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预制缺陷球轴承剥落研究

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为研究航空发动机球轴承的剥落规律,在4套球轴承外圈滚道表面预制不同数量和分布形式的压坑,模拟轴承实际剥落过程形成的麻坑或剥落坑,利用轴承试验器开展预制缺陷球轴承剥落试验.综合利用润滑油光谱分析、自动磨粒分析及铁谱分析方法对轴承试验润滑油中磨粒进行分析.结果表明:轴承剥落时产生的磨粒以疲劳磨粒为主,严重滑动磨粒和切削磨粒为辅,同时存在磨粒氧化现象;轴承剥落产生的球形磨粒主要在5μm以下,少量分布在6~10μm,个别在10 μm以上;轴承剥落过程中,磨粒总量和大尺寸磨粒数量出现明显增长.航空发动机球轴承的剥落机制为:预制凹坑边缘首先产生疲劳裂纹,然后因预制凹坑后方的一段区域内难以形成动压润滑,在交变接触应力作用下,外圈滚道表面或次表面出现疲劳裂纹,形成剥落区;滚道剥落区沿周向不断朝两侧扩展,并逐渐将预制凹坑区域覆盖,形成长条形的大面积剥落带,直至轴承最终失效.
Research on Spalling of Prefabricated Defective Ball Bearings
To study the spalling law of aviation engine ball bearings,four sets of ball bearings were used to simulate the actual pits or spalling pits by forming different numbers and distribution of pits on the surfaces of the outer races.The spal-ling tests of prefabricated defective main bearing were carried out on a bearing tester,and atomic emission spectroscopy,la-ser net fines analysis and ferrography were used to analyze wear particles in the lubricating oil.The results show that the wear particles generated during bearing peeling are mainly fatigue particles,supplemented by severe sliding particles and cutting particles,and oxidation phenomenon is also found.The spherical particles are mainly below 5 μm,a few distributes from 6 μm to 10 μm,barely above 10 μm.There is an increase(sometimes a sharp increase)in the total particles or the number of large-sized particles during the bearing peeling process.The spalling mechanism of aviation engine ball bearings is as follow:fatigue cracks first appear at the edges of prefabricated pits,and then diffuse to the surface or sub-surface of the outer ring raceway to form a peeling zone,which is caused by the poor dynamic lubrication behind the pits.The peeling area continues to expand along the circumference towards both sides,gradually covering the prefabricated pits,forming a large peeling zone and ultimately leading to bearing failure.

aero engineball bearingsspalling testwear particlesfault monitoring

杨景来、佟文伟、刘宇佳、孙继刚、刘东旭、田如钢

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中国航发沈阳发动机研究所,辽宁沈阳 110015

中国航空发动机集团航空发动机动力传输重点实验室,辽宁沈阳 110015

航空发动机 球轴承 剥落试验 磨粒 故障监测

航空动力基础研究项目

2024

润滑与密封
中国机械工程学会 广州机械科学研究院有限公司

润滑与密封

CSTPCD北大核心
影响因子:0.478
ISSN:0254-0150
年,卷(期):2024.49(4)
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