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Logistics transportation system, unmanned aerial vehicle, landing platform and control method thereof

A transportation system and control method technology, applied in the fields of unmanned aerial vehicles, landing platforms and their control, and logistics transportation systems, can solve the problems of short cruising range, high manufacturing and energy consumption costs, complex unmanned aerial vehicle structures, etc. The effect of self-weight and manufacturing cost, simple connection structure, improved automation and logistics and transportation efficiency

Pending Publication Date: 2021-01-15
BEIJING SANKUAI ONLINE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Embodiments of the present invention provide a logistics transportation system, a drone, a landing platform and a control method thereof, so as to at least solve the problems of high manufacturing and energy consumption costs and short cruising range caused by the complex structure of existing drones

Method used

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  • Logistics transportation system, unmanned aerial vehicle, landing platform and control method thereof
  • Logistics transportation system, unmanned aerial vehicle, landing platform and control method thereof
  • Logistics transportation system, unmanned aerial vehicle, landing platform and control method thereof

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Embodiment 1

[0054] refer to Figure 1 to Figure 4, the embodiment of the present invention provides a logistics transportation system, the logistics transportation system includes a drone 1 and a landing platform 2;

[0055] The drone 1 includes a drone body 10 and a landing gear assembly 11;

[0056] The landing gear assembly 11 includes a first bracket 111, a second bracket 112 and an elastic reset member 113;

[0057] The first bracket 111 is arranged opposite to the second bracket 112, at least one bracket in the first bracket 111 and the second bracket 112 is movably connected with the drone body 10, and the first bracket 111 A loading space for clamping the cargo box 12 is formed between the second bracket 112;

[0058] The elastic reset member 113 is arranged between the first bracket 111 and the second bracket 112, or, the elastic reset member 113 is arranged between any bracket and the drone body 10;

[0059] The landing platform 2 includes a platform base and a push-pull asse...

Embodiment 2

[0072] refer to figure 2 , the embodiment of the present invention provides a UAV 1, the UAV 1 includes a UAV body 10 and a landing gear assembly 11;

[0073] The landing gear assembly 11 includes a first bracket 111, a second bracket 112 and an elastic reset member 113;

[0074] The first bracket 111 is arranged opposite to the second bracket 112, at least one bracket in the first bracket 111 and the second bracket 112 is movably connected with the drone body 10, and the first bracket 111 A loading space for clamping the cargo box 12 is formed between the second bracket 112;

[0075] The elastic reset member 113 is arranged between the first bracket 111 and the second bracket 112 , or, the elastic reset member 113 is arranged between any bracket and the drone body 10 .

[0076] Specifically, as figure 2 As shown, a drone 1 provided in the embodiment of the present invention includes a drone body 10 and a landing gear assembly 11 . The UAV body 10 is the body where the p...

Embodiment 3

[0095] refer to figure 1 , the embodiment of the present invention provides a landing platform 2 for undertaking the landing of the UAV 1 in the second embodiment, the landing platform 2 includes a platform base and a push-pull assembly 21;

[0096] The push-pull assembly 21 includes a first push plate 211 and a second push plate 212, at least one of the first push plate 211 and the second push plate 212 is provided with a push-pull hook on the first surface, wherein, The first surface is a landing surface on which the UAV lands and stops;

[0097] The first push plate 211 is opposite to the second push plate 212 on the same horizontal plane, and at least one of the first push plate 211 and the second push plate 212 is slidably connected to the platform base ;

[0098] The push-pull hook drives the movement of the first support 111 and / or the second support 112 , wherein the distance between the container 12 and the first surface is at least equal to the height of the push-p...

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Abstract

The invention provides a logistics transportation system, an unmanned aerial vehicle, a landing platform and a control method thereof. The unmanned aerial vehicle lands and is parked on the landing platform, a first support in the unmanned aerial vehicle is in contact with a first surface of a first push plate in the landing platform, and a second support in the unmanned aerial vehicle is in contact with a first surface of a second push plate in the landing platform, wherein the first surface is a landing surface on which the unmanned aerial vehicle lands; and a push-pull hook on a push plateof the landing platform drives the first bracket and / or the second bracket to move. According to the unmanned aerial vehicle, electric energy does not need to be consumed when the unmanned aerial vehicle unloads, the cruising ability can be improved, the support and the connecting structure of the support and the unmanned aerial vehicle body are simple, and the dead weight and manufacturing cost can be reduced.

Description

technical field [0001] The present invention relates to the technical field of unmanned equipment, in particular to a logistics transportation system, an unmanned aerial vehicle, a landing platform and a control method thereof. Background technique [0002] With the development and progress of unmanned control technology, drones are gradually participating in the process of logistics and transportation. [0003] In the existing logistics transportation process, in order to carry the goods, the electric power of the drone battery is usually used to drive the action of the locking mechanism or the unloading device to realize the fixing and release of the goods. [0004] However, the above-mentioned locking mechanism or unloading device is fixed on the fuselage of the UAV, and its driving and operating mechanism is relatively complicated. On the one hand, it increases the weight of the UAV and increases energy consumption. On the other hand, it consumes the electric energy of t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 崔鹏
Owner BEIJING SANKUAI ONLINE TECH CO LTD
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