The invention provides a flying wing configuration drone aircraft invisibility control surface mounting structure. The flying wing configuration drone aircraft invisibility control surface mounting structure comprises an auxiliary wing unit and a resistance direction rudder unit, the auxiliary wing unit comprises an auxiliary wing steering engine, a first steering engine rocker arm, a first steering engine connecting rod, an inclined rib, a right side supporting base, a control surface and a left side connecting base, the resistance direction rudder unit comprises two resistance direction rudder steering engines, a second steering engine rocker arm, a second steering engine connecting rod, a resistance direction rudder upper control surface, a resistance direction rudder lower control surface, a right side mounting base, a left side mounting base, a transverse shaft, a resistance direction rudder pull base and a stabilizing plane rear beam, and the flying wing configuration drone aircraft invisibility control surface mounting structure is reasonable in design, capable of enabling the lower surface of an aircraft to be free of convex objects, small in reflection area during radar irradiation, capable of achieving the invisibility function and in addition capable of enabling the control surface to be detachable and convenient to maintain.
本发明提供一种飞翼布局靶机机隐身舵面安装结构,包括副翼单元和阻力方向舵单元,所述副翼单元包括副翼舵机、舵机摇臂一、舵机连杆一、斜肋、右侧支撑座、舵面和左侧连接座,所述阻力方向舵单元包括2个阻力方向舵舵机、舵机摇臂二、舵机连杆二、阻力方向舵上舵面、阻力方向舵下舵面、右侧安装座、左侧安装座、横轴、阻力方向舵拉座和安定面后梁,该飞翼布局靶机机隐身舵面安装结构设计合理,能够使飞机下表面无凸起物,在雷达的照射时,反射面积很小,能够达到隐身的效果,另外舵面可拆卸便于维护。
Flying wing configuration drone aircraft invisibility control surface mounting structure
一种飞翼布局靶机机隐身舵面安装结构
2020-07-07
Patent
Elektronische Ressource
Chinesisch
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