An aerodynamics control system for a vehicle may include a dive plane assembly operably coupled to a front portion of a vehicle body, an actuator assembly operable to transition the dive plane assembly between a deployed state and a retracted state, and a controller operably coupled to the actuator to provide automatic control of the dive plane assembly via the actuator based on a selectable control mode. The selectable control mode defines a position of the dive plane assembly based on vehicle parameters measured while driving the vehicle.


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    Titel :

    Aerodynamic deployable dive planes


    Beteiligte:
    TITUS MATTHEW (Autor:in) / PETERS BRETT (Autor:in)

    Erscheinungsdatum :

    2024-06-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B62D MOTOR VEHICLES , Motorfahrzeuge



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