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Electroactive-Polymer Actuators for Controlling Space Inflatable Structures

机译:用于控制空间充气结构的电活性聚合物致动器

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摘要

Space inflatable structures present a unique challenge to the design of actuators that can be used to effectively control the surface contour of the structures for the purposes of health monitoring and damage detection. Any actuator designed for space inflatable must be highly flexible and have low mass so that the structural integrity of the inflatable will not be severely compromised by the attachment of the actuator. Among current actuator designs, electroactive-polymer-based actuators are the most promising ones. Electroactive polymer is a new class of "smart" material that can convert electrical energy into mechanical energy. Ionic polymer metal composites and conductive polymers, which belong to the electroactive polymer group, can be effective actuation materials because of their low activation voltage of about 5 V and potentially large strains. Both types of actuators were fabricated, and their stress and strain outputs evaluated for use on inflatable structures.
机译:太空充气结构对致动器的设计提出了独特的挑战,该致动器可用于有效地控制结构的表面轮廓,以进行健康监测和损坏检测。设计用于太空充气的任何致动器都必须具有高度的柔韧性和低的质量,以使充气的结构完整性不会因致动器的安装而受到严重损害。在当前的执行器设计中,基于电活性聚合物的执行器是最有前途的。电活性聚合物是可以将电能转换为机械能的新型“智能”材料。属于电活性聚合物组的离子聚合物金属复合材料和导电聚合物,由于其约5 V的低活化电压和潜在的大应变,因此可以成为有效的驱动材料。两种类型的致动器都被制造出来,并评估了它们的应力和应变输出以用于充气结构。

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