基于单片机的样机飞机噪声监测系统设计

International Journal of Advanced Technology in Mechanical, Mechatronics and Materials Pub Date : 2021-11-18 DOI:10.37869/ijatec.v2i2.49

A. Ridwan, Triyanto Pangaribowo

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引用次数: 0

摘要

本文介绍了一种基于单片机的飞机噪声监测系统的设计。该系统用于监测噪声水平，使其更容易分析和测量可远程访问的噪声。测量结果通过带有IP地址访问(互联网协议)的浏览器从本地服务器esp32和OLED 0.96 inc.访问。飞机噪声源包括辅助动力装置(APU)、双包开启和发动机驱动，以每1秒采样一次的方式取10秒噪声值。噪声值分别为61.5 dB、75.6 dB和82.5 dB。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Design of Prototype Aircraft Noise Monitoring System Using Microcontroller

This paper was presented a design of aircraft noise monitoring system using microcontroller. This system is for monitoring noise levels to make it easier to analyze and measure noise that can be accessed remotely. The measurement results are accessed through a browser with IP address access (Internet Protocol) from the local server esp32 and also OLED 0.96 inc. Taking the noise value for 10 seconds with data samples every 1 second with aircraft noise sources consisting of APU (Auxiliary Power Unit), dual pack on and engine motoring. With each noise value of 61.5 dB, 75.6 dB and 82.5 dB.

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International Journal of Advanced Technology in Mechanical, Mechatronics and Materials

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