A wing airframe for a wing of a tiltrotor aircraft includes a wing airframe core assembly and a wing skin assembly disposed on the wing airframe core assembly. The wing skin assembly includes an outer skin and a damping sublayer, the damping sublayer interposed between the outer skin and the wing airframe core assembly. The tiltrotor aircraft includes a pylon assembly subject to aeroelastic movement during forward flight. The wing is subject to deflection in response to the aeroelastic movement of the pylon assembly. The damping sublayer reduces the deflection of the wing, thereby stabilizing the wing during forward flight


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Damping Structures for Tiltrotor Aircraft Wings



    Erscheinungsdatum :

    03.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Damping structures for tiltrotor aircraft wings

    PARHAM JR THOMAS CLEMENT / BOSWORTH JEFFREY / MILLER GARY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    DAMPING STRUCTURES FOR TILTROTOR AIRCRAFT WINGS

    PARHAM JR THOMAS CLEMENT / BOSWORTH JEFFREY / MILLER GARY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    TILTROTOR AIRCRAFT WINGS HAVING BUCKLE ZONES

    BAINES ANDREW G / KOOIMAN JAMES EVERETT / DECKER GEORGE RYAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Tiltrotor aircraft wings having buckle zones

    BAINES ANDREW G / KOOIMAN JAMES EVERETT / DECKER GEORGE RYAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Tiltrotor Aircraft Wings having Buckle Zones

    BAINES ANDREW G / KOOIMAN JAMES EVERETT / DECKER GEORGE RYAN et al. | Europäisches Patentamt | 2019

    Freier Zugriff