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Structural Health Monitoring Technology for Aerospace Composite Propellant Tank

机译:航天复合推进剂罐结构健康监测技术

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In this paper the experimental activities that were performed at Thales Alenia Space (TAS-I) System, Turin, Italy by Acellent Technologies Inc is presented. The final objective was defining a Vehicle / Vehicle Subsystem, built-in Health Management System which embeds self diagnosis and prognosis functions. Under this program a Composite Overwrapped Pressure Vessel (COPV) for space applications was monitored under pressure cycling (mechanical loading). The subscale demonstrator consisted of an aluminium metallic liner over wrapped by a CFRP layer. The metallic liner is seamless and manufactured by spin-forming. The liner material is aluminum AA6061 T6, with Yield Strength of 286 MPa, as declared by the bottle supplier (US Hydrospin); expected elongation to rupture is around 10%. The test was conducted for 3 days on a water filled COPV and at the end of three days the metal liner inside the propellant tank was cracked and caused water leakage. Acellent used a statistical data interpretation technique via feature extraction and data modeling approach to demonstrate that the system was able to generate the early alarm and also capable of localizing the damage which appeared at two hot spot locations.
机译:本文介绍了由Acellent Technologies Inc在意大利都灵的Thales Alenia Space(TAS-I)系统进行的实验活动。最终目标是定义一个内置了自我诊断和预后功能的内置健康管理系统的“车辆/车辆子系统”。在该程序下,在压力循环(机械负载)下监控了用于太空应用的复合式包裹压力容器(COPV)。超小型示威器由覆盖有CFRP层的铝制金属衬里组成。金属衬里是无缝的,并通过旋压成型制造。衬里材料为铝AA6061 T6,屈服强度为286 MPa,如瓶供应商所声明(美国Hydrospin);预期断裂伸长率约为10%。在充满水的COPV上进行了3天的测试,三天后,推进剂罐内的金属衬里破裂并导致漏水。 Acellent通过特征提取和数据建模方法使用了统计数据解释技术,以证明该系统既可以生成早期警报,又可以定位出现在两个热点位置的损坏。

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