Prediction of environmental benefits introducing hybrid-electric propulsion on regional aircraft

• Published in: Journal of physics. Conference series 2024-03, Vol.2716 (1), p.12015
• Main Authors: Sirtori, Gabriele, Trainelli, Lorenzo, Riboldi, Carlo E.D.
• Format: Article
• Language: English
• Subjects: Aircraft; Aircraft landing; Aircraft performance; Airlines; Commercial aircraft; Emissions; Greenhouse gases; Hybrid propulsion; Hybrid systems; Networks; Reduction; Retrofitting; Turbine engines; Turboprop aircraft
• ISSN: 1742-6588; 1742-6596
• DOI: 10.1088/1742-6596/2716/1/012015

The objective of this paper is to assess the environmental benefits arising from the introduction of hybrid-electric propulsion on regional and commuter turboprop aircraft. A great focus is put on the propulsion based on a turbine engine coupled with batteries, combining mature technologies. The introduction of novel propulsion architectures on aircraft deployed on regional and commuter networks allows a substantial reduction of the fuel needed by airlines. In this work, scenarios based on real airline networks are presented, in order to quantify the reduction of greenhouse gas emissions possible considering the expected technological advancement for 2035 and 2050. This analysis is conducted by retrofitting the hybrid-electric propulsive system onto existing aircraft that can carry 19 passengers (Dornier DO228) or 70 passengers (ATR72-600). For the 19-seat class, a clean sheet design is also considered to overcome some limitations of the reference aircraft. A precise assessment of the peculiarities linked to the chosen propulsive configuration shows that networks that have shorter flights are better suited to the introduction of this technology, as the restriction on the design payload is less stringent. The proposed propulsive architecture allows a reduction of the operators’ yearly fuel budget of up to 50% in 2035 and 80% in 2050. At last, the taxi phase is of particular importance for regional aircraft that perform several rotations a day, therefore a further analysis of this phase is carried out. The result shows that the considered aircraft are capable of completing a full Landing & Take-Off (LTO) cycle without resorting to the thermal part of the propulsive system, reducing considerably the impact of the aircraft on the airport area.