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Search: (WFRF:(Kyprianidis Konstantinos)) pers:(Kavvalos Mavroudis) pers:(Kyprianidis Konstantinos) conttype:(refereed) > (2021) > Enabling the potent...

Enabling the potential of hybrid electric propulsion through lean-burn-combustion turbofans

Vouros, Stavros (author)
Mälardalens universitet,Framtidens energi
Kavvalos, Mavroudis (author)
Mälardalens universitet,Framtidens energi
Sahoo, Smruti (author)
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Kyprianidis, Konstantinos (author)
Mälardalens universitet,Framtidens energi
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 (creator_code:org_t)
2021-09-16
2021
English.
In: Journal of the Global Power and Propulsion Society. - : Global Power and Propulsion Society. - 2515-3080. ; 5, s. 164-176
  • Journal article (peer-reviewed)
Abstract Subject headings
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  • Hybrid-electric propulsion has emerged as a promising technology to mitigate the adverse environmental impact of civil aviation. Boosting conventional gas turbines with electric power improves mission performance and operability. In this work the impact of electrification on pollutant emissions and direct operating cost of geared turbofan configurations is evaluated for an 150-passenger aircraft. A baseline two-and-a-half-shaft geared turbofan, representative of year 2035 entry-into-service technology, is employed. Parallel hybridization is implemented through coupling a battery-powered electric motor to the engine low-speed shaft. A multidisciplinary design space exploration framework is employed comprising modelling methods for multi-point engine design, aircraft sizing, performance and pollutant emissions, mission and economic analysis. A probabilistic approach is developed considering uncertainties in the evaluation of direct operating cost. Sensitivities to electrical power system technology levels, as well as fuel price and emissions taxation are quantified at different time-frames. The benefits of lean direct injection are explored along short-, medium-, and long-range missions, demonstrating 32% NOx savings compared to traditional rich-burn, quick-mix, lean-burn technologies in short-range operations. The impact of electrification on the enhancement of lean direct injection benefits is investigated. For hybrid-electric powerplants, the take-off-to-cruise turbine entry temperature ratio is 2.5% lower than the baseline, extending the corresponding NOx reductions to the level of 46% in short-range missions. This work sheds light on the environmental and economic potential and limitations of a hybrid-electric propulsion concept towards a greener and sustainable civil aviation. 

Subject headings

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Energiteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Energy Engineering (hsv//eng)
TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)

Keyword

Design space exploration
Economic analysis
Environmental impact
Hybrid electric propulsion
Lean direct injection
Uncertainty quantification

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Vouros, Stavros
Kavvalos, Mavrou ...
Sahoo, Smruti
Kyprianidis, Kon ...
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ENGINEERING AND TECHNOLOGY
ENGINEERING AND ...
and Mechanical Engin ...
and Energy Engineeri ...
ENGINEERING AND TECHNOLOGY
ENGINEERING AND ...
and Mechanical Engin ...
and Aerospace Engine ...
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Mälardalen University

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