A proprotor system for tiltrotor aircraft having a helicopter mode and an airplane mode. The proprotor system includes a hub and a plurality of proprotor blades coupled to the hub such that each proprotor blade is operable to independently flap relative to the hub about a flapping axis and independently change pitch about a pitch change axis. The proprotor blades have a first in-plane frequency less than 1.0/rev.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Proprotor Systems for Tiltrotor Aircraft


    Beteiligte:

    Erscheinungsdatum :

    2018-06-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    PROPROTOR SYSTEMS FOR TILTROTOR AIRCRAFT

    CHOI JOUYOUNG JASON / MILLER GARY / RAUBER RICHARD ERLER et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    PROPROTOR SYSTEMS FOR TILTROTOR AIRCRAFT

    CHOI JOUYOUNG JASON / MILLER GARY / RAUBER RICHARD ERLER et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Proprotor Systems for Tiltrotor Aircraft

    CHOI JOUYOUNG JASON / MILLER GARY / RAUBER RICHARD ERLER et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Proprotor systems for tiltrotor aircraft

    CHOI JOUYOUNG JASON / MILLER GARY / RAUBER RICHARD ERLER et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY

    ROSS BRENT C / RINEHART MICHAEL E / WILLIAMS JEFFREY M et al. | Europäisches Patentamt | 2018

    Freier Zugriff