A wing structure includes: a main wing that extends in a second direction intersecting a first direction as a fluid flow direction; and an auxiliary wing that is disposed so as to be separated from the main wing and faces the main wing at the front part side of the main wing, wherein a wing chord length of the auxiliary wing is shorter than a wing chord length of the main wing. A fluid contacts the auxiliary wing which is formed at the front part side of the main wing, the fluid is guided between the auxiliary wing and the main wing, and the fluid is compressed when passing between the auxiliary wing and the main wing, thereby appropriately forming a fluid compression process region on the surface of the main wing and increasing an acting force.


    Access

    Download


    Export, share and cite



    Title :

    Wing structure and fairing device


    Contributors:

    Publication date :

    2015-07-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B62D MOTOR VEHICLES , Motorfahrzeuge



    WING STRUCTURE AND FAIRING DEVICE

    KIMURA YUKIHIDE / MORIMOTO TOMOAKI | European Patent Office | 2019

    Free access

    Aircraft wing and wing tip device with fairing

    ERIC WILDMAN / MATT HARDING / ALAN HADDRELL | European Patent Office | 2019

    Free access

    Aircraft wing and wing tip device with fairing

    European Patent Office | 2017

    Free access

    ICAS2016_0282: FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE

    Zhang, R. / Cui, D.-G. / Song, G. | British Library Conference Proceedings | 2016


    Rotor wing fairing of composite wing aircraft

    YU LEI / WU WENHUA / TU MENGLEI et al. | European Patent Office | 2021

    Free access