROMIUM CONTENT
CN107604257A (en) * 2016-08-25 2018-01-19 机械科学研究总院先进制造技术研究中心 A kind of HM3 powder steels and its preparation technology
CN107604257B (en) * 2016-08-25 2019-03-29 北京机科国创轻量化科学研究院有限公司 A kind of HM3 powder steel and its preparation process
US12378647B2 (en) 2018-03-29 2025-08-05 Oerlikon Metco (Us) Inc. Reduced carbides ferrous alloys
CN109023061B (en) * 2018-08-30 2019-10-18 宁波帅特龙集团有限公司 A kind of sunshade torque arm
CN109023061A (en) * 2018-08-30 2018-12-18 宁波帅特龙集团有限公司 A kind of sunshade torque arm
US11939646B2 (en) 2018-10-26 2024-03-26 Oerlikon Metco (Us) Inc. Corrosion and wear resistant nickel based alloys
US12227853B2 (en) 2019-03-28 2025-02-18 Oerlikon Metco (Us) Inc. Thermal spray iron-based alloys for coating engine cylinder bores
CN110042322A (en) * 2019-04-23 2019-07-23 浙江德得贸易有限公司 A kind of pre- hard mold steel and preparation method thereof substituting 45 mould steel
US12076788B2 (en) 2019-05-03 2024-09-03 Oerlikon Metco (Us) Inc. Powder feedstock for wear resistant bulk welding configured to optimize manufacturability
EP4426872A4 (en) * 2021-11-05 2025-01-22 Uddeholms AB WEAR RESISTANT ALLOY

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