Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance
文献类型：期刊论文
| 作者 | Fengtong ZHAO2; Xiaodong JING2; Mingsui YANG3; Deyou WANG1; Yundong SHA1; Xiaochi LUAN1 |
| 刊名 | Chinese Journal of Aeronautics
 |
| 出版日期 | 2020 |
| 卷号 | 33期号:3页码:870-878 |
| 关键词 | Motor vehicles. Aeronautics. Astronautics TL1-4050 |
| ISSN号 | 1000-9361 |
| 其他题名 | Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance |
| 英文摘要 | Rotor blades fault of aeroengine compressor is mostly caused by mechanical and aerodynamic excitation. And the excitation factor of high intensity sound wave to rotor blades should not be ignored. Experimental researches are conducted on a multistage high pressure compressor. When high level vibration occurs on the first stage of rotor blades, the noise spectrum presents typical characteristic for discrete multi-tone in the compressor. The amplitude of blade vibration displacement and the sound pressure level of characteristic frequency noise increases and decreases simultaneously and reaches the maximum value at the same time. This frequency merely occur on a certain speed range and is locked in a specific range which presents no variation with the rotating speed. When high level vibration occurs on the first stage of rotor blades, the noise spectrum presents a sharp peak and the propagation state of the characteristic frequency is a helix structure in the compressor. It can be confirmed that acoustic resonance occurs in the multistage compressor. The acoustic resonance frequency and its side band frequencies are generated by modulation of a rotating noise source at the rotor speed which is the excitation source of the rotor blades vibration. Keywords: Acoustic resonance, Blades vibration, Characteristic frequency, Multistage compressor, Source identification |
| 资助项目 | [National Natural Science Foundation of China] ; [Aeronautical Science Foundation of China] |
| 语种 | 英语 |
| CSCD记录号 | CSCD:6693914 |
| 源URL | [http://ir.imr.ac.cn/handle/321006/87166]  |
| 专题 | 金属研究所_中国科学院金属研究所 |
| 作者单位 | 1.Liaoning Province Key Laboratory of Advanced Measurement And Test Technology of Aviation Propulsion Systems,Shenyang Aerospace University 2.School of Energy and Power Engineering,Beihang University 3.中国科学院金属研究所 |
| 推荐引用方式 GB/T 7714 | Fengtong ZHAO,Xiaodong JING,Mingsui YANG,et al. Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance[J]. Chinese Journal of Aeronautics,2020,33(3):870-878. |
| APA | Fengtong ZHAO,Xiaodong JING,Mingsui YANG,Deyou WANG,Yundong SHA,&Xiaochi LUAN.(2020).Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance.Chinese Journal of Aeronautics,33(3),870-878. |
| MLA | Fengtong ZHAO,et al."Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance".Chinese Journal of Aeronautics 33.3(2020):870-878. |
入库方式： OAI收割
来源：金属研究所
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