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Logistics aircraft, cargo hold and control system and method for automatic docking and disconnecting between logistics aircraft and cargo hold

A control system and aircraft technology, applied to equipment for loading and unloading cargo, aircraft parts, transportation and packaging, etc., can solve the problems of small chute gap, easy deformation of slide rail, long slide rail, etc., and achieve short time and mobile The effect of the short path

Active Publication Date: 2019-03-29
GUANGDONG UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The invention can solve the problems in the prior art that the cargo hold is loaded and unloaded on the horizontal plane, the slide rail is long, the slide rail is easy to change, and the gap between the chute in the slide rail is small, which leads to low loading and unloading efficiency of the cargo hold.

Method used

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  • Logistics aircraft, cargo hold and control system and method for automatic docking and disconnecting between logistics aircraft and cargo hold
  • Logistics aircraft, cargo hold and control system and method for automatic docking and disconnecting between logistics aircraft and cargo hold
  • Logistics aircraft, cargo hold and control system and method for automatic docking and disconnecting between logistics aircraft and cargo hold

Examples

Experimental program
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Embodiment 1

[0051] Such as Figure 1 to Figure 7 As shown, a logistics aircraft and a cargo compartment, wherein a fixed locking device is provided between the aircraft and the cargo compartment, and the aircraft can be detachably connected to the cargo compartment through the fixed locking device; the fixed locking device includes The first locking block 1 provided on the aircraft, and the second locking block 2 arranged on the cargo hold and matched with the first locking block 1; the first locking block 1 is uniform Distributed on the same plane of the aircraft, the second locking block 2 is evenly distributed on the same plane of the cargo compartment, the first locking block 1 can cooperate with the second locking block 2, so that the aircraft connected to the cargo compartment.

[0052] Such as Figure 1 to Figure 7 As shown, the first locking block 1 includes a first fixing plate 11 and a first locking block main body 12 arranged on the first fixing plate 11, and the first lockin...

Embodiment 2

[0058] Such as Figure 8 to Figure 11 As shown, a control system for automatically docking and separating a logistics aircraft and a cargo compartment, including a logistics platform, an aircraft control system and a cargo compartment control system capable of communicating with the logistics platform, and the aircraft control system includes sequentially connected:

[0059] The first receiving / sending signal module is used to receive the signal of the logistics platform, obtain the relevant information of the cargo compartment therefrom, and send the relevant information of the aircraft;

[0060] The first position coordinate detection module is used to detect the coordinate position of the point on the aircraft;

[0061] The flight attitude detection module is used to detect the flight attitude of the aircraft in the air;

[0062] and onboard the aircraft:

[0063] The first processor is used to receive information sent by the first receiving / sending signal module, and pro...

Embodiment 3

[0073] Such as Figure 12 Shown, a kind of control method of logistics aircraft and cargo hold automatic docking, wherein, comprises the following steps:

[0074] S1. The cargo cabin to be loaded sends the cargo cabin request loading information to the logistics platform. At this time, the logistics platform detects the aircraft carrying event, and the logistics platform determines the obtained cargo cabin center coordinate point A as the first target point; then, the logistics platform obtains the aircraft center point coordinates of A', and analyze the height of the center point A' of the aircraft to determine whether the height value is greater than a certain preset threshold, if not, control the aircraft to move upward according to the height value, and obtain After the movement, the height value of the center point A' of the new aircraft is judged again; if it is greater than the preset threshold value, then keep or not less than this height value and proceed to step S2; ...

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PUM

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Abstract

The invention provides a logistics aircraft and a cargo hold. A fixing and locking device is arranged between the aircraft and the cargo hold, and the aircraft can be detachably connected with the cargo hold through the fixing and locking device; the fixing and locking device comprises first locking blocks arranged on the aircraft and second locking blocks arranged on the cargo hold and matched with the first locking blocks; the first locking blocks are evenly distributed on the same plane of the aircraft, the second locking blocks are evenly distributed on the same plane of the cargo hold, and the first locking blocks and the second locking blocks can be matched with each other to make the aircraft and the cargo hold connected together. The invention further provides a control system andmethod for automatic docking and disconnecting between the logistics aircraft and the cargo hold. By means of the logistics aircraft, the cargo hold and the control system and method, the problems that in the prior art, a cargo hold is loaded and unloaded on a horizontal plane, sliding rails are long and likely to deform, sliding groove gaps in the sliding rails are small, and consequently the cargo hold loading and unloading efficiency is low are solved.

Description

technical field [0001] The present invention relates to the technical field of aircraft logistics transportation, and more specifically, relates to a logistics aircraft and a cargo compartment, a control system and a control method for automatically docking and separating the logistics aircraft and the cargo compartment. Background technique [0002] The application number is CN106114866.A, and the Chinese invention patent with the patent name UAV cargo compartment provides a UAV cargo compartment, which includes: a set of first connecting plates parallel to each other and a set of first connecting plates parallel to each other. Two connecting plates, the bottoms of one group of the first connecting plates and one group of the second connecting plates are closed by the bottom plate, and the adjacent first connecting plates and the second connecting plates are connected by columns at the corners; At least one of the first connecting plates is provided with a first locking blo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D9/00
CPCB64D9/00Y02T50/40
Inventor 杨杰张志明李蓉梁凯王丽丽陈秋露
Owner GUANGDONG UNIV OF TECH