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A digital mems-based strain gage for structural health monitoring

机译:基于数字MEMS的结构健康监测应变计

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One approach for structural health monitoring of aging aircraft is to take discrete airframe strain measurements and record the flight loads history. A complementary methhod consists of measuring changes in dynamic response due to fatigue crack growth. The challenge in implementing such methods is the need for inexpensive networks of distributed strain sensors which possess high resolution with no drift over time. The Uni-Axial Strain Transducer (UAST) has been developed as a digital, absolute encoding device to address these very issues. The UAST is a micro-electro-mechanical system (MEMS) which exploits the capacitive coupling between an array of electrostatic field emitters and an array of 64 field detectors on a CMOS IC chip. The slightly different array element sapcings form a vernier scale and digital signal processing of the detector outputs is used to calculate the absolute translational displacement of the emitter array relative to the CMOS detector chip. The UAST provides a dynamic range of 11,500 mu -strain and displacements of 2.5 nm are easily resolved. The sensor sampling rate is dynamically configurable for 150, 290, 540, 1000, 1600 or 2500 Hz, providing 15, 14, 13, 12, 11, or 10 bits of resolution (equal to 0.35, 0.7, 1.4, 2.8, 5.6, or 11.4 mu -strain), respectively. The sensor network can communicate with up to 128 UASTs on a common 5-wire digital bus, eliminating the need for shielding and considerably reducing the number of wires which will have to be routed through the airframe. A network technology demonstration is being conducted on a 1/2 scale F-18 vertical tail where dynamic loads are appleid to evaluate network performance related to monitoring of fatigue crack growth or rivet-line filures. Application of the UAST in a helicopter rotor health usage crack growth or rivet-line failures. Application of the UAST in a helicopter rotor health usage and monitoring system, and the design of a bi-axial transducer under development, are also mentioned.
机译:老化飞机结构健康监测的一种方法是采取离散机身应变测量并记录飞行负荷历史。互补的筛选者包括由于疲劳裂纹增长导致动态响应的变化。实施此类方法方面的挑战是需要具有高分辨率的分布式应变传感器的廉价网络,其随着时间的推移没有漂移。单轴应变换能器(UAST)已被开发为数字,绝对编码设备,以解决这些问题。 UAST是一种微机电系统(MEMS),其利用CMOS IC芯片上的静电场发射器和64个场检测器阵列之间的电容耦合。稍微不同的阵列元素皂状物形成vernier刻度,并且检测器输出的数字信号处理用于计算发射极阵列相对于CMOS检测器芯片的绝对平移位移。 UAST提供了11,500亩粒子的动态范围,并且容易解决2.5nm的位移。传感器采样率可动态可配置为150,290,540,1000,1600或2500 Hz,提供15,14,13,12,11或10位分辨率(等于0.35,0.7,1.4,2.8,5.6,分别为11.4亩粒子)。传感器网络可以在共同的5线数字总线上与最多128个无能为力通信,从而消除了对屏蔽的需求,并且显着减少必须通过机身布线的电线的数量。在一个1/2级F-18垂直尾部进行网络技术演示,其中动态载荷是AppleID,以评估与监测疲劳裂纹生长或铆钉线污垢相关的网络性能。 UAST在直升机转子健康用法裂纹生长或铆钉线故障中的应用。还提到了UAST在直升机转子卫生使用量和监测系统中的应用,以及在开发中的双轴传感器的设计。

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