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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    Title :

    Aerodynamic deployable dive planes


    Contributors:

    Publication date :

    2024-06-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B62D MOTOR VEHICLES , Motorfahrzeuge



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