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Impedance Measurements of Motor Drive and Supply in SPEED TestbedMany electrified aircraft configurations consist of a number of power components operating on the same shared electrical bus. Understanding the impedance performance of electrical loads and sources is key to understanding, and designing for, acceptable overall vehicle power quality and power system stability. To enable these measurements, personnel at NASA’s Glenn Research Center have designed and built the Scaled Power ElEctrified Drivetrain (SPEED) Testbed. This paper will present data taken in the SPEED lab, including impedance measurements of a DC supply (source) and a motor drive and electric machine (load) under a number of conditions. Impacts of load power, drive controller tuning, and field-weakening on load impedance are measured, presented, and discussed; as are source impedance data, stability, and DC bus current spectra at different loading levels.
Document ID
20230006178
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Timothy P. Dever
(Glenn Research Center Cleveland, Ohio, United States)
Xavier Collazo
(Glenn Research Center Cleveland, Ohio, United States)
Patrick Hanlon
(Glenn Research Center Cleveland, Ohio, United States)
Keith R. Hunker
(Glenn Research Center Cleveland, Ohio, United States)
David J. Sadey
(Glenn Research Center Cleveland, Ohio, United States)
Casey Theman
(Glenn Research Center Cleveland, Ohio, United States)
Brian P. Malone
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
April 21, 2023
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: AIAA/IEEE Electric Aircraft Technologies Symposium (EATS)
Location: San Diego, CA
Country: US
Start Date: June 12, 2023
End Date: June 16, 2023
Sponsors: American Institute of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 770848.01.03.10.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
electrified aircraft propulsion
stability
electrical power system
impedance measurement
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