Abstract

View Video Presentation: https://doi.org/10.2514/6.2023-3874.vid GKN Aerospace is committed to making a substantial difference commitment to the achievement of sustainable aviation at the earliest practical opportunity. As part of this, one of the technologies being considered is Hydrogen Electric Propulsion (H2EP) as part of the Hybrid Hydrogen Electric Architecture (H2GEAR) programme. The system comprises hydrogen fuel cells supplied with hydrogen from a liquid hydrogen source which is used for both its energetic and heat sink potential. The synergistic benefits of a cryogenically cooled system and how this can be used to give an optimised energy conversion and low specific mass system is highlighted. Some of the configuration selection decisions considered for the powertrain in a notional aircraft configuration context are presented including safety driven configuration decisions. Expected trends and requirements for technology growth are presented that enable the scalability of the powertrain concept and its applicability to larger scale vehicles. The H2GEAR technology demonstrator is expected progress to complete system demonstration by 2025.

Keywords:
Powertrain Aerospace Propulsion Scalability Automotive engineering Hydrogen vehicle Context (archaeology) Engineering Electrically powered spacecraft propulsion Hydrogen technologies Liquid hydrogen Hydrogen fuel Hydrogen economy Systems engineering Computer science Hydrogen Aerospace engineering Fuel cells

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Citation History

Topics

Advanced Combustion Engine Technologies
Physical Sciences →  Chemical Engineering →  Fluid Flow and Transfer Processes
Spacecraft and Cryogenic Technologies
Physical Sciences →  Engineering →  Aerospace Engineering
Advanced Aircraft Design and Technologies
Physical Sciences →  Environmental Science →  Global and Planetary Change

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