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Force Analysis of IPMC Actuated Fin and Wing Assembly of a Micro Scanning Device through Two-way Fluid Structure Interaction Approach

机译:IPMC驱动的微扫描装置翅片和机翼组件的双向流体结构相互作用力分析

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摘要

In this paper, a methodology is presented to perform force analysis of wing and fin assembly of a micro fish like device through strongly coupled two-way fluid structure interaction approach. The scanning device operates underwater and is towed by a surface vessel through a tow cable. Device fins are actuated by ionic polymer metal composite (IPMC) actuators, an EAP actuator. Fins act as riser, depressor and stabiliser against roll motion of the device. During tow, wing and fin assembly of the device come under hydrodynamic forces. These forces are influenced by fin displacement under IPMC actuation and wing's angle of attack for same towing conditions. The interaction of wing and fin assembly with the fluid must be considered, through fluid structure interaction (FSI) analysis, to appraise its performance as depressor, riser and stabilizer against hydrodynamic forces. To obtain an accurate prediction to the hydrodynamic forces on wing and fin assembly of the device, it is necessary to conduct dynamic analysis of the surrounding fluid by computational fluid dynamics (CFD). A numerical simulation of three dimensional model of the assembly is performed in ANSYS WORKBENCH by coupling transient structural and Fluid Flow (CFX) analysis systems. The lift and drag forces acting on wing, along with their corresponding coefficients, are also quantified and the influence of wing's angle of attack and fin displacement, on generation of these forces, has also been revealed. The presented methodology is also applicable to self- propelled micro robots.
机译:在本文中,提出了一种通过强耦合双向流体结构相互作用方法对微型鱼状设备的机翼和鳍组件进行力分析的方法。扫描装置在水下运行,并由拖船通过拖缆拖曳。器件鳍由离子聚合物金属复合材料(IPMC)致动器(EAP致动器)致动。鳍片充当提升器,抑制器和稳定器,以防止设备滚动。在拖曳期间,该装置的机翼和散热片组装受到流体动力的作用。在相同的牵引条件下,这些力受IPMC驱动下的鳍片位移和机翼的迎角影响。必须通过流体结构相互作用(FSI)分析来考虑机翼和散热片组件与流体的相互作用,以评估其作为降压器,立管和稳定器抵抗流体动力的性能。为了获得对装置的机翼和翅片组件上的水动力的准确预测,有必要通过计算流体力学(CFD)对周围流体进行动力学分析。通过耦合瞬态结构和流体流动(CFX)分析系统,在ANSYS WORKBENCH中对组件的三维模型进行了数值模拟。还对作用在机翼上的升力和阻力及其相应的系数进行了量化,并且还揭示了机翼的迎角和鳍片位移对这些力的产生的影响。所提出的方法也适用于自行式微型机器人。

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