航空电力推进试验台的振动分析,具有主动主旋转器的试验台
Rafał Kliza1, Mirosław Wendeker2, Paweł Drozd1
1Department of Technology Fundamentals, Faculty of Production Engineering, University of Life Sciences in Lublin, 13 Akademicka Street, 20-950 Lublin, Poland.
Sensors (Basel, Switzerland)
|November 13, 2025
概括
这项研究分析了直升机转子测试台的振动,重点关注电动推进系统.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 振动分析 振动分析
背景情况:
- 直升机转子测试站需要精确的动态响应分析.
- 旋翼飞机中的电推进系统容易受到振动引起的问题.
- 复合转子叶片与形状记忆合金 (SMA) 执行器引入复杂的动力学.
研究的目的:
- 为了研究电机转速和攻击角 (AoA) 对直升机旋转机测试台电推进系统振动响应的影响.
- 识别主导的振动频率及其来源,包括转子波和SMA激活.
- 对旋翼飞机驱动系统的军事标准进行振动水平的评估.
主要方法:
- 使用三轴压电加速度计系统进行结构振动测量.
- 采用高分辨率数据采集用于时间同步的动态响应记录.
- 应用快速里埃转换 (FFT) 和功率光谱密度 (PSD) 分析到频域数据.
主要成果:
- 在16°攻击角度 (AoA) 记录了最高的振动幅度.
- 确定了与旋转波和形状记忆合金 (SMA) 激活相关的主导频率.
- 所有测量的振动水平都符合旋翼飞机驱动系统的MIL-STD-810H标准.
结论:
- 基于传感器的诊断对于在动态负载下评估机电推进系统至关重要.
- 诸如电机转速和AoA之类的操作参数显著影响系统振动.
- 经过测试的旋转机测试台设计在指定的范围内显示了可接受的振动性能.
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