在空气液压系统中的圆型门的稳定性分析和降噪
Wenjie Chen1,2, Yong Chen3, Yongxiang Xu2
1Commercial Aircraft Corporation of China, Shanghai, China.
Scientific reports
|January 7, 2026
概括
优化飞机转向控制孔可显著降低噪音. 匹配返回和入口孔的大小可以提高卷轴的稳定性,减少振动引起的噪音,改善驾驶声学.
科学领域:
- 航空航天工程 航空航天工程
- 声学 声学 在声学方面
- 流体动力学 流体动力学
背景情况:
- 飞机的转向控制系统会产生宽带噪声.
- 门组装动态,特别是卷轴行为,对于噪音产生至关重要.
- 了解流体力量是减轻噪声的关键.
研究的目的:
- 调查来自飞机转向控制的宽带噪声.
- 开发和验证一个非线性线圈动态模型.
- 确定减少噪音的设计参数.
主要方法:
- 建立了一个非线性卷轴动力学模型与合的流体力.
- 使用AMESim模拟和实验测试验证该模型.
- 分析了返回孔大小对门稳定性的影响.
主要成果:
- 揭示了返回孔大小和圆型门稳定性之间的关键相互作用.
- 证明了最佳的孔匹配可以提高卷轴的稳定性.
- 实现了压力波动和振动引起的噪音的显著降低.
结论:
- 优化的孔径尺寸为噪音控制提供了实用的解决方案.
- 在实验室测试中,总体声压水平 (OSPL) 降低了超过10 dB (A).
- 在飞机上测试中实现了超过20dB (A) 的峰值降噪,有助于实现"静音驾驶"目标.
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