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Experimental workbench for aircraft ram air micro-turbine generators

机译:飞机冲压空气微型涡轮发电机的实验工作台

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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.
机译:风力涡轮机实验台的实施对于在风力发电系统的受控条件下进行测试至关重要。这些系统的一个特殊情况是安装在飞机上的发电机。介绍了实验室级测试平台的设计,构造和测试。目的是开发一种用于研究,设计和验证小型无人机的风力涡轮机的设施。获得了基于节点分析的模型,该模型通过发电机实际升压电路的时间响应进行识别。通过静态,动态和风洞测试对模型进行了验证。事实证明,所获得的模型是控制系统设计的基础,该控制系统在操作范围内具有很高的性能。该测试台是为风洞测试以及所需的仪器和数据采集系统而开发的。数据处理和控制实现是在LabVIEW®中开发的。包括一些表明实验台有效性的结果。

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