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

A technology of transportation system and control method, which is applied in the field of landing platform and its control, unmanned aerial vehicle, and logistics transportation system. It can solve the problems of short cruising range, complex structure of unmanned aerial vehicles, high manufacturing and energy consumption costs, and reduce its own weight. and manufacturing costs, improving the degree of automation and logistics transportation efficiency, and the effect of simple connection structure

Inactive Publication Date: 2019-11-01
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 is landed and stopped on the landingplatform, a first bracket in the unmanned aerial vehicle is in contact with the first side of a first push plate in the landing platform, and a second bracket in the unmanned aerial vehicle is in contact with the first side of a second push plate in the landing platform, wherein the first side is a landing surface where the unmanned aerial vehicle is landed and stopped; and a push-pull hook on thepush plate of the landing platform drives the movement of the first bracket and/or the second bracket. The unmanned aerial vehicle of the invention does not need to consume the own electric energy when unloading, and contributes to improving the endurance capability; and the brackets and the connection structure between the brackets and the main body of the unmanned aerial vehicle are relativelysimple, so that the self-weight and the 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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