飞机结构静力试验测量系统

2014 IEEE Metrology for Aerospace (MetroAeroSpace) Pub Date : 2014-05-29 DOI:10.1109/METROAEROSPACE.2014.6865927

Piotr Cieciński, J. Pieniążek, Lukasz Swiech

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引用次数: 3

摘要

本文介绍了一种用于记录电动滑翔机AOS-71(该滑翔机由Rzeszów和华沙理工大学设计)静态试验数据的测量系统。该试验是获得飞机适航性认可的一个证据部分。所述研究的特点是必须在较高温度下进行强度试验。

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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A measurement system for static test of airplane structure

The paper describes a measurement system made for registering data from the static tests of motor glider AOS-71 (the motor glider was designed in Rzeszów and Warsaw Universities of Technology). The experiment was an evidence part leading to obtaining the acceptance of the aircraft flight worthiness. The characteristic feature of the described studies was the necessity of running the strength tests in higher temperature.

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2014 IEEE Metrology for Aerospace (MetroAeroSpace)

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