摘要
为分析评价基本作战单元修复性维修保障方案,准确计算故障修复时间,根据系统工程建模思想,建立了基本作战单元站点间、站点内修复性维修过程仿真模型,对其修复性维修活动进行了详细描述,提出了累积维修比、维修模式比和拆卸率因子参数,为基本作战单元修复性维修过程的定量分析提供了度量方法,并根据Monte Carlo仿真原理给出仿真算法,为型号工作人员进行保障性设计分析提供了理论方法和技术手段,最后以某型飞机组成的基本作战单元为例,对其修复性维修保障方案进行仿真试验验证,分析了修复性维修过程的改进对保障资源和维修时间的影响.
To analyze base operational unit(BOU) corrective maintenance stratagem and accurately calculate fault recovery time, BOU corrective maintenance process simulation models among depots was set up, the models in depot was also set up tenance activities was described. A according to system engineering modeling ideology, BOU corrective mainccumulate maintenance rate (AMR) , maintenance mode rate (MMR) and remove rate(RR) parameters were presented. Measurement methods based on the parameters were given via to which BOU corrective maintenance process was quantitatively analyzed. The simulation algorithm was made out according to Monte Carlo simulation method. Theory and technology means were offered to equipment designer in the supportability design and analysis working areas. The corrective maintenance concept(CMC) was validated in an airplane individual unit example making use of simulation tests. The effects to support resource and maintenance time was analyzed with the bettered CMC.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
2007年第1期27-31,71,共6页
Journal of Beijing University of Aeronautics and Astronautics
关键词
故障
维修
建模
仿真
failure
maintenance
models
simulation