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Measuring device for structure transfer characteristics of unmanned aerial vehicle and unmanned aerial vehicle

A measurement device and technology of transfer characteristics, applied in the field of unmanned aerial vehicles, can solve the problems of unmanned aerial vehicle application matching, unsuitable measurement, large quality, etc., and achieve the effects of low cost, low weight and low delay

Inactive Publication Date: 2021-06-18
BEIJING SANKUAI ONLINE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The first purpose of the present disclosure is to provide a measuring device for the structural transfer characteristics of UAVs. The measuring device can solve the problem that the current measuring devices for the structural transfer characteristics use ground equipment, which has a large mass and cannot match the application of UAVs; and uses The wired method cannot be applied to the measurement of the UAV flight process

Method used

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  • Measuring device for structure transfer characteristics of unmanned aerial vehicle and unmanned aerial vehicle
  • Measuring device for structure transfer characteristics of unmanned aerial vehicle and unmanned aerial vehicle
  • Measuring device for structure transfer characteristics of unmanned aerial vehicle and unmanned aerial vehicle

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Embodiment approach

[0040] According to an embodiment of the present disclosure, the electrical signal transmission component 300 can be FPC (Flexible Printed Circuit), FFC (Flexible Flat Cable) or coaxial cable, all of which are made of flexible materials and weigh It is light, and it is convenient to arrange the digital sensor 100 flexibly, greatly reducing the influence of the quality of the line.

[0041] combine Figure 1-Figure 3 , in a specific embodiment of the present disclosure, the size of the mounting carrier 200 can be designed to be 50mm·40mm·4mm, which is small enough and light enough for easy installation; the electrical signal transmission component 300 can be an FPC, and the weight of a single FPC can be about 2g; The digital sensor 100 can adopt the aforementioned MEMS sensor with relatively small weight; in this way, the mass of the entire measurement device can be less than 50g. In addition, the measurement device is installed on the fuselage of the UAV. According to its dis...

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Abstract

The invention relates to a measuring device for structure transfer characteristics of an unmanned aerial vehicle and the unmanned aerial vehicle. The measuring device comprises a plurality of digital sensors which are respectively fixed to a to-be-measured structure on a fuselage; an installation carrier, which is used for being detachably installed on the fuselage, wherein a processor is arranged on the installation carrier, and the processor is used for calculating the acceleration of the to-be-detected structure according to the vibration signals detected by the digital sensors; and an electric signal transmission assembly,which is made of a flexible material, connects the plurality of digital sensors to the mounting carrier and is electrically connected with a processor. Therefore, the vibration signals of the to-be-detected structure are detected through the digital sensors and transmitted to the processor through the electric signal transmission assembly for data analysis to obtain the acceleration of the to-be-detected structure, and the multiple digital sensors can obtain data at the same time so as to calculate the transfer function and the vibration characteristic of the structure. Therefore, vibration signals at any structural position of the unmanned aerial vehicle in a flight state can be independently acquired, and the digital sensors are flexibly distributed.

Description

technical field [0001] The present disclosure relates to the technical field of unmanned aerial vehicles, and in particular, relates to a measuring device for structural transfer characteristics of an unmanned aerial vehicle and an unmanned aerial vehicle. Background technique [0002] During the flight of the UAV, various vibrations and shocks will be generated due to the rotation of the propeller motor and the air flow. Long-term operation leads to structural fatigue and deterioration, and regular structural health inspections of UAVs are required. [0003] In related technologies, cargo drones lack the measurement method of structural transfer characteristics, while the structural health detection of civil aircraft is complicated and the detection device is large, which cannot match the application of drones. At present, the detection of conventional structures uses ground equipment, through wired To connect the sensor and the acquisition system by means of a 220V power ...

Claims

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Application Information

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IPC IPC(8): G01M7/02
CPCG01M7/025
Inventor 毛一年陆宏伟陈庆领高焓
Owner BEIJING SANKUAI ONLINE TECH CO LTD
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