内燃机工程2024,Vol.45Issue(4) :89-97.DOI:10.13949/j.cnki.nrjgc.2024.04.011

船用发动机连杆大端轴承润滑特性及损伤研究

Research on Lubrication Characteristics and Damage of the Connecting Rod Big End Bearing of a Marine Engine

周方贤 刘硕 李虎林 崔毅 宋雅丽 屠丹红
内燃机工程2024,Vol.45Issue(4) :89-97.DOI:10.13949/j.cnki.nrjgc.2024.04.011

船用发动机连杆大端轴承润滑特性及损伤研究

Research on Lubrication Characteristics and Damage of the Connecting Rod Big End Bearing of a Marine Engine

周方贤 1刘硕 1李虎林 1崔毅 1宋雅丽 2屠丹红2
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作者信息

  • 1. 上海交通大学 动力机械与工程教育部重点实验室,上海 200240
  • 2. 中船动力研究院有限公司,上海 200120
  • 折叠

摘要

基于多柔体系统动力学和润滑理论,建立活塞-连杆-曲轴的多柔体摩擦动力学耦合模型.模型中采用绝对节点坐标框架分析多柔体动力学特性,采用平均雷诺方程和微凸体接触理论描述混合润滑和磨损特性,在空间、时间上分别采用有限元法和向后欧拉法求解.对某船用中速发动机连杆大端轴承的润滑、磨损和疲劳特性进行了计算分析.结果表明,轴承润滑域中心的轴颈-轴瓦相对速度呈现规律变化,混合润滑状态主要发生在燃烧上止点后 90°附近;磨损集中在连杆轴承上瓦周向 50°区域的两侧边缘位置,单循环最大磨损量为 1.7×10-6 μm,是刚体模型的 20.5 倍,磨损寿命为 1.1×104 h;疲劳损伤位置与易发生磨损位置相同,疲劳寿命为 7.8×104 h.

Abstract

Based on the theories of flexible multibody system dynamics and lubrication,the coupling model of piston,connecting rod and crankshaft was established.In the model,the absolute node coordinate frame was used to analyze the dynamic characteristics of the flexible multi-body.The average Reynolds equation and the asperity contact theory were used to describe the mixed lubrication and wear characteristics.The finite element method and backward Euler method were used to solve the equations in space and time,respectively.The lubrication,wear and fatigue characteristics of the connecting rod big end bearing of a marine medium-speed engine were calculated and analyzed.The results show that the relative velocity of the journal and bearing bush in the center of the bearing lubrication domain change regularly,and the mixed lubrication state mainly occurs around 90° after the top dead center of the combustion.The wear is concentrated on the edges of both sides of the 50° circumferent region of the upper shell of the connecting rod bearing.The maximum single-cycle wear amount of the flexible model is 1.7×10-6 μm,which is 20.5 times that of the rigid model,and the wear life is 1.1×104 h.The location of fatigue damage is the same as the location of wear,and the fatigue life is 7.8×104 h.

关键词

连杆大端轴承/混合润滑/磨损/疲劳/多柔体系统/有限元法

Key words

connecting rod big end bearing/mixed lubrication/wear/fatigue/flexible multibody system/finite element method

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基金项目

国家自然科学基金面上项目(52171315)

出版年

2024
内燃机工程
中国内燃机学会

内燃机工程

CSTPCD北大核心
影响因子:0.601
ISSN:1000-0925
参考文献量8
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