The invention discloses a recoverable carrier aircraft. The recoverable carrier aircraft comprises an aircraft main body with a set landing surface; the mass center adjusting module is provided with a separable mechanism, and when the separable mechanism is triggered, the mass center adjusting module is separated from the aircraft body; the aircraft has two states, when the aircraft is in the first state, neither the carried load nor the mass center adjusting module is thrown out, and at the moment, the mass center of the aircraft is located at a first set position; when the aircraft is in the second state, the carried load and the mass center adjusting module are thrown out, and at the moment, the mass center of the aircraft is located at a second set position; when the mass center of the aircraft is located at the first set position, a first constraint condition is met; when the mass center of the aircraft is located at a second set position, a second constraint condition is met, and the second constraint condition comprises that the aircraft lands on the landing surface. The recyclable carrying type aircraft is simple in design, low in cost and beneficial to improving the carrying efficiency of the aircraft.

    本申请公开了一种可回收的运载式飞行器,包括:具有设定的着陆面的飞行器主体;具有可分离机构的质心调节模块,当可分离机构被触发时,质心调节模块与飞行器主体分离;飞行器具有两种状态,当其处于第一状态时,被运负载和质心调节模块均未被抛出,此时飞行器的质心位于第一设定位置;当其处于第二状态时,被运负载和质心调节模块均被抛出,此时飞行器的质心位于第二设定位置;当飞行器的质心位于第一设定位置时,满足第一约束条件;当飞行器的质心位于第二设定位置时,满足第二约束条件,第二约束条件包括:飞行器以着陆面着陆。该可回收的运载式飞行器设计简单、成本低且有利于提高飞行器运载效率。


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    Title :

    Recyclable carrying type aircraft


    Additional title:

    一种可回收的运载式飞行器


    Publication date :

    2023-07-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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