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Converters

Overview

Power converters are an essential component in most EAP aircraft concepts, as they are used to convert from ac to dc power, or vice versa. They are an order of magnitude larger, lower weight, and higher efficiency compared to state of the art on aircraft.

NASA is sponsoring or performing work to achieve power densities 2-3 times the state of the art for converters in the MW or larger class. Research work conducted by NASA sets the path to achieving the performance, functions, and safety needed for large electric and hybrid electric aircraft.

  • X-57 HLMC

    Image of a High Lift Motor Controller (HLMC)

    High Lift Motor Controller (HLMC)
    • IASP – X-57 Aircraft
    • 11-14kW*, 11kW/kg, η = 97.6%, 538V
    • 6 Switch, DC -> AC 3-phase
    • Microcontroller-Based Control
    • OML Passive Air Cooling

  • GIMC-HEIST

    Image of a Generalized Intelligent Motor Control (GIMC) – Hybrid Electric Integrated System Testbed (HEIST) converter

    Generalized Intelligent Motor Control (GIMC) Hybrid Electric Integrated System Testbed (HEIST)
    • AAVP – Advanced Air Transport Technology (AATT)
    • 11kW, 3.5kW/kg, 400V
    • 6 Switch, DC -> AC 3-phase
    • Microcontroller-Based Control
    • OML Passive Air Cooling

  • HEATheR

    Image of NASA's High-Efficiency Electrified Aircraft Thermal Research project

    High-Efficiency Electric Aircraft Thermal Research (HEATheR) Converter
    • CAS
    • 72kW, η = 98.6%, 538V
    • 36 Switch multi-level interleaved
    • DC -> AC 3-phase
    • COTS FPGA Control
    • Liquid Cold Plate Cooling


  • X-57 CMC

    Image of the Cruise Motor Controller (CMC)

    Cruise Motor Controller (CMC)
    • IASP – X-57 Aircraft
    • 36kW, 4.4kW/kg, η > 97%, 538V
    • 6 Switch, DC -> AC 3-phase
    • Outsourced FPGA Control
    • Passive Air Cooling

  • 250 kW Converter

    Image of the Advanced Power Electronics Group 250kW Converter

    Advanced Power Electronics Group 250kW Converter
    • AAVP – Advanced Air Transport Technology (AATT)
    • 250kW, 10.6kW/kg, η =99.3%*, 1kV
    • 72 Switch multi-level interleaved
    • DC -> AC 3-phase
    • Custom FPGA Control
    • Liquid Cold Plate Cooling

  • SUSAN 25% MAGIC

    Image of the Motor And Generator Intelligent Converter (MAGIC)

    Motor And Generator Intelligent Converter (MAGIC)
    • CAS – SUSAN 25% Aircraft
    • 37.5kW, 5kW/kg*, η > 97%*, 270V
    • 6 Switch, DC -> AC 3-phase, or AC 3-phase -> DC
    • Microcontroller-Based Control
    • Liquid Immersion Cooling

  • Additional Power Converter Efforts

    Silicon carbide and gallium nitride converters are being developed with conventional cooling as well as a cryogenically cooled converter

    Continuous
    power rating,
    MW
    Specific
    power goal,
    kW/kg
    Efficiency
    goal,
    %
    Topology Switch material Cooling
    General Electric 1 19 99 3 level SiC/Si Liquid
    University of Illinois 0.2 19 99 7 level GaN Liquid
    Boeing 1 26 99.3 Si Cryogenic

    Related Publications

    TitleAuthorsDate
    Combined Analysis of NASA's High Efficiency Megawatt Motor and Its ConverterAnderson et al.11 February 2022
    Concept Design of a 1.4 MW Drive for Rotor Loss Minimization in a Partially Superconducting MotorJansen et al.07 July 2022
    Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric AircraftAvanesian et al.28 July 2021
    Development of an 11 kW Lightweight, High Efficiency Motor Controller for NASA X-57 Distributed Electric Propulsion Using SiC MOSFET SwitchesKowalewski et al.27 December 2019

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