复合材料结构的低功耗冲击区域监测方法
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    摘要:

    复合材料凭借优异性能而被广泛应用于民用飞机结构,但复合材料结构可能会因冲击而产生内部损伤并严重降低结构的性能。因此,以低功耗方法不间断地对飞行器复合材料结构进行冲击监测就显得尤为关键。面向机载提出了一种基于反向加权和的低功耗冲击区域定位算法,该算法基于数字化冲击监测原理,依据冲击响应数字序列进行冲击事件的区域定位。算法运算过程简单高效,便于通过嵌入式软件编程至核心处理器,并显著减少在核心处理器执行算法所需的功耗、时间和存储空间,有利于冲击监测系统的低功耗设计和应用。此外,将算法应用在低功耗小型化冲击监测系统中,并评估了冲击区域定位算法在复合材料机翼盒段结构上的准确率。评估结果显示,低功耗冲击区域监测方法可以准确的监测每次冲击事件,且冲击区域定位准确率达到了96%。

    Abstract:

    Composite materials are widely used in civil aircraft structures due to their excellent properties. But composite structures may be subjected to internal damages caused by impact events, which can seriously degrade the property of the structures. So, it is critical to continuously monitor the impact of aircraft composite structures with low power consumption method. In this paper, a low power impact region localization method based on reverse weighted sum is proposed for airborne. The method is based on the principle of digital impact monitoring and the impact region localization is carried out according to the impact response digital sequences. The method is simple and efficient, and it is easy to program to the processor through embedded software. The power consumption, time and storage space of the processor are significantly reduced, which is beneficial to the low power design and application of the impact monitoring system. In addition, the method is applied to a low power miniaturized impact monitoring system, and experiment is carried out to verify the accuracy of impact region localization on the composite wing box structure. The evaluation results show that the low power impact monitoring method can accurately monitor each impact event, and the location accuracy is up to 96%.

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林晓冬,邱雷,袁慎芳,等.复合材料结构的低功耗冲击区域监测方法[J].民用飞机设计与研 究,2020(4):63-68LIN Xiaodong, QIU Lei, YUAN Shenfang, et al.[J]. Civil Aircraft Design and Research,2020,(4):63-68. ( in Chinese)

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  • 在线发布日期: 2021-01-06
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