Assessment of hydrogen gas turbine-fuel cell powerplant for rotorcraft

Simple item page
dc.contributor.authorBaena Mejıas, Rafael
dc.contributor.authorSaias, Chana Anna
dc.contributor.authorRoumeliotis, Ioannis
dc.contributor.authorPachidis, Vassilios
dc.contributor.authorBacic, Marko
dc.date.accessioned2024-03-11T14:22:18Z
dc.date.available2024-03-11T14:22:18Z
dc.date.issued2023-12-11
dc.description.abstractConventional turboshaft engines are high power density movers suffering from low efficiency at part power operation and producing significant emissions. This paper presents a design exploration and feasibility assessment of a hybrid hydrogen-fueled powerplant for Urban Air Mobility (UAM) rotorcraft. A multi-disciplinary approach is devised comprising models for rotorcraft performance, tank and subsystems sizing and engine performance. The respective trade-offs between payload-range and mission level performance are quantified for kerosene-fueled and hybrid hydrogen tilt-rotor variants. The effects of gas turbine scaling and fuel cell pressurization are evaluated for different hybridization degrees. Gas turbine scaling with hybridization (towards the fuel cell) results in up to 21% benefit in energy consumption relative to the non-scaled case with the benefits being more pronounced at high hybridization degrees. Pressurizing the fuel cell has shown significant potential as cell efficiency can increase up to 10% when pressurized to 6 bar which translates to a 6% increase in overall efficiency. The results indicate that current fuel cells (1 kW/kg) combined with current hydrogen tank technology severely limit the payload-range capability of the tilt-rotor. However, for advanced fuel cell technology (2.5 kW/kg) and low ranges, hybrid powerplant show the potential to reduce energy consumption and reduce emissions footprint.en_UK
dc.description.sponsorshipRolls-Royce plcen_UK
dc.identifier.citationMejías RB, Saias CA, Roumeliotis I, et al., (2024) Assessment of hydrogen gas turbine-fuel cell powerplant for rotorcraft. International Journal of Hydrogen Energy, Volume 50, Part B, January 2024, pp.772-783en_UK
dc.identifier.eissn1879-3487
dc.identifier.issn0360-3199
dc.identifier.urihttps://doi.org/10.1016/j.ijhydene.2023.07.076
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20958
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectHybrid propulsionen_UK
dc.subjectVTOLen_UK
dc.subjectHydrogenen_UK
dc.subjectFuel cellsen_UK
dc.subjectUAMen_UK
dc.titleAssessment of hydrogen gas turbine-fuel cell powerplant for rotorcraften_UK
dc.typeArticleen_UK
dcterms.dateAccepted2023-07-08

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
Hydrogen_gas_turbine-fuel_cell-2023.pdf
Size:
1.97 MB
Format:
Adobe Portable Document Format
Description:
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.63 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

Staff publications (SATM)