首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES
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RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES

机译:飞机复合结构结构健康监测技术的最新进展

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Advanced composites including carbon fiber reinforced plastic (CFRP) are extensively being used in recent aircraft structures due to a strong demand for high efficiency and reasonable affordability. However, inspection and maintenance of CFRP structures are of concern to the safety of new aircraft. The damage in operation can be more complicated in CFRP structures than in conventional metallic ones. Efficient inspection and maintenance procedure of aircraft CFRP structures has been highly demanded using structural health monitoring (SHM) technologies under development.In Japan, we have been developing optical fiber based SHM technologies in recent industry-university collaboration programs. After some important fundamental developments, such as small-diameter optical fiber sensors for embedment in CFRP structures without introducing any deterioration, we are now applying to sub-component structure prototypes. This presentation provides some recent development of optical fiber based SHM technologies for near-future aircraft composite structures.
机译:由于对高效和合理价格的强烈需求,包括碳纤维增强塑料(CFRP)在内的先进复合材料已广泛用于新型飞机结构中。但是,CFRP结构的检查和维护与新飞机的安全有关。与传统的金属结构相比,CFRP结构的运行中的损坏可能更为复杂。使用正在开发的结构健康监测(SHM)技术,对飞机CFRP结构的有效检查和维护程序提出了很高的要求。 在日本,我们最近的产学合作计划中一直在开发基于光纤的SHM技术。在进行了一些重要的基础开发之后,例如将小直径光纤传感器嵌入CFRP结构中而不会引起任何劣化,我们现在将其应用于子组件结构原型。本演示文稿提供了用于近期飞机复合结构的基于光纤的SHM技术的一些最新进展。

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