The invention relates to dynamic fault isolation for aircraft. A method includes the step of receiving fault code data identifying one or more fault conditions detected onboard an aircraft and receiving fault context data indicating one or more conditions of the aircraft in a time frame associated with the condition(s). The method also includes the step of generating (based on the fault code data, the fault context data, state data indicating a current state of the aircraft, and historical maintenance data) a first checklist display including a first set of incomplete checklist items. The method further includes the step of receiving input indicating completion of one or more checklist items of the first set of incomplete checklist items and updating the state data based on the input. The method also includes the step of generating (based on the fault code data, the fault context data, the updated state data, and historical maintenance data) a second checklist display including a second set of incomplete checklist items.

    本申请涉及用于飞行器的动态故障隔离。一种方法包括接收标识飞行器上检测的一个或多个故障状况的故障代码数据以及接收指示在与该(一个或多个)状况相关联的时间框架中飞行器的一个或多个状况的故障情景数据。该方法还包括(基于故障代码数据、故障情景数据、指示飞行器的当前状态的状态数据和历史维护数据)生成包括第一组未完成检查列表项的第一检查列表显示。该方法进一步包括接收指示第一组未完成检查列表项的一个或多个检查列表项的完成的输入以及基于输入更新状态数据。该方法还包括(基于故障代码数据、故障情景数据、更新后的状态数据和历史维护数据)生成包括第二组未完成检查列表项的第二检查列表显示。


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    Title :

    DYNAMIC FAULT ISOLATION FOR AIRCRAFT


    Additional title:

    用于飞行器的动态故障隔离


    Contributors:

    Publication date :

    2021-09-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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