Double-layered eight-rotor-wing unmanned aerial vehicle

An octa-rotor and unmanned aerial vehicle technology, applied in the field of double-layer eight-rotor unmanned aerial vehicles, can solve the problems such as the inability to exert the maximum efficiency of the rotor, the limitation of the size and efficiency of the rotor, and the limited space for assembling the rotor, so as to improve the translation efficiency and reduce the The effect of arm length, control and stability

Pending Publication Date: 2017-09-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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AI Technical Summary

Problems solved by technology

[0004] In order to increase the load capacity of UAVs, one of the existing multi-rotor distribution schemes has single-layer multi-rotors, but the distance between the adjacent rotors of the single-layer structure is very close, resulting in limited space for assembling the rotors, which limits the size and efficiency of the rotors

Method used

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  • Double-layered eight-rotor-wing unmanned aerial vehicle

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Embodiment Construction

[0027] Below in conjunction with accompanying drawing, technical scheme of the present invention is described in further detail:

[0028] Such as figure 1 As shown, the present invention discloses a double-deck eight-rotor UAV, comprising a fuselage, four upper arms, four lower arms and eight flight mechanisms;

[0029] The fuselage includes an upper platform and a lower platform;

[0030] The roots of the four upper plane arms are fixedly connected to the upper platform, and the ends extend toward the outside of the fuselage;

[0031] The roots of the four lower plane arms are fixedly connected to the lower platform, and the ends extend toward the outside of the fuselage;

[0032] The lower plane arm comprises a first connecting rod, a second connecting rod and a folding mechanism, wherein one end of the first connecting rod is fixedly connected to the lower platform, and the other end is connected to one end of the second connecting rod through a folding mechanism; The me...

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Abstract

The invention discloses a double-layered eight-rotor-wing unmanned aerial vehicle which comprises a body, four upper arms, four lower arms and eight flying mechanisms. The body comprises an upper platform and a lower platform; the four upper arms and the four lower arms are separately arranged on the upper platform and the lower platform; each of the lower arms comprises a first connecting rod, a folding mechanism and a second connecting rod which are successively connected; the eight flying mechanisms are separately arranged on the tail ends of the four upper arms and the four lower arms; each of the flying mechanisms comprises a brushless motor and a rotor wing fixedly connected to the output shaft of the brushless motor; and the rotating ranges of the rotor wings of the eight flying mechanisms are staggered for generating upward lift forces. By adopting a double-layered structure, the arm length of a common eight-rotor-wing unmanned aerial vehicle is reduced, the weight of the structure is alleviated, and the storage space is expanded; meanwhile, the double-layered eight-rotor-wing unmanned aerial vehicle is more stable to control, longer in time of endurance and higher in efficiency, and the safety of inner loads of the body is effectively guaranteed.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a double-deck eight-rotor unmanned aerial vehicle. Background technique [0002] Because of its good mobility, low cost, and good cost-effectiveness, multi-rotor drones are now widely used in various military and civilian fields such as military investigation, geological exploration, forest fire prevention, plant maintenance, and aerial photography. [0003] With the increase in the load requirements of UAVs, there are more and more rotors for UAVs, and there are also various rotor configurations. [0004] In order to increase the load capacity of UAVs, one of the existing multi-rotor distribution schemes has single-layer multi-rotors, but the distance between the adjacent rotors of the single-layer structure is very close, resulting in limited space for assembling the rotors, which limits the size and efficiency of the rotors; another This kind of coaxial multi...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/32B64C1/30B64C1/00
CPCB64C1/00B64C1/30B64C27/08B64C27/32
Inventor 朱赫聂宏张明彭争雷波
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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