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Lithium–sulfur battery

Type of rechargeable battery

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Li-S battery working principle and shuttle effect
Egibe · CC BY-SA 4.0

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Through Rechargeable battery, Sulfur and Aliphatic compound

Lithium–sulfur batteries could displace lithium-ion cells because of their higher energy density and lower cost. The use of metallic lithium instead of intercalating lithium ions allows for much higher energy density, as less substances are needed to hold "lithium" and lithium is directly oxidized. Li–S batteries have a high theoretical specific energy (≈2600 Wh/kg for the Li/S redox chemistry), but practical cell-level specific energies in pouch-cell formats are typically ~300–450 Wh/kg today; values above ~400 Wh/kg generally require high sulfur loading, lean-electrolyte operation, and limited excess lithium.

Li–S batteries with up to 1,500 charge and discharge cycles were demonstrated in 2017, but cycle life tests at commercial scale and with lean electrolyte have not been completed. As of early 2021, none were commercially available.

Several issues have slowed acceptance. One is the polysulfide "shuttle" effect that is responsible for the progressive leakage of active material from the cathode, resulting in too few recharge cycles. Also, sulfur cathodes have low conductivity, requiring extra mass for a conducting agent in order to exploit the contribution of active mass to the capacity. Volume expansion of the sulfur cathode during S to Li2S conversion and the large amount of electrolyte needed are also issues.

Progress has been made toward high-stability sulfurized-carbon cathodes. Sulfurized-carbon cathodes (e.g., sulfurized polyacrylonitrile, also known as SPAN) may offer some advantages. Their polysulfide shuttle free feature facilitates proper operation under lean electrolyte conditions (< 3 g·(A·h)−1).

Although Li–S chemistry is attractive for its high theoretical energy density, practical pouch cells require minimizing inactive mass and operating under conditions that resemble commercial batteries. Some practical targets include: (i) high areal sulfur loading (typically ≥5 mgs cm−2) to avoid overestimating capacity in thin electrodes; (ii) lean electrolyte operation, often expressed as electrolyte-to-sulfur ratio E/S ≤5 μL mg/s (or electrolyte-to-capacity ratio E/C ≲5 μL/mAh), because electrolyte can account for a large fraction of pouch-cell mass; and (iii) a controlled negative-to-positive capacity ratio (N/P), since excess lithium metal improves coin-cell cycling but strongly lowers cell-level energy density. These constraints are interdependent: increasing sulfur loading or lowering E/S improves projected energy density, but can also increase polarization and lower reversible capacity if ion/electron transport and interfacial stability are not maintained. Pouch-cell specific energies are often near 400–450 Wh/kg are reached only when these metrics are satisfied simultaneously.

History

Li–S batteries were invented in the 1960s, when Herbert and Ulam patented a primary battery employing lithium or lithium alloys as anodic material, sulfur as cathodic material and an electrolyte composed of aliphatic saturated amines. A few years later the technology was improved by the introduction of organic solvents as PC, DMSO and DMF yielding a 2.35–2.5 V battery. By the end of the 1980s a rechargeable Li–S battery was demonstrated employing ethers, in particular DOL, as the electrolyte solvent.

The critical parameters needed for achieving commercial acceptance have been described. Specifically, Li–S batteries need to achieve a sulfur loading of >5 mg·cm−2, a carbon content of <5%, electrolyte-to-sulfur ratio of <5 μL·mg−1, electrolyte-to-capacity ratio of <5 μL·(mA·h)−1, and negative-to-positive capacity ratio of <5 in pouch-type cells.

They were used on the longest and highest-altitude unmanned solar-powered aeroplane flight (at the time) by Zephyr 6 in August 2008.

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