Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept

Borer, Nicholas K ; Geuther, Steven C ; Litherland, Brandon L ; Kohlman, Lee

关键词: AIRCRAFT DESIGN;    DESIGN ANALYSIS;    ELECTRIC PROPULSION;    ENGINE AIRFRAME INTEGRATION;    FLIGHT OPTIMIZATION;    FUEL CELLS;    FUEL SYSTEMS;    HYDROCARBON FUELS;    PROVING;    SAFETY FACTORS;    SOLID OXIDE FUEL CELLS;    SYSTEMS ANALYSIS;    SYSTEMS ENGINEERING;   

RP-ID  :  NF1676L-29000

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

As electric powertrain and propulsion-airframe integration technologies advance, airborne electric propulsion concepts appear to be on the cusp of disrupting or transforming aviation markets. One of the many challenges to this transformation lies within the onboard energy storage and generation technologies. State-of-the-art battery technology is heavy and lacks support infrastructure; purely combustion-based solutions to electrical power generation suffer from increased inefficiency as compared to a traditional combustion powertrain. This paper explores another alternative: a hybrid-electric, solid oxide fuel cell power system. This power system reforms traditional fuels to feed fuel cells that generate electrical power for the aircraft electric powertrain. A representative power system is designed based on the requirements for NASA’s X-57 Mod II electric flight demonstrator platform, and is shown to exceed system feasibility goals of 300 W/kg and 60% efficiency in at least one configuration. The hybrid-electric fuel cell power system is shown to be competitive with the range performance of a combustion-based power architecture and comparable in mission energy cost to a battery-electric power system.