The invention discloses a fast parachute-opening parachute bay structure for an unmanned aerial vehicle. The fast parachute-opening parachute bay structure comprises a parachute bay body and a parachute cover. The parachute bay body is provided with a steering engine mounting support, a steering engine, a bidirectional steering engine sheet, a left hanging point lug sheet and a right hanging point lug sheet are fixedly mounted on the steering engine mounting support, the bidirectional steering engine sheet is connected with the steering engine, and the left hanging point and the right hanging point lug sheet are connected with the bidirectional steering engine sheet. The left hanging point lug sheet is connected with the bidirectional steering engine sheet through a left unlocking transmission shaft, and the right hanging point lug sheet is connected with the bidirectional steering engine sheet through a right unlocking transmission shaft. Guide sleeves for being fixedly hung on the left hanging point lug sheet and the right hanging point lug sheet are fixedly arranged on the parachute cover, and are fixedly mounted on the parachute cover through screws. After a parachute is mounted in a non-power-up state, the unmanned aerial vehicle can be automatically locked, operation is easy, when an emergency situation occurs or a task is completed and parachuting is needed, the parachute cover can be automatically opened to complete parachuting of the unmanned aerial vehicle, and safety and convenience are achieved.


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    Titel :

    Fast parachute-opening parachute bay structure for unmanned aerial vehicle


    Beteiligte:
    CUI YANHONG (Autor:in)

    Erscheinungsdatum :

    03.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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




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