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Numerical Simulation on the Response Characteristics of a Pneumatic Microactuator for Microfluidic Chips

机译:用于微流控芯片的气动微执行器响应特性的数值模拟

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This article presents a multiphysical system modeling and simulation of a pneumatic microactuator, which significantly influences the performance of a particular pneumatic microfluidic device. First, the multiphysical system modeling is performed by developing a physical model for each of its three integrated components: microchannel with a microvalve, a gas chamber, and an elastomer membrane. This is done for each step of operation for the whole system. The whole system is then considered a throttle blind capacitor model, and it is used to predict the response time of the pneumatic microactuator by correlating its characteristics such as gas pressurizing, hydraulic resistance, and membrane deformation. For this microactuator, when the maximum membrane deformation is 100 mu m, the required actuated air pressure is 80 kPa, and the response time is 1.67 ms when the valve-opening degree is 0.8. The response time is 1.61 ms under fully open conditions. These simulated results are validated by the experimental results of the current and previous work. A correlation between the simulated and experimental results confirms that the multiphysical modeling presented in this work is applicable in developing a proper design of a pneumatic microactuator. Finally, the influencing factors of the response time are discussed and analyzed.
机译:本文介绍了气动微执行器的多物理场系统建模和仿真,该系统显着影响特定气动微流体装置的性能。首先,通过为其三个集成组件中的每一个开发物理模型来执行多物理系统建模:带有微型阀的微通道,气室和弹性体膜。这是针对整个系统的每个操作步骤完成的。然后将整个系统视为节流盲电容器模型,并通过关联其特性(如气体增压,液力阻力和膜变形)来预测气动微执行器的响应时间。对于该微致动器,当最大膜变形为100μm时,所需的驱动气压为80 kPa,并且当阀开度为0.8时响应时间为1.67 ms。在完全打开的条件下,响应时间为1.61 ms。这些模拟结果已通过当前和先前工作的实验结果验证。仿真结果与实验结果之间的相关性证实,本文中提出的多物理场模型可用于开发气动微执行器的正确设计。最后,讨论并分析了响应时间的影响因素。

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