| 高声强声场模拟装置设计与声试验1/3倍频程控制技术研究 |
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| 引用本文： | 刘大志,朱子宏,张俊刚,晏廷飞,向树红.高声强声场模拟装置设计与声试验1/3倍频程控制技术研究[J].航天器环境工程,2016,33(3):312-315. |
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| 作者姓名： | 刘大志 朱子宏 张俊刚 晏廷飞 向树红 |
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| 作者单位： | 北京卫星环境工程研究所, 北京 100094 |
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| 摘 要： | 为了提高混响室声场模拟能力,北京卫星环境工程研究所自研一套高声强声场模拟试验设备。文章介绍了该设备的行波管发声系统设计和消声降噪处理过程——行波终端设计以及声试验控制仪器的原理。经过调试试验验证,测量结果满足声压级165 d B行波声场的要求,行波管试验段性能良好,达到167.9 d B,消声道出口噪声能够满足环境模拟需求。
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| 关 键 词： | 高声强声场 行波管 1/3倍频程 消声降噪 |
| 收稿时间： | 2015/9/22 0:00:00 |
| 修稿时间： | 2016/5/14 0:00:00 |
Design of high-intensity acoustic field simulator and 1/3 octave band control for acoustic test |
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| Liu Dazhi,Zhu Zihong,Zhang Jungang,Yan Tingfei,Xiang Shuhong.Design of high-intensity acoustic field simulator and 1/3 octave band control for acoustic test[J].Spacecraft Environment Engineering,2016,33(3):312-315. |
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| Authors: | Liu Dazhi Zhu Zihong Zhang Jungang Yan Tingfei Xiang Shuhong |
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| Institution: | Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China |
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| Abstract: | A high intensity acoustic test system designed by BISEE is presented in this paper, including the acoustic design, the anechoic approach and the noise elimination, and the development of a closed-loop acoustic control system. The test results show that with the overall sound power level of 165 dB, the TWT performs well, and the noise at the end of the exhaust flow meets the environmental requirements. |
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| Keywords: | high intensity acoustic field traveling wave tube 1/3 octave band noise elimination |
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