JP2019203553A - Half-split bearing and bearing - Google Patents

Half-split bearing and bearing Download PDF

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JP2019203553A
JP2019203553A JP2018098648A JP2018098648A JP2019203553A JP 2019203553 A JP2019203553 A JP 2019203553A JP 2018098648 A JP2018098648 A JP 2018098648A JP 2018098648 A JP2018098648 A JP 2018098648A JP 2019203553 A JP2019203553 A JP 2019203553A
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bearing
half bearing
lining layer
less
test
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大輔 岩城
Daisuke Iwaki
大輔 岩城
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Taiho Kogyo Co Ltd
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Taiho Kogyo Co Ltd
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Priority to DE102019113442.0A priority patent/DE102019113442A1/en
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    • 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
    • F16C33/20Sliding surface consisting mainly of plastics
    • F16C33/203Multilayer structures, e.g. sleeves comprising a plastic lining
    • F16C33/205Multilayer structures, e.g. sleeves comprising a plastic lining with two layers
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/003Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent
    • 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
    • F16C33/046Brasses; Bushes; Linings divided or split, e.g. half-bearings or rolled sleeves
    • 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
    • F16C2202/00Solid materials defined by their properties
    • F16C2202/02Mechanical properties
    • F16C2202/04Hardness
    • 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
    • F16C2204/10Alloys based on copper
    • 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
    • F16C2204/10Alloys based on copper
    • F16C2204/12Alloys based on copper with tin as the next major constituent
    • 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
    • F16C2204/10Alloys based on copper
    • F16C2204/18Alloys based on copper with bismuth as the next major constituent
    • 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
    • F16C2204/20Alloys based on aluminium
    • 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
    • F16C2208/00Plastics; Synthetic resins, e.g. rubbers
    • F16C2208/20Thermoplastic resins
    • F16C2208/40Imides, e.g. polyimide [PI], polyetherimide [PEI]
    • F16C2208/42Polyamideimide [PAI]
    • 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
    • F16C2240/00Specified values or numerical ranges of parameters; Relations between them
    • F16C2240/40Linear dimensions, e.g. length, radius, thickness, gap
    • F16C2240/54Surface roughness
    • 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
    • F16C33/10Construction relative to lubrication
    • F16C33/1095Construction relative to lubrication with solids as lubricant, e.g. dry coatings, powder
    • 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
    • F16C9/00Bearings for crankshafts or connecting-rods; Attachment of connecting-rods
    • F16C9/04Connecting-rod bearings; Attachments thereof

Abstract

To provide a bearing having fatigue resistance, wear resistance, and foreign matter resistance in an improved balance.SOLUTION: A half-split bearing according to one embodiment has a lining layer formed of a copper alloy and having a hardness of 120HV0.2 or less, and a coating layer that is formed on the lining layer, contains at least a binder resin, and has a surface roughness of 0.6 μmRa or less.SELECTED DRAWING: Figure 2

Description

本発明は軸受に関する。   The present invention relates to a bearing.

基材上に樹脂コーティング層を形成した摺動部材が知られている。例えば特許文献1には、基板上に、バインダー樹脂及びFe2O3を含むコーティング層を形成した摺動部材が記載されている。   A sliding member having a resin coating layer formed on a substrate is known. For example, Patent Document 1 describes a sliding member in which a coating layer containing a binder resin and Fe2O3 is formed on a substrate.

特表2012−514170号公報Special table 2012-514170 gazette

特許文献1に記載の技術においても、耐疲労性、耐摩耗性、及び耐異物性のバランスに改善の余地があった。これに対し本発明は、耐疲労性、耐摩耗性、及び耐異物性のバランスが改善された軸受を提供する。   The technique described in Patent Document 1 also has room for improvement in the balance of fatigue resistance, wear resistance, and foreign matter resistance. In contrast, the present invention provides a bearing with an improved balance of fatigue resistance, wear resistance, and foreign matter resistance.

本発明は、銅系合金で形成され、硬さ120HV0.2以下のライニング層と、前記ライニング層の上に形成され、少なくともバインダー樹脂を含み、表面粗さ0.6μmRa以下のコーティング層とを有する半割軸受を提供する。   The present invention includes a lining layer formed of a copper-based alloy and having a hardness of 120 HV 0.2 or less, and a coating layer formed on the lining layer and including at least a binder resin and having a surface roughness of 0.6 μm Ra or less. Provide half bearings.

前記ライニング層の硬さが100HV0.2以下であってもよい。   The lining layer may have a hardness of 100 HV 0.2 or less.

前記コーティング層の表面粗さが0.2μmRzJIS以下であってもよい。   The surface roughness of the coating layer may be 0.2 μm Rz JIS or less.

前記銅系合金が、0.5〜15質量%のBi、及び1〜15質量%のSnを含んでもよい。   The copper-based alloy may include 0.5 to 15% by mass of Bi and 1 to 15% by mass of Sn.

また、本発明は、第1半割軸受と、前記第1半割軸受よりも低い荷重がかかる第2半割軸受とを有し、前記第1半割軸受は、アルミニウム系合金で形成された第1ライニング層と、少なくともバインダー樹脂を含む第1コーティング層とを有し、前記第2半割軸受は、銅系合金で形成され、硬さ120HV以下の第2ライニング層と、前記第2ライニング層の上に形成され、少なくともバインダー樹脂を含み、表面粗さ0.6μmRa以下の第2コーティング層とを有する軸受を提供する。   In addition, the present invention has a first half bearing and a second half bearing to which a load lower than that of the first half bearing is applied, and the first half bearing is made of an aluminum-based alloy. The second lining bearing has a first lining layer and a first coating layer containing at least a binder resin, and the second half bearing is made of a copper-based alloy and has a hardness of 120 HV or less, and the second lining. Provided is a bearing having a second coating layer formed on the layer and containing at least a binder resin and having a surface roughness of 0.6 μmRa or less.

本発明によれば、耐疲労性、耐摩耗性、及び耐異物性のバランスが改善された軸受を提供することができる。   According to the present invention, it is possible to provide a bearing with an improved balance of fatigue resistance, wear resistance, and foreign matter resistance.

一実施形態に係る軸受1の構造を例示する図。The figure which illustrates the structure of the bearing 1 which concerns on one Embodiment. 半割軸受2(及び半割軸受3)の断面構造を例示する図。The figure which illustrates the cross-section of the half bearing 2 (and half bearing 3). 異物投入試験の条件を示す図。The figure which shows the conditions of a foreign material injection | throwing-in test. 片当たり試験の条件を示す図。The figure which shows the conditions of a one-piece test.

1.構造
図1は、一実施形態に係る軸受1の構造を例示する図である。軸受1は、半割軸受2及び半割軸受3を組み合わせたすべり軸受である。軸受1は、例えばコネクティングロッドにおいて用いられる、いわゆるコンロッド軸受である。半割軸受2はアッパ側の半割軸受(第1半割軸受の一例)であり、半割軸受3はロア側の半割軸受(第2半割軸受の一例)である。半割軸受2には、半割軸受3よりも高い荷重がかかる。なお、軸受1の用途はコンロッド軸受に限定されず、いわゆる主軸受等、他の用途に用いられてもよい。
1. Structure FIG. 1 is a diagram illustrating a structure of a bearing 1 according to an embodiment. The bearing 1 is a sliding bearing in which a half bearing 2 and a half bearing 3 are combined. The bearing 1 is a so-called connecting rod bearing used in, for example, a connecting rod. The half bearing 2 is an upper half bearing (an example of a first half bearing), and the half bearing 3 is a lower half bearing (an example of a second half bearing). A load higher than that of the half bearing 3 is applied to the half bearing 2. The application of the bearing 1 is not limited to the connecting rod bearing, but may be used for other applications such as a so-called main bearing.

図2は、半割軸受2(及び半割軸受3)の断面構造を例示する図である。図2は、半割軸受2の、軸方向に平行かつ摺動面に垂直な断面を示している。半割軸受2は、裏金21、ライニング層22、及びコーティング層23を有する。裏金21は、半割軸受2に形状及び機械的な強度を与えるための層であり、例えば、鋼、鋳鉄、又は樹脂で形成される。   FIG. 2 is a diagram illustrating a cross-sectional structure of the half bearing 2 (and half bearing 3). FIG. 2 shows a cross section of the half bearing 2 parallel to the axial direction and perpendicular to the sliding surface. The half bearing 2 has a back metal 21, a lining layer 22, and a coating layer 23. The back metal 21 is a layer for giving the half bearing 2 a shape and mechanical strength, and is formed of, for example, steel, cast iron, or resin.

ライニング層22は、摺動特性を改善するための層である。ライニング層22の材料としては、半割軸受2(又は軸受1)の用途において要求される特性を満足できる材料が選択される。この例において、ライニング層22は、銅系合金で形成される。銅系合金とは、銅を主成分とした合金をいう。一例において、この銅系合金は、0.5〜15質量%のBi及び1〜15質量%のSnを含み、残部がCu及び不可避不純物で構成される。   The lining layer 22 is a layer for improving sliding characteristics. As the material of the lining layer 22, a material that satisfies the characteristics required for the application of the half bearing 2 (or the bearing 1) is selected. In this example, the lining layer 22 is formed of a copper-based alloy. The copper-based alloy refers to an alloy mainly composed of copper. In one example, this copper-based alloy contains 0.5 to 15% by mass of Bi and 1 to 15% by mass of Sn, with the balance being Cu and inevitable impurities.

耐異物性(異物埋収性)を向上させる観点から、ライニング層22の硬さは、120HV0.2であることが好ましく、100HV0.2以下であることがより好ましく、90HV0.2以下であることがさらに好ましい。また、ライニング層22に銅系合金を用いることにより、例えばライニング層にアルミニウム系合金を用いた半割軸受と比較して、耐疲労性を向上させることができる。一例において、ライニング層22の厚みは0.15〜0.30mmである。   From the viewpoint of improving the foreign matter resistance (foreign matter embedding property), the hardness of the lining layer 22 is preferably 120HV0.2, more preferably 100HV0.2 or less, and 90HV0.2 or less. Is more preferable. Further, by using a copper-based alloy for the lining layer 22, fatigue resistance can be improved as compared with, for example, a half bearing using an aluminum-based alloy for the lining layer. In one example, the thickness of the lining layer 22 is 0.15 to 0.30 mm.

コーティング層23は、摺動特性を改善するための層である。コーティング層23の材料としては、半割軸受2(又は軸受1)の用途において要求される特性を満足できる材料が選択される。この例において、コーティング層23は、少なくともバインダー樹脂を含む。バインダー樹脂としては、例えば熱硬化性樹脂が用いられる。具体的には、バインダー樹脂は、ポリアミドイミド(PAI)樹脂、ポリイミド(PI)樹脂、ポリアミド樹脂、エポキシ樹脂、フェノール樹脂、ポリアセタール樹脂、ポリエーテルケーテルケトン樹脂、及びポリフェニレンサルファイド樹脂のうち少なくとも一種を含む。   The coating layer 23 is a layer for improving sliding characteristics. As the material of the coating layer 23, a material that can satisfy the characteristics required for the application of the half bearing 2 (or the bearing 1) is selected. In this example, the coating layer 23 includes at least a binder resin. As the binder resin, for example, a thermosetting resin is used. Specifically, the binder resin is at least one of a polyamide-imide (PAI) resin, a polyimide (PI) resin, a polyamide resin, an epoxy resin, a phenol resin, a polyacetal resin, a polyether catheter ketone resin, and a polyphenylene sulfide resin. Including.

コーティング層23は、バインダー樹脂に加え、バインダー樹脂中に分散された添加物を含んでもよい。添加物は、例えば、固体潤滑剤、軟質物、硬質物、及びカップリング剤のうち少なくとも一種を含む。   The coating layer 23 may include an additive dispersed in the binder resin in addition to the binder resin. The additive includes, for example, at least one of a solid lubricant, a soft material, a hard material, and a coupling agent.

固体潤滑材は、摩擦特性を改善するために添加される。固体潤滑剤は、例えば、MoS2、WS2、ポリテトラフルオロエチレン(PTFE)、グラファイト、h−BN、及びSB2O3のうち少なくとも一種を含む。例えばMoS2は、良好な潤滑性を与える。また、PTFEは分子間凝集力が小さいので、摩擦係数を低減する効果がある。さらに、グラファイトは濡れ性を向上させ、初期なじみ性を向上させる。初期なじみ性とは、摺動開始後に相手材と摺接する際、摺動面が摩耗して平滑になり、摺動性を向上させる性質である。初期なじみ性の発現により摺動性が向上すると、摺動層全体としての摩耗量が低減される。   Solid lubricant is added to improve the friction properties. The solid lubricant includes, for example, at least one of MoS2, WS2, polytetrafluoroethylene (PTFE), graphite, h-BN, and SB2O3. For example, MoS2 gives good lubricity. Further, PTFE has an effect of reducing the friction coefficient because of its low intermolecular cohesion. In addition, graphite improves wettability and improves initial conformability. The initial conformability is a property of improving the slidability when the sliding surface wears and becomes smooth when slidably contacting with the counterpart material after the start of sliding. When the slidability is improved by the expression of the initial conformability, the wear amount of the entire sliding layer is reduced.

軟質物は、異物埋収性を改善するために添加される。軟質物は、例えば、Sn、Al、又はBiのうち少なくとも一種を含む。硬質物は、耐摩耗性を改善するために添加される
。硬質物は、例えば、SiC、Al2O3、TiN、AlN、CrO2、Si3N4、ZrO2、Fe3Pのうち少なくとも一種を含む。
The soft material is added in order to improve the foreign material burying property. The soft material includes, for example, at least one of Sn, Al, or Bi. Hard materials are added to improve wear resistance. The hard material includes, for example, at least one of SiC, Al2O3, TiN, AlN, CrO2, Si3N4, ZrO2, and Fe3P.

カップリング剤は、バインダー樹脂と基材(ライニング層22)との結合を強化するために添加される。カップリング剤としては、例えば、シランカップリング剤が用いられる。   The coupling agent is added to reinforce the bond between the binder resin and the base material (lining layer 22). For example, a silane coupling agent is used as the coupling agent.

耐異物性を向上させる観点から、コーティング層23の表面粗さは、0.6μmRa以下であることが好ましく、0.4μmRa以下であることがより好ましく、0.2μm以下であることがさらに好ましい。また、コーティング層23に樹脂を含むコーティング材を用いることにより、例えばコーティング材としてめっきを用いた半割軸受と比較して、耐摩耗性を向上させることができる。   From the viewpoint of improving the foreign matter resistance, the surface roughness of the coating layer 23 is preferably 0.6 μmRa or less, more preferably 0.4 μmRa or less, and further preferably 0.2 μm or less. Further, by using a coating material containing a resin for the coating layer 23, for example, wear resistance can be improved as compared to a half bearing using plating as the coating material.

一例において、コーティング層23は、35〜55質量%のポリアミドイミド(PAI)、43〜63質量%のグラファイト(Gr.)、及び0.1〜10質量%のSiCを含み、残部が不可避不純物から構成される。なお、SiCは他の硬質物に置換されてもよいし、硬質物は一切添加されなくてもよい。一例において、コーティング層23の厚みは0.001〜0.02mmである。   In one example, the coating layer 23 includes 35 to 55% by mass of polyamideimide (PAI), 43 to 63% by mass of graphite (Gr.), And 0.1 to 10% by mass of SiC, with the remainder being inevitable impurities. Composed. Note that SiC may be replaced with another hard material, or no hard material may be added. In one example, the thickness of the coating layer 23 is 0.001 to 0.02 mm.

半割軸受3も半割軸受2と同様の断面構造を有している。ただしこの例において、ライニング層32の材料は、ライニング層22よりも柔らかいものが用いられる。一例において、ライニング層32の材料は、アルミニウム系合金である。アルミニウム系合金とは、アルミニウムを主成分とした合金をいう。一例において、このアルミニウム系合金は、1〜15質量%のSn及び1〜8質量%のSiを含み、残部がAl及び不可避不純物で構成される。ライニング層32にアルミニウム系合金を用いることにより、例えば銅系合金を用いたライニングと比較して、耐異物性を向上させることができる。   The half bearing 3 also has the same cross-sectional structure as the half bearing 2. However, in this example, the material of the lining layer 32 is softer than that of the lining layer 22. In one example, the material of the lining layer 32 is an aluminum-based alloy. An aluminum-based alloy refers to an alloy mainly composed of aluminum. In one example, this aluminum-based alloy contains 1 to 15% by mass of Sn and 1 to 8% by mass of Si, with the balance being composed of Al and inevitable impurities. By using an aluminum-based alloy for the lining layer 32, the foreign matter resistance can be improved as compared with, for example, a lining using a copper-based alloy.

2.実験例
本願の発明者らは、上記で説明した軸受について、実際に試料を作製した。発明者らはさらに、これらの試料について物性及び機械特性の試験を行った。なお以下においては実験例においては、具体的な寸法、原料、及び組成を有する試料を準備したが、これらはあくまで一例であり、本発明はこれらに限定されるものではない。
2. Experimental Example The inventors of the present application actually produced a sample for the bearing described above. The inventors further tested physical properties and mechanical properties of these samples. In the following, in the experimental examples, samples having specific dimensions, raw materials, and compositions were prepared, but these are merely examples, and the present invention is not limited to these.

2−1.試料
表1は、本願の発明者らが準備した2つの試料(試料1及び2)について、アッパ側の半割軸受2のライニング層22及びコーティング層23の組成(質量%)を示す。なおどの試料も、表に記載された原料以外のものは意図的には含まれない(ただし、表に記載されていない原料が不可避不純物として含まれる可能性がある)。表1に記載されているとおり、どの試料もライニング層は銅系合金により形成される。コーティング層においては、バインダー樹脂としてPAIが用いられた。固体潤滑剤として、グラファイト(試料1)、BN(試料2)、又はMoS2(試料3)が用いられた。その他の添加物としてSiC(試料1)又はFe2O3(試料2)が用いられた。

Figure 2019203553
2-1. Sample Table 1 shows the composition (mass%) of the lining layer 22 and the coating layer 23 of the half bearing 2 on the upper side for two samples (samples 1 and 2) prepared by the inventors of the present application. None of the samples intentionally includes materials other than those listed in the table (however, materials not listed in the table may be included as inevitable impurities). As described in Table 1, the lining layer is formed of a copper-based alloy in any sample. In the coating layer, PAI was used as a binder resin. As the solid lubricant, graphite (sample 1), BN (sample 2), or MoS2 (sample 3) was used. As other additives, SiC (sample 1) or Fe2O3 (sample 2) was used.
Figure 2019203553

2−2.硬さ試験
発明者らは、試料1及び2について、ライニング層の硬さ試験を行った。硬さ試験は、「JIS Z 2244 − ビッカース硬さ試験 試験方法」によった。なお試験は試験力200gで行った。試験結果は以下のとおりである。
試料1: 90HV0.2
試料2: 150HV0.2
2-2. Hardness Test The inventors conducted a hardness test of the lining layer for Samples 1 and 2. The hardness test was based on “JIS Z 2244-Vickers hardness test test method”. The test was conducted with a test force of 200 g. The test results are as follows.
Sample 1: 90HV0.2
Sample 2: 150HV0.2

2−3.表面粗さ試験
発明者らは、試料1及び2について、表面粗さ試験を行った。ここでは、表面粗さとして算術平均粗さRaを測定した。測定には、表面段差計(株式会社小坂研究所製、SE−3400)を用いた。試験結果は以下のとおりである。
試料1: 0.146μmRa
試料2: 0.733μmRa
2-3. Surface Roughness Test The inventors performed a surface roughness test on Samples 1 and 2. Here, the arithmetic average roughness Ra was measured as the surface roughness. For the measurement, a surface step meter (SE-3400, manufactured by Kosaka Laboratory Ltd.) was used. The test results are as follows.
Sample 1: 0.146 μm Ra
Sample 2: 0.733 μm Ra

2−4.異物投入試験
図3は、異物投入試験の条件を示す図である。発明者らは、試料1及び2をアッパ側(荷重側)半割軸受(第2半割軸受の一例)として用いた軸受A〜Cについて、異物投入試験を行った。異物投入試験は、異物が混入した潤滑油を供給しつつ軸受を相手軸と摺動させ、焼付き面圧を測定する試験である。試験は以下の条件で行った。
軸受負荷: 3.6MPaずつステップアップ(3分毎)
回転速度: 6000rpm(摺動速度:15.01m/s)
潤滑油温度:160℃
相手軸: 焼入れ鋼
軸受形状: φ47.8mm×17.5mm
異物: 鉄片(1mm×0.6mm×0.1mm)
2-4. Foreign Object Injection Test FIG. 3 is a diagram showing the conditions of the foreign material input test. The inventors conducted a foreign matter insertion test on bearings A to C using Samples 1 and 2 as upper side (load side) half bearings (an example of second half bearings). The foreign material insertion test is a test in which the bearing pressure is measured by sliding the bearing against the counterpart shaft while supplying lubricating oil mixed with foreign material. The test was conducted under the following conditions.
Bearing load: Step up by 3.6 MPa (every 3 minutes)
Rotational speed: 6000 rpm (sliding speed: 15.01 m / s)
Lubricating oil temperature: 160 ° C
Mating shaft: Hardened steel Bearing shape: φ47.8mm × 17.5mm
Foreign object: Iron piece (1mm x 0.6mm x 0.1mm)

なお、軸受A〜Cにおいて、試料1又は2と組み合わせるロア側(非荷重側)半割軸受(第1半割軸受の一例)としては以下のものが用いられた。

Figure 2019203553
In the bearings A to C, the following was used as the lower side (non-load side) half bearing (an example of the first half bearing) combined with the sample 1 or 2.
Figure 2019203553

異物投入試験の結果得られた焼付き面圧は以下のとおりである。なお、軸受A及びCについては2回、軸受Bについては3回の試験を行った。下記の面圧はその平均値である。
軸受A: 77.4MPa
軸受B: 54.0MPa
軸受C: 46.8MPa
The seizure surface pressure obtained as a result of the foreign matter insertion test is as follows. The bearings A and C were tested twice and the bearing B was tested three times. The following surface pressure is the average value.
Bearing A: 77.4 MPa
Bearing B: 54.0 MPa
Bearing C: 46.8 MPa

軸受Aと軸受Bとを対比すると、アッパ側半割軸受において、より柔らかい材料で形成されたライニング層、及びより表面粗さが小さい(平坦な)コーティング層を用いた半割軸受を採用することにより、耐異物性が向上したことがわかる。また、軸受Aと軸受Cとを対比すると、ロア側(非荷重側)において、アルミニウム系合金をライニング層として用いた半割軸受を用いることにより、耐異物性が向上したことがわかる。   When bearing A and bearing B are compared, in the upper side half bearing, a half bearing using a lining layer made of a softer material and a coating layer having a smaller surface roughness (flat) is adopted. Thus, it can be seen that the foreign matter resistance has been improved. Further, when comparing the bearing A and the bearing C, it can be seen that the foreign matter resistance is improved by using a half bearing using an aluminum-based alloy as a lining layer on the lower side (non-load side).

2−5.片当たり試験
図4は、片当たり試験の条件を示す図である。発明者らは、試料1及び2について、各2片の半割軸受を組み合わせた軸受を用いて片当たり試験を行った。片当たり試験は、相手軸51をサポート軸受52及び53、及び試験対象の軸受1で支持し、これら軸受の中心に対して相手軸51を傾けた状態で摺動させ、焼付き面圧を測定する試験である。なお、軸受1はコネクティングロッド54の軸受である。試験は以下の条件で行った。
試験機: 静荷重試験機
潤滑油温度:140℃
負荷: 3kNずつステップアップ(3分毎)
回転速度: 8000rpm
傾斜角: 0.2°
2-5. Per-piece test FIG. 4 is a diagram showing conditions for a single-piece test. The inventors performed a one-piece test on Samples 1 and 2 using a bearing in which two half bearings were combined. In the one-piece test, the mating shaft 51 is supported by the support bearings 52 and 53 and the bearing 1 to be tested, and the mating shaft 51 is slid relative to the center of these bearings to measure the seizure surface pressure. It is a test to do. The bearing 1 is a connecting rod 54 bearing. The test was conducted under the following conditions.
Testing machine: Static load testing machine Lubricating oil temperature: 140 ° C
Load: Step up by 3kN (every 3 minutes)
Rotation speed: 8000rpm
Tilt angle: 0.2 °

片当たり試験の結果得られた焼付き面圧は以下のとおりである。なお、各試料について3回ずつ試験を行った。下記の面圧はその平均値である。
試料1: 42MPa
試料2: 15MPa
The seizure surface pressure obtained as a result of the one-piece test is as follows. Each sample was tested three times. The following surface pressure is the average value.
Sample 1: 42 MPa
Sample 2: 15 MPa

試料1と試料2とを対比すると、試料1の方が、片当たり性能(耐片当たり性)が良好である。これも、荷重側の半割軸受のライニング層に柔らかい材料を用いたことの効果であると考えられる。   When sample 1 and sample 2 are compared, sample 1 has better performance per one piece (per piece resistance). This is also considered to be an effect of using a soft material for the lining layer of the half bearing on the load side.

1…軸受、2…半割軸受、3…半割軸受、21…裏金、22…ライニング層、23…コーティング層、32…ライニング層、51…相手軸、52…サポート軸受、53…サポート軸受、54…コネクティングロッド DESCRIPTION OF SYMBOLS 1 ... Bearing, 2 ... Half bearing, 3 ... Half bearing, 21 ... Back metal, 22 ... Lining layer, 23 ... Coating layer, 32 ... Lining layer, 51 ... Opposite shaft, 52 ... Support bearing, 53 ... Support bearing, 54 ... Connecting rod

Claims (5)

銅系合金で形成され、硬さ120HV0.2以下のライニング層と、
前記ライニング層の上に形成され、少なくともバインダー樹脂を含み、表面粗さ0.6μmRa以下のコーティング層と
を有する半割軸受。
A lining layer formed of a copper-based alloy and having a hardness of 120HV0.2 or less;
A half bearing having a coating layer formed on the lining layer and containing at least a binder resin and having a surface roughness of 0.6 μmRa or less.
前記ライニング層の硬さが100HV0.2以下である
請求項1に記載の半割軸受。
The half bearing according to claim 1, wherein the lining layer has a hardness of 100 HV 0.2 or less.
前記コーティング層の表面粗さが0.2μmRzJIS以下である
請求項1又は2に記載の半割軸受。
The half bearing according to claim 1, wherein the coating layer has a surface roughness of 0.2 μm Rz JIS or less.
前記銅系合金が、0.5〜15質量%のBi、及び1〜15質量%のSnを含む
請求項1乃至3のいずれか一項に記載の半割軸受。
The half bearing according to any one of claims 1 to 3, wherein the copper-based alloy includes 0.5 to 15 mass% Bi and 1 to 15 mass% Sn.
第1半割軸受と、
前記第1半割軸受よりも低い荷重がかかる第2半割軸受と
を有し、
前記第1半割軸受は、
アルミニウム系合金で形成された第1ライニング層と、
少なくともバインダー樹脂を含む第1コーティング層と
を有し、
前記第2半割軸受は、
銅系合金で形成され、硬さ120HV以下の第2ライニング層と、
前記第2ライニング層の上に形成され、少なくともバインダー樹脂を含み、表面粗さ0.6μmRa以下の第2コーティング層と
を有する
軸受。
A first half bearing;
A second half bearing that receives a lower load than the first half bearing;
The first half bearing is
A first lining layer formed of an aluminum-based alloy;
A first coating layer containing at least a binder resin,
The second half bearing is
A second lining layer formed of a copper-based alloy and having a hardness of 120 HV or less;
A bearing having a second coating layer formed on the second lining layer and including at least a binder resin and having a surface roughness of 0.6 μmRa or less.
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