Multi-rotor aircraft elevating turnover device and carrying and elevating device thereof

The technology of a multi-rotor aircraft and a turning device is applied in the field of aircraft, which can solve the problems of cumbersome loading process, high damage rate of aircraft, and easy crushing of aircraft, etc., and achieves the effect of improving efficiency, simple structure and improving lifting effect.

Inactive Publication Date: 2017-11-10
成都鑫晨航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, during the transportation of the aircraft, the first problem is to load the packaged multi-rotor aircraft on the transport equipment.
Most of the existing packaged finished aircraft products are stacked into stacks and then loaded onto the transportation equipment by forklifts and other equipment; after this method, the packaged finished aircraft products need to be manually palletized, and then the finished products are loaded by forklifts. Lifting and transporting to the compartment, and manual handling and stacking at the designated position in the compartment, this makes the entire loading process more cumbersome and the loading efficiency is low
In addition, affected by the material, the finished aircraft is a vulnerable part. When it is stacked and stacked, the aircraft at the lower position is easily crushed, resulting in a high damage rate of the aircraft

Method used

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  • Multi-rotor aircraft elevating turnover device and carrying and elevating device thereof
  • Multi-rotor aircraft elevating turnover device and carrying and elevating device thereof
  • Multi-rotor aircraft elevating turnover device and carrying and elevating device thereof

Examples

Experimental program
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Effect test

Embodiment 1

[0026]A lifting and flipping device for a multi-rotor aircraft includes rails 1 installed on a compartment 8, two groups of rails 1 are arranged, and two groups of rails 1 are arranged side by side along the length direction of the compartment 8 at a certain distance in parallel. Also be provided with guide piece on track 1, can guide some parts by guide piece. The guide member may be a groove provided on the side of the guide rail 67, and some parts are located in the groove, so as to realize movement along the track direction of the groove. This track 1 becomes L-shaped structure, and one side of this L-shaped track 1 is connected on the top surface of compartment 8, and the other side of this L-shaped track 1 is positioned on compartment 8 side, and is connected with compartment 8 side. A rotary assembly 2 is arranged between the L-shaped rails 1 on the top surface of the compartment 8, and a rotary drive assembly 3 is provided on the top surface of the compartment 8 or the...

Embodiment 2

[0028] On the basis of Embodiment 1, the other end of the first lifting rod 5 is also hinged with a second lifting rod, which is an L-shaped second lifting rod, and the end of the long side of the second lifting rod is connected to The end of the long side of the first lifting rod 5 is hinged, and the end of the short side of the second lifting rod is connected with the guide and can move along the track of the guide on the guide. And under the action of the second lifting rod, the turning angle of the first lifting rod 5 can be prevented from being too large.

Embodiment 3

[0030] A multi-rotor aircraft handling and lifting device includes a compartment 8 for storing and transporting finished aircraft products 10 . A lifting and turning device 9 is connected to the compartment 8, and the lifting and turning device 9 is mainly used for turning. The lifting and turning device 9 can be arranged corresponding to each compartment 8, that is, the lifting and turning device 9 is fixedly connected to the car body of the compartment 8; of course, the compartment 8 can also be reused with multiple compartments 8, that is, the lifting and turning device 9 is detachable Ground is connected on the car body of compartment 8. An accommodating mechanism is provided on the lifting and turning device 9, and the accommodating mechanism is mainly used for placing the finished aircraft 10 and effectively preventing the finished aircraft 10 from being crushed.

[0031] Lifting and flipping device comprises track 1 installed on the compartment 8, two groups of tracks ...

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PUM

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Abstract

The invention discloses a lifting and turning device for a multi-rotor aircraft and its handling and lifting device, which belongs to the technical field of aircraft, and provides a lifting and turning device for a multi-rotor aircraft with high lifting efficiency and a handling and lifting device for improving the lifting and turning of finished aircraft products Efficiency, thereby improving the efficiency of finished aircraft loading. The lifting and flipping device includes a track and a guide; the track is connected with a rotating assembly and a rotating drive assembly, and the rotating assembly is connected with a rotating rod. The end of the rotating rod is hinged with a connecting rod, and the other end of the connecting rod is hinged with a first lifting rod. One end of the first lifting rod is matched with the guide member and can move on the guide member along the track of the guide member; the first lifting rod is connected with a turning plate. The transporting and lifting device includes a carriage, a lifting and turning device, and an accommodating mechanism, and the lifting and turning device adopts the above-mentioned lifting and turning device. The invention is suitable for storing and transporting the multi-rotor aircraft.

Description

technical field [0001] The invention belongs to the technical field of aircraft, relates to a multi-rotor aircraft, in particular to the transportation of the multi-rotor aircraft. Background technique [0002] In recent years, multi-rotor aircraft has broad application prospects in military and civilian fields due to its low cost, high cost-effectiveness ratio, no risk of casualties, and the ability to enter many unreachable areas, such as low-altitude reconnaissance, meteorological survey, Aerial photography, traffic patrol, etc. With the needs of the development of the industry, many professional multi-axis and long-wheelbase multi-rotor aircraft have appeared on the market. The long-wheelbase multi-axis multi-rotor aircraft meets the needs of many customers. Due to the long wheelbase and the large size of the aircraft, the packaging size is also large and the weight is heavy. [0003] However, during the transportation of the aircraft, the first problem is to load the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60P1/44B60P3/11
CPCB60P1/4407B60P3/11
Inventor 石存岭
Owner 成都鑫晨航空科技有限公司
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