The invention belongs to the technical field of take-off and landing of aircrafts, and particularly relates to an auxiliary take-off and landing cabin for emergency landing of aerospace aircrafts, which comprises a take-off and landing cabin fixedly mounted on a ground facility; the number of the electromagnetic ejection rails is two, the two electromagnetic ejection rails are fixedly connected to the inner side of the top of the take-off and landing cabin and the inner side of the bottom of the take-off and landing cabin respectively, a tractor is in transmission connection with the interiors of the electromagnetic ejection rails, and the tractor is detachably connected with an onboard traction device through a vehicle-mounted locking device; the two airborne traction devices are installed on the aerospace vehicle, one airborne traction device is located at the top of the aerospace vehicle and located at the front end of the advancing direction, and the other airborne traction device is located at the bottom of the aerospace vehicle and located at the tail end of the advancing direction. No undercarriage needs to be used in the take-off and landing processes, the problem that the undercarriage cannot be unfolded or the weight of the aircraft body is too large after the undercarriage is unfolded, so that the bearing capacity is insufficient is solved, fuel oil does not need to be released, and the safety during landing and forced landing is improved.

    本发明属于飞行器起飞和着陆技术领域,尤其涉及一种面向空天飞行器应急着陆的辅助起降舱,包括:起降舱,固定安装在地面设施上;电磁弹射轨道,设置有两条,两条电磁弹射轨道分别固接在起降舱顶部内侧和起降舱底部内侧,电磁弹射轨道内传动连接有牵引车,牵引车通过车载锁定装置可拆卸连接有机载牵引装置;两个机载牵引装置分别安装在空天飞行器上,其中一个机载牵引装置位于空天飞行器顶部且位于行进方向的前端,另一个机载牵引装置位于空天飞行器底部且位于行进方向的尾端。本发明在起飞和降落过程均无需使用起落架,避免起落架无法展开或展开后机体重量过大导致的承载力不足的问题,且无需释放燃油,提高降落和迫降时的安全性。


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    Title :

    Auxiliary take-off and landing cabin for emergency landing of aerospace vehicle


    Additional title:

    一种面向空天飞行器应急着陆的辅助起降舱


    Contributors:
    LIANG TAOTAO (author) / TANG YUTONG (author) / WEI XIAOHUI (author) / LIU JIA (author) / NIE HONG (author)

    Publication date :

    2025-04-25


    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



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