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Aircraft health diagnostic equipment and aircraft health diagnostic methods

机译:飞机健康诊断设备和飞机健康诊断方法

摘要

To provide an air vehicle soundness diagnostic system which enables peeling of an adhesion structure and progress of the peeling etc. in an airframe of an air vehicle to be diagnosed, and to provide an air vehicle soundness diagnostic method.SOLUTION: An air vehicle soundness diagnostic system 10 includes a control part 40 for performing a structure soundness monitoring of an airframe 2 of an air vehicle 1. The control part 40 has: a first risk evaluation part 50 which evaluates a risk of occurrence of damage of the airframe 2 based on a correlation between a signal data set 106 based on measurement data 101 measured by a measuring instrument 20 and reference data 105 stored in a storage part 30; a second risk evaluation part 60 which evaluates the risk of the occurrence of the damage of the airframe 2 based on behavior of time series variation of the signal data set 106; and a maintenance evaluation part 70 which evaluates life, repair timing, and a maintenance plan of the airframe 2 based on the behavior of the time series variation of the signal data set 106.SELECTED DRAWING: Figure 1
机译:提供一种空气车辆合理诊断系统,其能够在要诊断的空气车辆的机身上剥离粘合结构和剥离等的进展,并提供空气车辆合理诊断方法。概况:空气车辆合理诊断系统10包括用于执行空气车辆1的机身2的结构声音监测的控制部分40具有:控制部分40具有:第一风险评估部分50,其基于a评估机身2损坏的风险。基于测量数据101的信号数据集106之间的相关性通过测量仪器20测量和存储在存储部分30中的参考数据105;基于信号数据集106的时间序列变化的行为,第二风险评估部分60评估机身2的损坏的风险;和一种维护评估部分70,其基于信号数据集106的时间序列变化的行为来评估机身2的寿命,修复时序和维护计划。选择绘图:图1

著录项

  • 公开/公告号JP6983027B2

    专利类型

  • 公开/公告日2021-12-17

    原文格式PDF

  • 申请/专利权人 三菱重工業株式会社;

    申请/专利号JP20170196140

  • 发明设计人 齋藤 望;石岡 昌人;

    申请日2017-10-06

  • 分类号B64D45;B64F5/60;

  • 国家 JP

  • 入库时间 2022-08-24 22:54:44

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