NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Conceptual Design of a Single-Aisle Turboelectric Commercial Transport With Fuselage Boundary Layer IngestionA single-aisle commercial transport concept with a turboelectric propulsion system architecture was developed assuming entry into service in 2035 and compared to a similar technology conventional configuration. The turboelectric architecture consisted of two underwing turbofans with generators extracting power from the fan shaft and sending it to a rear fuselage, axisymmetric, boundary layer ingesting fan. Results indicate that the turbo- electric concept has an economic mission fuel burn reduction of 7%, and a design mission fuel burn reduction of 12% compared to the conventional configuration. An exploration of the design space was performed to better understand how the turboelectric architecture changes the design space, and system sensitivities were run to determine the sensitivity of thrust specific fuel consumption at top of climb and propulsion system weight to the motor power, fan pressure ratio, and electrical transmission efficiency of the aft boundary layer ingesting fan.
Document ID
20160007674
Document Type
Conference Paper
Authors
Welstead, Jason R.
(NASA Langley Research Center Hampton, VA, United States)
Felder, James L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 17, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-21577
Meeting Information
2016 AIAA SciTech Conference(San Diego, CA)
Funding Number(s)
CONTRACT_GRANT: NNL08AA16B
WBS: WBS 081876.02.07.30.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 20160007674.pdf STI
No Preview Available