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An Approach for Utilizing Power Flow Modeling for Simulations of Hybrid Electric Propulsion SystemsThis paper describes an approach to creating simulations of the electric components for a hybrid electric propulsion system. The proposed modeling technique is based on power/load flow modeling and is designed to provide a modular framework that includes buses, lines, and other electrical components that can be connected together to form the electrical distribution system. The purpose of this paper is to detail an electric distribution system modeling technique and to demonstrate how these models may be integrated with turbomachinery simulations. These general modeling techniques were created to be utilized for system and control design studies. Additionally, steady-state and dynamic performance for a proposed model example is compared with data from a hardware in the loop simulation.
Document ID
20180005201
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chapman, Jeffryes W.
(NASA Glenn Research Center Cleveland, OH, United States)
Litt, Jonathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 10, 2018
Publication Date
July 12, 2018
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN56356
Meeting Information
Meeting: AIAA/IEEE Electric Aircraft Technologies Symposium (EATS)
Location: Cincinnati, OH
Country: United States
Start Date: July 12, 2018
End Date: July 13, 2018
Sponsors: Institute of Electrical and Electronics Engineers, Illinois Univ., American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.03.01.10.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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