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Mini spherical aircraft and working method thereof

An aircraft and spherical technology, applied in the field of aircraft, can solve problems such as collision avoidance and easy damage, the rotor is easily damaged, and the aircraft cannot rotate freely and flexibly in 360 degrees, so as to achieve the effect of not easy to damage and uniform force.

Inactive Publication Date: 2016-07-20
ANHUI UNIVERSITY OF TECHNOLOGY AND SCIENCE
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Chinese patent ZL201520934512.5 discloses a stable four-axis rotor aircraft, which is driven by the rotor and has a stable flight state, but the exposed rotor is easy to hurt people, and the anti-collision is easily damaged; Chinese patent ZL201320642644.1 discloses a spherical aircraft , the cost is low, the hardware is simple and easy to operate, but the outer surface of the aircraft is not closed and cannot cope with wind and rain; High-quality video, but the fuselage of the aircraft cannot rotate freely in 360 degrees

Method used

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  • Mini spherical aircraft and working method thereof

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Embodiment Construction

[0025] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

[0026] Such as figure 1 Shown, a kind of miniature spherical aircraft comprises duct fan 101, screw 102 fan support 103, ventilation hole 104 and central shaft 105, also comprises left hemispherical shell 106, guide tube 107, right hemispherical shell 108, fixed tube 109, balance The fan 110 balances the duct 111, the central axis 105 runs through the left hemispherical shell 106, the guide cylinder 107 and the right hemispherical shell 108, the guide cylinder 107 is connected to the plane of the left hemispherical shell 106 through the central axis 105, and guides The cylinder 107 is connected to the plane of the right hemispherical shell 108 through the central axis 105, the guide cylinder 107 is located between the left hemispherical shell 10...

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Abstract

The invention relates to a mini spherical aircraft and a working method thereof. The mini spherical aircraft comprises ducted fans, screw fan brackets, vent holes, a central shaft as well as a left hemisphere shell, a guide barrel, a right hemisphere shell, fixing tubes, balance fans and balance ducts, wherein the central shaft penetrates through the left hemisphere shell, the guide barrel and the right hemisphere shell; the guide barrel is connected with the plane of the left hemisphere shell through the central shaft; the guide barrel is connected with the plane of the right hemisphere shell through the central shaft, and is positioned between the left hemisphere shell and the right hemisphere shell; the plane of the left hemisphere shell is connected with the plane of the right hemisphere shell through two fixing tubes; two symmetric balance ducts are communicated with each other in the position of the equatorial zone of the left hemisphere shell and the right hemisphere shell; the balance fans are connected with the inside of the middle sections of the balance ducts through the fan brackets. As the left hemisphere shell and the right hemisphere shell form a sphere, the mini spherical aircraft is high in security coefficient, uniform in stress when being landed and not easy to damage, and due to the balance fans, the mini spherical aircraft can rotate horizontally and then can be adjusted to an expected direction.

Description

technical field [0001] The invention relates to an aircraft, in particular to a miniature spherical aircraft and an operation method thereof. Background technique [0002] At present, domestic drones have developed rapidly in recent years. In addition to military use, due to the advantages of UAVs such as relatively low cost, no risk of casualties, strong survivability, good maneuverability, and ease of use, UAVs are used in aerial photography, geological surveys, high-voltage transmission line inspections, etc. Oilfield pipeline inspection, expressway management, forest fire prevention inspection, poisonous gas investigation, anti-drug and emergency rescue, ambulance and other civilian fields have extremely broad application prospects. [0003] Chinese patent ZL201520934512.5 discloses a stable four-axis rotor aircraft, which is driven by the rotor and the flight state is stable, but the exposed rotor is easy to hurt people, and the anti-collision is easily damaged; Chines...

Claims

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Application Information

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IPC IPC(8): B64D27/24B64C1/00B64C27/20B64C27/12
CPCB64C1/00B64C27/12B64C27/20B64D27/24B64C2001/0045B64U50/19B64U50/14
Inventor 刘有余朱先绮徐天殷
Owner ANHUI UNIVERSITY OF TECHNOLOGY AND SCIENCE
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