Predicting Maximum Temperatures of a Li-ion Battery on a Simulated Flight Profile using a Model-based PrognosticsOne of the challenges in using Li-ion packs in aeronautics is their safety, and thermal runaway (TR) is a major concern. The current engineering solutions to prevent a Li-ion pack from a catastrophic TR require additional mass and volume to isolate cells. The excess mass could be reduced by improving detection and, thus, preventing a TR event. One of the possible early warning indicators of a TR is crossing a threshold temperature. We have developed an approach, based on the Unscented Kalman Filter (UKF), to predict the likelihood of reaching the threshold temperature for simulated flight profiles. The current battery prognostics algorithms for aerospace predict state-of-charge (SOC) and end-of-life (EOL) [1]. We extended this two-level algorithm to predict the maximum temperature during discharge. The amount of heat generated in a cell depends on factors such as cell chemistry, cell packaging, total cycles, operating temperature, and abuse history [2]. Our semi-empirical thermal model depends on three phenomenological parameters which account for those factors. In addition, a two-parameter reduced-order model is developed to predict the temperature rise for short bursts of “random-walk” (RW) discharge current sequence, which simulates a flight's current-loading profile. The performance of these models on different datasets and types of current loading will be presented. To predict the maximal temperatures for future cycles we must estimate the evolution of thermal parameters as the batteries age. It is found that the parameters of the 3-parametric thermal model cannot be estimated only from the RW data. To address the issue, we will present two alternative approaches: i) expanding the datasets to include discharge profiles beyond RWs; ii) model reduction to a two-parametric model. The two approaches will be illustrated by an application to the cycling data from a commercial LG 18650 cell.
References: 1. M. Daigle, C.S. Kulkarni, End-of-discharge and End-of-life Prediction in Lithium-ion Batteries with Electrochemistry-based Aging Models, in: AIAA Infotech @ Aerospace, American Institute of Aeronautics and Astronautics, San Diego, California, USA, 2016. 2. M. Börner, et. al, Correlation of aging and thermal stability of commercial 18650-type lithium ion batteries, Journal of Power Sources. 342 (2017) 382–392.
Document ID
20220016376
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Mohit Mehta (Wyle (United States) El Segundo, California, United States)
Michael Khasin (Ames Research Center Mountain View, California, United States)
Chetan Kulkarni (Wyle (United States) El Segundo, California, United States)
John Lawson (Ames Research Center Mountain View, California, United States)
Date Acquired
October 31, 2022
Subject Category
Mathematical And Computer Sciences (General)Electronics And Electrical Engineering
Meeting Information
Meeting: NASA Aerospace Battery Workshop
Location: Holiday Inn - Research Park, 5903 University Dr., Huntsville, AL
Country: US
Start Date: November 15, 2022
End Date: November 17, 2022
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
CONTRACT_GRANT: 80ARC020D0010
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Thermal runawayBattery prognosticsReduced-order model