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Dynamic test optimization device of rotor wing unmanned aerial vehicle and duct unmanned aerial vehicle as well as optimization method thereof

A technology of unmanned rotor and optimized device, applied in the field of unmanned aerial vehicle, can solve the problems of single transmission movement, large friction force, inability to transmit tensile force and torsion force at the same time, and achieve the effect of eliminating the simple structure

Active Publication Date: 2019-02-22
武汉卓尔无人机制造有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These rotary-wing UAVs and ducted UAV power test optimization devices have a single transmission motion, cannot transmit pulling force and torsion at the same time, and the friction force is large during transmission. The computer is slow in calculating data and cannot achieve real-time response. Dynamic testing The work energy consumption during calculation is also very large

Method used

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  • Dynamic test optimization device of rotor wing unmanned aerial vehicle and duct unmanned aerial vehicle as well as optimization method thereof
  • Dynamic test optimization device of rotor wing unmanned aerial vehicle and duct unmanned aerial vehicle as well as optimization method thereof
  • Dynamic test optimization device of rotor wing unmanned aerial vehicle and duct unmanned aerial vehicle as well as optimization method thereof

Examples

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Embodiment

[0021] Example: A power test optimization device for rotary-wing drones and ducted drones of the present invention includes a computer, a connector 1, an optical axis 2, two linear rotary bearings 3, two bolt rolling bearings 7, and a tension pressure sensor 13 The torsion sensor 16, the connecting sleeve 8, and the connecting plate 4. The tension and pressure sensor 13 and the torsion sensor 16 are both connected to the computer via a wireless network, and a first flat pad 18 is installed inside the connector 1, and the optical axis 2 One end is installed in the socket of the first flat washer 18 and fixed by the first screw 19 and the first nut 20. The connecting sleeve 8 and the two linear rotation bearings 3 are both installed on the optical shaft 2. The connecting sleeve 8 is located between the two linear rotary bearings 3, the outer wall of one end of the connecting sleeve 8 is provided with a connecting sleeve side plate 25, and the bottom of the two side plates of the c...

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Abstract

The invention discloses a dynamic test optimization device of a rotor wing unmanned aerial vehicle and a duct unmanned aerial vehicle as well as an optimization method thereof, comprising a computer,a connecting head, an optical shaft, two linear rotary bearings, two bolt rolling bearings, a tension and pressure sensor, a torque sensor, a connecting sleeve, a connecting plate, etc. The dynamic test optimization device of the rotor wing unmanned aerial vehicle and the duct unmanned aerial vehicle as well as the optimization method thereof provided by the invention has the following beneficialeffects: the delivery movement and force of a mechanism are effectively combined so as to eliminate the defects of simple structure, single drive and great friction resistance of a traditional conduction mechanism; for the dynamic test equipment of the rotor wing unmanned aerial vehicle and the duct unmanned aerial vehicle deployed in a complex outdoor environment, the invention can reduce the energy consumption and prolong the working service life of these sensors so as to complete the conduction of the movement and force in high quality.

Description

Technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a power test and optimization device for rotary wing unmanned aerial vehicles and ducted unmanned aerial vehicles and an optimization method thereof. Background technique [0002] According to the flight platform configuration, drones can be divided into fixed-wing drones, rotary-wing drones, unmanned airships, para-wing drones, and flapping-wing drones. The value of unmanned aerial vehicles is to replace humans in completing aerial operations. The most direct driving factors for its development mainly come from two aspects: (1) reducing direct personnel input and coping with extreme conditions; (2) scientific research and industry, through the use of unmanned Machine to complete the job quickly and efficiently. Therefore, the current UAVs are widely used in aerial photography, exploration, surveying and mapping, sampling, transportation, military monitoring, power i...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 欧阳星徐强霍甜田云张文祺
Owner 武汉卓尔无人机制造有限公司
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