The invention provides a parachute separating mechanism for a microminiature throwing robot, which is used for solving a problem that the microminiature throwing robot is connected with a parachute in the throwing process and separated from the parachute after landing. The parachute separating mechanism comprises a hoop, a slab, reinforcing plates, an arch-shaped power elastic sheet, a contact end, a connecting screw, a cushion block and a supporting sleeve. After the robot lands, the landing impact is transmitted to the contact end; the arch-shaped power elastic sheet is deformed under the impact to push the slab to move upwards; the hoop generates an outward elastic force due to deformation; and the hood is separated from the slab under the effect of the impact and the elastic force so that the robot and the parachute are separated. As a control element and a power device are not needed in the automatic separating mechanism provided by the invention, the parachute separating mechanism for the microminiature throwing robot, provided by the invention, has the advantages of small volume, light weight, simple structure, easiness in realization, high reliability and great application value and is especially suitable for laying the parachute of the microminiature robot for collecting environment data after disasters.


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    Titel :

    Parachute separating mechanism for microminiature throwing robot


    Beteiligte:
    GAO JUNYAO (Autor:in) / LI JUAN (Autor:in) / TIAN YE (Autor:in) / ZHANG WEIMIN (Autor:in) / HUANG QIANG (Autor:in) / ZHAO JINGCHAO (Autor:in) / LIU YI (Autor:in) / SHI XUANYANG (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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