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Size estimation tools for conventional actuator system prototyping in aerospace

机译:航空传统执行器系统原型设计的大小估计工具

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Predicting the size of an actuator capable of reaching given performance requirements is a critical step for any systems design. Thus, to help in the prototyping and early development stages of such devices, simple mathematical models were developed, which can be used with little knowledge in actuation system design. Based on physical phenomenons at the heart of the actuation mechanism, these models can be used to estimate diameter and length, and therefore volume and weight of conventional actuators as a function of performance requirements. Models include linear hydraulic pistons and electric motors, divided into radial and axial flux machines. Off-the-shelf actuators and more aerospace specific products were used to validate and assess the accuracy of the models over a wide range of force and torque requirements. Simple sizing examples for aerospace actuation systems are also given as use-cases of the different tools. A discussion on model applicability, for various aircraft scales and applications concludes the paper.
机译:预测可抵给定的性能要求的致动器的大小为任何系统设计中的关键步骤。因此,在这样的设备的原型和早期开发阶段的帮助,简单的数学模型,开发的,它可以在驱动系统设计一知半解使用。基于在该致动机构的心脏物理现象,这些模型可用于估计的直径和长度,因此体积和重量的常规致动器的作为性能要求的函数。模型包括线性液压活塞和电动马达,分为径向和轴向磁通电机。关的,现成的致动器,更具体的航空航天产品被用来验证和评估在宽范围内的力和扭矩要求的模型的准确性。航天驱动系统简单上浆例子也给出不同工具使用情况。对模型的适用性的讨论,对各种飞机规模和应用总结全文。

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