影响液冷定子热系统设计的变量选择

A. Woodworth, Andrew D. Smith, R. Jansen, Gerald Szpak
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引用次数: 6

摘要

美国宇航局格伦研究人员一直在努力创造一种高功率密度、高效率的电动机,称为高效率兆瓦电动机(HEMM),其目标是效率超过98%,功率为1.46兆瓦。之所以设定这些雄心勃勃的目标,是因为提高电机(电机和发电机)的功率密度和效率是实现电气化飞机(EA)商业化的必要条件。到目前为止,定子绕组的电阻损耗是该设计总能量损耗的最大贡献者(34%)。先前对类似hemm的定子测试件(定子)的测试表明,测量性能与模型预测之间具有良好的一致性。从而为电机设计中遇到的其他工程参数的测试提供了基础。特别令人感兴趣的是灌封过程中环氧树脂厚度变化的影响,末端绕组周围流体体积/流动路径的变化,以及冷却液粘度变化对装置整体热性能的影响。本文的重点是通过对某定子试验段的第三代构建、试验和有限元模型分析,揭示了这些参数的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Select Variables Affecting Thermal System Design of a Liquid-Cooled Stator
NASA Glenn Researchers have endeavored to create a high-power-density, efficient electric motor called the High Efficiency Megawatt Motor (HEMM) with a goal of exceeding 98% efficiency and 1.46 MW of power. These aggressive goals were set because increasing the power density and efficiency of electric machines (motors and generators) is integral to bringing electrified aircraft (EA) to commercial realization. Resistive losses in the stator windings are by far the largest (34%) contributor to this design’s total energy losses. Previous testing of a HEMM-like stator test article (statorette) showed good agreement between measured performance and model predictions. Therefore, a foundation was provided to test other engineering parameters that are encountered when designing an electric machine. Of particular interest are the effects of changes to the thickness of the epoxy from the potting process, changes in the fluid volume/flow path around the end windings, and changes in the viscosity of the cooling fluid on the overall thermal performance of the unit. The impact of those parameters as revealed through a third-generation build, test, and finite element model analysis of a statorette test section is the focus of this paper.
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