ACCELERATION DEVICE AND VEHICLE
    2.
    发明公开

    公开(公告)号:US20240286484A1

    公开(公告)日:2024-08-29

    申请号:US18572386

    申请日:2022-10-18

    CPC classification number: B60K26/02 G05G5/005 G05G5/05 G05G2505/00

    Abstract: An acceleration device can prevent abnormal acceleration of a vehicle even when an accelerator pedal is erroneously abnormally stepped on instead of a brake pedal, and alert a driver of occurrence of erroneously stepping on the accelerator pedal. Assuming that a driver erroneously steps on an accelerator pedal hard instead of a brake pedal, a magnet of a fixation part of a transmission/blocking mechanism and a magnetic opposing surface of a movable part are disengaged and separated from each other. Accordingly, movement of the accelerator pedal with respect to an accelerator lever is blocked, and the accelerator lever is returned to an idling state due to the action of the accelerator mechanism. Also, an impact and sound of the disengagement of the magnet is transmitted to the driver, and the foot takes a position different from a normal position. Accordingly, the driver can notice erroneous stepping on the accelerator pedal.

    Throttle control levers
    3.
    发明授权

    公开(公告)号:US12071254B2

    公开(公告)日:2024-08-27

    申请号:US18315667

    申请日:2023-05-11

    CPC classification number: B64D31/04 G05G1/01 G05G1/04 G05G5/005 G05G2505/00

    Abstract: A throttle control lever suitable for controlling the magnitude and direction of thrust of one or more aircraft engines is described. The throttle control lever comprises a frame, a trigger mechanism, a connection element, a cam engagement mechanism, a biasing means, a cam, and a grip suitable for gripping by a user when the throttle control lever is in use, The cam comprises a slot having first and second slot portions and a stop portion. The stop portion extends between and connects the first and second slot portions. The cam engagement mechanism comprises a cam lever and a slot engagement element, the cam lever is pivotally attached to the frame via a cam lever pivot, and the slot engagement element is attached to the cam lever. The trigger mechanism comprises a trigger lever and a trigger, the trigger lever is pivotally attached to the frame via a trigger pivot.

    BLOCKING UNIT, ELECTROMECHANICAL UNIT, AND AIRCRAFT

    公开(公告)号:US20240176381A1

    公开(公告)日:2024-05-30

    申请号:US18499008

    申请日:2023-10-31

    CPC classification number: G05G5/005

    Abstract: The present disclosure relates to a blocking unit for a component of an aircraft movable by at least one movement means, wherein the component can assume at least one blocking position and at least one movement position, wherein the blocking unit comprises blocking means, wherein the blocking means are arranged and designed to block a movement of the component when a blocking condition is fulfilled, wherein the blocking unit has locking means, wherein the locking means are arranged and designed such that the blocking means are prevented from blocking the movement of the component when the component is in a movement position, and wherein the locking means are arranged and designed such that the blocking means are not prevented from blocking the movement of the component when the component is in a blocking position.

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