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Unmanned aerial vehicle fuselage running-in platform

A technology for drones and fuselage, applied in the direction of aircraft component testing, etc., can solve the problems of limited production efficiency, affecting production efficiency, etc., to achieve the effect of improving production efficiency, improving running-in effect, and facilitating running-in

Pending Publication Date: 2018-11-13
FEIRUI AVIATION SCI & TECH JIANGSU
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage is that production efficiency is limited by the number of pilots, and one aircraft must be controlled by one pilot; and subject to external weather, bad weather cannot be used for run-in flight, which seriously affects production efficiency

Method used

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  • Unmanned aerial vehicle fuselage running-in platform

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Embodiment

[0019] Embodiment: A running-in platform for a fuselage of an unmanned aerial vehicle, comprising a base 1, a first machine platform 2 and a second machine platform 3 installed on the base, a fuselage assembly 4 installed on the first machine platform 2, and The electric motor 5 installed on the second machine platform 3.

[0020] The second machine platform 3 is fixedly installed on one side of the base 1, and the first machine platform 2 is movably installed on the other side of the base 1, and is locked in an active position by a lock.

[0021] The second transmission wheel 7 is installed on the main shaft of motor 5, and the second transmission wheel 7 is connected with the first transmission wheel 6 on the fuselage assembly 4 by transmission belt 8, and the diameter of the first transmission wheel 6 is less than the diameter of the second transmission wheel 7. diameter, forming a variable speed structure. The main shaft of the motor 5 drives the second transmission wheel...

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Abstract

The invention discloses an unmanned aerial vehicle fuselage running-in platform. The unmanned aerial vehicle fuselage running-in platform comprises a base, a machine platform mounted on the base and an electromotor mounted on any side portion of the machine platform. A fuselage assembly of an unmanned aerial vehicle is installed on the other side portion of the machine platform. A first transmission wheel on the fuselage assembly is connected to the electromotor through a transmission mechanism, and the electromotor drives the first transmission wheel to rotate to simulate the rotating speed of an engine of the unmanned aerial vehicle. An unmanned aerial vehicle fuselage after being assembled is fixed to the running-in platform, the first transmission wheel on the fuselage assembly is driven by the electromotor on the platform, the engine used in actual working of the unmanned aerial vehicle is replaced, and the actual working condition of the unmanned aerial vehicle is simulated, so that manpower required for running-in of a new unmanned aerial vehicle can be greatly reduced, and the entire running-in process can be completed indoors without being affected by weather factors; andmeanwhile, one person can simultaneously perform running-in of multiple unmanned aerial vehicle fuselages, the situation that one person operates one machine is not required, and the production efficiency is greatly improved.

Description

technical field [0001] The invention relates to the field of drones, in particular to the technical field of running-in of drone fuselages. Background technique [0002] Plant protection UAVs have many advantages such as low cost, low loss, zero casualties, reusability and high mobility, and play a huge role in agriculture, such as: sowing, spraying, insect control, etc. [0003] After the assembly of the UAV fuselage is completed, it needs to be run-in for a specified period of time, so that the aircraft can reach the ideal working condition before leaving the factory. The existing traditional UAV milling method is that after the assembly of the whole machine is completed, the UAV pilot actually controls it on the flight site and runs it on site. The disadvantage is that the production efficiency is limited by the number of pilots, and one aircraft must be controlled by one pilot; and due to external weather effects, it is impossible to perform run-in flights in bad weathe...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 王凭慧沈伟龚昊韩松
Owner FEIRUI AVIATION SCI & TECH JIANGSU
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