High-altitude rescue unmanned aerial vehicle with damping device and using method of high-altitude rescue unmanned aerial vehicle

A shock absorption device and high-altitude rescue technology, applied in the field of unmanned aerial vehicles, can solve the problems of inability to adjust the posture of the fuselage of the unmanned aerial vehicle, low safety, low reliability, and unsatisfactory shock absorption effect, so as to increase the practicability and reliability. Highly adjustable, reliable and practical, shock absorbing and effective

Active Publication Date: 2021-01-05
BEIJING ZHAOYANG SCI TECH CULTURE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] Aiming at the above-mentioned deficiencies in the prior art, the present invention provides a high-altitude rescue UAV with a shock absorbing device, which is used to solve the problem of high load of the rescue UAV in the prior art after rescue. Under certain circumstances, the shock absorption effect when landing is not ideal; and the rescue UAV of the prior art cannot adjust the fuselage attitude of the UAV after landing and shock absorption, which may easily cause the UAV to slip and fall twice, which is safe. In order to solve problems such as low performance and low reliability, the present invention also provides a method for using the unmanned aerial vehicle

Method used

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  • High-altitude rescue unmanned aerial vehicle with damping device and using method of high-altitude rescue unmanned aerial vehicle
  • High-altitude rescue unmanned aerial vehicle with damping device and using method of high-altitude rescue unmanned aerial vehicle
  • High-altitude rescue unmanned aerial vehicle with damping device and using method of high-altitude rescue unmanned aerial vehicle

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Experimental program
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Effect test

Embodiment 1

[0057] Such as Figure 1-8 As shown, a high-altitude rescue UAV with a shock absorbing device includes several flight systems 1, a frame 2, a balance system 3, a control adjustment system 4, four shock absorbing devices 5 and a video acquisition system 6, and several The flight system 1 is evenly installed on the side of the frame 2, the balance system 3, the control adjustment system 4 and the video acquisition system 6 are all installed on the frame 2, and the flight system 1, the balance system 3, the four shock absorbers 5 and The video acquisition system 6 is respectively connected with the control adjustment system 4 by wires;

[0058] The balance system 3 includes two induction structures 31 and a housing 32, the two induction structures 31 are installed inside the housing 32, one induction structure 31 is above the other induction structure 31, and the two induction structures 31 are perpendicular to each other;

[0059] The damping device 5 comprises a swivel base 51...

Embodiment 2

[0070] This embodiment is as a further improvement of the previous embodiment, such as Figure 1-8 As shown, a high-altitude rescue UAV with a shock absorbing device includes several flight systems 1, a frame 2, a balance system 3, a control adjustment system 4, four shock absorbing devices 5 and a video acquisition system 6, and several The flight system 1 is evenly installed on the side of the frame 2, the balance system 3, the control adjustment system 4 and the video acquisition system 6 are all installed on the frame 2, and the flight system 1, the balance system 3, the four shock absorbers 5 and The video acquisition system 6 is respectively connected with the control adjustment system 4 by wires;

[0071] The balance system 3 includes two induction structures 31 and a housing 32, the two induction structures 31 are installed inside the housing 32, one induction structure 31 is above the other induction structure 31, and the two induction structures 31 are perpendicular ...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a high-altitude rescue unmanned aerial vehicle with a damping device, wherein the high-altitude rescue unmanned aerial vehicle comprises a plurality of flight systems, a rack, a balance system, a control adjusting system, four damping devices and a video acquisition system; a plurality of flight systems are uniformly mounted on the sides of the rack; the balance system, the control adjusting system and the video collecting system are all mounted on the rack. Under the condition that the unmanned aerial vehicle is high in load after rescue, and the damping effect is reliable and effective when the unmanned aerial vehicle falls to the ground; and after shock absorption, a fuselage of the unmanned aerial vehicle can be quickly adjusted to a horizontal posture. The invention further provides a using method of the unmanned aerial vehicle, the using method comprises the steps of unmanned aerial vehicle control, landing site selection, first-time damping, second-time damping and the like; the method is high in automation degree, an operator only needs to manually control the landing siteof the unmanned aerial vehicle, the operation difficulty is low, and the method is high in operability.

Description

technical field [0001] The invention belongs to the technical field of drones, and in particular relates to a high-altitude rescue drone with a shock absorbing device and a use method thereof. Background technique [0002] After decades of development, drones are relatively mature from a technical point of view. Its advantages are low cost, high flexibility, and the ability to carry some important equipment to complete special tasks from the air, such as air detection, air surveillance, air signaling, air shouting, emergency rescue, etc.; Causing casualties, strong survivability, good maneuverability, practical and convenient, can play an important role in dealing with natural disasters, accident disasters and social security incidents. [0003] However, in order to make drones more intelligent, reduce their difficulty in use, and improve their work efficiency, more and more sensors and processing chips are mounted on drones to make their functions more perfect and complete...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C25/62B64C25/58
CPCB64C39/02B64C25/62B64C25/58B64U2101/00
Inventor 李文美
Owner BEIJING ZHAOYANG SCI TECH CULTURE
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