主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
对转螺旋桨气动噪声试验系统设计与试验研究
作者:
作者单位:

1.中国飞机强度研究所 强度与结构完整性全国重点实验室;2.陕西飞机工业有限责任公司 研发中心

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中图分类号:

V231.3

基金项目:

工信部资助课题


Aeroacoustic Test System Design and Experimental Research for Counter-rotating Propeller
Author:
Affiliation:

National Key Laboratory of Strength and Structural Integrity,Aircraft Strength Research Institute of China,Xi,an

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    摘要:

    当前风洞内对转螺旋桨气动噪声试验具有时间协调难、成本高的问题,依托地面声学环境,研制能够模拟对转螺旋桨地面开车状态的对转螺旋桨气动噪声试验系统。对某穿孔结构的对转螺旋桨和基准桨开展气动噪声试验,对试验系统进行验证并对穿孔结构对转螺旋桨的降噪效果进行评估。结果表明:在所测试的工况范围内,穿孔结构对转螺旋桨可以在保证气动性能的前提下有效降低噪声;在对飞机舱内影响最显著的90°指向角处,二阶通过频率处降噪量达5 dB。本文设计的气动噪声试验系统,能够为对转螺旋桨气动噪声评估和降噪设计提供帮助。

    Abstract:

    Aiming at the problems of difficult time coordination and high cost of the aerodynamic noise test of counter-rotating propellers in wind tunnels, the aerodynamic noise test system of counter-rotating propellers, which is capable of simulating the driving state of counter-rotating propellers on the ground, has been developed by relying on the acoustic environment of the ground. The aerodynamic noise test was carried out on a perforated counter-rotating propeller and a reference propeller to validate the test system and evaluate the noise reduction effect of the perforated counter-rotating propeller, and the results show that the perforated counter-rotating propeller can effectively reduce the noise under the prerequisite of guaranteeing the aerodynamic performance in the range of the tested working conditions. In the 90° pointing angle, which has the most significant effect on the aircraft cabin, the noise reduction at the second-order passing frequency reaches 5dB.The designed aerodynamic noise test system can provide assistance for the evaluation of aerodynamic noise of the rotary propeller and the design of noise reduction.

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引用本文

曹琦,卫凯,聂彦平,燕群,陈永辉.对转螺旋桨气动噪声试验系统设计与试验研究[J].航空工程进展,2024,15(5):148-154

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历史
  • 收稿日期:2023-11-23
  • 最后修改日期:2024-01-12
  • 录用日期:2024-01-28
  • 在线发布日期: 2024-09-02
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