An air data system for an aircraft (10) includes a multi-function probe (MFP) (12A, 12B, 12C) and an inertial reference unit (IRU) (14). The MFP (12A, 12B, 12C) is positioned to sense a pressure of airflow about an exterior of the aircraft (10). A first electronics channel (51) of the MFP (12A, 12B, 12C) is electrically coupled to the IRU (14) to generate air data parameter outputs based on the pressure sensed by the MFP (12A, 12B, 12C) and inertial data sensed by the IRU (14).


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    Title :

    DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL


    Additional title:

    ZWEIKANALIGES LUFTDATENSYSTEM MIT TRÄGE KOMPENSIERTEM BACKUP-KANAL
    SYSTÈME DE DONNÉES D'AIR À DOUBLE CANAL COMPRENANT UN CANAL DE SAUVEGARDE À COMPENSATION INERTIELLE


    Contributors:

    Publication date :

    2019-12-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL

    NASLUND BRIAN BRENT / WINTER JOHN D / BOELKE JOEL | European Patent Office | 2019

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