A fixed shaft type full-moving
rudder surface mounting structure provided by the invention comprises a rotating shaft, a limiting bolt, a beam, a
cushion block, a tightening nut and a
rocker arm, andthe rotating shaft is inserted into a
fuselage supporting structure and is fixed through the limiting bolt. The beam and the
cushion block are sleeved on the rotating shaft and are locked by the tightening nut combined with the rotating shaft, the
rocker arm is fixedly connected with the beam through bolts, and a steering engine controls the
rocker arm to drive the beam to rotate around the rotating shaft. The fixed shaft type full-moving
rudder surface mounting structure has the characteristics of only one key mounting procedure, simple limiting structure and limiting mode, clear limiting effect of each fulcrum, no over-constraint, effectiveness in guaranteeing that the installation position of the full-moving
rudder surface is within the reasonable tolerance range relative to the theoretical position of the full-moving rudder surface, stable rudder surface control gap, no increase of the rotating
friction force of the rudder surface, and facilitation of improvement of the service life of related structural parts, the
airplane flutter speed and the flight quality.