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Pod landing buffer device

A buffer device and pod technology, applied in the field of unmanned aerial vehicles, can solve the problems of unsatisfactory shock absorption effect, high cost, and complex structure of shock absorber buffer devices, and achieve the advantages of small footprint, small mass, and impact relief Effect

Active Publication Date: 2021-05-07
北京吾天科技有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention aims to solve the problems of complex structure, high cost and unsatisfactory shock-absorbing effect of the existing shock-absorbing and buffering devices for UAVs, and further provides a pod landing buffering device

Method used

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specific Embodiment approach 1

[0026] Specific implementation mode one: combine Figure 1-7 Describe this embodiment, a pod landing buffer device, which includes a sliding buffer assembly and a support buffer assembly, the sliding buffer assembly includes a connecting rod 1 and two sliding rods 2, wherein the two ends of the connecting rod 1 are respectively connected to the two The middle part of the sliding rod 2 is fixed, and the connecting rod 1 and the two sliding rods 2 are arranged in the shape of "I",

[0027] The support buffer assembly includes two guide buffer rods 3 and several diagonally braced buffer rods 4, wherein the two guide buffer rods 3 are fixed vertically above the middle of the two sliding rods 2, and several diagonally braced buffer rods 4 are respectively hinged On the connecting rod 1 and the two sliding rods 2, some diagonally braced buffer rods 4 on each sliding rod 2 are symmetrically located on both sides of the guide buffer rod 3, and some diagonally braced buffer rods 4 on t...

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Abstract

The invention discloses a pod landing buffer device, which belongs to the technical field of unmanned aerial vehicles. The problems that an existing damping buffer device for the unmanned aerial vehicle is complex in structure, high in cost and not ideal in damping effect can be solved. The sliding buffer assembly comprises a connecting rod and two sliding rods, the two ends of the connecting rod are fixedly connected with the middles of the two sliding rods respectively, the connecting rod and the two sliding rods are arranged in an I shape, and the supporting buffer assembly comprises two guiding buffer rods and a plurality of inclined supporting buffer rods. The two guiding buffer rods are vertically and fixedly connected to the upper portions of the middles of the two sliding rods respectively, the multiple inclined supporting buffer rods are hinged to the connecting rod and the two sliding rods respectively, and the multiple inclined supporting buffer rods on each sliding rod are symmetrically located on the two sides of the guiding buffer rod on the sliding rod. The multiple inclined supporting buffer rods on the connecting rod are symmetrically arranged relative to the middle of the connecting rod.

Description

technical field [0001] The invention relates to a pod landing buffer device, which belongs to the technical field of unmanned aerial vehicles. Background technique [0002] UAV is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device. Civilian UAV has important applications in aerial photography, agriculture, plant protection, disaster relief and other fields; UAV needs to take off and land Shock absorption is carried out to protect the fuselage. Most of the shock absorption buffer devices currently used are complicated in structure or unreasonable in setting, resulting in unsatisfactory shock absorption effects. Contents of the invention [0003] The present invention aims to solve the problems of complex structure, high cost and unsatisfactory shock-absorbing effect of the existing shock-absorbing and buffering devices for unmanned aerial vehicles, and further provides a pod landing buffering device. [0004] The tec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/58
CPCB64C25/58Y02T50/40
Inventor 马超范伯钧施维慰易满满刘炜高蓓贾志昂
Owner 北京吾天科技有限公司