F. Rahmawati, Istyawan Priyahapsara, Rindy Alriavindra Funny, Denisa Trisma Wati
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引用次数: 0
摘要
Grob G 120 TP - beta系统飞机是一个调节螺旋桨角度大小的系统。从2016年8月到2021年5月,测试系统发生了42次故障,导致测试系统在达到2500飞行小时的年龄限制之前不得不更换。使用FTA(故障树分析)方法,开始定义失败和边界条件的确定测试系统,描述故障树模型,识别故障树的最小割集,执行故障树的定性分析和故障树的定量分析,可以看出,经常发生的故障的测试版系统Grob G 120 TP-A飞机发生高油温超过84℃,定性分析发现了beta系统发生故障的12个原因,定量分析得出beta系统发生故障的概率为0.76363。
GROB G 120 TP-A AIRCRAFT BETA SYSTEM ANALYSIS USING FTA (FAULT TREE ANALYSIS) METHOD
Grob G 120 TP - A beta system aircraft is a system that regulates the size of the angle on the propeller. 42 failures occurred in the beta system from August 2016 to May 2021, resulting in the beta system having to be replaced even before reaching its 2500 flight hour age limit. Using the FTA (Fault Tree Analysis) method, which begins with defining the failure and determining the boundary conditions of the beta system, describing the fault tree model, identifying the minimum cut set from the fault tree, performing a qualitative analysis of the faults tree, and doing a quantitative analysis of the fault tree, it can be seen that the failure that often occurs in the beta system of the Grob G 120 TP-A aircraft is the occurrence of high oil temperature over 84 ℃, the qualitative analysis found 12 causes of failure on the beta system, and based on quantitative analysis obtained probability the occurrence of beta system failure is 0.76363.