WO2014101772A1 - Cobalt-chromium-molybdenum alloy with high wear resistance - Google Patents
Cobalt-chromium-molybdenum alloy with high wear resistance Download PDFInfo
- Publication number
- WO2014101772A1 WO2014101772A1 PCT/CN2013/090440 CN2013090440W WO2014101772A1 WO 2014101772 A1 WO2014101772 A1 WO 2014101772A1 CN 2013090440 W CN2013090440 W CN 2013090440W WO 2014101772 A1 WO2014101772 A1 WO 2014101772A1
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- WIPO (PCT)
- Prior art keywords
- wear resistance
- cobalt
- chromium
- high wear
- elements
- Prior art date
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
Definitions
- the present invention belongs to the technical field of high-temperature alloys, and in particular provides a cobalt-chromium-molybdenum alloy with high wear resistance.
- cobalt-based alloys There are two main sets of cobalt-based alloys: cobalt-chromium-tungsten (CoCrW) and cobalt-chromium-molybdenum (CoCrMo).
- CoCrW cobalt-chromium-tungsten
- CoCrMo cobalt-chromium-molybdenum
- the object of the present invention is to provide a CoCrMo alloy with high wear resistance, which solves the problem of inadequate wear resistance in existing CoCrMo alloys well.
- the product can be manufactured by casting, forging or powder metallurgy, etc. It can meet the requirements of the zinc industry, etc., or of demanding industrial environments where resistance to high temperatures, corrosion and wear are all required. It can satisfy the requirements of the jewellery industry for products such as rings, bracelets and watch cases to be scratch-resistant and shinier, and can be used to manufacture sputtering targets for electroplating, wherein a compact and shiny surface layer with high wear resistance is formed by physical vapour deposition, satisfying the higher demands people place on the appearance, colour, lustre and impression of jewellery.
- the present invention is an alloy material in which cobalt is the matrix, with the weight percentages of the component elements thereof being as follows: chromium Cr: 24 - 35%; molybdenum Mo: 5 - 20%; carbon C: 0.35 - 2.5%; nickel Ni: 0 - 4%; iron Fe: 0 - 4%; silicon Si: 0 - 2%; manganese Mn: 0 - 2%; with the remainder being cobalt Co and other unavoidable impurity elements and process elements.
- Solid solution strengthening is the main method used to strengthen common cobalt-chromium-molybdenum (CoCrMo) series alloys in China and abroad, with materials formed by this strengthening method having a maximum hardness of about HRC35.
- CoCrMo alloy with high wear resistance to which the present invention relates two improvements are made which build upon solid solution strengthening. The first is increased weighting in the solid-solution-strengthened alloy, such as a significantly increased Mo content in the solid-solution-strengthened alloy. The second is a significantly increased content of C amongst the components, leading to the formation of a large amount of carbides in the material.
- the various carbides have a far higher microhardness than the solid solution, so a significant increase in the hardness of the material is achieved, solving the problems of existing CoCrMo alloy products in having insufficient hardness and inadequate wear resistance despite resistance to oxidation and corrosion.
- the CoCrMo alloy with high wear resistance to which the present invention relates has a hardness range of 36 - 65 HRC.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physical Vapour Deposition (AREA)
- Powder Metallurgy (AREA)
- Adornments (AREA)
Abstract
Disclosed is a cobalt-chromium-molybdenum alloy with high wear resistance, belonging to the technical field of high-temperature alloys. The weight percentages of the component elements thereof are as follows: Cr: 24-35%; Mo: 5-20%; C: 0.35-2.5%; Ni: 0-4%; Fe: 0-4%; Si: 0-2%; Mn: 0-2%; the remainder being Co and other unavoidable impurity elements and process elements. The advantages thereof are: it solves the problem of inadequate wear resistance in existing CoCrMo alloys well; the product can be manufactured by casting, forging or powder metallurgy, etc.; it can meet the requirements of the zinc industry, etc., or of demanding industrial environments where resistance to high temperatures, corrosion and wear are all required; it can satisfy the requirements of the jewellery industry for products such as rings, bracelets and watch cases to be scratch-resistant and shinier, and can be used to manufacture sputtering targets for electroplating, wherein a compact and shiny surface layer with high wear resistance is formed by physical vapour deposition, satisfying the higher demands people place on the appearance, colour, lustre and impression of jewellery.
Description
Cobalt-chromium-molybdenum alloy with high wear resistance
FIELD OF THE INVENTION
The present invention belongs to the technical field of high-temperature alloys, and in particular provides a cobalt-chromium-molybdenum alloy with high wear resistance.
BACKGROUND OF THE INVENTION
There are two main sets of cobalt-based alloys: cobalt-chromium-tungsten (CoCrW) and cobalt-chromium-molybdenum (CoCrMo). The cobalt-chromium- tungsten (CoCrW) series of alloys are resistant to high temperatures and have excellent wear resistance, but inadequate corrosion resistance, whereas the cobalt-chromium-molybdenum (CoCrMo) series of alloys are resistant to high temperatures and have excellent corrosion resistance, but inadequate wear resistance.
The following table shows standard component ranges and hardness indices for common cobalt-chromium-molybdenum (CoCrMo) series alloys in China and abroad:
1 YY0605. 12-2007/ISO5832-12:1996
Table 1 Unit: Wt%
Table 2 Unit: Wt%
SUMMARY OF THE INVENTION
The object of the present invention is to provide a CoCrMo alloy with high wear resistance, which solves the problem of inadequate wear resistance in existing CoCrMo alloys well. The product can be manufactured by casting, forging or powder metallurgy, etc. It can meet the requirements of the zinc industry, etc., or of demanding industrial environments where resistance to high temperatures, corrosion and wear are all required. It can satisfy the requirements of the jewellery industry for products such as rings, bracelets and watch cases to be scratch-resistant and shinier, and can be used to manufacture sputtering targets for electroplating, wherein a compact and shiny surface layer with high wear resistance is formed by physical vapour deposition, satisfying the higher demands people place on the appearance,
colour, lustre and impression of jewellery.
The present invention is an alloy material in which cobalt is the matrix, with the weight percentages of the component elements thereof being as follows: chromium Cr: 24 - 35%; molybdenum Mo: 5 - 20%; carbon C: 0.35 - 2.5%; nickel Ni: 0 - 4%; iron Fe: 0 - 4%; silicon Si: 0 - 2%; manganese Mn: 0 - 2%; with the remainder being cobalt Co and other unavoidable impurity elements and process elements.
Solid solution strengthening is the main method used to strengthen common cobalt-chromium-molybdenum (CoCrMo) series alloys in China and abroad, with materials formed by this strengthening method having a maximum hardness of about HRC35. In the CoCrMo alloy with high wear resistance to which the present invention relates, two improvements are made which build upon solid solution strengthening. The first is increased weighting in the solid-solution-strengthened alloy, such as a significantly increased Mo content in the solid-solution-strengthened alloy. The second is a significantly increased content of C amongst the components, leading to the formation of a large amount of carbides in the material. The various carbides have a far higher microhardness than the solid solution, so a significant increase in the hardness of the material is achieved, solving the problems of existing CoCrMo alloy products in having insufficient hardness and inadequate wear resistance despite resistance to oxidation and corrosion.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The above-mentioned domestic and foreign CoCrMo alloy materials have a hardness range of HRC 25 - 35, so the wear resistance thereof is clearly inadequate.
Materials were mixed in the component proportions given below, steel ingots were produced by vacuum casting, and the hardness of the alloys produced were
tested. The results are shown in Table 3:
Table 3 Wt%
In summary, the CoCrMo alloy with high wear resistance to which the present invention relates has a hardness range of 36 - 65 HRC.
Claims
1. Cobalt-chromium- molybdenum alloy with high wear resistance, characterized in that the weight percentages of the component elements thereof are as follows: chromium Cr: 24 - 35%; molybdenum Mo: 5 - 20%; carbon C: 0.35 - 2.5%; nickel Ni: 0 - 4%; iron Fe: 0 - 4%; silicon Si: 0 - 2%; manganese Mn: 0 - 2%; with the remainder being cobalt Co and other unavoidable impurity elements and process elements.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201210576100.X | 2012-12-26 | ||
CN201210576100XA CN103060617A (en) | 2012-12-26 | 2012-12-26 | Co-Cr-Mo alloy with high wear resistance |
Publications (1)
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WO2014101772A1 true WO2014101772A1 (en) | 2014-07-03 |
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PCT/CN2013/090440 WO2014101772A1 (en) | 2012-12-26 | 2013-12-25 | Cobalt-chromium-molybdenum alloy with high wear resistance |
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CN (1) | CN103060617A (en) |
WO (1) | WO2014101772A1 (en) |
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EP3000728A1 (en) * | 2014-09-26 | 2016-03-30 | Goodrich Corporation | Landing gear components having improved joints |
JP2018151299A (en) * | 2017-03-14 | 2018-09-27 | セイコーエプソン株式会社 | Watch component and watch |
JP2018151298A (en) * | 2017-03-14 | 2018-09-27 | セイコーエプソン株式会社 | Watch component and watch |
EP3382056A1 (en) * | 2017-03-27 | 2018-10-03 | Seiko Epson Corporation | Timepiece part, and timepieces |
EP3375903A3 (en) * | 2017-03-14 | 2018-10-10 | Seiko Epson Corporation | Timepiece part, and timepiece |
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US11155904B2 (en) | 2019-07-11 | 2021-10-26 | L.E. Jones Company | Cobalt-rich wear resistant alloy and method of making and use thereof |
US11224915B2 (en) * | 2017-06-05 | 2022-01-18 | General Electric Company | Method of repairing a component using an additive manufacture replacement coupon, and alloy for additive manufacturing |
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Cited By (11)
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---|---|---|---|---|
EP3000728A1 (en) * | 2014-09-26 | 2016-03-30 | Goodrich Corporation | Landing gear components having improved joints |
US9452827B2 (en) | 2014-09-26 | 2016-09-27 | Goodrich Corporation | Landing gear components having improved joints |
JP2018151299A (en) * | 2017-03-14 | 2018-09-27 | セイコーエプソン株式会社 | Watch component and watch |
JP2018151298A (en) * | 2017-03-14 | 2018-09-27 | セイコーエプソン株式会社 | Watch component and watch |
EP3375903A3 (en) * | 2017-03-14 | 2018-10-10 | Seiko Epson Corporation | Timepiece part, and timepiece |
EP3382056A1 (en) * | 2017-03-27 | 2018-10-03 | Seiko Epson Corporation | Timepiece part, and timepieces |
JP2018163085A (en) * | 2017-03-27 | 2018-10-18 | セイコーエプソン株式会社 | Watch component and watch |
JP2018163086A (en) * | 2017-03-27 | 2018-10-18 | セイコーエプソン株式会社 | Watch component and watch |
US11224915B2 (en) * | 2017-06-05 | 2022-01-18 | General Electric Company | Method of repairing a component using an additive manufacture replacement coupon, and alloy for additive manufacturing |
US11155904B2 (en) | 2019-07-11 | 2021-10-26 | L.E. Jones Company | Cobalt-rich wear resistant alloy and method of making and use thereof |
CN115698351A (en) * | 2020-05-11 | 2023-02-03 | 海恩斯国际公司 | Deformable chromium-containing cobalt-based alloys with improved resistance to galling and chloride-induced crevice attack |
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