在飞行测试中使用张力计传感器对直升机转子的空气动力学分析
Shuaike Jiao1, Jiahong Zheng1,2
1Chinese Flight Test Establishment, Xi'an 710089, China.
Sensors (Basel, Switzerland)
|April 28, 2025
概括
这项研究引入了一种新的方法,用于测量直升机转子在飞行过程中使用张力计的空气动力学负荷. 这种技术比传统的模拟和风洞方法提供了更准确的负载计算.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 应用物理 应用物理
背景情况:
- 准确的空气动力学负载数据对于直升机的设计和性能至关重要.
- 目前的模拟和风洞等方法在现实世界飞行条件下存在局限性.
研究的目的:
- 提出和验证一种用于测量直升机旋转机在飞行中的空气动力学负荷的新方法.
- 为了提高旋翼飞机空气动力学负载计算的准确性.
主要方法:
- 张力计传感器安装在旋翼叶片上的各种位置.
- 测量的应变被整合到刀片的运动方程中.
- 建立了空气动力学负载和动矩之间的关系,并用于计算.
主要成果:
- 提出的方法成功地测量了飞行期间旋转机的空气动力学负荷.
- 计算的负载分布与理论预测保持一致.
- 飞行测量技术比模拟和风洞测试更准确.
结论:
- 基于张力计的折叠时刻测量为确定旋转机空气动力学负载提供了更精确的方法.
- 这种方法为直升机旋翼叶片设计优化提供了有价值的数据.
- 飞行测量提高了对旋翼飞机空气动力学的理解.
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