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High stability hexarotor aircraft

A high-stability, aircraft technology, applied to aircraft, unmanned aircraft, rotorcraft, etc., can solve the problems of unadjustable rotor angle, unclear, impossible to complete tasks, etc., to improve flight stability and reduce wind resistance , the effect of improving flight efficiency

Pending Publication Date: 2017-06-30
LIAOYANG POWER SUPPLY COMPANY OF STATE GRID LIAONING ELECTRIC POWER SUPPLY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] UAVs are usually used to replace humans to perform various aerial photography and monitoring tasks. During the mission, due to the vibration of the UAV propeller, the non-adjustable rotor angle, and the influence of wind on the interior of the UAV, etc., aerial photography and monitoring tasks The picture is not clear or even impossible to complete the task, so it is urgent to invent a drone with high stability

Method used

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  • High stability hexarotor aircraft
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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0027] see figure 1 , providing a high-stability six-rotor aircraft, including: a regular hexagonal center plate 1, the center plate 1 includes an upper center plate 101 and a lower center plate 102, and six ailerons 2 are connected through the aileron main rod 201 At the six corners of the regular hexagon between the upper center plate 101 and the lower center plate 102, the aileron main rod 201 is a three-section bending structure, and the end of the aileron 2 is equipped with a propeller 202, and the aileron main rod 201 is connected The rod section of the propeller 202 is higher than the rod section of the aileron main rod 201 connected to the center plate 1, so that the overall center of gravity of the aircraft is lowered and the flight stability is improved. , the lift of the aircraft is inward, thereby saving the efficiency of the motor and improving the flight time at the same time.

Embodiment 2

[0029] see figure 1 and figure 2 , providing a high-stability six-rotor aircraft, including: a regular hexagonal center plate 1, the center plate 1 includes an upper center plate 101 and a lower center plate 102, and six ailerons 2 are connected through the aileron main rod 201 At the six corners of the regular hexagon between the upper center plate 101 and the lower center plate 102, the aileron main rod 201 is a three-section bending structure, and the end of the aileron 2 is equipped with a propeller 202, and the aileron main rod 201 is connected The rod section of the propeller 202 is higher than the rod section of the aileron main rod 201 connected to the center plate 1, so that the overall center of gravity of the aircraft is lowered and the flight stability is improved. , the lift of the aircraft is inward, which saves the efficiency of the motor and improves the flight time;

[0030] The aileron 2 is connected to the regular hexagonal central plate 1 through the ail...

Embodiment 3

[0032] see figure 1 , figure 2 , image 3 and Figure 4 , providing a high-stability six-rotor aircraft, including: a regular hexagonal center plate 1, the center plate 1 includes an upper center plate 101 and a lower center plate 102, and six ailerons 2 are connected through the aileron main rod 201 At the six corners of the regular hexagon between the upper center plate 101 and the lower center plate 102, the aileron main rod 201 is a three-section bending structure, and the end of the aileron 2 is equipped with a propeller 202, and the aileron main rod 201 is connected The rod section of the propeller 202 is higher than the rod section of the aileron main rod 201 connected to the center plate 1, so that the overall center of gravity of the aircraft is lowered and the flight stability is improved. , the lift of the aircraft is inward, which saves the efficiency of the motor and improves the flight time;

[0033] The aileron 2 is connected to the regular hexagonal centra...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle preparation, and in particular relates to a high stability hexarotor aircraft including a orthohexagonal center plate, the center plate includes an upper center plate and a lower center plate, and is provided with six ailerons, the six ailerons are connected with six corners of the regular hexagon via aileron main rods, the six corners of the regular hexagon are between the upper center plate and the lower center plate, the aileron main rods are three-section bending structures, the end part of each aileron is provided with a propeller, each aileron main rod is connected with one section of the propeller, wherein the section of the propeller is higher than one section, connected with the center plate, of the aileron main rod, and when the propeller rotates, a produced push gas flows towards the outer side of the center plate. The flight stability of an unmanned aerial vehicle is improved by absorbing of propeller vibration, rotor angle adjustment, cabin body closing and other methods, aerial photography, monitoring and other tasks can be successfully completed, and a clear picture can be taken.

Description

Technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle preparation, and specifically relates to a high-stability six-rotor aircraft. Background technique [0002] UAVs are usually used to replace humans in performing various aerial photography and monitoring tasks. During the task, due to the vibration of the UAV propeller, the unadjustable rotor angle, the impact of wind on the interior of the UAV, etc., the aerial photography and monitoring The unclear picture may even make it impossible to complete the task, so there is an urgent need to invent a drone with high stability. Contents of the invention [0003] In order to solve the above technical problems, the present invention provides a highly stable six-rotor aircraft. By absorbing propeller vibration, adjusting the rotor angle, closing the cabin, etc., the stability of the drone flight is improved, allowing it to successfully complete aerial photography and monitoring. Wait for...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/52B64C1/06B64C1/00B64D27/26
CPCB64C1/0009B64C1/06B64C27/08B64C27/52B64U2101/30B64U10/10B64D27/40
Inventor 刘东兴刘文娟焦明程张浩杨忠诚王远航苗忠杰王楚涵闵杰张强李佳儒
Owner LIAOYANG POWER SUPPLY COMPANY OF STATE GRID LIAONING ELECTRIC POWER SUPPLY
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