徐志刚,陈荣,李权,姚起杭.某型飞机进气道在噪声环境中的振动疲劳分析[J].装备环境工程,2011,8(4):100-103. XV Zhi-gang,CHEN Rong,LI Quan,YAO Qi-hang.Vibration Fatigue Analysis of Plane Inlet Channel under Noise Environment[J].Equipment Environmental Engineering,2011,8(4):100-103.
某型飞机进气道在噪声环境中的振动疲劳分析
Vibration Fatigue Analysis of Plane Inlet Channel under Noise Environment
投稿时间:2011-01-21  修订日期:2011-08-15
DOI:
中文关键词:  噪声激振  振动疲劳  阻尼层
英文关键词:noise excitation  vibration fatigue  damping layer
基金项目:
作者单位
徐志刚 北京航空工程技术研究中心,北京 100076 
陈荣 北京航空工程技术研究中心,北京 100076 
李权 北京航空工程技术研究中心,北京 100076 
姚起杭 西北工业大学,西安 710076 
AuthorInstitution
XV Zhi-gang Beijing Aeronautical Engineering Technology Research Centre, Beijing 100076, China 
CHEN Rong Beijing Aeronautical Engineering Technology Research Centre, Beijing 100076, China 
LI Quan Beijing Aeronautical Engineering Technology Research Centre, Beijing 100076, China 
YAO Qi-hang Northwestern Polytechnic University, Xi′ an 710076, China 
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中文摘要:
      某型飞机进气道常出现蒙皮裂纹、 铆钉松动及掉铆钉头等故障, 给飞行安全带来隐患。研究发现, 此类故障是进气道在强噪声环境下,噪声脉动压力引起的结构振动疲劳损伤。应用阻尼层可降低强噪声对进气道蒙皮和铆钉的破坏。发动机地面试验结果表明, 进气道阻尼层的应用显著降低了蒙皮壁板的振动量级。
英文摘要:
      Failures usually appeared in inlet channel of certain plane such as skin cracking, rivet loosing and rivet head broking, which are becoming incipient fault of flight safety. Research results showed that the failure is structure vibration fatigue damage caused by pulsating noise pressure in intense noise environment. Application of damping layer can lower the influence of intense noise on skin and rivet. Ground experiment results of engine showed that application of the damping layer has lowered vibration level of the inlet channel skin obviously.
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