The invention is related to a control system (10) for controlling collective and cyclic pitch of rotor blades (1b, 1c) of a multi-blade rotor 1a in a rotary-wing aircraft (1), said control system (10) comprising a swash plate assembly (11) with at least one non-rotating plate (12a) and at least one rotating plate (12b) that is mounted rotatably to said at least one non-rotating plate (12a), said at least one rotating plate (12b) and said at least one non-rotating plate (12a) being mounted to a non-rotating sliding sleeve (13), wherein a spherical bearing (14) is provided on said non-rotating sliding sleeve (13), wherein at least one non-rotating stop arm (21) is provided for non-rotatably connecting said at least one non-rotating plate (12a) to said non-rotating sliding sleeve (13).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    A control system for controlling collective and cyclic pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft


    Beteiligte:

    Erscheinungsdatum :

    03.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge