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A dynamic regulating mechanism for increased airflow speed range in micro piezoelectric turbines

机译:一种用于提高微型压电涡轮机气流速度范围的动态调节机构

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摘要

© 2016 IEEE.The paper reports the design and fabrication of a micro-planar spring for a dynamic regulating mechanism to decrease the cut-in (start-up) airflow speed of a piezoelectric turbine. This mechanism is implemented by adjusting the magnetic coupling between the turbine rotor and a piezoelectric cantilever using the spring. Varied spring shapes and dimensions were analyzed with the finite element method (FEM) to optimize the structure. A micro spring with an ultra-low spring constant of 0.78 N/m was fabricated from titanium foil by laser machining. The spring was installed into a miniaturized air turbine to achieve the self-regulation. The cut-in speed was 2.34 m/s, showing a 30% improvement against a non-regulated turbine.
机译:©2016 IEEE。该论文报告了一种用于动态调节机构的微平面弹簧的设计和制造,该弹簧可降低压电涡轮的切入(启动)气流速度。通过使用弹簧调节涡轮转子和压电悬臂之间的磁耦合来实现该机制。使用有限元方法(FEM)分析了各种弹簧形状和尺寸,以优化结构。由钛箔通过激光加工制成具有0.78 N / m的超低弹簧常数的微型弹簧。弹簧被安装到小型空气涡轮机中以实现自我调节。切入速度为2.34 m / s,与非调节式涡轮机相比提高了30%。

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