4.5 Article

Thermal Management System Architecture for Hydrogen-Powered Propulsion Technologies: Practices, Thematic Clusters, System Architectures, Future Challenges, and Opportunities

Journal

ENERGIES
Volume 15, Issue 1, Pages -

Publisher

MDPI
DOI: 10.3390/en15010304

Keywords

thermal management system; hydrogen-powered propulsion; fuel cells; scientometrics; co-word analysis

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This study critically reviews and assesses the thermal management system architectures for hydrogen-powered propulsion technologies. The objectives are to identify system-level shortcomings and recognize remaining challenges and research questions. The study conducts a co-word analysis and historical review to identify milestones and proposed embodiments. Feasible architectures are classified and components discussed, with a specific focus on the application of hydrogen-powered fuel cells in aviation. The study also examines why no hydrogen-powered propulsion thermal management system architecture has been approved for commercial production and identifies remaining research challenges.
The thermal management system architectures proposed for hydrogen-powered propulsion technologies are critically reviewed and assessed. The objectives of this paper are to determine the system-level shortcomings and to recognise the remaining challenges and research questions that need to be sorted out in order to enable this disruptive technology to be utilised by propulsion system manufacturers. Initially, a scientometrics based co-word analysis is conducted to identify the milestones for the literature review as well as to illustrate the connections between relevant ideas by considering the patterns of co-occurrence of words. Then, a historical review of the proposed embodiments and concepts dating back to 1995 is followed. Next, feasible thermal management system architectures are classified into three distinct classes and its components are discussed. These architectures are further extended and adapted for the application of hydrogen-powered fuel cells in aviation. This climaxes with the assessment of the available evidence to verify the reasons why no hydrogen-powered propulsion thermal management system architecture has yet been approved for commercial production. Finally, the remaining research challenges are identified through a systematic examination of the critical areas in thermal management systems for application to hydrogen-powered air vehicles' engine cooling. The proposed solutions are discussed from weight, cost, complexity, and impact points of view by a system-level assessment of the critical areas in the field.

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