WO2011071033A1 - 焼結摺動部材 - Google Patents

焼結摺動部材 Download PDF

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Publication number
WO2011071033A1
WO2011071033A1 PCT/JP2010/071879 JP2010071879W WO2011071033A1 WO 2011071033 A1 WO2011071033 A1 WO 2011071033A1 JP 2010071879 W JP2010071879 W JP 2010071879W WO 2011071033 A1 WO2011071033 A1 WO 2011071033A1
Authority
WO
WIPO (PCT)
Prior art keywords
sliding member
resistance
sintered sliding
boron nitride
sintered
Prior art date
Application number
PCT/JP2010/071879
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
石井 義成
丸山 恒夫
佳樹 田村
Original Assignee
株式会社ダイヤメット
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 株式会社ダイヤメット filed Critical 株式会社ダイヤメット
Priority to BR112012013137-0A priority Critical patent/BR112012013137B1/pt
Priority to EP10835953.0A priority patent/EP2511388B1/en
Priority to CN2010800542081A priority patent/CN102648299B/zh
Priority to JP2011545209A priority patent/JP5337884B2/ja
Priority to US13/504,645 priority patent/US8709124B2/en
Publication of WO2011071033A1 publication Critical patent/WO2011071033A1/ja

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/08Alloys with open or closed pores
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/002Alloys based on nickel or cobalt with copper as the next major constituent
    • 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
    • C22C30/02Alloys containing less than 50% by weight of each constituent containing copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0068Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only nitrides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121Use of special materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2204/00Metallic materials; Alloys
    • F16C2204/52Alloys based on nickel, e.g. Inconel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00Shaping
    • F16C2220/20Shaping by sintering pulverised material, e.g. powder metallurgy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2300/00Application independent of particular apparatuses
    • F16C2300/40Application independent of particular apparatuses related to environment, i.e. operating conditions
    • F16C2300/54Application independent of particular apparatuses related to environment, i.e. operating conditions high-temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/22Internal combustion engines

Definitions

  • the present invention relates to a sintered sliding member having excellent heat resistance, corrosion resistance and wear resistance.
  • a bearing used for a recirculation exhaust gas flow rate adjustment valve of an EGR (Exhaust Gas ⁇ ⁇ ⁇ Recirculation) type internal combustion engine.
  • the bearing used for the recirculation exhaust gas flow control valve of the EGR internal combustion engine is made of graphite or a sintered Cu alloy containing Sn: 7 to 10% and C: 5 to 9% by mass. The ones made are known.
  • Patent Document 2 discloses a structure composed of a sintered Cu alloy having a structure in which free graphite is dispersed and distributed on a substrate of a Cu—Ni—Sn solid solution.
  • examples of sintered sliding materials that are exposed to seawater and snow melting agents include sliding materials for outboard motors and exhaust throttle valve bearings used in diesel exhaust gas purification systems. These require high corrosion resistance, but especially exhaust throttle valve bearings are required to have heat resistance, corrosion resistance, and wear resistance in environments where heating and cooling are repeated while being exposed to high-temperature chlorides. Yes. In addition, the thing made from stainless steel is used for this bearing.
  • the sintered Cu alloy of Patent Document 2 can exhibit excellent wear resistance even in a high temperature environment, but a sintered sliding member having further excellent heat resistance and corrosion resistance is desired.
  • stainless steel bearings can exhibit excellent heat resistance and corrosion resistance in an environment where heating and cooling are repeated while being exposed to high-temperature chloride, but wear resistance is not sufficient.
  • an object of the present invention is to provide a novel sintered sliding member having excellent heat resistance, corrosion resistance, and wear resistance.
  • the sintered sliding member of the present invention comprises, by mass, 7.7 to 30.3% Cu, 2.0 to 20.0% Sn, 0.3 to 7.0% boron nitride, And the balance consists of Ni and inevitable impurities.
  • the porosity is 5 to 25%.
  • the sintered sliding member of the present invention comprises, by mass, 7.7 to 30.3% Cu, 2.0 to 20.0% Sn, 0.3 to 7.0% boron nitride, When the balance is made of Ni and inevitable impurities, the heat resistance, corrosion resistance, and wear resistance are excellent.
  • the sintered sliding member of the present invention comprises, by mass, 7.7 to 30.3% Cu, 2.0 to 20.0% Sn, 0.3 to 7.0% boron nitride, And the balance consists of Ni and inevitable impurities.
  • the sintered sliding member of the present invention has a lower Cu content than a conventional sintered Cu-based alloy, relatively increases the Ni content, and further contains boron nitride, thereby improving heat resistance and corrosion resistance. It will be excellent.
  • the porosity is 5 to 25%. And by this composition, friction resistance falls and it becomes what was further excellent in abrasion resistance.
  • Cu Cu has the effect of forming a solid solution of Ni and Sn and improving the wear resistance of the sintered sliding member. If the Cu content is less than 7.7%, the wear resistance is insufficient. On the other hand, if it exceeds 30.3%, the heat resistance and corrosion resistance become insufficient, such being undesirable. Therefore, the Cu content is 7.7 to 30.3%.
  • Sn Sn lowers the melting point to improve the sinterability, forms a solid solution with Cu and Ni, improves the strength of the sintered sliding member, and contributes to improved wear resistance. If the Sn content is less than 2%, the predetermined wear resistance cannot be obtained. On the other hand, if it exceeds 20%, the aggression against the sliding partner material is increased and the counterpart material is worn, which is not preferable. Therefore, the Sn content is set to 2.0 to 20.0%.
  • Boron nitride imparts excellent lubricity to the sintered sliding member as a solid lubricant and reduces metal contact between the sliding members, thereby contributing to improvement in wear resistance of the sintered sliding member. Furthermore, there is an effect of improving high temperature salt damage resistance. If the ratio is less than 0.3%, the desired effect cannot be obtained. On the other hand, if it exceeds 7.0%, the strength of the sintered sliding member decreases, which is not preferable. Therefore, the boron nitride content is set to 0.3 to 7.0%.
  • the porosity is less than 5%, the deformation resistance of the sintered sliding member increases, and the dimensional accuracy in the correction process cannot be sufficiently obtained.
  • the porosity exceeds 25%, the mechanical characteristics are deteriorated, and characteristics such as strength are not satisfied even when sizing and coining are performed. Therefore, in the above composition, the porosity is in the range of 5 to 25%.
  • the sintered sliding member of the present invention is not limited to a following example, A various deformation
  • a bearing having a sliding surface on the inner periphery will be described.
  • the present invention is not limited to this and can be implemented in various sintered sliding members.
  • Raw material powders particle size—100 mesh Ni-30% Cu atomized powder, average particle size 4.0 ⁇ m Ni powder, particle size—200 mesh Cu powder, particle size—250 mesh Sn atomized powder, particle size— A 75 ⁇ m boron nitride powder and a graphite powder having a particle size of ⁇ 150 mesh were prepared. These raw material powders are blended so as to have the final component composition shown in Table 1, 0.5% of zinc stearate is added, mixed for 30 minutes with a V-type mixer, and then pressed to produce a green compact. did.
  • This green compact is mixed with natural gas and air, and passed through a heated catalyst, and in an endothermic gas (endothermic gas) atmosphere that has been decomposed and transformed, at a sintering temperature of 1050 ° C. for 20 minutes. Sintering followed by sizing.
  • High temperature salt damage cycle test The high-temperature salt damage cycle test was repeated 15 times on the ring-shaped test pieces of Invention Examples 1 to 15 and Comparative Examples 1 to 8, and the amount of change in the inner diameter of the ring-shaped test pieces before and after the test was determined. The degree of corrosion when exposed was evaluated. The results are shown in Table 1 as resistance to high temperature salt damage (change in inner diameter dimension). In addition, the amount of change in the inner diameter dimension is smaller as the material is more resistant to high temperature salt damage.
  • the test piece was heated at 500 ° C. for 8 hours, cooled at room temperature for 30 minutes, immersed in 5% saline for 20 minutes at room temperature, and dried at 50 ° C. for 60 minutes. Again, 15 cycles of heating at 500 ° C. for 8 hours were performed.
  • the sintered sliding member of the present invention was excellent in wear resistance, heat resistance and corrosion resistance.
  • FIG. 2 shows a scanning electron micrograph of the cross-sectional structure of the sintered sliding member of the first invention. It was confirmed that the boron nitride powder was dispersed in the Ni—Cu—Sn matrix.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Sliding-Contact Bearings (AREA)
  • Powder Metallurgy (AREA)
  • Ceramic Products (AREA)
PCT/JP2010/071879 2009-12-07 2010-12-07 焼結摺動部材 WO2011071033A1 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
BR112012013137-0A BR112012013137B1 (pt) 2009-12-07 2010-12-07 Sintered sliding element
EP10835953.0A EP2511388B1 (en) 2009-12-07 2010-12-07 Sintered sliding member
CN2010800542081A CN102648299B (zh) 2009-12-07 2010-12-07 烧结滑动部件
JP2011545209A JP5337884B2 (ja) 2009-12-07 2010-12-07 焼結摺動部材
US13/504,645 US8709124B2 (en) 2009-12-07 2010-12-07 Sintered sliding member

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2009278052 2009-12-07
JP2009-278052 2009-12-07

Publications (1)

Publication Number Publication Date
WO2011071033A1 true WO2011071033A1 (ja) 2011-06-16

Family

ID=44145577

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2010/071879 WO2011071033A1 (ja) 2009-12-07 2010-12-07 焼結摺動部材

Country Status (6)

Country Link
US (1) US8709124B2 (zh)
EP (1) EP2511388B1 (zh)
JP (1) JP5337884B2 (zh)
CN (1) CN102648299B (zh)
BR (1) BR112012013137B1 (zh)
WO (1) WO2011071033A1 (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013057365A (ja) * 2011-09-08 2013-03-28 Ntn Corp 配光可変型前照灯装置用すべり軸受
JP2015121324A (ja) * 2015-01-20 2015-07-02 Ntn株式会社 配光可変型前照灯装置用すべり軸受

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6440297B2 (ja) * 2014-09-04 2018-12-19 株式会社ダイヤメット Cu基焼結軸受
JP6468766B2 (ja) * 2014-09-11 2019-02-13 株式会社ダイヤメット 耐食性、耐熱性、耐摩耗性に優れた焼結摺動材及びその製造方法
WO2017150271A1 (ja) * 2016-03-04 2017-09-08 株式会社ダイヤメット Cu基焼結摺動材およびその製造方法
JP6769007B2 (ja) * 2017-06-29 2020-10-14 株式会社ダイヤメット モータ式燃料ポンプ用焼結軸受及びその製造方法
CN110484915B (zh) * 2019-09-09 2021-06-11 南京工程学院 一种于轴套类零件内表面制备减摩耐磨多孔涂层的方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63109131A (ja) * 1986-10-24 1988-05-13 Nippon Funmatsu Gokin Kk 焼結合金摩擦材料
JPH11158511A (ja) * 1997-11-26 1999-06-15 Oiles Ind Co Ltd 多孔質静圧気体軸受用の軸受素材及びこれを用いた多孔質静圧気体軸受
JP2000309807A (ja) * 1999-04-23 2000-11-07 Daido Metal Co Ltd 摺動部材
JP2002521610A (ja) 1998-07-30 2002-07-16 シーメンス カナダ リミテッド 排気ガス再循環アセンブリ
JP2004068074A (ja) 2002-08-06 2004-03-04 Mitsubishi Materials Corp 高温環境下ですぐれた耐摩耗性を示すEGR式内燃機関の再循環排ガス流量制御弁の焼結Cu合金製軸受
JP2006097797A (ja) * 2004-09-29 2006-04-13 Oiles Ind Co Ltd 多孔質静圧気体軸受及びその製造方法

Family Cites Families (8)

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JP3782446B2 (ja) * 1994-04-28 2006-06-07 新日本製鐵株式会社 高強度高温用自己潤滑性複合材料およびその製造方法
JPH09285888A (ja) * 1996-04-25 1997-11-04 Nhk Spring Co Ltd ステンレス鋼用ろう材
JP4385618B2 (ja) * 2002-08-28 2009-12-16 オイレス工業株式会社 多孔質静圧気体軸受用の軸受素材及びこれを用いた多孔質静圧気体軸受
JP2004148469A (ja) * 2002-10-31 2004-05-27 Mitsui Kensaku Toishi Kk メタルボンド研削工具
JP4521871B2 (ja) * 2005-01-18 2010-08-11 株式会社ダイヤメット 耐食性、耐摩耗性および高強度を有するモータ式燃料ポンプの軸受
CN102773488A (zh) * 2006-01-16 2012-11-14 奥依列斯工业株式会社 铜类烧结滑动部件
RU2326952C1 (ru) * 2006-11-07 2008-06-20 Юлия Алексеевна Щепочкина Спеченный антифрикционный материал на основе меди
JP5266682B2 (ja) * 2007-07-31 2013-08-21 キャタピラージャパン株式会社 複層焼結摺動部材

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63109131A (ja) * 1986-10-24 1988-05-13 Nippon Funmatsu Gokin Kk 焼結合金摩擦材料
JPH11158511A (ja) * 1997-11-26 1999-06-15 Oiles Ind Co Ltd 多孔質静圧気体軸受用の軸受素材及びこれを用いた多孔質静圧気体軸受
JP2002521610A (ja) 1998-07-30 2002-07-16 シーメンス カナダ リミテッド 排気ガス再循環アセンブリ
JP2000309807A (ja) * 1999-04-23 2000-11-07 Daido Metal Co Ltd 摺動部材
JP2004068074A (ja) 2002-08-06 2004-03-04 Mitsubishi Materials Corp 高温環境下ですぐれた耐摩耗性を示すEGR式内燃機関の再循環排ガス流量制御弁の焼結Cu合金製軸受
JP2006097797A (ja) * 2004-09-29 2006-04-13 Oiles Ind Co Ltd 多孔質静圧気体軸受及びその製造方法

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013057365A (ja) * 2011-09-08 2013-03-28 Ntn Corp 配光可変型前照灯装置用すべり軸受
JP2015121324A (ja) * 2015-01-20 2015-07-02 Ntn株式会社 配光可変型前照灯装置用すべり軸受

Also Published As

Publication number Publication date
CN102648299A (zh) 2012-08-22
BR112012013137A2 (pt) 2017-03-21
JP5337884B2 (ja) 2013-11-06
EP2511388B1 (en) 2018-03-14
EP2511388A4 (en) 2017-05-03
EP2511388A1 (en) 2012-10-17
CN102648299B (zh) 2013-11-06
US8709124B2 (en) 2014-04-29
BR112012013137B1 (pt) 2018-02-06
US20120204677A1 (en) 2012-08-16
JPWO2011071033A1 (ja) 2013-04-22

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