A bionic aircraft is characterized in that left and right ends of a motor are provided with transmission shafts, a motor bin frame is fixedly connected with a diverter, the diverter comprises a diverter frame, the diverter frame is relatively rotationally connected with a horizontally arranged diverter inner rotary shaft, the diverter inner rotary shaft is also relatively rotationally connected with a vertical rod, the lower end of the vertical rod is fixedly connected with a control handle, the upper end of the vertical rod is fixedly connected with transverse rods which horizontally move all the time, the transverse rods are bilaterally symmetric relative to the vertical rod, a flapping wing control mechanism which comprises a crank shaft is arranged between each transverse rod and the corresponding transmission shaft of the motor on the same side, one end of each crank shaft is in transmission connection with the corresponding transmission shaft, a crank shaft part where the other end of each crank shaft is located is relatively rotationally connected with a crank shaft sleeve which is fixedly connected with a wing and an inner edge rod located at the inner side of the wing, the free end of each inner edge rod is connected with a multidirection device, each multidirection device comprises an outer frame and a multidirection device inner rotary shaft which are relatively rotationally connected, and each inner edge rod is relatively rotationally connected with the corresponding multidirection device inner rotary shaft.
Bionic aircraft
2016-01-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |