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Design of a Bidirectional Piezoelectric Actuator for Blade Trailing-Edge Flap

机译:叶片后缘襟翼双向压电执行器的设计

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摘要

The present research investigates the feasibility of a compact piezoelectric actuator mechanism to oscillate the rotorblade trailing-edge flap for active vibration suppression. The main components of the actuator are two piezostack segments and a dual-stage stroke amplifier. Each piezostack segment is fabricated by bonding five identical piezostacks. A bidirectional double-lever amplification concept is developed, that involves an extended dual-stage lever-fulcrum stroke amplifier and two parallel rows of piezostacks. Both design and fabrication of the trailing-edge flap actuator are addressed. The designed actuator is of size 8-inch length (spanwise), 1.25-inch width (chordwise), 0.75-inch height, and the weight of the prototype is 1.05 lbs. The bench-top test showed 94 % of ideal displacement output. To validate the feasibility of the designed actuator, the spin test in the vacuum chamber is planned to evaluate the performance in rotating environment up to 700g of centrifugal loading.
机译:本研究研究了一种紧凑的压电致动器机构来振荡转子叶片后缘襟翼以主动抑制振动的可行性。执行器的主要组件是两个压电堆栈段和一个双级行程放大器。每个压电叠层段都是通过结合五个相同的压电叠层来制造的。双向双向杠杆放大概念得到发展,它涉及一个扩展的双级杠杆支点行程放大器和两排平行的压电堆栈。后缘襟翼致动器的设计和制造均得到解决。设计的执行器尺寸为8英寸长(横向),1.25英寸宽(弦向),0.75英寸高,原型的重量为1.05磅。台式测试显示了理想排量输出的94%。为了验证设计的执行器的可行性,计划在真空室中进行旋转测试,以评估在高达700g离心负载的旋转环境中的性能。

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