A piloting device for piloting an aircraft, comprising a piloting member suitable for being actuated by a pilot; a mechanism for mounting and guiding in rotation the piloting member about at least one rotation axis with respect to a frame; at least one force sensor connected between the piloting member and the mechanism comprising at least one sensing element configured to produce a signal upon deformation indicative of a force applied to the piloting member; wherein the force sensor comprises at least one pair of bearing surfaces; at least one pair of stops configured to limit the angular amplitude of rotation of the piloting member with respect to the frame on abutment of the at least one pair of bearing surfaces with at least one pair of stops; wherein at least one of the stops and/or at least one of the bearing surfaces comprises a compliant material.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    STOPS FOR FORCE SENSOR


    Weitere Titelangaben:

    BUTEES POUR CAPTEUR DE FORCE


    Beteiligte:

    Erscheinungsdatum :

    2023-10-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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



    STOPS FOR FORCE SENSOR

    ANTRAYGUE CEDRIC | Europäisches Patentamt | 2023

    Freier Zugriff

    STOPS FOR FORCE SENSOR

    ANTRAYGUE CEDRIC | Europäisches Patentamt | 2023

    Freier Zugriff

    “THROTTLE STOPS”

    Axelson, O. A. | SAE Technical Papers | 1937


    Bump stops

    GLENN CURTIS | Europäisches Patentamt | 2023

    Freier Zugriff

    Railway stops

    Beeler, John A. | Engineering Index Backfile | 1917