The invention relates to a double unmanned aerial vehicle with improved endurance and relates to the technical field of aircrafts. The double unmanned aerial vehicle comprises a main unmanned aerial vehicle, an auxiliary unmanned aerial vehicle and a butt joint mechanism. A butt joint controller is arranged in the middle of the main unmanned aerial vehicle, and the lower end of the butt joint controller is connected with the upper end of the auxiliary unmanned aerial vehicle through the butt joint mechanism. The splicing and separation of the double unmanned aerial vehicle are achieved through the insertion and separation of sockets and plugs of the main unmanned aerial vehicle and the auxiliary unmanned aerial vehicle, and a task execution device is installed at the lower end of the auxiliary unmanned aerial vehicle. The sockets are preferably cone-shaped sockets, and the plugs are preferably cone-shaped plugs. The endurance is improved on the basis of an existing unmanned aerial vehicle system, the shortcomings of task execution interruption and position inaccuracy during the long-endurance of two existing split unmanned aerial vehicles are overcome, and the shortcoming that existing unmanned aerial vehicles fail to be flexible and variable in load and endurance is overcome.
Double unmanned aerial vehicle with improved endurance
2015-11-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Double-engine small long-endurance unmanned aerial vehicle
European Patent Office | 2023
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