The invention discloses a wing flutter model. The model comprises a leading edge, a main box section and a wing beam, wherein the main box section is installed on the wing beam, the leading edge comprises a leading edge dimensional shape rib, a leading edge web and a leading edge skin, the main box section comprises a main box section dimensional shape rib, a trailing edge web, a main box section web and a main box section skin, the leading edge is hinged to a front end of the main box section through a shaft, and the front edge web is flexibly connected with the rear edge web of the main box section through a control cable.

    一种机翼颤振模型,含有前缘、主盒段和机翼梁,主盒段安装在机翼梁上,所述的前缘含有前缘维形肋、前缘腹板、前缘蒙皮,所述的主盒段含有主盒段维形肋、后缘腹板、主盒段腹板、主盒段蒙皮,前缘通过轴与主盒段的前端铰接,前缘腹板与主盒段的后缘腹板通过操纵索柔性连接。


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    Title :

    Wing flutter model


    Additional title:

    一种机翼颤振模型


    Contributors:
    CHEN HAI (author) / MA XIANG (author) / HUANG GUONING (author) / PU LIDONG (author) / ZENG XIAN'ANG (author)

    Publication date :

    2021-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



    Supercritical Wing Flutter

    J. A. McGrew / J. P. Giesing / R. M. Pearson et al. | NTIS | 1978



    Aeroplane Wing Flutter

    Frazer, R.A. | Emerald Group Publishing | 1929


    Aeroplane Wing Flutter

    Frazer, R.A. | Emerald Group Publishing | 1929