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UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle

A technology of unmanned aerial vehicles and trimming, which is applied in aircraft assembly, aircraft component testing, aircraft parts, etc. It can solve the problems of not being able to meet the production schedule, low work efficiency, and high labor intensity, and achieve shortened assembly time, convenient movement, and energy saving. Workplace Effects

Active Publication Date: 2014-05-07
NO 60 RES INST OF GENERAL STAFF DEPT PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, during the assembly process of mass-produced UAVs, because of the complex structure and precise requirements, it is often necessary to repeat many times in the process of debugging, weighing, and balancing.
When weighing and balancing, multiple people are required to operate at the same time, and it can be completed after repeated times. The work efficiency is low and the labor intensity is high, which cannot meet the requirements of the production schedule.

Method used

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  • UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle
  • UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle

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Embodiment Construction

[0013] An unmanned aerial vehicle assembly and debugging vehicle provided in this embodiment, such as figure 1 and figure 2 As shown, it is mainly composed of a chassis 1, a weighing pan 2, a trim device 12, a display mechanism 3, a support frame 4 and a lifting mechanism. There are four pressure sensors 5 between the weighing pan and the pressure sensor are connected to the display mechanism 3 installed on the chassis through wires. The chassis is connected to the weighing pan; T-shaped support frames 4 are respectively installed at the front and rear ends of the weighing pan, and four polyurethane rubber wheels 7 with locking mechanisms are arranged on both sides of the upper part of the support frame; A lifting mechanism is fixedly installed. The lifting mechanism is mainly composed of a motor, an electric push rod 8 and a linear guide rail 9. The electric push rod driven by the motor pushes the support rod mounted on the linear guide rail up and down. It is composed of ...

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Abstract

The invention relates to a UAV (Unmanned Aerial Vehicle) assembling and debugging vehicle which mainly comprises a chassis, a weighing disk, a balancing device, a display mechanism, support frames and lifting mechanisms. The weighing disk is arranged on the chassis; at least two pressure sensors are arranged between the chassis and the weighing disk; the T-shaped support frames are respectively arranged at the front and rear ends of the weighing disk; both sides of the upper parts of the support frames are provided with roller wheels; the chassis at both sides of the weighing disk is fixedly provided with the lifting mechanisms; each lifting mechanism is mainly formed by a motor, an electric push rod and a linear guide rail; the support frames arranged on the linear guide rails are pushed to ascend and descended by the electric push rods driven by the motors; the balancing device consists of balancing knife edges at both sides and a balancing cross bar; the balancing cross bar is fixedly arranged on supporting rods at both sides; and the balancing knife edges are symmetrically fixed at both sides of the balancing cross bar. The UAV assembling and debugging vehicle integrates each set of tool in each link of debugging, weighing, balancing and turnover of a UAV; the equipment is simple to operate, has reliable performance and is convenient to move; a work place is saved; and the UAV assembling and debugging vehicle can be suitable for the requirements for assembling and debugging of various types of UAVs.

Description

technical field [0001] The invention relates to a UAV debugging device, in particular to a UAV assembly and debugging vehicle, which belongs to the technical field of UAV assembly equipment. Background technique [0002] At present, in the assembly process of mass-produced UAVs, because of the complex structure and precise requirements, it often needs to be repeated many times in the process of debugging, weighing, and balancing. When weighing and balancing, multiple people are required to operate at the same time, and it can be completed after repeated times. The work efficiency is low and the labor intensity is high, which cannot meet the requirements of the production schedule. For this reason, it is very necessary to develop technological equipment integrating debugging, weighing, balancing and shipping functions. Contents of the invention [0003] In view of the above-mentioned defects in the prior art, the object of the present invention is to provide a UAV assembly...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00B64F5/10B64F5/50B64F5/60
Inventor 闫涛庄震宇赵敏杨连明郭友利黄红端
Owner NO 60 RES INST OF GENERAL STAFF DEPT PLA
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