The invention relates to a
locking mechanism of a tilting wing and a using method of the
locking mechanism, and belongs to the technical field of low-altitude economical and electric tilting wing vertical take-off and landing aircrafts, the
locking mechanism comprises a first locking unit and a second locking unit, each locking unit is arranged on the top edge strip and the bottom edge strip of a wing spar, and the locking units are arranged on the top edge strip and the bottom edge strip respectively. Each locking unit is provided with a corresponding groove mechanism and a corresponding wedge block mechanism on the tilting section spar and the fixed section spar, the
wedge angle between a wedge block and a clamping groove face is 5 degrees, clamping grooves are matched for one-way pressing, a gap is eliminated, the wedge block gradually presses a wave
washer in the process that a push rod stretches out, and the wedge block and the wedge block are matched for one-way pressing. The wave
gasket provides elastic force for the wedge-shaped block after being pressed and deformed so as to eliminate gaps caused by vibration, abrasion, deformation and the like, the actuating direction of the push rod is perpendicular to the pressing direction of the wave
gasket, and the situation that too large pressing force is needed due to the fact that the push rod directly presses the wave
gasket is avoided. The wing spar web and the edge strip are connected through the rivets, so that load transmission is achieved.