A control interface for an aircraft electric taxi system (ETS) may be incorporated in a housing positioned in a flight deck of the aircraft. The control interface may include an actuator, an electronic control sensor interconnected with the ETS to provide speed and direction signals to the ETS and an extendable shaft interposed between the actuator and the electronic control sensor. The actuator may be configured to rotate around an axis of the shaft between a first rotational position, in which the actuator is stowed within the housing, and a second rotational position in which the actuator is outside of the housing.


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    Title :

    Aircraft electric taxi control interface and system


    Contributors:

    Publication date :

    2017-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten



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