Discloses an aircraft stall spin recovery apparatus. The present invention relates to an aircraft stall spin recovery apparatus for recovering from a stall spin phenomenon caused by rolling caused by asymmetry of lift and asymmetry of drag in asymmetric drag on the left and right wings of an aircraft A parachute having a plurality of supporting cables for bundling; A case mounted on both sides of the wing and fitted with a parachute; A deploying means seated on the case and deploying the parachute outside the case; And a signal transmission unit for sensing the angular velocity of rotation and providing an electrical signal to the deployment means to operate the deployment means if the angular velocity is greater than a predetermined size. By employing the present invention, there is an advantage that a strong drag can be generated at the time of stall spin generation, and can be quickly restored to a stable state.
展开▼
