Battery Thermal Management Systems Design Considering Model Fidelity Levels and Design Optimization Utility

Nowsheen Sharmili, Yong Hoon Lee, James T. Allison

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The electrification of transportation requires a robust and efficient design of battery thermal management systems (BTMSs). This study introduces a resistance-capacitance (RC) based reduced order model (ROM) with additional auxiliary state variables for accurately capturing transient thermal behavior. The study explores the trade-offs between model fidelity and utility in BTMS control co-design (CCD) applications. BTMSs manage the temperature to ensure battery performance, safety, and longevity. Although computational fluid dynamics (CFD) is useful in steady and transient battery thermal analysis, full-fidelity CFD simulations are computationally expensive, particularly within CCD optimization loops. RC-based ROMs commonly used in early-stage design can mitigate the computational effort. These models can be formulated at different fidelity levels by representing various battery components as single or multiple LC bodies connected by resistance elements. The proposed augmented RC-based ROM enhances transient simulation accuracy while maintaining low computational cost, thereby, facilitating thorough design exploration using the CCD approach. This study focuses on comparing model fidelity levels, and their quantifiable utility measures, such as design accuracy and computational cost.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107115
DOIs
StatePublished - 2024
EventAIAA SciTech Forum and Exposition, 2024 - Orlando, United States
Duration: Jan 8 2024Jan 12 2024

Publication series

NameAIAA SciTech Forum and Exposition, 2024

Conference

ConferenceAIAA SciTech Forum and Exposition, 2024
Country/TerritoryUnited States
CityOrlando
Period1/8/241/12/24

ASJC Scopus subject areas

  • Aerospace Engineering

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