The invention discloses an aircraft with folding arms. The aircraft comprises an aircraft body (1) and further comprises the multiple folding arms (2). Each folding arm (2) comprises a first arm body (21), a second arm body (22) and a rotating mechanism (23), wherein the first arm body (21) and the second arm body (22) are connected with the aircraft body (1), and the second arm body (22) can rotate relative to the first arm body (21) through the rotating mechanism (23). Rotor wings (3) are installed on each first arm body (21) and each second arm body (22). The aircraft with the folding arms has the advantages that the structure of the first arm bodies and the second arm bodies rotationally connected with the first arm bodies is adopted for the aircraft, when the aircraft is used, the external dimension of the aircraft can be changed, so that the aircraft can adapt to different flying spaces, and thus the application field of the aircraft is wider.
Aircraft with folding arms
2015-11-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |