NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Exploring Li-Air Batteries for High Specific Energy and High Power Applications: A Simulation StudyCommercialization of lithium-air batteries face many challenges, such as electrolyte decomposition, short cycle life, low energy efficiency, low power density, etc. However, commercialization of Li-air batteries for mass sensitive applications such as electric vehicles, portable power source, and drones is more challenging due to additional constraints of safety, electrolyte evaporation, high specific energy requirements, and reliable discharge times. In this presentation, we will present our finite element simulation results comparing Li-O2 and Li-air batteries using power density, energy density, specific power, and discharge times as metrics to evaluate different electrolytes and electrode geometry to reduce total mass and maximize discharge current. We use a finite element model and a discharge product model developed in which is based on porous electrode and concentrated electrolyte theories and the discharge product is modeled using quantum tunneling; for reaction kinetics and oxygen diffusion, an improved model was used. The electrolyte properties such as ion conductivity and ion diffusion were obtained from Molecular Dynamics (MD) simulations while the other parameters for the finite element model were calibrated to match experiments at high discharge current densities (>1.5 mA/cm2). The mass densities of different electrolytes were computed using MD simulations as well. For this presentation, we examine the practical electrochemical mass of a system at different current ratings, the sensitivity of mass to the use of ambient air as compared to pure oxygen as well as the electrolyte, which affects maximum current density and the total mass associated with the electrolyte (which includes the mass of additional components), and, the optimization of battery geometry for total discharge time, average discharge voltage, maximum discharge current, and minimum electrochemical mass.
Document ID
20180004928
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Mehta, M.
(Analytical Mechanics Associates, Inc. Edwards, CA, United States)
Haskins, J.
(Analytical Mechanics Associates, Inc. Edwards, CA, United States)
Lawson, John W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2018
Publication Date
July 24, 2018
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
ARC-E-DAA-TN58914
Report Number: ARC-E-DAA-TN58914
Meeting Information
Meeting: Beyond Lithium Ion
Location: Cleveland, OH
Country: United States
Start Date: July 24, 2018
End Date: July 26, 2018
Sponsors: NASA Ames Research Center
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available