螺旋桨飞机风洞试验动力参数实时监测系统
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Real-time Monitoring System for Dynamic Parameters of Propeller Aircraft in Wind Tunnel Test
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    摘要:

    针对螺旋桨带动力试验系统地面调试问题,设计一种螺旋桨动力参数实时监测系统。利用NI便携式数采系统测量螺旋桨天平信号,通过创建虚拟仪器数据采集任务和表格化天平公式,实时获得螺旋桨的拉力和扭矩等动力参数;在地面调试时,通过获取实测螺旋桨动力参数,可实时掌握当前螺旋桨在不同桨叶角、转速工况下的负载特性,结合对驱动器参数的监测获取电机出力性能。结果表明:在风洞试验时,该系统作为备份的快捷测试手段,可帮助快速排除或定位数据测试方面的问题。

    Abstract:

    A real-time monitoring system for propeller dynamic parameters is designed to solve the ground debugging problem of propeller with power test system. The signal of propeller balance is measured by NI portable data acquisition system, and the dynamic parameters of propeller, such as tension and torque, are obtained in real time by creating virtual instrument data acquisition tasks and tabulating balance formulas; During ground debugging, the load characteristics of the current propeller under different blade angles and rotating speeds can be grasped in real time by obtaining the measured propeller dynamic parameters, and the motor output performance can be obtained by monitoring the driver parameters. The results show that the system can be used as a backup and quick test means to help quickly eliminate or locate data test problems in wind tunnel tests.

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顾 艺.螺旋桨飞机风洞试验动力参数实时监测系统[J].,2026,45(02).

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  • 收稿日期:2024-11-16
  • 最后修改日期:2024-12-20
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  • 在线发布日期: 2026-03-13
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