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Six-rod tensioning integral frame and anti-impact unmanned aerial vehicle

A tensegrity and unmanned aerial vehicle technology, applied in the field of robotics, can solve the problems of providing the ground, the limited cushioning effect of the squirrel cage structure, and the inability of the unmanned aerial vehicle to take off again, and achieve the effect of high-strength impact resistance

Active Publication Date: 2021-09-03
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] After extensive research, it is found that there are currently two main buffer structures for UAVs. One is to install an elastic, spherical buffer structure outside the UAV, and use the spherical structure to buffer external forces to protect the UAV. , but this drone cannot take off again after being hit and landed
The other is to install a structure similar to a squirrel cage on the outside of the UAV, so that the UAV relies on its own gravity to maintain the level of the wings. The buffering effect of the force is limited, and it cannot provide a stable landing ground for the UAV. This UAV can also only fly but cannot perform controllable rolling on the ground

Method used

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  • Six-rod tensioning integral frame and anti-impact unmanned aerial vehicle
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  • Six-rod tensioning integral frame and anti-impact unmanned aerial vehicle

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Embodiment Construction

[0028] The implementation of the present invention will be described in detail below in conjunction with the accompanying drawings and examples, so as to fully understand and implement the process of how to apply technical means to solve technical problems and achieve corresponding technical effects in the present invention. The embodiments of the present application and the various features in the embodiments can be combined with each other under the premise of no conflict, and the formed technical solutions are all within the protection scope of the present invention.

[0029] figure 1 A schematic structural view of a six-bar tensegrity frame according to an embodiment of the present disclosure is shown. Such as figure 1 As shown, the six-bar tensegrity frame can include: six rigid compression bars and twenty-four elastic cables, four elastic cables are drawn from the two end points of each rigid compression bar, and the four elastic cables at each end point are respectivel...

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Abstract

According to the six-rod tensioning integral frame and the anti-impact unmanned aerial vehicle, the six rigid pressing rods and the twenty-four elastic cables are included, the four elastic cables are led out of the two end points of each rigid pressing rod correspondingly, the four elastic cables of each end point are connected with the four end points closest to the end point correspondingly, the six rigid pressing rods are averagely divided into three groups, and the six rigid pressing rods are divided into three groups; in the spatial position, any two sets of rigid pressing rods in the three sets of rigid pressing rods are perpendicular to each other, and the two rigid pressing rods in each set are parallel to each other. The structure is light in weight and can provide high-strength impact resistance, the influence on the cruising ability of the unmanned aerial vehicle is reduced while the mechanical structure of the unmanned aerial vehicle is protected, and the unmanned aerial vehicle can fly in the air, can orderly and controllably roll on the ground and can take off again after falling off.

Description

technical field [0001] The invention belongs to the technical field of robots, and in particular relates to a six-bar tensioned integral frame and an impact-resistant unmanned aerial vehicle. Background technique [0002] For ordinary drones, it is very challenging to fly in a complex environment where obstacles are difficult to detect and avoid. Obstacles in the environment are a great threat to the safety and integrity of the UAV's mechanical structure. A little carelessness will damage the UAV's rotor or arm, causing the UAV to crash. [0003] After extensive investigation, it is found that there are two main buffer structures for UAVs. One is to install an elastic, spherical buffer structure outside the UAV, and use the spherical structure to buffer external forces to protect the UAV. , but this drone cannot take off again after being hit and landed. The other is to install a structure similar to a squirrel cage on the outside of the UAV, so that the UAV relies on its ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C27/08
CPCB64C1/062B64C27/08B64U10/10
Inventor 杨庆凯刘奇刘松源赵欣悦李若成肖凡方浩曾宪琳陈杰
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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