Multi-rotor aeromarine unmanned aerial vehicle

Abstract

The invention provides a multi-rotor aeromarine unmanned aerial vehicle. The multi-rotor aeromarine unmanned aerial vehicle comprises a machine body. The peripheral side of the machine body is evenly provided with a plurality of machine arms. Each machine arm is provided with a motor. Each motor is fixedly provided with a propeller. The peripheral side of the machine body is further provided with a floating mat. According to the multi-rotor aeromarine unmanned aerial vehicle, by arranging the floating mat on the machine body, the problem that when the unmanned aerial vehicle flies on the sea, the unmanned aerial vehicle falls into the sea and submerges owing to air crush is solved, effective combination can be formed between the floating mat and the machine body, and the normal operation and using of the unmanned aerial vehicle are not influenced; and compared with the prior art, when the unmanned aerial vehicle falls into the sea, the unmanned aerial vehicle floats on the sea surface, workers can conveniently carry out search and rescue work, the safety and reliability of working of the unmanned aerial vehicle are greatly improved, and meanwhile, the unmanned aerial vehicle is effectively prevented from being damaged.

Description

technical field [0001] The present invention relates to unmanned aerial vehicles, in particular to a multi-rotor marine flying unmanned aerial vehicle device, especially an unmanned aerial vehicle device that crashes into the sea due to a fault while flying at sea, and can be easily salvaged by ground personnel. Background technique [0002] The miniature multi-rotor unmanned aerial vehicle with vertical take-off and landing and stable hovering has very broad application prospects in military fields such as civil aerial photography, power patrol, fire detection, public security law enforcement, and maritime duty. Common unmanned rotorcraft, during the flight, other failure factors such as the main rotor, engine, operator, external force, etc., will have an adverse effect on the control of the entire flight control system, causing the aircraft to lose control, causing "explosion, "Plane crash", especially when flying at sea, once the above-mentioned phenomenon occurs, it may ...

AI Technical Summary

Problems solved by technology

Common unmanned rotorcraft, during the flight, other failure factors such as the main rotor, engine, operator, external force, etc., will have an adverse effect on the control of the entire flight control system, causing the aircraft to lose control, causing "explosion, "Plane crash", especially when flying at sea, once the above phenomenon occurs, it may cause the plane to crash into the seabed, causing expensive search and rescue costs and huge losses

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