Connecting mechanism capable of being used for combination and separation of aircrafts

The invention discloses a connecting mechanism capable of being used for combination and separation of aircrafts, and particularly relates to the technical field of structural design of supersonic aircrafts. Comprising a telescopic taper sleeve, a telescopic limiting pin and a connecting body, the telescopic taper sleeve and the telescopic limiting pin are arranged at the wingtip of any unmanned aerial vehicle in a spaced mode and electrically connected with a control system of the unmanned aerial vehicle, and the connecting body is fixedly arranged at the wingtip of another unmanned aerial vehicle and electrically connected with the control system of the unmanned aerial vehicle. An opening matched with the telescopic limiting pin is formed in the connecting body. By the adoption of the technical scheme, the problem that existing small and medium-sized unmanned aerial vehicles are short in cruising time is solved, and the method can be used for combination of multiple unmanned aerial vehicles. 本发明专利公开了一种可用于飞行