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Implementing the Digital Design Process for the Development of a Centrifugal Fan Impeller in the Undergraduate Engineering Curriculum

机译:在本科工程课程中实施数字化设计过程以开发离心式风扇叶轮

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For the past two years, Mechanical & Aerospace Engineering students at the University of Florida have been designing and manufacturing impellers for a centrifugal fan. The method is taught in our Thermo-Fluids Lab and Design class and involves using Euler's Turbomachine Equation and creating velocity diagrams to predict performance. A limitation of the Euler Turbomachine Equation is that it is based on a finite control volume analysis which prescribes blade angles at the entrance and exit of the impeller, but provides no information on the number or geometry of the blades within the impeller. Another limitation of the equation is that it assumes an infinite number of blades of zero thickness that results in uniform flow at the inlet and the exit, while a real impeller has a distinct velocity profile in between each blade that leads to losses not predicted by the equation. A Digital Design Process has evolved whereby students create an initial design using the Euler method, and then create a digital model using Solidworks, and then follow that up with a computational fluid dynamics (CFD) to optimize their design. After optimization, the students manufacture a prototype of their impeller using a 3-D printer, and then test the impeller in the lab fan performance apparatus. The results of their efforts as well as the issues involved in managing such a project with about 125 students per semester will be discussed in this paper.
机译:在过去的两年中,佛罗里达大学的机械与航天工程专业的学生一直在设计和制造离心风机的叶轮。该方法在我们的Thermo-Fluids实验室和设计课程中进行了讲授,涉及使用Euler的Turbomachine方程并创建速度图来预测性能。欧拉涡轮机方程式的局限性在于它基于有限的控制体积分析,该分析方法规定了叶轮入口和出口的叶片角度,但没有提供有关叶轮内叶片数量或几何形状的信息。该方程式的另一个局限性在于,它假设无数个厚度为零的叶片会导致进口和出口处的流量均匀,而实际的叶轮在每个叶片之间具有明显的速度分布,这会导致损耗无法预测。方程。数字设计过程已经发展,学生可以使用欧拉方法创建初始设计,然后使用Solidworks创建数字模型,然后再进行计算流体动力学(CFD)来优化他们的设计。经过优化后,学生将使用3-D打印机制造叶轮的原型,然后在实验室风扇性能设备中测试叶轮。本文将讨论他们的努力结果以及管理每学期约125名学生的项目管理所涉及的问题。

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