VERTICAL TAKEOFF AND LANDING AIRCRAFT FOR FIRE CONTROL

摘要

The present invention relates to a vertical takeoff and landing aircraft for fire control, comprising: a body part; a control part combined with the body part; a pair of frames whose one end is combined with the body part and radially extended from the center of the body part; a propulsion unit including an engine combined with the other end of the frame and driven by receiving a signal from the control part, and a propeller combined with one end of the engine and rotated by the engine to generate a thrust in a vertical direction; a fuel supply unit including a fuel container installed in the body part, and a fuel line fixed to the frame to supply fuel to each engine; a fire control unit installed in the body part to collect and transmit video and audio of a disaster area; and a ground control unit to transmit a flying signal to the control part and to wirelessly control a vertical takeoff and landing aircraft. The present invention improves capacity and mileage, provides high stability using multiple propellers, and reduces failure due to a simple structure.