Bionic double-wing aircraft flapping mechanism and working method thereof

The invention relates to a bionic double-wing aircraft flapping mechanism and a working method thereof. The flapping mechanism comprises a base, a first wing, a second wing and a transmission mechanism. The transmission mechanism comprises a motor; the output end of the motor is connected with a transmission gear; the transmission gear comprises a first transmission gear and a second transmission gear; the first transmission gear is an incomplete gear; a first wing base and a second wing base are arranged on the two sides of the first transmission gear. A first gear and a first pulley are mounted on the first wing seat; a second gear and a second pulley are mounted on the second wing seat; the first pulley is in transmission fit with the second pulley through the conveying component; a first elastic component and a second elastic component are arranged between the base and the first wing seat and between the base and the second wing seat. According to the invention, the problems of asymmetric periodic motion