A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other wing segments, to minimize inter-segment loads. Wing dihedral is controlled by separately controlling the local pitch-control devices consisting of a control surface on a boom, such that inboard and outboard wing segment pitch changes relative to each other, and thus relative inboard and outboard lift is varied.


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    Title :

    Active Dihedral Control System for a Torsionally Flexible Wing


    Contributors:

    Publication date :

    2017-09-19


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Active dihedral control system for a torsionally flexible wing

    KENDALL GREG T / LISOSKI DEREK L / MORGAN WALTER R et al. | European Patent Office | 2017

    Free access

    Active Dihedral Control System for a Torsionally Flexible Wing

    KENDALL GREG T / LISOSKI DEREK L / MORGAN WALTER R et al. | European Patent Office | 2016

    Free access

    Active Dihedral Control System for a Torsionally Flexible Wing

    KENDALL GREG T / LISOSKI DEREK L / MORGAN WALTER R et al. | European Patent Office | 2018

    Free access

    Active Dihedral Control System for a Torisionally Flexible Wing

    Kendall, Greg T. / Lisoski, Derek L. / Morgan, Walter R. et al. | NTRS | 2015


    Active dihedral control system for a torisionally flexible wing

    KENDALL GREG T / LISOSKI DEREK L / MORGAN WALTER R et al. | European Patent Office | 2015

    Free access