角动量流量计的响应和流量特征
Hao Zan1,2, Qiusheng Jia3, Chengli Liu4
1Ningbo Institute, Northwestern Polytechnical University, Ningbo 315103, China.
Sensors (Basel, Switzerland)
|November 13, 2025
概括
这项研究可视化了用于航空燃料测量的角动量流量计动态. 它揭示了三种流量模式,以及弹配置如何提高测量极限和稳定性.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 机械工程 机械工程
背景情况:
- 准确的航空燃料流量测量对于商业飞行安全和效率至关重要.
- 现有的流量计在动态响应和测量范围方面面临挑战.
- 角动量流量计提供了一个潜在的解决方案,但需要详细的操作理解.
研究的目的:
- 设计一个可视化平台,用于观察角度运动量流量计中的内部组件动态.
- 为了模拟旋转器的动态旋转,并在不同的流量条件下计算偏移角度.
- 阐明操作机制,并确定结构优化的领域.
主要方法:
- 采用了滑动网格方法与角动量算法相结合,用于动态模拟.
- 开发了一个可视化平台来观察组件响应.
- 进行实验分析,根据弹的行为对流动模式进行分类.
主要成果:
- 根据弹反应,确定了三种流量模式:前弹,单弹和双弹.
- 观察到稳定的上游旋转器旋转速度为1.1rad/s,流量为0.091kg/s.
- 证明平弹配置通过分散二次流来提高测量极限和高压区稳定性.
结论:
- 该研究提供了对角动量流量计操作机制的清晰理解.
- 平弹设计通过延长下限测量和稳定操作来提高性能.
- 这些发现为未来这些流量计的结构优化提供了理论基础.
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