Examples for logical to physical mapping of aircraft electronic components are presented. A system may include aircraft electronic components coupled sequentially to a power wire, corresponding controllers, and a master computing device. The computing device may receive a first identifier for a first component from a first controller in response to the first controller receiving power at a first time from the power wire and a second identifier for a second component from a second controller in response to the second controller receiving power at a second time from the power wire. The second time is subsequent to the first time. The computing device determines locations for the first and second component within the aircraft based on an order of reception of the identifiers.


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    Titel :

    Logical to physical mapping of aircraft electronic components


    Beteiligte:
    CALLAHAN KEVIN S (Autor:in) / WHETTEN DENNIS (Autor:in)

    Erscheinungsdatum :

    31.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H04B TRANSMISSION , Übertragung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr



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    CALLAHAN KEVIN S / WHETTEN DENNIS | Europäisches Patentamt | 2020

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    CALLAHAN KEVIN S / WHETTEN DENNIS | Europäisches Patentamt | 2020

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    Guenov, M. / Molina-Cristóbal, A. / Riaz, A. et al. | British Library Conference Proceedings | 2018


    PLATE COOLER FOR AIRCRAFT ELECTRONIC COMPONENTS

    TOMESCU DANA / BERTON GUILLAUME | Europäisches Patentamt | 2021

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