CAJ | 학술논문

通过对气缸套-活塞环进行润滑分析 ,得到了不同曲轴转角位置活塞环的微凸体载荷分布及磨损速率.结合动载荷特点对A rchard磨损计算模型进行了修正 ,同时根据载荷分级对发动机工况进行了离散 ,计算得到了各离散网格单元内的磨损参数 ,基于发动机整机载荷谱 ,采用时间插值方法 ,编制了典型任务剖面下的气缸套磨损谱.
통과대기항투-활새배진행윤활분석 ,득도료불동곡축전각위치활새배적미철체재하분포급마손속솔.결합동재하특점대A rchard마손계산모형진행료수정 ,동시근거재하분급대발동궤공황진행료리산 ,계산득도료각리산망격단원내적마손삼수 ,기우발동궤정궤재하보 ,채용시간삽치방법 ,편제료전형임무부면하적기항투마손보.
Based on the lubrication analysis between cylinder liner and piston ring ,the asperity load and wear rate of piston ring at different crank angles were calculated .The Archard wear calculation model was modified according to the dynamic load characteristics ,the engine operating conditions were discretized according to the load classification and the wear parameters of each discrete mesh were acquired .Based on the engine load spectrum ,the cylinder liner wear spectrum under typical mission profile was compiled using the time interpolation method .