Journal of The Electrochemical Society, 151 ͑2͒ A291-A295 ͑2004͒
A291
0
013-4651/2004/151͑2͒/A291/5/$7.00 © The Electrochemical Society, Inc.
Investigation on the First-Cycle Charge Loss
of Graphite Anodes by Coating of the Pyrolytic Carbon
Using Tumbling CVD
Young-Soo Han,a,z Jae-Han Jung, and Jai-Young Lee *
b
c,
a
LG Electronics Institute of Technology, Devices and Materials Laboratory, Seoul 137-724, South Korea
LG Chemical, Limited, Battery Research Center, Taejon 305-380, South Korea
b
c
Department of Materials Science and Engineering, Korea Advanced Institute of Science and Technology,
Taejon 305-701, South Korea
The first-cycle charge loss of graphite coated with pyrolytic carbon using a tumbling chemical vapor deposition ͑CVD͒ process has
been studied for the active material of anodes in lithium-ion secondary batteries. Through the coating of pyrolytic carbons on the
surface of graphite particles, carbon materials with a core ͑graphite͒-shell ͑pyrolytic carbon͒ structure can be obtained. The
irreversible capacity of these carbons at first charge/discharge cycle has been examined using a charge-discharge cycler. The
coating of the pyrolytic carbon on the surface of graphite can effectively reduce the initial irreversible capacity, which leads to
ϩ
improvement of first cycle coulombic efficiency from 87.21 to 93.32%. The irreversible capacity formed above 0.8 V vs. Li/Li
at the first charging cycle is proportional to the surface area of the carbon, that is, the coating time of pyrolytic carbon. The plateau
of the first-cycle charging curve disappears distinctly with the coating of pyrolytic carbon. The reduction of the initial irreversible
capacity in graphite coated with pyrolytic carbon results from this disappearance of the plateau. This means that the coating layer
of pyrolytic carbon is more compatible with the electrolyte than the surface of bare graphite. From electrochemical impedance
ϩ
spectroscopy spectra, the increase of contact resistance in bare graphite electrodes occurs at 0.8-0.2 V vs. Li/Li in the first
charging and the coating of pyrolytic carbon on the surface of graphite can suppress the increment of contact resistance.
©
2004 The Electrochemical Society. ͓DOI: 10.1149/1.1639156͔ All rights reserved.
Manuscript submitted March 17, 2003; revised manuscript received August 27, 2003. Available electronically January 9, 2004.
Graphite has been used widely for lithium ͑Li͒ ion secondary
surface structure of graphite particles. In the this study, we examine
the cause of the first-cycle charge loss by investigating the electro-
chemical phenomena of graphite coated with pyrolytic carbon.
batteries because of its advantages of practical energy density,
1
charge-discharge reversibility, and safety aspects. Graphite consists
of hexagonal arrays of carbon atoms arranged in benzene-type struc-
tures. The hexagonal arrays form ordered layer structures and the
layer planes are separated by 3.354 Å. The surface of graphite par-
ticles consists of the basal planes and the prismatic ͑edge͒ planes of
the hexagonal arrays. It has been recognized that the chemical reac-
tivity of the prismatic plane was much higher than that of the basal
Experimental
Coating of pyrolytic carbons.—The new type of carbon materials
with core ͑graphite͒—shell ͑pyrolytic carbon͒ structure was ob-
7
tained by the tumbling CVD process. For improving the uniformity
of the pyrolytic carbon shell, graphite particles tumbled in the rotat-
ing reactor tube during the pyrolytic carbon tumbling were depos-
ited on the surface of graphite particles. The rotation speed of the
reactor tube varied from 10 to 50 rpm. Four grooves parallel to the
tube axis were placed on the inner wall of the tube to promote the
tumbling action of the graphite particles. The coating of pyrolytic
carbon on graphite was carried out by introducing a gas mixture of
liquid propane gas ͑LPG͒ and argon under 1 atm pressure in the
temperature range from 1000 to 1200°C. The coating time varied
from 0.5 to 3 h. The concentration of LPG varied from 10 to 100%,
and the total flow rate varied from 1 to 6 L/min. The specific surface
area of each sample was determined with Brunauer-Emmett-Teller
2
,3
plane.
The irreversible capacity loss of graphite anodes in Li-ion sec-
ondary batteries originates from the decomposition of electrolyte to
form both a solid electrolyte interface ͑SEI͒ layer and gaseous prod-
ucts on the electrode during the initial charge/discharge cycles. Win-
4
ter et al. reported that both the total surface area and the average
ratio of the basal plane and edge thickness dimension influenced the
5
irreversible capacity loss. Bar-Tow et al. showed that the mecha-
nism of electrolyte decomposition was different on the basal and
prismatic planes in an electrolyte consisting of LiAsF in ethylene
6
carbonate ͑EC͒—diethyl carbonate ͑DEC͒. The SEI layer formed on
the prismatic planes is rich in inorganic compounds, whereas that
formed on the basal planes is rich in organic compounds. Zaghib
͑
BET͒ measurement with nitrogen gas. Prior to measurements, all
samples were heated at 300°C for 10 h under vacuum to remove
surface-adsorbed moisture and hydrocarbons.
6
et al. demonstrated that the distribution of basal and prismatic
Cell assembly and electrochemical measurement.—Carbon elec-
trodes were prepared by coating slurries of the above new type
carbon powder and polyvinylidene fluoride ͑PVDF͒ dissolved in
N-methyl pyrrolidinone on copper foils. After coating, the electrodes
were dried at 150°C for 3 h in vacuum (10 Torr͒ and then pressed
at about 150 kg/cm . The diameter and thickness of the circular-
shaped carbon electrodes were 16 mm and about 50 m, respec-
tively. Coin-type test cells were constructed from these electrodes. A
microporous film ͑Celgard 2400͒ wetted with electrolyte ͓1 M
LiPF6 dissolved in a 50/50 volume percent ͑vol%͒ mixture of EC
DEC; Merck & Co., Inc.͔ was sandwiched between the carbon-
aceous cathode and Li metal foil anode. All cells were assembled in
an argon-filled glove box. These cells were charged and discharged
in the potential range of 0 to 2 V vs. Li/Li using a galvanostatic
cycler ͑Toscat-3100U; Toyo Corp.͒. The constant current density
was 18.6 mA/g ͑0.05 C͒.
planes was associated with the extent of electrolyte decomposition
and the prismatic planes ͑edge sites͒ were active sites for chemical/
electrochemical reactions.
The factors responsible for the irreversible capacity loss are still
a subject of intense research and debate. Both the catalytic proper-
ties and physical structure of graphite are believed to play important
roles in the irreversible capacity loss. In an effort to investigate the
irreversible capacity loss of graphite electrode for Li-ion secondary
batteries, we made new-type carbon materials with a core
Ϫ3
2
͑
graphite͒-shell ͑pyrolytic carbon͒ structure by a tumbling chemical
7
vapor deposition ͑CVD͒ process. In previous work, we reported
that the coating of pyrolytic carbon could reduce significantly the
irreversible capacity without the loss of reversible capacity. The
coating of pyrolytic carbon is a useful process for modifying the
ϩ
The irreversible capacity was defined as the difference between
the charge and discharge capacity at the first cycle. For a detailed
examination of the charge loss we subdivided the first charge curve
*
Electrochemical Society Active Member.
E-mail: hyszzz@lge.com
z