Novel three-rotor-wing unmanned aerial vehicle structure

Abstract

The invention relates to a novel three-rotor-wing unmanned aerial vehicle structure. The novel three-rotor-wing unmanned aerial vehicle structure comprises a bearing keel, a fuselage, vertical rotor wings, horizontal rotor wings, stub wings, rotary table mechanisms, angle sensors, wind pressure sensors and a flight control system, wherein the bearing keel covers the outer surface of a rear half section of the fuselage; the vertical rotor wings are mutually connected with a side face of the bearing keel outside the fuselage through the stub wings; the horizontal rotor wings are located on a rear end face of the bearing keel; each stub wing is provided with at least three wind pressure sensors; at least three wind pressure sensors are uniformly distributed on a front side face of the fuselage. According to the novel three-rotor-wing unmanned aerial vehicle structure provided by the invention, on one hand, a sufficient lifting force can be effectively provided for unmanned aerial vehicleequipment; on the other hand, the flexibility and convenience of vertical takeoff and landing and horizontal operation work of an unmanned aerial vehicle can be effectively realized; adjustment and replacement of a lifting force system of an unmanned aerial vehicle system also can be rapidly realized.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle structure, specifically a novel three-rotor unmanned aerial vehicle structure. Background technique [0002] In the currently used rotor-type UAV equipment, the rotor mechanism is often installed on the side surface of the fuselage or directly on any position of the front, rear and upper surfaces of the fuselage through the connecting beam. The aircraft provides the lift required for flight to meet the needs of UAV flight operations, but on the one hand, the structure of the UAV’s lift body is fixed, and the direction of the lift of the UAV cannot be flexibly adjusted according to the airflow changes during flight. On the one hand, the operating energy consumption of UAVs is relatively high when flying, and on the other hand, the ability to adjust and adapt to complex airflow environments is poor when UAVs are flying, which seriously affects the flexibility and reliability of UAVs. At the same time, ...

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