The invention discloses a novel helicopter with a separable escape cabin. The novel helicopter comprises a cabin and a cabin positioned in the cabin, wherein the cabin can be separated from the cabin,a parachute device is arranged on the cabin, and the novel helicopter is characterized by further comprising a locking device for locking and unlocking the cabin and the cabin, a cylinder piston roddevice which is arranged on the cabin; and an air storage tank which is arranged on the cabin and provides power for the air cylinder piston rod device. The novel helicopter is advantaged in that thenovel helicopter is simple and easy to implement, and the design is very suitable for civil helicopters, small and medium-sized fixed-wing aircrafts and even military aircrafts with different tonnagesin the general aviation field.

    本发明公开了一种具有可分离逃生座舱的新型直升机,包括机舱、位于机舱内的座舱,所述座舱与机舱能够分离,所述座舱上设置有降落伞装置,其特征在于:还包括实现所述机舱与座舱锁定及解锁的锁定装置;设置在机舱上的气缸活塞杆装置;以及设置在机舱上的储气罐,所述储气罐为气缸活塞杆装置提供动力。本发明设计简单且容易实现,该设计非常适合用于不同吨位的通用航空领域民用直升机、中小型固定翼飞机甚至军用飞机上。


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    Title :

    Novel helicopter with separable escape cabin


    Additional title:

    一种具有可分离逃生座舱的新型直升机


    Contributors:
    HUANG SHIBIAO (author) / HU QIANCHENG (author) / CHEN TAIYU (author) / ZHANG YU (author) / JIANG ZEHAO (author) / WU JUNLING (author) / ZHU KE (author)

    Publication date :

    2021-01-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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