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.