The invention discloses a damping device for reducing the jolt degree of an airplane, and belongs to the technical scheme of product inventions in the field of B64. Once the airplane enters a bumpy area, the airplane is generally separated as soon as possible by changing heading and height. The damping device for reducing the jolt degree of the airplane is a buffering device composed of an upper layer, a middle layer and a lower layer which are connected into a whole, and the installation position of the buffering device is determined through the shell shape of an original airplane body according to the appearance characteristics (figure 8) of bird stick figures. When airflow entering a jolt area is similar to a diversion method of Dayu's water-control, a longitudinal and transverse pressure reduction method is adopted to achieve the purpose of reducing the jolt degree of an airplane and absorbing shock. The tropospheric airflow in the longitudinal direction impacts the shock absorption of the buffer firstly and then impacts the fuselage shell of the aircraft, and the shock absorption purpose is achieved through the buffer method. The transverse convection layer airflow achieves the purpose of shock absorption through the structures of the texture grooves and the air bags in a method of guiding, shunting and storing the airflow.

    一种用于降低飞机颠簸程度的减震装置,属于B64领域产品发明类的技术方案。飞机一旦进入颠簸区,现在一般采用改变航向和高度等办法尽快脱离。①一种用于降低飞机颠簸程度的减震装置,本装置由上、中、下三层连为一体的结构而组成的缓冲装置,根据小鸟简笔画的外形特点(图8),确定原有机体的外壳形状进行缓冲装置的安装的位置。当进入颠簸区的气流,类似大禹治水的分流方法,采用纵、横减压法,来达到降低飞机颠簸程度减震的目的。纵向方面的对流层气流,先冲击则缓冲的减震,再冲击飞机的机身外壳,之缓冲方法达到减震目的。横向方面的对流层气流,通过纹理槽和气囊的结构,以引流、分流和存储气流的方法,达到减震目的。


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    Title :

    Damping device for reducing jolt degree of airplane


    Additional title:

    一种用于降低飞机颠簸程度的减震装置


    Publication date :

    2021-04-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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