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Electronic Speed Controller Thermal Management This experiment was coupled with an acoustic test for NASA’s QUiet Electric ENgine (QUEEN). A cold plate with water was used to cool the electronic speed controller of the motor under different conditions (shown on right). Part 1: Fixed motor RPM, translating to fixed power/heat dissipation (4W per MOSFET) of electrical components, with variable cooling capacity measured by flow rate of cold plate water in gpm. Part 2: Fixed cooling power (1 gpm) with variable RPM.
Document ID
20240010364
Acquisition Source
Glenn Research Center
Document Type
Poster
Authors
Sarah Freeman
(Miami University Oxford, United States)
Date Acquired
August 9, 2024
Subject Category
Aircraft Propulsion and Power
Aircraft Design, Testing and Performance
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Cleveland, OH
Country: US
Start Date: August 26, 2024
End Date: August 30, 2024
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 770848.01.03.10.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
thermal
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