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Turbo- and Hybrid-Electrified Aircraft Propulsion Concepts for Commercial Transport
This review of aircraft electric propulsion architectures conveys that several aircraft system studies have indicated a potential benefit associated with using electrical systems to replace or augment the traditional fuel-based propulsion system. This exciting new approach for designing aircraft opens the door for new configurations. It is also important to convey that this field of study is in its infancy and much improvement is required across the breadth of supporting technologies if the promise of these aircraft concepts is to be realized.
High Voltage Insulation for Electrified Aircraft
The paper will present an overview of the current NASA project on development of electric propulsion technologies and in particular, a newly discovered insulation technology, namely micromultilayer multifunctional electrical insulation (MMEI). Results of extensive dielectric performance evaluations and its potential capabilities including efforts of demonstrating scale-up and commercial applicability of MMEI will be summarized.
NASA - GRC Materials Research Activities in High Voltage High Frequency Power Transmission Systems for Electrified Aircraft
This presentation describes the NASA GRC Multifunctional Materials Team activities in high voltage materials testing capabilities build up and recent research activities.
Electromagnetic Mass and Efficiency of Magnetic Gears for Electrified Aircraft
Magnetic gears are currently being developed for use in a variety of industries such as wind and automotive, because of their higher reliability and lower maintenance cost than their mechanical counterparts. The bulk of magnetic gear development to date has focused on maximizing the technology's volumetric torque density. In contrast, the primary performance metrics for an aircraft's gear box are its mass and efficiency. To that end this paper presents a study of the achievable electromagnetic specific torque and efficiency of concentric magnetic gears. NASA's second magnetic gear prototype is used as the baseline for this study. Achievable electromagnetic specific torque and efficiency trends are presented with respect to higher level design variables such as gear ratio and radius.
Safety, Standards, and Regulations for Electrified Aircraft
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Heat Flux Requirements for Electrified Aircraft Wing Anti-Ice Systems
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An Electrical Modeling and Thermal Analysis Toolbox for Electrified Aircraft Propulsion Simulation
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Establishing Electrified Aircraft Propulsion Concepts
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High Voltage Power Transmission Cable for Electrified Aircraft Propulsion
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Design and Development of Nano-electro Fuel Batteries and Rim-driven Motors for Electrified Aircraft Applications
The National Aeronautics and Space Administration Convergent Aeronautics Solutions project seeks to determine feasibility of emerging technologies in aeronautics. The Aqueous, QUick-Charging Battery Integration For Electric flight Research study pursued the feasibility of nano-electro fuel and rim-driven motor technologies integrated together for aircraft implementation. Development of the NEF technology was in partnership with Influit Energy, LLC (Chicago, Illinois). A rim-driven motor, designed by the project team, sized to represent one of 24 motors in the propulsion system of the tandem electric super-short takeoff and landing aircraft is discussed. The development of this electric super-short takeoff and landing concept was in partnership with The Boeing Company (Chicago, Illinois). The integrated system design of the nano-electro fuel and rim-driven motor technologies within the wing section was in partnership with Empirical Systems Aerospace, Inc. (ESAero) (San Luis Obispo, California). The feasibility benchmark for the nano-electro fuel battery was to attain 100 mA/sq. cm within two years, a 50-fold increase over the demonstrated cell performance before the Convergent Aeronautics Solutions Aqueous, QUick-Charging Battery Integration For Electric flight Research activity. The team achieved 85 mA/sq. cm in the nano-electro fuel flow cell at the end of the two years. The Aqueous, QUick-Charging Battery Integration For Electric flight Research project team determined the technology to be both inflammable and nonexplosive (unless multiple, simultaneous system failures occur) which would provide a safer alternative to conventional lithium-ion based battery systems.
NASA Aeronautics Electrified Aircraft Propulsion (EAP) Research Overview
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Overview of NASA Glenn Research Center’s Development of Boron Nitride Composites for Electrified Aircraft Propulsion
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NASA Electrified Aircraft Drivetrain Summary
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NASA AERONAUTICS: Electrified Aircraft Propulsion Research Overview
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