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Scaling laws based metamodels for the selection of the cooling strategy of electromechanical actuators in the early design stages

机译:在设计初期,基于缩放定律的元模型用于选择机电执行器的冷却策略

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The integration of electromechanical actuation systems for aerospace applications requires additional thermal stress considerations during the preliminary design, which were not necessary within the hydraulic technology. The favored models during this design phase are simple, continuous and explicit mathematical expressions to enable easy analytical manipulations or implementations in worksheets or optimization loops. The paper shows how such models can be obtained for the desired applications, illustrating the example of a Limited Angle Torque Motor (LATM) with different cooling strategies. The used method for gathering the models is a regression process on data obtained by finite element simulations. The originality of the method stands in the physical insight of the regression function which is based on scaling laws and dimensional analysis. An example of preliminary design of a LATM illustrates the use of the obtained models for the comparison of two possible architectures intended to minimize the mass of the actuator by implementing different cooling strategies. (C) 2015 Elsevier Ltd. All rights reserved.
机译:用于航空航天应用的机电致动系统的集成需要在初步设计过程中考虑其他热应力因素,这在液压技术中是不必要的。在设计阶段喜欢的模型是简单,连续和明确的数学表达式,以使工作表或优化循环中的分析操作或实现变得容易。本文展示了如何针对所需应用获得此类模型,并举例说明了具有不同冷却策略的限角扭矩电动机(LATM)。用于收集模型的方法是对通过有限元模拟获得的数据进行回归处理。该方法的独创性体现在回归函数的物理洞察力上,该函数基于缩放定律和尺寸分析。 LATM初步设计的示例说明了如何使用获得的模型来比较两种可能的体系结构,以通过实施不同的冷却策略来最大程度地减小执行器的质量。 (C)2015 Elsevier Ltd.保留所有权利。

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