Acoustic Emission Detection and Location for Hypervelocity Impacts
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摘要: 当高速运行的空间碎片撞击到在轨运行的航天器时,会对结构产生损伤,如果能够判断撞击的位置及产生损伤的严重程度,就可以及时采取相应的措施保证航天器和航天员的安全。通过利用高速弹丸撞击铝板产生的损伤模拟上述撞击,采用声发射检测技术,对撞击事件的定位进行了探索。在试验过程中,采集弹丸高速撞击铝板产生的撞击信号,并对应力波到达各个声发射传感器的时差进行分析,通过二维矩形平面定位算法,对损伤部位进行了初步定位。试验结果表明,声发射在撞击源定位方面具有适用性。Abstract: There is already so much space debris in low orbits that it poses a significant threat to satellites and other spacecrafts in orbit. The satellites and the spacecrafts will lose their functions when space debris impacts on the key parts of them. Hypervelocity impacts on aluminum plates are utilized to simulate the impacts resulted from space debris. Acoustic emission (AE) analysis is used for characterization and location for hypervelocity Impacts. Two different Acoustic Emission (AE) sensors are used to detect the arrival time and signals of the hits. Hypervelocity Impacts are generated with a two-stage light-gas gun firing small aluminum ball projectiles(3.97 mm, 6.35 mm). In the impact studies, the results make clears that the location obtained by the resonant R15 sensors are as excellently accurate to these obtained by wideband sensors. The multi-source impact simultaneously is observed during the impacts in that it is difficult for the current conventional localized-algorithm to locate the sources.
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Keywords:
- Acoustic emission testing /
- Space debris /
- Hypervelocity impact /
- Localization
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[1] Frank Schafer, Rolf Janovsky. Impact sensor network for detecting of hypervelocity impacts on spacecraft[C]. 55th International Astronautical Congress. Vancouver, Canada: 2004. [2] Willian H Prosser, Michael R Gorman, Donald H Humes. Acoustic emission signals in thin plates produced by Impact Damage[J]. Journal of Acoustic Emission,1999,17(1):29-36. [3] Graziani F, Porfilio M, Santoni F. An in situ impact sensor on board a UNISAT microsatellite for monitoring the microparticles environment[EB/OL]. [2005-06-27] http://techrepots.larc.nasa.gov. [4] 张 伟,庞宝君,贾 斌,等.弹丸超高速撞击防护屏碎片云数值模拟[J].高压物理学报,2004,18(1):47-52. [5] 张 伟,庞宝君,张泽华,等.航天器波纹防护屏高速撞击实验研究[J].宇航学报,2000,21(1):79-84. [6] 袁振明,任荣镇.飞机机翼疲劳试验的声发射检测[C].全国第二届声发射会议.桂林:1983. [7] 魏文慧.声发射技术在飞机部件疲劳试验中裂纹监测的应用[C].全国第二届声发射会议.桂林:1983. [8] 耿荣生,景 鹏,雷 洪,等.飞机主梁疲劳裂纹萌生声发射信号的识别方法[J].航空学报,1996,17(3):368-372. [9] 耿荣生,景 鹏,雷 洪,等.Prediction of Fatigue Crack Initiation of Aircraft Using AE[C].国际失效分析和预防会议论文集.北京:1995. [10] 杨明纬,耿荣生.国防科工委声发射无损检测培训教材[M].北京:机械工业出版社,2005. [11] 李家伟,陈积懋.无损检测手册[M].北京:机械工业出版社,2004. [12] Yajai Promboo. Acoustic Emission Source Location[D]. US: The University of Taxas at Austin,2000.
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