用于飞机起落架测试的嵌入式轮力传感器

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI:10.1109/METROAEROSPACE.2018.8453511

J. Pytka, J. Józwik, T. Łyszczyk, E. Gnapowski

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引用次数: 7

摘要

本文介绍了一种用于飞机起落架测试的车轮测功机系统。测功机的目的是测量作用在飞机起落架上的力和力矩。该测功机采用应变片作为自主测量装置，采用无线数据传输系统。提出的系统是为PZL 104 Wilga 35A多用途飞机设计的，但是它可以被重新设计用于任何其他通用航空轻型飞机。本文包含了设计和开发的详细描述以及早期测试测量的样本结果。提出的测功机系统已经考虑了飞机地面和飞行试验的认证。

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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Embedded Wheel Force Sensor for Aircraft Landing Gear Testing

The paper presents a wheel dynamometer system developed for testing aircraft landing gear. The purpose of the dynamometer is to measure forces and moments acting on an aircraft landing gear wheel. The dynamometer was designed with the use of strain gages, as an autonomous measuring device, with a wireless data transferring system. The presented system was designed for the PZL 104 Wilga 35A multipurpose aircraft, but it could be re-designed for any other general aviation, light aircraft. The paper contains detailed descriptions of the design and development as well as sample results from early test measurements. Certification for ground and flight tests of airplanes has been considered for the presented dynamometer system.

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2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)

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