Patent Grant
8071238
This invention relates to electrode compositions useful in lithium-ion batteries, methods of making such compositions, and batteries including such compositions.
Metal alloys have been proposed as anodes for lithium ion batteries. These alloy-type anodes generally exhibit higher capacities relative to intercalation-type anodes such as graphite. One problem with such alloys, however, is that they often exhibit relatively poor cycle life and poor coulombic efficiency due to fragmentation of the alloy particles during the expansion and contraction associated with compositional changes in the alloys.
There is described an electrode composition for a lithium ion battery having the formula SixSnqMyCz where q, x, y, and z represent atomic percent values and (a) (q+x)>2y+z; (b) x>0, (c) each of q and z, independently, is ≧0; and (d) M is one or more metals selected from the group consisting of manganese, molybdenum, niobium, tungsten, tantalum, iron, copper, titanium, vanadium, chromium, nickel, cobalt, zirconium, yttrium, and combinations thereof. The Si, Sn, M, and C elements are arranged in the form of a multi-phase microstructure comprising: (a) an amorphous phase comprising silicon; (b) a nanocrystalline phase comprising a metal silicide; and (c) a phase comprising silicon carbide when z>0; and (d) an amorphous phase comprising Sn when q>0.
An “amorphous phase” is a phase that lacks long range atomic order and whose x-ray diffraction pattern lacks sharp, well-defined peaks.
A “nanocrystalline phase” is a phase having crystallites no greater than about 50 nanometers that exhibits long range atomic order and has an x-ray diffraction pattern characterized by sharp, well-defined peaks.
In some embodiments, the value of x may be chosen such that x≧60 and the value of z may be chosen such that z>0, z≧10, or z≧15. For example, in one embodiment, x≧60, ≧70, or even higher, z>0 or ≧10, and M is one or more metals selected from the group consisting of cobalt, nickel, iron, titanium, molybdenum, and combinations thereof. In another embodiment, M includes Co, x≧60, and z>0.
The electrode composition may be used as the anode for a lithium-ion battery that also includes a cathode and an electrolyte. The electrolyte may include any known electrolyte, e.g., fluoroethylene carbonate. Preferably, the anode is in the form of a composite that includes the electrode composition in combination with a binder (any known binder, e.g., a polyimide) and a conductive diluent (any known conductive diluent, e.g., carbon black).
The electrodes, when incorporated in lithium-ion batteries, exhibit good cycle life and coulombic efficiency.
The details of one or more embodiments of the invention are set forth in the accompanying drawings and the description below. Other features, objects, and advantages of the invention will be apparent from the detailed description and from the claims.
All numbers are herein assumed to be modified by the term “about.” The recitation of numerical ranges by endpoints includes all numbers subsumed within that range (e.g., 1 to 5 includes 1, 1.5, 2, 2.75, 3, 3.80, 4, and 5).
Electrode compositions are described that are particularly useful as anodes for lithium-ion batteries. The electrode compositions feature an electrode composition for a lithium ion battery having the formula SixSnqMyCz where q, x, y, and z represent atomic percent values and (a) (q+x)>2y+z; (b) q≧0, (c) z≧0; and (d) M is one or more metals selected from the group consisting of manganese, molybdenum, niobium, tungsten, tantalum, iron, copper, titanium, vanadium, chromium, nickel, cobalt, zirconium, yttrium, and combinations thereof. The Si, Sn, M, and C elements are arranged in the form of a multi-phase microstructure comprising: (a) an amorphous phase comprising silicon (thus, x>0); (b) a nanocrystalline phase comprising a metal silicide; and (c) a phase comprising silicon carbide when z>0; and (d) an amorphous phase comprising Sn when q>0.
Preferably, the electrode compositions are prepared by ball-milling silicon, the metal(s), and, in embodiments were carbon is used, a carbon source (e.g., graphite), under high shear and high impact for an appropriate period of time. Ball-mills such as a vertical ball mill (ATTRITOR, Union Process Inc., Akron, Ohio), a SPEXMILL (Spex CertiPrep, Metuchen, N.J.), a horizontal rotary ball mill (SIMOLOYER, Zoz GmbH, Werden, Germany) or other ball mills known in the art also may be used.
The electrode compositions are particularly useful as anodes for lithium-ion batteries. The anode preferably is a composite in which the electrode composition is combined with a binder and a conductive diluent. Examples of suitable binders include polyimides and polyvinylidene fluoride. Examples of suitable conductive diluents include carbon blacks.
To prepare a battery, the anode is combined with an electrolyte and a cathode (the counter electrode). The electrolyte may be in the form of a liquid, solid, or gel. Examples of solid electrolytes include polymeric electrolytes such as polyethylene oxide, fluorine-containing polymers and copolymers (e.g., polytetrafluoroethylene), and combinations thereof. Examples of liquid electrolytes include ethylene carbonate, diethyl carbonate, propylene carbonate, fluoroethylene carbonate (FEC), and combinations thereof. The electrolyte is provided with a lithium electrolyte salt. Examples of suitable salts include LiPF6, LiBF4, lithium bis(oxalato)borate, LiN(CF3SO2)2, LiN(C2F5SO2)2, LiAsF6, LiC(CF3SO2)3, and LiClO4. Examples of suitable cathode compositions include LiCoO2, LiCO0.2Ni0.8O2, and LiMn2O4. Additional examples include the cathode compositions described in the following documents, each of which is incorporated by reference in its entirety: (1) Lu et al., U.S. Pat. No. 6,964,828; (2) Lu et al., U.S. Pat. No. 7,078,128; (3) Le, U.S. Publ. Pat. Appln. No. 2004/0121234; (4) Dahn et al., U.S. Publ. Pat. Appln. No. 2003/0108793; (5) Eberman et al., U.S. Publ. Pat. Appln. No. 2005/0112054; (6) Dahn et al., U.S. Publ. Pat. Appln. No. 2004/0179993; (7) Obrovac et al., U.S. Pat. No. 6,680,145; and (8) Dahn et al., U.S. Pat. No. 5,900,385.
Silicon, iron, nickel, titanium, cobalt and tin were obtained from either Alfa Aesar of Ward Hill, Mass., Aldrich Chemical Company of Milwaukee, Wis. or Alcan Metal Powders of Berkeley, Calif.
X-ray diffraction patterns were collected using a Siemens Model Kristalloflex 805 D500 diffractometer equipped with a copper target x-ray tube and a diffracted beam monochromator. The data presented in the column labeled “Observed Phases from X-ray data” of Table 1A and Table 1B are based on the presence or absence of characteristic patterns of peaks obtained for each of the alloy samples listed. For example, a phase was considered to be amorphous when the X-ray diffraction pattern was absent or lacked sharp, well-defined peaks. The grain sizes of the crystalline phases were determined by the Scherer equation. When the grain size was calculated to be less than 50 nanometers, the phase was considered to be nanocrystalline.
Samples 1-14 listed in Table 1A were prepared by milling the recorded amounts of silicon chips (Alfa Aesar, catalog no. 00311), metal(s), and graphite powder (MCMB-1028, MMM Carob, Belgium) with 28 tungsten carbide balls ( 5/16-inches each, approximately 108 grams) for 4 hours in a 45 milliliter tungsten carbide vessel using a SPEX MILL (Model 8000-D, Spex CertiPrep, Metuchen, N.J.) under an argon atmosphere. The vessel was then opened, chunks of caked powder were broken up, and the milling was continued for an additional hour in an argon atmosphere. The temperature of the tungsten carbide vessel was maintained at about 30° C. by air cooling.
Examples 15-16 listed in Table 1A were prepared by the same general procedure as Examples 1-14 with the following differences. Silicon powder (325 mesh; Alfa Aesar, catalog no. 35662), tin powder (<10 microns, Aldrich, catalog no. 520373) and metal powders (Cobalt, 1.6 microns; Alfa Aesar, catalog no. 10455C Alfa Aesar; Nickel, Alcan Metal Powder, Type 123) were used. Examples 15 and 16 were milled with 14 tungsten carbide balls (0.415 millimeter diameter; approximately 54 grams total weight) in the SPEX MILL for 16 hours in an argon atmosphere. The temperature of the tungsten carbide vessel was maintained at about 30° C. by air cooling
Each of the Examples 1-16 listed in Table 1A was formed into an electrode and characterized in an electrochemical cell that had a lithium metal counter electrode. The electrodes were prepared by the following procedure. An amount of 1.8 g of the milled material, 0.06 g conductive carbon (SUPER P from MMM Carbon, Belgium) and 0.70 g PI2555 (PYRALIN PI2555, a 20 weight percent solution in N-methyl-2-pyrrolidinone from HD Microsystems, Cheesequake Road, Parlin, N.J.) were mixed in a 45-milliliter stainless steel vessel using four tungsten carbide balls (12.75 mm diameter). The mixing was done in a planetary micro mill (PULVERISETTE 7, from Fritsch GmbH, Idon-Oberstein, Germany) at a speed setting of 3 for 2 hours. The resulting solution was then coated onto a 13 micrometer thick copper foil using a notch bar coating die with a 0.0075 inch (76.2 micrometer) gap. The coating was dried in a vacuum oven at 150° C. for 2 hours, and then used to construct 2325 coin cells consisting of a 380 micrometer thick metallic lithium foil counter electrode, two layers of a flat sheet polypropylene membrane separator (CELGARD 2400, from CELGARD Inc., Charlotte, N.C.), and 1 M LiPF6 in an electrolyte (mixture containing 90 parts of 1:2 volume mixture of ethylene carbonate and diethyl carbonate and 10 parts of fluoroethylene carbonate from SynQuest Laboratories of Alachua, Fla.). This mixture was dried over molecular sieves (3A type) for 12 h before use. The 2325 coin cell hardware is described in A. M. Wilson and J. R. Dahn, J. Electrochem. Soc., 142, 326-332 (1995).
Electrochemical cells prepared from Examples 1-16 were cycled between 0.9 V and 5 mV using a cell tester (Maccor Inc., Tulsa Okla.). The 200 mA/gram current was allowed to relax to 10 mA/gram, at the lower voltage cutoff, before the next charge cycle. The measured charge efficiency and coulombic efficiency values were recorded in Table 2.
Example 17 was prepared by melting 65.461 grams of silicon lumps (Alfa Aesar/99.999%, catalog no. 39101), 18.596 grams of iron pieces (AlfaAesar/99.97%, catalog no. 10454) and 15.943 grams of titanium sponge (Alfa Asear/99.7%, catalog no. 10582) in an ARC furnace. The alloy ingot (Si70Fe10Ti10) was broken into small chunks and was treated in a hammer mill to produce 150-micron size powder. The Si70Fe10Ti10 alloy powder (3.8462 g) and graphite (0.1528 g, SFG44/Tim Rex) were milled in the SPEX MILL together with 28 tungsten carbide balls (10.5 millimeter each, total weight 108 grams) for 1 hour in a 45-milliliter tungsten carbide vessel (Model 8001, Spex CertiPrep, Metuchen, N.J.) filled with argon. The vessel was cooled with air jet during milling. The vessel temperature was about 30° C. during milling.
Example 18 was prepared by milling 3.9409 grams of Si70Fe10Ti10 alloy powder made by the procedure of Example 17 and 0.0591 grams of graphite in the SPEX MILL as in Example 17.
Example 19 was prepared by the same procedure as in Example 17, except by using 64.605 g of silicon lumps, 27.528 g of iron pieces and 7.867 g of titanium sponge to prepare the Si70Fe15Ti5 alloy powder. Then 3.8481 g of Si70Fe15Ti5 alloy powder and 0.1519 g of graphite were milled in the SPEX MILL as in Example 17.
Example 20 was prepared by milling 3.9417 g of Si70Fe15Ti5 alloy powder made by the procedure of Example 19 and 0.0583 g of graphite in the PSEX MILL as in Example 17.
Each of the Examples 17-20 was formed into an electrode and characterized in an electrochemical cell that had a lithium counter electrode. The electrodes containing Examples 17-20 were prepared by the following procedure. A sample of the milled material (1.84 g), conductive carbon (0.024 g, Ketjen Black, Akzo Nobel) and NMP (2 g) were mixed in a 45-mL stainless steel vessel using four tungsten carbide balls (12.5 millimeter each) in the planetary micro mill at a speed setting of 1 for 30 minutes, then PYRALIN PI2555 (0.68 g, 20 wt % PI2555 solids in NMP) was added and mixed at a speed setting of 2 for 1 hour. The resulting solution was coated onto a 13-micron thick copper foil using a notch bar coating die set with a 125 micrometer gap. The coated sample was dried in a vacuum oven at 150° C. for 2 hours. Disks (16-mm diameter) were punched from the coating.
The coatings prepared from Examples 17-20 were tested in 2325 coins cells assembled in the same manner as for Example 1. The coins cells prepared with Examples 17-20 were cycled as for Example 1, except a current density of 250 mA/gram-alloy was used and a 15 minute period at open circuit was used at the end of each half-cycle. The measured charge efficiency and coulombic efficiency values were recorded in Table 2.
Example 21 was prepared by milling 903.602 g silicon powder (−100+325 mesh, Globe Metallurgical Inc., Beverly, Ohio), 406.307 g of cobalt (99.8% pure, 1.6 μm particles from Alfa Aesar, catalog no. 10455C), 134.885 g nickel powder (99.9% pure, 2-3 μm particles, Alfa Aesar, catalog no. 10255) and 55.206 g graphite powder (Timrex SFG44, TimCal Ltd., Bodio, Switzerland) with 25 kg of chrome steel balls (5 mm, 100Cr6 steel) in a high-impact, horizontal mill (Simoloyer, CM20-Solm, Zoz GmbH) at 550 rpm for 45 seconds and then at 300 rpm for 15 seconds in repeated cycles. Example 21 was milled for a total of three hours. Examples 22 and 23 were prepared by the same procedure as Example 21, except the milling times were 5 h and 7.5 h, respectively.
Each of the Examples 21-23 was formed into an electrode and characterized in an electrochemical cell, as in Example 17, and the cells were cycled by the same procedure as Example 17. Each of these Examples included an amorphous phase comprising silicon. The specific capacity (mAh/g) of each of these materials after 30 cycles was: Example 21, 1220; Example 22, 1050; and Example 23, 920.
A number of embodiments of the invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the invention. Accordingly, other embodiments are within the scope of the following claims.
This application is a continuation of U.S. application Ser. No. 11/469,561, filed Sep. 1, 2006, now U.S Pat. No. 7,906,238 now allowed, which claims priority to Provisional U.S. Application No. 60/743,075, filed Dec. 23, 2005, the disclosure of which is incorporated by reference in its entirety herein.
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| Child | 13009981 | US |
