Design of test system for large⁃scale propeller power simulation in wind tunnel

Hongsheng LEI; Zhengwu CHEN; Zheng WANG; Manfeng DOU; Yu ZHAO

doi:10.13224/j.cnki.jasp.20210191

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Design of test system for large⁃scale propeller power simulation in wind tunnel

Aerothermodynamics and Aeroengine Design | 更新时间：2025-04-07

- Design of test system for large⁃scale propeller power simulation in wind tunnel
- Journal of Aerospace Power Vol. 36, Issue 11, Pages: 2261-2270(2021)
- 作者机构：
  
  1.中国空气动力研究与发展中心低速空气动力研究所气动噪声控制重点实验室，四川绵阳 621000
  2.西北工业大学自动化学院，西安 710129
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210191
  CLC：
- 稿件说明：
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Hongsheng LEI, Zhengwu CHEN, Zheng WANG, et al. Design of test system for large⁃scale propeller power simulation in wind tunnel[J]. Journal of Aerospace Power, 2021, 36(11): 2261-2270.
DOI：

Hongsheng LEI, Zhengwu CHEN, Zheng WANG, et al. Design of test system for large⁃scale propeller power simulation in wind tunnel[J]. Journal of Aerospace Power, 2021, 36(11): 2261-2270. DOI： 10.13224/j.cnki.jasp.20210191.

摘要

以开展某型飞机螺旋桨气动力和气动噪声研究为目的，结合5.5 m×4 m航空声学风洞实际，设计了一套动力模拟试验系统。该系统以300 kW高功率密度永磁电动机为核心，通过配套相应的电源、驱动、控制、支撑等，实现了大尺度螺旋桨的动力模拟，并开展了相关试验验证。结果表明：该系统额定转速和转矩分别高达5 000 r/min和573

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、转速控制精度优于±0.5 r/min，且具有较低的自身噪声级和良好的电磁兼容性能，拉力系数试验重复性精度优于0.000 7等。该系统的建立能有效地满足大尺度飞机螺旋桨相关风洞试验研究的动力模拟需求，进一步拓展了国内低速空气动力学试验模拟能力。

Abstract

In order to study the aerodynamic and aeroacoustic properties of a certain type of aircraft propeller，a set of power simulation test system was designed in 5.5 m×4 m aeroacoustic wind tunnel.Taking the 300 kW high power density permanent magnet motor as the core，the system realized the power simulation of large⁃scale propeller by matching the corresponding power supply，drive，control，support and so on.Meanwhile the test verification was carried out.The results showed that the speed and torque of the equipment were as high as 5 000 r/m and 573 N·m respectively，and the speed control accuracy was better than ±0.5 r/min.And also it had low noise level and good electromagnetic compatibility，and the test repeatability accuracy was better than 0.000 7.The establishment of the system can effectively meet the requirements of the large⁃scale propeller power simulation and further expand the low⁃speed aerodynamic test simulation capabilities.

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references

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