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Stiction-Induced Sealing of Surface Micromachined Channels

机译:表面微机械通道的静摩擦密封

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摘要

We established a technique to achieve low temperature hermetic sealing of surface micromachined channels by exploiting stiction. Using a wing-shaped structural layer, microchannels automatically seal during the drying step that follows the sacrificial etch. This avoids the need of plugging layers to close the apertures of the sacrificial etch. To demonstrate the technique, we designed a surface micromachined channel with a structural layer made of polycrystalline silicon carbide (poly-SiC). This layer integrates an array of anchored pillars to achieve long and wide microchannels (5.4 mm $times,$0.43 mm $times,$ 0.001 mm). To dimension the sealing-wing, we estimate the minimum adhesion energy between the poly-SiC and silicon. This is done by analytical modeling and experimental characterization of test structures in the shape of centrally-supported circular plates. The bending and adhesion of the sealing-wing is followed in situ by optical microscopy. The closed microchannels are annealed at 100$^{circ}{rm C}$. Some structures are exposed to thermal stress at 760$^{circ}{rm C}$. The results are inspected by white light interferometry, scanning electron microscopy, and helium leak testing. Microchannels result hermetically sealed showing leak rates below the detection limit $(4times 10^{-9}~{rm Pa}cdot{rm m}^{3}/{rm s})$. The seal is effective to at least 600 kPa. $hfill[2013hbox{-}0122]$
机译:我们建立了一种通过利用粘滞力来实现表面微加工通道的低温气密密封的技术。使用翼形结构层,微通道在牺牲蚀刻之后的干燥步骤中自动密封。这避免了堵塞层以关闭牺牲蚀刻的孔的需要。为了演示该技术,我们设计了一个表面微加工通道,该通道具有由多晶硅碳化硅(poly-SiC)制成的结构层。该层集成了一系列锚定柱,以实现长而宽的微通道(5.4毫米×0.43毫米×0.001毫米)。为了确定密封翼的尺寸,我们估算了聚碳化硅和硅之间的最小粘附能。这是通过对以中心支撑的圆盘形状的测试结构进行分析建模和实验表征来完成的。通过光学显微镜原位跟踪密封翼的弯曲和粘附。封闭的微通道在100 $ ^ {circ} {rm C} $下退火。一些结构受到760 $ ^ {circ} {rm C} $的热应力。通过白光干涉仪,扫描电子显微镜和氦气泄漏测试检查结果。微通道被密封,显示泄漏率低于检测极限$(4 x 10 ^ {-9}〜{rm Pa} cdot {rm m} ^ {3} / {rm s})$。密封至少可有效达到600 kPa。 $ hfill [2013hbox {-} 0122] $

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