首页> 外国专利> Avionic system's post-flight report failure determining method for aircraft, involves selecting post-flight report among constructed post-flight reports relative to plausibility criterions

Avionic system's post-flight report failure determining method for aircraft, involves selecting post-flight report among constructed post-flight reports relative to plausibility criterions

机译:航空电子系统的飞机飞行后报告故障确定方法,涉及相对于合理性标准在构建的飞行后报告中选择飞行后报告

摘要

The method involves acquiring post-flight reports of built-in test equipments, where the post-flight reports emitted by the test equipments are relative to line replaceable units e.g. controller or sensors, monitored by the test equipments. Post-flight reports are constructed from the acquired post-flight reports, and a plausibility criterion is determined for each line replaceable unit associated with each constructed post-flight report, from a determined unitary criterion. One post-flight report is selected among the constructed post-flight reports relative to the plausibility criterions. An independent claim is also included for a device for determining post-flight report failure of an avionic system.
机译:该方法涉及获取内置测试设备的飞行后报告,其中由测试设备发出的飞行后报告是相对于生产线可更换单元而言的。控制器或传感器,由测试设备监控。从获取的飞行后报告中构建飞行后报告,并根据确定的统一标准为与每个构建的飞行后报告相关联的每个生产线可替换单元确定合理性标准。相对于合理性标准,在构建的飞行后报告中选择一个飞行后报告。还包括用于确定航空电子系统的飞行后报告故障的设备的独立权利要求。

著录项

  • 公开/公告号FR2914764A1

    专利类型

  • 公开/公告日2008-10-10

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20070054393

  • 发明设计人 BORDRY CHRISTOPHE;

    申请日2007-04-06

  • 分类号G06Q90;B64D47;

  • 国家 FR

  • 入库时间 2022-08-21 19:46:59

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