Conceptual design of a metal hydride system for the recovery of gaseous hydrogen boil-off losses from LH2 tanks

Abstract Liquid hydrogen (LH2) is a promising energy carrier to decrease the climate impact of aviation. However, the inevitable formation of hydrogen boil-off gas (BOG) is a main drawback of LH2. As the venting of BOG reduces the overall efficiency and implies a safety risk at the airport, means for capturing and re-using should be implemented. Metal hydrides (MHs) offer promising approaches for BOG recovery, as they can directly absorb the BOG at ambient pressures and temperatures. Hence, this study elaborates a design concept for such an MH-based BOG recovery system at hydrogen-ready airports. The conceptual design involves the following process steps: identify the requirements, establish a functional structure, determine working principles and combine the working principles to generate a promising solution.

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Publication Details

Journal
The Aeronautical Journal
Published
2025-10-27
DOI
https://doi.org/10.1017/aer.2025.10087
Citations
1
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
4.99
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article

Conceptual design of a metal hydride system for the recovery of gaseous hydrogen boil-off losses from LH2 tanks

Florian Franke, Stefan Kazula
1 citations
The Aeronautical Journal
Spacecraft and Cryogenic Technologies
4.99
article

Conceptual design of a metal hydride system for the recovery of gaseous hydrogen boil-off losses from LH2 tanks

Florian Franke, Stefan Kazula
article en
1 citations

Abstract

Abstract Liquid hydrogen (LH2) is a promising energy carrier to decrease the climate impact of aviation. However, the inevitable formation of hydrogen boil-off gas (BOG) is a main drawback of LH2. As the venting of BOG reduces the overall efficiency and implies a safety risk at the airport, means for capturing and re-using should be implemented. Metal hydrides (MHs) offer promising approaches for BOG recovery, as they can directly absorb the BOG at ambient pressures and temperatures. Hence, this study elaborates a design concept for such an MH-based BOG recovery system at hydrogen-ready airports. The conceptual design involves the following process steps: identify the requirements, establish a functional structure, determine working principles and combine the working principles to generate a promising solution.

The Aeronautical JournalVol. 130(1343)
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR) (DE)
Openalex Percentile: Top 4%
Spacecraft and Cryogenic Technologies
4.99
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