Book Description
As large airline companies compete to reduce emissions, fuel, noise, and maintenance costs, it is expected that more of their aircraft systems will shift from using turbofan propulsion, pneumatic bleed power, and hydraulic actuation, to instead using electrical motor propulsion, generator power, and electrical actuation. This requires new flight-weight and flight-efficient powertrain components, fault tolerant power management, and electromagnetic interference mitigation technologies. Moreover, initial studies indicate some combination of ambient and cryogenic thermal management and relatively high bus voltages when compared to state of practice will be required to achieve a net system benefit. Developing all these powertrain technologies within a realistic aircraft architectural geometry and under realistic operational conditions requires a unique electric aircraft testbed. This report will summarize existing testbed capabilities located in the U.S. and details the development of a unique complementary testbed that industry and government can utilize to further mature electric aircraft technologies. Dyson, Rodger W. Glenn Research Center ELECTRIFICATION; ENGINE TESTING LABORATORIES; FLY BY WIRE CONTROL; FULL SCALE TESTS; HYPERSONIC WIND TUNNELS; TEST STANDS; ELECTRIC MOTORS; EVOLUTION (DEVELOPMENT); FABRICATION; FLIGHT SIMULATION; INSTALLING; PRODUCT DEVELOPMENT; RESEARCH FACILITIES