The present invention relates to a vehicle launching, and more particularly to an improved pneumatic system for launching aircraft. It is an object of the present invention to provide an improved aircraft launching system wherein a longitudinally slotted pneumatic launch cylinder withstands distortion along the slot from the thrust pressure internal of the cylinder during operation, while retaining a degree of longitudinal flexibility so as to accommodate minor lateral movements of the launching mechanism during operation. Other objects are: to provide a launching system wherein the high-speed motion of the unlaunched moving mechanism is effectively dampened within a limited brake stroke so as to avoid damage to the system structure; and to provide an aircraft launcher which is lightweight and simple in construction, yet sturdy and reliable in operation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Vehicle Launching Device


    Contributors:
    J. Hammond (author)

    Publication date :

    1979


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Launching platform of unmanned aerial vehicle launching vehicle

    LI HONG / JI RENXIN / GENG RONGMEI et al. | European Patent Office | 2022

    Free access

    Rotary launching device and launching method of unmanned aerial vehicle

    OU JUN / LIU TAO / WEI SHUXIAO et al. | European Patent Office | 2021

    Free access

    LAUNCHING DEVICE AND LAUNCHING METHOD

    KIN HIROAKI / TAKAHASHI MASAMI / ISHIKAWA RYO et al. | European Patent Office | 2022

    Free access

    Unmanned aerial vehicle launching device

    ZHANG XIAOYANG / ZHOU HONGKAI / QIU GUOLIN et al. | European Patent Office | 2023

    Free access

    Unmanned aerial vehicle launching device

    GUO BINXIN / ZHAI BIN / XUE MINGXU | European Patent Office | 2021

    Free access