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SOI 技术中的稳健压力传感器,具有用于翼型集成的蝶形布线。

Robust Pressure Sensor in SOI Technology with Butterfly Wiring for Airfoil Integration.

机构信息

Institute of Microtechnology, TU Braunschweig, 38124 Brunswick, Germany.

Institute of Sensor and Actuator Systems, TU Wien, 1040 Vienna, Austria.

出版信息

Sensors (Basel). 2021 Sep 13;21(18):6140. doi: 10.3390/s21186140.

DOI:10.3390/s21186140
PMID:34577355
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC8473241/
Abstract

Current research in the field of aviation considers actively controlled high-lift structures for future civil airplanes. Therefore, pressure data must be acquired from the airfoil surface without influencing the flow due to sensor application. For experiments in the wind and water tunnel, as well as for the actual application, the requirements for the quality of the airfoil surface are demanding. Consequently, a new class of sensors is required, which can be flush-integrated into the airfoil surface, may be used under wet conditions-even under water-and should withstand the harsh environment of a high-lift scenario. A new miniature silicon on insulator (SOI)-based MEMS pressure sensor, which allows integration into airfoils in a flip-chip configuration, is presented. An internal, highly doped silicon wiring with "butterfly" geometry combined with through glass via (TGV) technology enables a watertight and application-suitable chip-scale-package (CSP). The chips were produced by reliable batch microfabrication including femtosecond laser processes at the wafer-level. Sensor characterization demonstrates a high resolution of 38 mVV bar. The stepless ultra-smooth and electrically passivated sensor surface can be coated with thin surface protection layers to further enhance robustness against harsh environments. Accordingly, protective coatings of amorphous hydrogenated silicon nitride (a-SiN:H) and amorphous hydrogenated silicon carbide (a-SiC:H) were investigated in experiments simulating environments with high-velocity impacting particles. Topographic damage quantification demonstrates the superior robustness of a-SiC:H coatings and validates their applicability to future sensors.

摘要

目前,航空领域的研究积极考虑为未来的民用飞机采用主动控制的高升力结构。因此,必须在不影响流动的情况下从翼型表面获取压力数据,因为传感器的应用会对流动造成影响。因此,对于风洞和水槽实验以及实际应用,对翼型表面的质量要求很高。因此,需要一种新的传感器类别,这种传感器可以齐平集成到翼型表面,可以在潮湿条件下使用,甚至可以在水下使用,并且能够承受高升力场景的恶劣环境。本文提出了一种新型的基于微型硅绝缘体(SOI)的微机电系统(MEMS)压力传感器,它可以采用倒装芯片配置集成到翼型中。内部的高掺杂硅布线采用“蝴蝶”几何形状,并结合玻璃通孔(TGV)技术,实现了密封且适用于应用的芯片级封装(CSP)。这些芯片是通过可靠的批量微加工生产的,包括晶圆级的飞秒激光工艺。传感器特性分析表明,分辨率高达 38 mVV bar。传感器表面采用超平滑且无台阶的电钝化处理,可以涂覆薄的表面保护层,以进一步增强对恶劣环境的鲁棒性。因此,在模拟具有高速撞击颗粒的环境的实验中,研究了非晶氢化硅氮(a-SiN:H)和非晶氢化碳化硅(a-SiC:H)的保护涂层。形貌损伤量化证明了 a-SiC:H 涂层的卓越鲁棒性,并验证了其在未来传感器中的适用性。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/a9cd4bad3478/sensors-21-06140-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/65b5d90e969e/sensors-21-06140-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/788167be9856/sensors-21-06140-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/0437eb2ef709/sensors-21-06140-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/ef7f5a45f13e/sensors-21-06140-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/07df53412ce2/sensors-21-06140-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/a9cd4bad3478/sensors-21-06140-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/65b5d90e969e/sensors-21-06140-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/788167be9856/sensors-21-06140-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/0437eb2ef709/sensors-21-06140-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/ef7f5a45f13e/sensors-21-06140-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/07df53412ce2/sensors-21-06140-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2302/8473241/a9cd4bad3478/sensors-21-06140-g006.jpg

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