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Propulsion Electric Grid Simulator (PEGS) for Future Turboelectric Distributed Propulsion AircraftNASA Glenn Research Center, in collaboration with the aerospace industry and academia, has begun the development of technology for a future hybrid-wing body electric airplane with a turboelectric distributed propulsion (TeDP) system. It is essential to design a subscale system to emulate the TeDP power grid, which would enable rapid analysis and demonstration of the proof-of-concept of the TeDP electrical system. This paper describes how small electrical machines with their controllers can emulate all the components in a TeDP power train. The whole system model in Matlab/Simulink was first developed and tested in simulation, and the simulation results showed that system dynamic characteristics could be implemented by using the closed-loop control of the electric motor drive systems. Then we designed a subscale experimental system to emulate the entire power system from the turbine engine to the propulsive fans. Firstly, we built a system to emulate a gas turbine engine driving a generator, consisting of two permanent magnet (PM) motors with brushless motor drives, coupled by a shaft. We programmed the first motor and its drive to mimic the speed-torque characteristic of the gas turbine engine, while the second motor and drive act as a generator and produce a torque load on the first motor. Secondly, we built another system of two PM motors and drives to emulate a motor driving a propulsive fan. We programmed the first motor and drive to emulate a wound-rotor synchronous motor. The propulsive fan was emulated by implementing fan maps and flight conditions into the fourth motor and drive, which produce a torque load on the driving motor. The stator of each PM motor is designed to travel axially to change the coupling between rotor and stator. This feature allows the PM motor to more closely emulate a wound-rotor synchronous machine. These techniques can convert the plain motor system into a unique TeDP power grid emulator that enables real-time simulation performance using hardware-in-the-loop (HIL).
Document ID
20140017746
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Choi, Benjamin B.
(NASA Glenn Research Center Cleveland, OH United States)
Morrison, Carlos
(NASA Glenn Research Center Cleveland, OH United States)
Dever, Timothy
(NASA Glenn Research Center Cleveland, OH United States)
Brown, Gerald V.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
December 30, 2014
Publication Date
July 28, 2014
Subject Category
Electronics And Electrical Engineering
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN16241
Report Number: GRC-E-DAA-TN16241
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 473452.02.03.05.05.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
electric power grid emulator
turboelectric distributed propulsion
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