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Design of a Battery Cooling System for Hybrid Electric Aircraft
Hagen Kellermann
, Samuel Fuhrmann
, Michael Shamiyeh
,
Mirko Hornung
Bauhaus Luftfahrt e. V.
Technical University of Munich
Research output
:
Contribution to journal
›
Article
›
peer-review
31
Scopus citations
Overview
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Keyphrases
Battery Thermal Management System
100%
Hybrid-electric Aircraft
100%
Battery Cooling System
100%
Thermoelectric Module
50%
Heat Pump Technology
50%
Computational Model
25%
Ambient Temperature
25%
Sensitivity Analysis
25%
Operating Temperature
25%
Design Space
25%
Range Extension
25%
Battery Temperature
25%
Combustion Engine
25%
Temperature Deviation
25%
Take-off
25%
All-electric
25%
Heat Pump
25%
Finning
25%
Down-selection
25%
Heat Sink
25%
Hot Days
25%
Heat pipe Model
25%
Standard Atmosphere
25%
Battery Efficiency
25%
Thermoelectric Cooling
25%
Three-dimensional Design
25%
Ram Air
25%
Take-off Mass
25%
Puller
25%
Electric Design
25%
Snowball Effect
25%
Air-cooled Heat Exchanger
25%
Three-parameter
25%
Engineering
Battery Thermal Management System
100%
Cooling System
100%
Hybrid electric aircraft
100%
Heat Pump
75%
Thermoelectricity
75%
Design Space
25%
Battery Temperature
25%
Dimensional Design
25%
Discrete Value
25%
Atmosphere (Standard)
25%
Operating Temperature
25%
Heat Pipes
25%
Air Heat Exchanger
25%
Material Science
Aircraft
100%
Battery Thermal Management System
100%
Thermoelectrics
75%