基于相似体系的民机结构超手册维修案例分析

doi:10.12305/j.issn.1001-506X.2022.09.34

Abstract

Abstract:

In order to solve the problem of civil aircraft structure maintenance beyond the scope of the manual, a civil aircraft structure over manual maintenance case system model based on similar system is proposed. By extracting the damage information and maintenance scheme information of the existing civil aircraft structure cases of airlines, according to the nature of the information, the systematic similarity analysis is carried out by using numerical analysis, hierarchical method, attribute measurement and term frequency-inverse document frequency (TF-IDF) method, and the case similarity index system is established. Import the maintenance case data, distribute the weight of the index system through support vector machine (SVM) classification and elastic network regression, and verify that its reliability reaches 82%. Finally, the feasibility of the system is deeply analyzed through an example. The example shows that the weight distribution and differentiation effect of the case similarity index system are generally in line with the reality, which has important reference significance for the formulation of civil aircraft structure over manual maintenance cases.

Key words: over manual, structure maintenance cases, characteristic index, similarity system, classification regression

CLC Number:

V267+.41

Junzhou WANG, Huawei WANG, Zhaoguo HOU. Case analysis of civil aircraft structure maintenance over manual based on similarity system[J]. Systems Engineering and Electronics, 2022, 44(9): 2978-2985.

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References 31

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维度	元素	说明
飞机信息	飞机型号飞机注册号飞机序列号	描述飞机本身的属性特点, 对手册有巨大影响
运行信息	飞行时长飞行循环运行维修记录	描述飞机运行情况以及维修历史
手册信息	章节号部位零部件标号	描述在手册中的表现形式
损伤细节信息	损伤结构损伤类型损伤成因损伤尺寸损伤位置	描述了损伤的具体情况, 具体化信息便于工程分析
其他信息	材料损伤发现方法	-

指标	内容
飞机机型	机型属性
飞行循环	飞行循环记录
手册信息	章节号部位零件号编号
损伤结构	结构描述
损伤类型	损伤成因损伤描述
其他	损伤发现方法材料

特征指标	相似度计算方法
飞机机型	属性度量决策
飞行循环	数值区间计算
手册信息	布尔赋值, 层次法
损伤结构	布尔赋值
损伤类型	属性度量决策
其他指标	布尔赋值
维修方案	术语频率-逆文档频率计算

运行阶段	循环数值
初步运行阶段	0~2 000
稳定运行阶段	2 000~10 000
中期运行阶段	10 000~40 000
长期运行阶段	40 000以上

属性	特征
损伤成因	环境损伤、偶然损伤、疲劳损伤
损伤数量	1, 2, …, n
损伤尺寸维度	1, 2, …, n

Case analysis of civil aircraft structure maintenance over manual based on similarity system

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模型	准确率	精确率	AUC
相似指标模型	0.919	0.920	0.89
一般逻辑模型	0.886	0.895	0.70

参数	相似体系	逻辑体系
准确率	0.767	0.496
精确率	0.768	0.512
可决系数	0.823	0.770
MAE	0.046	0.044
MSE	0.015	0.018
MSRE	0.121	0.135

机型	A	B
飞行循环	10000FC	12000FC
手册信息	53-00-00	53-00-00
损伤结构	蒙皮	长桁
损伤类型	裂纹疲劳损伤	裂纹疲劳损伤
其他信息	2024T3包铝板一般目视	7075T6金属型材一般目视

机型	A	B
飞行循环	3600FC	24000FC
手册信息	53-00-00	53-00-00
损伤结构	蒙皮	蒙皮
损伤类型	划痕意外损伤	划痕意外损伤
其他信息	2024T3包铝板一般目视	2024T3包铝板一般目视

机型	A	B
飞行循环	12600FC	14000FC
手册信息	53-00-00	53-00-00
损伤结构	蒙皮	蒙皮
损伤类型	裂纹疲劳损伤	腐蚀意外损伤
其他信息	2024T3包铝板一般目视	2024T3包铝板一般目视

案例组编号	传统案例指标体系相似度	相似度指标体系相似度	维修方案相似度
1	0.59	0.88	0.90
2	0.85	0.62	1.00
3	0.8	0.61	0.58
4	0.14	0.39	0.40

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