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Select Variables Affecting Thermal System Design of a Liquid-Cooled StatorNASA 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.
Document ID
20205005270
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Andrew Woodworth
(Glenn Research Center Cleveland, Ohio, United States)
Andrew Smith
(Glenn Research Center Cleveland, Ohio, United States)
Ralph Jansen
(Glenn Research Center Cleveland, Ohio, United States)
Gerald Szpak
(HX5, LLC Brook Park, Ohio, United States)
Date Acquired
July 28, 2020
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: AIAA/IEEE Electric Aircraft Technologies Symposium
Location: Virtural
Country: US
Start Date: August 26, 2020
End Date: August 28, 2020
Sponsors: American Institute of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 081876.02.03.50.10.01.04
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
EAP
stator
thermal
electric machine
generator
motor
Electric Aircraft Propulsion
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