The invention relates to a flexible flat panel wing mechanism for a flapping wing flying robot, and provides a design and manufacture scheme of an asymmetric-rigidity flexible flat panel wing mechanism for a flapping wing flying robot. An auxiliary skeleton is made of a carbon fiber pipe or bar, positioned above a wing film, and in parallel contact with the wing film. One end of the auxiliary skeleton is firmly connected with a main skeleton at the front edge of a wing in a binding manner through a thin wire, and the other end of the auxiliary skeleton is hung in the air freely. In each cycle that the robot flaps the wing, air resistance acts on a wing film during forward flapping and reverse flapping, so that the flexural rigidities of the film wing in the forward and reverse directions are different to form an asymmetric-rigidity flexible flat panel wing. Compared with a symmetric-rigidity flexible flat panel wing, the asymmetric-rigidity flexible flat panel wing can improve the equivalent lift in each flapping cycle, so that the power consumption rate during flying of the robot can be effectively reduced, and the flying efficiency and the loading flying capacity of the robot are improved.
Flexible flat panel wing mechanism for flapping wing flying robot
2015-11-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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