Innovators at NASA’s Glenn Research Center have developed a variable-frequency, alternating current (AC) power system to enable turbo-electric and hybrid electric propulsion. Glenn’s technology uses double-fed electric machines and a high-voltage, variable-frequency power system to significantly decrease (by 85%) the weight of an aircraft’s power electronics for turbo-electric propulsion, while still providing high specific power and variable thrust. To provide a safe system, the lightweight electric machines operate at high frequency, allowing fast detection and clearance of faults without requiring switchgear that interrupts the current. This design also reduces the protection system’s weight, while improving reliability by minimizing fault energy and collateral damage potential. In addition, the system permits either sub-synchronous or super-synchronous operation relative to throttle position, without having to adjust turbine settings.

Glenn’s novel system supports the NASA Aeronautics Research Mission Directorate (ARMD) strategic plan to leverage advancements in technologies over the next 25 years and beyond, leading to new aircraft configurations with enhanced performance, improved energy efficiency, and reduced CO2 emissions. The electric system is a multi-megawatt micro-grid that converts mechanical energy to electric via generators, and electric energy to mechanical via motor-driven fans. This innovation would use the variation in aircraft throttle settings to produce a high-voltage (20 kilovolts), variable-frequency, 9-phase AC distribution system. Using doubly fed electric machines (generator, propulsor, and flywheel) allows for field excitation that can cause variable-frequency or variable-speed operation around the commanded throttle setting.

The high-voltage power system reduces weight and improves efficiency in turbo-electric and hybrid-electric aircraft propulsion.

The flywheel enables an energy storage system that recovers and reuses energy, while the flywheel slews with the throttle control using the electromagnetic torque produced by the doubly fed electric machine. This design permits both sub-synchronous and super-synchronous operation using limited field excitation power provided through power converters. Finally, the reduced switchgear mass facilitated through the use of a high-frequency AC system, setting-less protection zones, and simplified switches for fault clearance provides enhanced operational capability. This system can be controlled so that fault energy is minimized, preventing collateral damage to aircraft structures, even with high voltage distribution. Glenn’s innovative system adds performance, efficiency, reliability, and cost savings to cutting-edge hybrid electric technology.

NASA is seeking partners to further develop this technology through joint cooperative research and development. For more information about this technology and to explore opportunities, please contact This email address is being protected from spambots. You need JavaScript enabled to view it.; 216-433-3484. Follow this link here  for more information.