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Self-obstacle-avoiding and fixed-point-tracking spherical aircraft

An aircraft, spherical technology, applied in the direction of aircraft, unmanned aircraft, instruments, etc., can solve problems such as limitations, achieve the effect of light weight, flexible operation without dead center, simple mechanical structure

Inactive Publication Date: 2016-10-12
YANSHAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its shortcoming: It imposes certain restrictions on the environment required for vertical take-off and lift-off of the aircraft, that is, the take-off ground must be relatively flat, so as to ensure that the wing surface of the propeller or rotor can be kept relatively horizontal

Method used

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  • Self-obstacle-avoiding and fixed-point-tracking spherical aircraft

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Embodiment Construction

[0015] exist figure 1 , figure 2 , image 3 , Figure 4 and Figure 5 In the schematic diagram of the present invention shown, the spherical skeleton shell 1 is a spherical network structure composed of carbon fiber tubes. The shape of the unit body is tripod-shaped, and the space is 120 degrees, 120 degrees and 108 degrees. An infrared sensor 14 is arranged on the spherical skeleton shell. The outer ring 2 of the gyro stabilization system is arranged inside the spherical skeleton, and the outer ring of the gyro stabilization system is circular, and the outer side of the outer ring of the gyro stabilization system is movably connected with the shell of the spherical skeleton through a pair of pins A27. A gyro stabilization system inner ring 3 is provided inside the gyro stabilization system outer ring, the gyro stabilization system inner ring is circular, and the outside of the gyro stabilization system inner ring is movably connected with the inner side of the gyro stab...

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PUM

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Abstract

The invention discloses a self-obstacle-avoiding and fixed-point-tracking spherical aircraft which mainly comprises a spherical framework shell, a gyroscopic stabilizing system outer ring, a gyroscopic stabilizing system inner ring, a motor supporting frame A, a paddle A, paddle tacking knobs, a brushless motor A, a socket cap screw A, a pan-tilt seat, a motor supporting frame B, a brushless motor B, a paddle B, a control system single chip microcomputer, an infrared sensor, a platform, a brushless motor C, a paddle C, a motor supporting frame C, a brushless motor D, a paddle D, a motor supporting frame D, a socket cap screw B, a socket cap screw C, a battery, tee couplings, carbon fiber tubes, a pin A and a pin B. The self-obstacle-avoiding and fixed-point-tracking spherical aircraft runs flexibly without a dead point, is light in weight, small in size and simple in mechanical structure, has better flexibility and adaptability, can be controlled remotely, has an automatic obstacle avoiding function, is provided with an expansion interface in a reservation manner, and can expand a miniature camera and a WIFI (wireless fidelity) module later.

Description

technical field [0001] The invention relates to a spherical aircraft. Background technique [0002] Spherical robots are spherical mobile robots that can move in mud, sand, snow, and even water, and can also move in toxic gas leakage, radiation, and biohazardous environments. They are suitable for dangerous environment detection, space development, fire disaster relief, military activities, and scientific investigations. , family services and entertainment and other fields. [0003] In terms of micro-aircraft research, developed countries in Europe and America are currently in a leading position in the world, and have successfully developed various micro-aircraft of fixed-wing, rotary-wing and flapping-wing types. Some universities and research institutes in my country have also launched Relevant research, and produced some related prototypes. Throughout the structure of unmanned aerial vehicles at home and abroad, most of them are leg-supported propellers or rotors. The in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00G05D1/10
CPCG05D1/101B64C39/00B64U10/00
Inventor 解明利宋忠义陈镇喜李泽运林实秋
Owner YANSHAN UNIV
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