| 光纤式航空发动机叶片边角振动测量系统 |
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| 引用本文： | 周雷,张承,司淑平.光纤式航空发动机叶片边角振动测量系统[J].中国电子科学研究院学报,2007,2(2):169-172. |
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| 作者姓名： | 周雷 张承 司淑平 |
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| 作者单位： | 中国电子科技集团公司第8研究所,安徽淮南,232001;中国电子科技集团公司第8研究所,安徽淮南,232001;中国电子科技集团公司第8研究所,安徽淮南,232001 |
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| 摘 要： | "光纤式航空发动机叶片边角振动测量系统"用于将航空发动机多达44路的测试信号通过光纤传输.该系统具有非接触、传输速率高、抗干扰能力强和信号质量好等优点,很好地解决了发动机参数测试问题.介绍了系统的测试原理,所要解决的关键技术,以及最终获得的研究成果等.
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| 关 键 词： | 非接触 高传输速率 多路传输 |
| 文章编号： | 1673-5692（2007）02-169-04 |
| 修稿时间： | 2007-01-30 |
Optical Fiber Edge Vibration Measurement System for Aircraft Engine Blades |
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| ZHOU Lei,ZHANG Cheng,SI Shu-ping.Optical Fiber Edge Vibration Measurement System for Aircraft Engine Blades[J].Journal of China Academy of Electronics and Information Technology,2007,2(2):169-172. |
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| Authors: | ZHOU Lei ZHANG Cheng SI Shu-ping |
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| Affiliation: | The 8th Research Institute of CETC,Anhui Huainan 232001,China |
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| Abstract: | The optical fiber edge vibration measurement system for aircraft engine blades developed by our institute is used for transmission testing signals of aircraft engine up to 44 channels through optical fiber.It has many advantages,such as non-contact,high transmission rate,strong anti-interference capability,and good signal quality,so the problem of parameters testing for aircraft engine is well solved.Finally,the testing principle of system,key technologies to be resolved,and research achievements are presented. |
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| Keywords: | non-contact high transmission rate multi-channel transmission |
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