TY - GEN
T1 - Hybrid-electric regional jet aircraft operation efficiency
AU - Wroblewski, Gabrielle E.
AU - Ansell, Phillip J.
N1 - Publisher Copyright:
© 2019 by American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - This work investigates the affect modifying the operation strategy during cruise has on hybrid-electric regional jet performance. Specifically investigated are mission range, fuel burn, and carbon dioxide emissions from fuel and battery sources. Accompanying the results from the hybrid-electric aircraft simulation is an investigation into the national aviation market, aimed at understanding the viability of missions with short ranges, those being most likely for hybrid-electric aircraft. Within the hybrid-electric simulation, a wide variety of current, near-future, and far-future battery technologies were tested, for a range of hybrid-electric configurations with increasing motor size and power. While the hybrid case with the lowest level of hybridization showed the greatest promise in terms of range capability, this configuration had drawbacks associated with fuel burn and emissions. Increases in BSED predicted for 2030-2040 would allow for the implementation of hybrid-electric regional jet transports that could meet up to 75% of the market demand. Increases in battery technology up to and exceeding the 2030 timeframe also demonstrated the capacity to reduce emissions compared to the conventional aircraft counterparts.
AB - This work investigates the affect modifying the operation strategy during cruise has on hybrid-electric regional jet performance. Specifically investigated are mission range, fuel burn, and carbon dioxide emissions from fuel and battery sources. Accompanying the results from the hybrid-electric aircraft simulation is an investigation into the national aviation market, aimed at understanding the viability of missions with short ranges, those being most likely for hybrid-electric aircraft. Within the hybrid-electric simulation, a wide variety of current, near-future, and far-future battery technologies were tested, for a range of hybrid-electric configurations with increasing motor size and power. While the hybrid case with the lowest level of hybridization showed the greatest promise in terms of range capability, this configuration had drawbacks associated with fuel burn and emissions. Increases in BSED predicted for 2030-2040 would allow for the implementation of hybrid-electric regional jet transports that could meet up to 75% of the market demand. Increases in battery technology up to and exceeding the 2030 timeframe also demonstrated the capacity to reduce emissions compared to the conventional aircraft counterparts.
UR - http://www.scopus.com/inward/record.url?scp=85095979019&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85095979019&partnerID=8YFLogxK
U2 - 10.2514/6.2019-4397
DO - 10.2514/6.2019-4397
M3 - Conference contribution
AN - SCOPUS:85095979019
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
Y2 - 19 August 2019 through 22 August 2019
ER -