Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling 2021
DOI: 10.1115/gt2021-59995
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Physics-Based Thermal Management System Components Design for All-Electric Propulsion Systems

Abstract: Although electrification allows a significant reduction in fuel burn, noise, and emissions, one of the main challenges in this technology is to deal with the thermal loads generated by the electrified propulsion system components. This is to guarantee the safe and optimal operation of the propulsion system as well as the aircraft. This challenge needs to be addressed to enable this important technology to be adopted by aircraft manufacturers. This paper presents a methodological approach to calculate the heat … Show more

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Cited by 2 publications
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“…The procedure of design and simulation of an aero-engine thermal management system could be started with physics-based modelling of engine heat sources in which a mathematical thermal model for engine bearings, gearboxes, pumps, etc., will be developed to calculate the values of the thermal loads generated in each source in various operating conditions. There is an in-house developed software at Cranfield University for this purpose [6][7][8], and a brief description of the models, how they can be developed and validated, and the related pseudo codes and equations are provided in the below section.…”
mentioning
confidence: 99%
“…The procedure of design and simulation of an aero-engine thermal management system could be started with physics-based modelling of engine heat sources in which a mathematical thermal model for engine bearings, gearboxes, pumps, etc., will be developed to calculate the values of the thermal loads generated in each source in various operating conditions. There is an in-house developed software at Cranfield University for this purpose [6][7][8], and a brief description of the models, how they can be developed and validated, and the related pseudo codes and equations are provided in the below section.…”
mentioning
confidence: 99%