Experimental workbench for aircraft ram air micro-turbine generators

2017 IEEE International Autumn Meeting on Power, Electronics and Computing (ROPEC) Pub Date : 2017-11-01 DOI:10.1109/ROPEC.2017.8261673

J. A. Sanchez-Flores, J. Y. Gonzalez-Valdes, J. Liceaga-Castro, E. Licéaga-Castro, L. Amezquita-Brooks, O. Garcia-Salazar, D. Martinez-Vazquez

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引用次数: 1

Abstract

The implementation of experimental benches for wind turbines is fundamental for performing tests under controlled conditions of wind power generation systems. A particular case of these systems are the generators mounted on aircraft. The design, construction, and testing of a test bench at laboratory level is presented. The aim is to develop a facility for the study, design and validation of wind turbines for small unmanned aerial vehicles. A model based on the node analysis and its identification through the time response of the actual boost-circuit of the generator is obtained. The validation of the model was carried out through static, dynamic and wind tunnel tests. The model obtained proved to be fundamental for the design of a control system which rendered high performance in the range of operation. The test bench was developed for wind tunnel tests together with the required instrumentation and data adquisition system. The data processing and the control implementation was developed in LabVIEW®. Some results showing the effectivity of the experimental bench are included.

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飞机冲压空气微型涡轮发电机实验台

风力发电机试验台的建立是风力发电系统在受控条件下进行试验的基础。这些系统的一个特殊例子是安装在飞机上的发电机。介绍了实验室级试验台的设计、建造和测试。其目的是开发一个用于研究、设计和验证小型无人机风力涡轮机的设施。建立了基于节点分析和通过发电机实际升压回路时间响应识别的模型。通过静、动、风洞试验对模型进行了验证。所得到的模型为控制系统的设计奠定了基础，使控制系统在工作范围内具有较高的性能。研制了风洞试验台架，并配备了所需的仪器和数据采集系统。数据处理和控制实现在LabVIEW®中开发。最后给出了一些实验结果，证明了该实验平台的有效性。

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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2017 IEEE International Autumn Meeting on Power, Electronics and Computing (ROPEC)

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