常庆东, 王斌, 高磊. 风机变桨轴承失效原因分析[J]. 电力科技与环保, 2023, 39(5): 443-449,464.
引用本文: 常庆东, 王斌, 高磊. 风机变桨轴承失效原因分析[J]. 电力科技与环保, 2023, 39(5): 443-449,464.
CHANG Qingdong, WANG Bin, GAO Lei. Failure analysis of fan variable propeller bearings[J]. Electric Power Technology and Environmental Protection, 2023, 39(5): 443-449,464.
Citation: CHANG Qingdong, WANG Bin, GAO Lei. Failure analysis of fan variable propeller bearings[J]. Electric Power Technology and Environmental Protection, 2023, 39(5): 443-449,464.

风机变桨轴承失效原因分析

Failure analysis of fan variable propeller bearings

  • 摘要: 为解决某风电场变桨轴承频繁开裂,严重影响机组安全稳定运行问题,本文以某开裂变桨轴承为研究对象,通过宏观检查、化学成分分析、非金属夹杂物分析、机械性能分析、金相分析、扫描与能谱分析等方法研究其失效原因。分析结果表明:(1)变桨轴承基体室温冲击吸收能量最小为22.4 J,远低于标准最小值35 J,易引起材料抗疲劳性能低、韧性差、应力集中敏感性高等问题;(2)变桨轴承滚道侧表面硬化层深度部分位置不足1.0 mm,表面硬化层硬度为46.7 HRC,低于标准要求(55~62 HRC),表明该加工工艺未能很好改善材料本身的耐磨性及耐疲劳性;(3)变桨轴承螺栓孔内壁存在在明显腐蚀坑,深度最大为0.36mm。因此可判断变桨轴承失效原因是表面加工不合格,在交变应力与腐蚀共同作用下易在螺栓孔表面周向产生腐蚀坑,长时间在空气中运行形成疲劳损伤累积,进一步萌生多个疲劳微裂纹,不断向金属基体内沿晶扩展,并且轴承基体性能的不合格对疲劳裂纹在其内部的扩展起促进作用,相邻的微裂纹逐步连接形成较大的疲劳裂纹并继续向滚道侧扩展,当裂纹进一步扩展至临界尺寸时将会发生失稳快速断裂。为防止变桨轴承开裂,提出螺栓孔表面防腐工艺、结构优化降低交变应力、严格把控轴承基体制造质量、定期对轴承内部无损检测等建议。

     

    Abstract: A variable propeller bearing in a wind farm frequently cracks, which seriously affects the safe and stable operation of the unit. This paper takes a cracked propeller bearing as the research object, and studies the cause of failure through macroscopic inspection, chemical composition analysis, non-metallic inclusion analysis, mechanical performance analysis, metallographic analysis, scanning and energy spectrum analysis and other methods. The analysis results show that:(1) the minimum room temperature impact absorption energy of the propeller bearing matrix is 22.4 J,which is far lower than the standard minimum value of 35 J, which is easy to cause problems such as low fatigue resistance, poor toughness and high stress concentration sensitivity of the material;(2) The depth part of the surface hardening layer on the side of the propeller bearing is less than 1.0 mm, and the hardness of the surface hardening layer is46.7 HRC, which is lower than the standard requirements(55~62 HRC), indicating that the processing process has failed to improve the wear resistance and fatigue resistance of the material itself;(3) There is a clear corrosion pit in the inner wall of the bolt hole of the variable propeller bearing, with a maximum depth of 0.36 mm. Therefore, it can be judged that the failure of variable propeller bearings is due to unqualified surface processing. Under the combined action of cross-variant stress and corrosion, it is easy to produce corrosion pits around the surface of the bolt hole. Fatigue damage accumulates after running in the air for a long time, further germinates multiple fatigue micro-cracks, constantly expanding along the crystal in the metal matrix, and the bearing matrix Unqualified performance promotes the expansion of fatigue cracks in its interior. Adjacent micro-cracks are gradually connected to form large fatigue cracks and continue to expand to the raceway side. When the cracks further expand to the critical size, unstable and rapid fractures will occur. In order to prevent the cracking of variable propeller bearings, suggestions are put forward such as anti-corrosion process on the surface of bolt holes, structural optimisation to reduce the intersection stress, strict control of bearing matrix manufacturing quality, and regular non-destructive testing of bearings.

     

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