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Vector-boost multi-rotor unmanned aerial vehicle structure

A multi-rotor unmanned aerial vehicle, vector propulsion technology, applied in the direction of rotorcraft, motor vehicles, aircraft parts, etc., can solve the problem of difficult to stably fly around, and achieve the effect of improving stability, controllability, and effective adjustment

Inactive Publication Date: 2017-10-10
韩孚楷
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Based on the problems existing in the prior art, the purpose of the present invention is to provide a multi-rotor unmanned aerial vehicle structure with vector propulsion, which can improve the controllability, flexibility and endurance of the multi-rotor unmanned aerial vehicle, and effectively solve the problem of traditional multi-rotor unmanned aerial vehicles. The problem that it is difficult for man-machine to fly around stably

Method used

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  • Vector-boost multi-rotor unmanned aerial vehicle structure
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Embodiment Construction

[0014] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the specific content of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0015] Such as figure 1 , 2 As shown, the embodiment of the present invention provides a vector propulsion multi-rotor UAV structure, including:

[0016] The main engine and a plurality of rotor assemblies, each rotor assembly is correspondingly connected to the main engine via a main frame, and each rotor assembly is arranged around the main engine;

[0017] Each main frame is provided with a steering gear 1, and each steering gear 1 is connected with the deflection mo...

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Abstract

The invention discloses a vector-boost multi-rotor unmanned aerial vehicle structure comprising a main vehicle and a plurality of rotor assemblies. Each rotor assembly is connected with the main vehicle through a corresponding main vehicle support. The rotor assemblies are arranged around the main vehicle in an encircling mode. A steering engine is arranged on each main vehicle support. The steering engines are connected with deflection-type motor fixing seats of the rotor assembles connected on the main vehicle frame through steering engine connecting rods. Motors and propellers are arranged on the deflection-type motor fixing seats. The steering engines can adjust the angles of the deflection-type motor fixing seats connected with the steering engines and the propellers arranged on the deflection-type motor fixing seats. The postures of the propellers of an unmanned aerial vehicle are changed by using the steering engines (servers), so that vector rotors are controlled in a mode of changing the tensile direction of the rotors on the basis of adjusting the rotating speed, the control effect is better than a traditional multi-rotor unmanned aerial vehicle, the controllability and flexibility of the unmanned aerial vehicle are improved, in addition, electric energy is better saved, and the endurance ability of the unmanned aerial vehicle is indirectly improved. The vector-boost multi-rotor unmanned aerial vehicle structure can be applied to the fields of aerial photographing unmanned aerial vehicles and the like.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a vector propulsion multi-rotor unmanned aerial vehicle structure. Background technique [0002] There are three common UAV structures: fixed-wing, multi-rotor and autogyro, which are used in different fields according to their control principles and characteristics. Among them, multi-rotor drones can be divided into four-rotor, six-rotor, eight-rotor and other types according to the number of rotors. Its biggest feature is that it has multiple pairs of rotors, and the steering of each pair of rotors is the same, which is used to offset each other. Counter torque torque. Compared with other unmanned aerial vehicles, multi-rotor drones have unique advantages. Compared with fixed-wing aircraft, it has the advantages of vertical take-off and landing, and can hover at a fixed point; compared with single-rotor helicopters, it has no tail rotor device, so It has the advantages ...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C9/00B64C27/12B64C27/32
CPCB64C27/08B64C9/00B64C27/12B64C27/32
Inventor 韩孚楷
Owner 韩孚楷
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