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推力螺旋桨噪声试验
引用本文:周家检,郝璇,付增良,梁彬,周平.推力螺旋桨噪声试验[J].航空动力学报,2021,36(2):225-232.
作者姓名:周家检  郝璇  付增良  梁彬  周平
作者单位:中国航天科技集团有限公司中国航天空气动力技术研究院第二研究所,北京100074;中国空气动力研究与发展中心气动噪声控制重点实验室,四川绵阳621000;中国航天科技集团有限公司中国航天空气动力技术研究院第二研究所,北京100074
基金项目:气动噪声控制重点实验室研究基金(ANCL20200201)
摘    要:针对某推力螺旋桨开展了噪声测试,获得了定桨矩角、不同转速工况的螺旋桨噪声频谱特性和典型工况下的螺旋桨噪声辐射指向性,分析了螺旋桨噪声与转速、桨矩角的变化规律,以及螺旋桨的纯音噪声、宽频噪声和总噪声的辐射指向性。结果表明:随桨矩角和转速增大,宽频噪声在总噪声中占比增大,在大桨矩角、高转速下,宽频噪声强度已经与纯音噪声相当。宽频噪声辐射指向性与螺旋桨桨叶自噪声相符。 

关 键 词:推力螺旋桨  宽频噪声  纯音噪声  桨叶自噪声  辐射指向性
收稿时间:2020/7/6 0:00:00

Noise tests of pusher-propeller
ZHOU Jiajian,HAO Xuan,FU Zengliang,LIANG Bin,ZHOU Ping,HAO Xuan,FU Zengliang,LIANG Bin,ZHOU Ping.Noise tests of pusher-propeller[J].Journal of Aerospace Power,2021,36(2):225-232.
Authors:ZHOU Jiajian  HAO Xuan  FU Zengliang  LIANG Bin  ZHOU Ping  HAO Xuan  FU Zengliang  LIANG Bin  ZHOU Ping
Institution:1.The Second Institute,China Academy of Aerospace Aerodynamics,China Aerospace Science and Technology Corporation,Beijing 100074,China2.Key Laboratory of Aerodynamic Noise Control,China Aerodynamics Research and Development Center,Mianyang Sihcuan 621000,China
Abstract:The noise of a pusher-propeller was tested. The noise frequency spectrum characteristics of propeller at different revolution speeds with fixed pitch were obtained to research the noise level varying with revolution speed and pitch. The directivity characteristics at typical operating condition were also tested to get the directivity of tone noise, broadband noise and overall noise. The results showed that as the revolution speed and pitch increased, the contribution of broadband noise to overall noise increased. The broadband noise was comparable with the tone noise at large pitch and high revolution speed. The directivity of broadband noise agreed with the characteristics of blade self-noise. It is probable that the broadband noise is dominated by blade self-noise.
Keywords:pusher-propeller  broadband noise  tone noise  blade self-noise  directivity
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