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


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    Titel :

    DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL


    Weitere Titelangaben:

    SYSTEME DE DONNEES AERIENNES A DEUX CANAUX AVEC CANAL DE SECOURS COMPENSE PAR INERTIE


    Beteiligte:
    NASLUND BRIAN BRENT (Autor:in) / WINTER JOHN D (Autor:in) / BOELKE JOEL (Autor:in)

    Erscheinungsdatum :

    15.12.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01K MEASURING TEMPERATURE , Messen der Temperatur / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / 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 | Europäisches Patentamt | 2019

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