|国家科技期刊平台
首页|期刊导航|航空材料学报|自润滑关节轴承在不同应力下的摩擦磨损特性

自润滑关节轴承在不同应力下的摩擦磨损特性OA北大核心CSTPCD

Friction and wear characteristics of self-lubricating spherical bearings under different stresses

中文摘要英文摘要

为了研究应力对自润滑关节轴承摩擦磨损性能的影响,依据SAE AS 81820对EN2584R12轴承在常温下分别进行了 50%、100%和 150%标准应力条件下的全寿命摆动磨损测试,并对粘贴衬垫的平板样件进行静应力承载测试.采用三维白光干涉形貌仪与金相显微镜(OM)观察静应力承载后衬垫的变形情况,采用体视显微镜(SM)、光学显微镜(OM)和扫描电子显微镜(SEM)观察不同应力下轴承全寿命摆动磨损后内外圈磨损形貌与磨屑形貌.结果表明:全寿命周期内,三种应力下的自润滑衬垫均已磨穿,磨损规律和摩擦因数差异不大,应力越大,轴承表面温度越高,磨屑颜色越深、尺寸越大,失稳期来得更早,破坏更为剧烈;应力对轴承的寿命有显著影响,低应力和中应力条件下的摆动磨损寿命分别是高应力条件的 17.95倍和 7.86倍;三种应力下的磨损机理均为磨粒磨损与黏着磨损的混合磨损,直接受力区的黏着磨损随载荷的增大而加剧,非直接受力区的磨粒磨损随载荷的增大而减弱.

In order to study the effect of stresses on the friction and wear properties of self-lubricating spherical plain bearings,the self-lubricating spherical bearings EN2584R12 was taken full life cycle tests under 50%,100%and 150%standard stresses conditions at room temperature according to SAE AS 81820.And the static stress tests of the flat samples with the liner were carried out.The deformation of the liner after static stresses were observed by using three-dimensional white light interference profilometer and optical microscopy.Stereo microscope,optical microscopy and scanning electron microscopy were used to observe the wear morphology and debris morphology of the inner and outer rings after full life swing wear under different stresses.Results show that the self-lubricating liners under three stresses have been worn through,the wear characteristics and friction coefficients of self-lubricating liners under three stresses have no significant difference.As the pressure increases,it is found the temperatures of the bearing surface are higher,the debris are darker and larger,the instability period become earlier,the liner is damaged more quickly.Different stresses have significant effects on the life of bearings.The oscillating wear life under low and medium stress conditions is increased to 17.95 times and 7.86 times compared to high stress conditions,respectively.The wear mechanisms under three stresses are the mixed wear of abrasive wear and adhesive wear.The adhesive wear in the direct pressuring zone increases with the increase of stress,while the abrasive wear in the non-direct pressuring zone decreases with the increase of stress.

黄雄荣

上海市轴承技术研究所有限公司,上海 201801||上海特种轴承工程技术中心,上海 201801

自润滑衬垫应力摩擦磨损

self-lubricatinglinerstressfrictionwear

《航空材料学报》 2024 (003)

132-141 / 10

10.11868/j.issn.1005-5053.2023.000141

评论