Amphibious unmanned aerial vehicle based on duct vector propulsion

Abstract

The invention discloses an amphibious unmanned aerial vehicle based on duct vector propulsion. The amphibious unmanned aerial vehicle at least comprises a machine body system, an aircraft control system and a propulsion system, wherein a left dust fan (4) and a right duct fan (3) which are arranged at the two sides of the machine body through a cabin rod are added in the machine body system; a duct posture control instruction matched with the left duct fan (4) and the right duct fan (3) are added in the aircraft control system; the installation distance h of the duct fan on the machine body isa product of 30 percent and H; the H represents the machine body length. By controlling the output direction of the duct vector, the posture and the power of the aircraft are controlled; the navigation water inlet and water outlet and submerged navigation functions of the aircraft can be realized, so that the operation capability of the amphibious aircraft in the complicated meteorologic and strange hydrological environment can be improved.

Description

technical field [0001] The invention relates to the shape of an amphibious aircraft, more particularly, refers to an amphibious unmanned aircraft based on duct vector propulsion. Background technique [0002] Amphibious unmanned aerial vehicle is a kind of unmanned intelligent mobile platform in the air and underwater. The maneuverability in the air has been relatively mature, and the navigation performance in the water has yet to be mature. Most of the underwater driving devices of the aircraft use propeller propulsion devices. At present, the traditional underwater vehicles propelled by propellers are equipped with a tail rotor and multiple sets of rudder blades. They control the attitude and position of the underwater vehicle by controlling the motor and steering gear to change the propeller speed and the rudder angle of the rudder blade. However, this attitude control method and the traditional underwater aircraft shape increase the self-load of the aircraft, and the re...

AI Technical Summary

Problems solved by technology

[0004] However, the current amphibious aircraft is faced with problems such as vertical take-off and landing for take-off and entry into the water, which is not flexible enough, and has a large power demand, which makes the cost of the engine high. At the same time, the power of the aircraft is mostly propeller or turbojet engine. The direction is not adjustable, and the amphibious performance is not good

Moreover, the structure of the fuselage is fixed, and the same structure is difficult to solve where there are contradictions between the water and air environments.

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