Adjustable type rotor-wing power machine head device for fixed-wing unmanned aerial vehicle

Abstract

The invention discloses an adjustable type rotor-wing power machine head device for a fixed-wing unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The adjustabletype rotor-wing power machine head device comprises a machine head, a power system, a first adjustable rotor wing mechanism and a second adjustable rotor wing mechanism, wherein the machine head comprises a first front end part, a first body and a first rear end part. The first adjustable rotor wing mechanism comprises a first screw propeller, a first motor, a first inclined rotary part and a first steering engine; the second adjustable rotor wing mechanism comprises a second screw propeller, a third motor, a second inclined rotary part and a second steering engine. The power supply part is provided with a first output opening, a second output opening, a third output opening and a fourth output opening; the displacement part comprises a first steering engine and a second steering engine; the driving part comprises a first motor and a second motor; the adjusting part comprises a first electronic speed control and a second electronic speed control. According to the adjustable type rotor-wing power machine head device, the cruising duration time of the unmanned aerial vehicle is increased and the requirements of each electrical appliance of the unmanned aerial vehicle on energy sources are met; when the unmanned aerial vehicle takes off, lands and flies, the adjustable type rotor-wing power machine head device has the technical effects of low requirements on fields and strong adaptability.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an adjustable rotor powered nose device for a fixed-wing unmanned aerial vehicle. Background technique [0002] Unmanned UAV, referred to as "UAV", is an unmanned UAV controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary UAV under radio remote control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. [0003] For fixed-wing drones, the drone head in the prior art mainly adopts a cylindr...

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is that the nose of the UAV will reduce the endurance time of the UAV; when the UAV takes off, lands and flies, it has high requirements on the site and poor adaptability; Appliances' energy needs

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