A system for an aircraft includes a tiltable proprotor that is tiltable between a lift position for providing lift for the aircraft and a forward flight position for providing forward propulsion for the aircraft is provided. The system includes at least one actuator for adjusting a tilt angle of the tiltable proprotor; and at least one passive damper connected to the tiltable proprotor and configured to limit a rate of change of the tilt angle of the tiltable proprotor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR


    Beteiligte:

    Erscheinungsdatum :

    11.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR

    BENO JONATHAN ANTHONY / DYER BENJAMIN SCOTT / STORRS NATHAN DANIEL | Europäisches Patentamt | 2024

    Freier Zugriff

    REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR

    BENO JONATHAN ANTHONY / DYER BENJAMIN SCOTT / STORRS NATHAN DANIEL | Europäisches Patentamt | 2025

    Freier Zugriff

    Redundant load path for powered lift tilt actuator

    BENO JONATHAN ANTHONY / DYER BENJAMIN SCOTT / STORRS NATHAN DANIEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Tilt-rotor unmanned aerial vehicle dual-safety redundant tilt actuator

    ZHAO QIJUN / YAN LEI / ZHANG XINLIN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTARY ACTUATOR WITH REDUNDANT LOAD PATHS

    SOBOLEWSKI PAWEL A / MAWLE CRAIG D | Europäisches Patentamt | 2025

    Freier Zugriff