The invention discloses a hollow annular retractable Mars rotor aircraft which is mounted on a rocket launch canister frame, the rocket launch canister frame is mounted in the center of the upper portion of a Mars lander, and a return rocket is mounted in the rocket launch canister frame. Comprising a Mars rotor aircraft body, a rotor folding and unfolding mechanism and a landing leg folding and unfolding mechanism, and the rotor folding and unfolding mechanism and the landing leg folding and unfolding mechanism are installed on the side edge of a rocket launching cylinder frame to achieve clamping and locking of the Mars rotor aircraft body. According to the Mars rotor aircraft, high-folding-unfolding-ratio storage of the Mars rotor aircraft body can be effectively achieved, independence of the Mars rotor aircraft and a return rocket working space can be achieved, and the reliability of a sampling return task is improved.

    本发明公开了一种中空环状的可收展火星旋翼飞行器,可收展火星旋翼飞行器安装在火箭发射筒架上,火箭发射筒架安装在火星着陆器上方的中央位置,返回火箭安装在火箭发射筒架内部,包括:火星旋翼飞行器本体、旋翼折展机构和着陆腿折展机构,旋翼折展机构和着陆腿折展机构安装在火箭发射筒架侧边,实现火星旋翼飞行器本体的夹紧与锁定。本发明可以有效实现火星旋翼飞行器本体的高折展比收纳,并可以实现火星旋翼飞行器与返回火箭工作空间的独立性,提高采样返回任务的可靠性。


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    Titel :

    Hollow annular retractable Mars rotor aircraft


    Weitere Titelangaben:

    一种中空环状的可收展火星旋翼飞行器


    Beteiligte:
    TANG DEWEI (Autor:in) / ZHU KAIJIE (Autor:in) / QUAN QIQUAN (Autor:in) / DENG ZONGQUAN (Autor:in)

    Erscheinungsdatum :

    2022-09-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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