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Materials challenges in rechargeable lithium-air batteries

Published online by Cambridge University Press:  09 May 2014

D.G. Kwabi
Affiliation:
Massachusetts Institute of Technology, USA; dkwabi@mit.edu
N. Ortiz-Vitoriano
Affiliation:
Massachusetts Institute of Technology, USA; nagore@mit.edu
S.A. Freunberger
Affiliation:
Graz University of Technology, Austria; freunberger@tugraz.at
Y. Chen
Affiliation:
University of St. Andrews, UK; yc21@st-andrews.ac.uk
N. Imanishi
Affiliation:
Mie University, Japan; imanishi@chem.mie-u.ac.jp
P.G. Bruce
Affiliation:
University of St. Andrews, UK; pgb1@st-andrews.ac.uk
Y. Shao-Horn
Affiliation:
Massachusetts Institute of Technology, USA; shaohorn@mit.edu

Abstract

Lithium-air batteries have received extraordinary attention recently owing to their theoretical gravimetric energies being considerably higher than those of Li-ion batteries. There are, however, significant challenges to practical implementation, including low energy efficiency, cycle life, and power capability. These are due primarily to the lack of fundamental understanding of oxygen reduction and evolution reaction kinetics and parasitic reactions between oxygen redox intermediate species and nominally inactive battery components such as carbon in the oxygen electrode and electrolytes. In this article, we discuss recent advances in the mechanistic understanding of oxygen redox reactions in nonaqueous electrolytes and the search for electrolytes and electrode materials that are chemically stable in the oxygen electrode. In addition, methods to protect lithium metal against corrosion by water and dendrite formation in aqueous lithium-air batteries are discussed. Further materials innovations lie at the heart of research and development efforts that are needed to enable the development of lithium-oxygen batteries with enhanced round-trip efficiency and cycle life.

Information

Type
Research Article
Copyright
Copyright © Materials Research Society 2014 
Figure 0

Figure 1. (a) Working principles of an Li-O2 cell and (b) gravimetric Ragone plot (power versus energy) of reported discharged Li-O2 cells containing various carbon cathodes: carbon nanotubes (CNTs),8 carbon nanofibers (CNFs),20 and freestanding hierarchically porous carbon (“graphene”).10 Cells based on conventional Li-ion positive electrodes, LiCoO218 and LiNi0.5Mn0.5O2,17 coupled with Li anodes for direct comparison are shown. Note that for Li-O2 cells, the total mass of the cathode was used (carbon + Li2O2). Open orange circles are for CNTs discharged to a limited capacity of 1,000 mAh/gC, while closed orange circles are from CNT electrodes discharged to 5,000 mAh/gC.19 The theoretical gravimetric energy of Li2O2 is calculated assuming a discharge voltage of 2.96 V versus Li and 1168 mAh/g Li2O2.

Figure 1

Figure 2. Transmission electron microscopy (TEM) images of carbon nanotube (CNT) electrodes discharged at (a) 10 mA/g to 4000 mAh gC–1 showing Li2O2 toroids, (b) 2.4 V to 5,000 mAh gC–1, (c) electron diffraction patterns of toroidal Li2O2, and (d) high-resolution TEM imaging of [001]-oriented Li2O2 plates, with lower magnification in inset. Reproduced with permission from References 19 and 23. © 2013 American Chemical Society. (e) In situ surface-enhanced Raman spectra during oxygen reduction reaction (ORR) and oxygen evolution reaction (OER) on an Au electrode in O2-saturated electrolyte. The peaks are assigned as follows: (1) C–C stretch of CH3CN at 918 cm–1, (2) O–O stretch of LiO2 at 1137 cm–1, (3) O–O stretch of Li2O2 at 808 cm–1, and (4) Cl–O stretch of ClO4 at 931 cm–1. Adapted with permission from Reference 25. (f) Surface-sensitive x-ray absorption near-edge structure O–K edge data of toroids formed at 10 mA/g to 4,000 mAh gC–1 and particles formed at 2.4 V to 5,000 mAh gC–1 showing that particles closely resemble stoichiometric Li2O2, while toroids exhibit LiO2-like features. (g) Constant-current charging of Li2O2 discharged at 2.0, 2.4, 2.5, and 2.76 V versus Li/Li+ at 100 mA/gC, showing the evolution of charge potential (E) with charge capacity (Q), with particle charging occurring at a lower average voltage penalty than toroid oxidation. Reprinted with permission from References 19 and 23. © 2013 American Chemical Society.

Figure 2

Figure 3. In situ transmission electron microscope (TEM) images showing oxidation of Li2O2 particles. (a) Schematic illustration of the in situ TEM microbattery superimposed over a low magnification TEM image of a solid electrolyte (SE)-coated Si nanowire contacting a single Li2O2 particle. (b) Higher magnification TEM image of the particles in (a) showing a multiwalled carbon nanotube (MWCNT) bundle contacting two physically separated Li2O2 particles labeled as Particle 1 and Particle 2, respectively. (c–g) Oxidation of Particles 1 and 2 during application of a 10 Vcell potential to the MWCNT/Li2O2 positive electrode against the Si nanowire (NW) negative electrode. CNT axes are delineated by the red, dashed lines. Reprinted with permission from Reference 28. © 2013 American Chemical Society.

Figure 3

Figure 4. (a) Discharge-charge curve showing evolution of reaction potential (U) with charge passed (Q) of a carbon paper-based cathode in 1 M LiTFSI (Li(CF3SO2)2N) in dimethoxyethane, along with reaction product quantification during oxygen reduction reaction and oxygen evolution reaction using iodometric titration and nuclear magnetic resonance techniques. Reaction product quantification shows that Li2O2 is the dominant product on discharge (along with carbonate species, R = Li or CH3), while CO2 and H2O are evolved during charge as a result of electrolyte decomposition. (b) Yield of Li2O2 ($Y_{{\rm{Li}}_2 {\rm{O}}_{\rm{2}} }$) as a function of Li-O2 battery discharge rate (i) for the same cathode, showing greater chemical reactivity between Li2O2 and the electrolyte at lower rates. Reprinted with permission from Reference 31. © 2013 American Chemical Society.

Figure 4

Figure 5. Quantification of carbon-containing by-products in carbon and TiC cathodes on discharge and charge, respectively. Data demonstrate significant side reactions both on discharge and charge at carbon electrodes. These are greatly suppressed at TiC cathodes. (a) Discharge-charge curve of a carbon cathode in 0.1 M LiClO4/dimethyl sulfoxide electrolyte on the first cycle. (b) Moles of CO2 evolved from the cathode stopped at certain points of discharge/charge indicated in (a) and then treated to decompose Li2CO3 and lithium carboxylates.32 (c) The same procedure applied to TiC electrodes in the same electrolyte at the indicated numbers of discharge (1D, 5D, . . . ) and charge (1C, 5C, . . . ); shown are inorganic and organic carbonaceous products. (d) Evolution of percentage of carbonate products with cycle number at a carbon and TiC electrode, respectively.34 Reprinted with permission from Reference 32. © 2013 American Chemical Society and Reference 34. © 2013 Nature Publishing Group.

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Figure 6. Possible reaction schemes for ether decomposition. (a) Proposed reaction scheme on discharge to explain decomposition of ether: electron reduction of O2 to superoxide (1), binding with Li+ (2), and disproportionation to Li2O2 (3) as the ideal sequence. Alternatively, superoxide may abstract a proton from the solvent (4) to give hydroperoxide (5), which may further react in a series of oxidative decomposition steps (6) or yield esters or polymeric compounds (7). Superoxide and CO2 from step (6) react to form Li2CO3 (8 and 9). (b) Alternative possible pathway with initial attack by autoxidation to give hydroperoxyl and alkyl radicals (I) and chain propagation by O2 addition and further proton abstraction (II and III). Note: The dot (•) denotes a free radical. (a) Reprinted with permission from Reference 44. © 2012 American Chemical Society. (b) Reprinted with permission from Reference 61. © 2011 American Chemical Society.

Figure 6

Table I. Dependence of lithium dendrite formation onset time (to) and short-circuit time (ts) on electrolyte formulation, temperature, and current density.

Figure 7

Figure 7. (a) Cycling performance for the Li/PEO18LiTFSI-SiO2-PP13TFSI/Li cell at 0.3 mA cm–2 and 60°C. The inset shows a comparison of the 11th cycle for Li/PEO18LiTFSI-SiO2-PP13TFSI/Li and Li/PEO18LiTFSI-PP13TFSI/Li. Cycling performance of the Li/PEO18LiTFSI-1.44PP13TFSI/LATP/aqueous 1 M LiCl-0.004 M LiOH/Pt-air cell at 0.3 mA cm–2 and 60°C between (b) 0 h and 400 h. The water-stable lithium electrode (WSLE) voltage was measured by a Pt-air reference electrode. Discharge and charge period are both two hours. Cycle was repeated without interval. Microscopic observations of the cell indicated no dendrite formation after cycling. Note: PEO, polyethylene oxide; LiTFSI, Li(CF3SO2)2N; PP13, N-methyl-N-propylpiperidinium; LATP, Li1+xAlxTi2–x(PO4)3. (a) Reprinted with permission from Reference 81. © 2014 Elsevier. (b) Reprinted with permission from Reference 82. © 2014 The Electrochemical Society.