Nickel-metal hydride battery and method for producing hydrogen storage alloy

Abstract

It is an object of the present invention to improve the cycle performance in a nickel-metal hydride battery using a rare earth-MgNi type alloy. The present invention provides a nickel-metal hydride battery having a negative electrode including an LaMgNi based hydrogen absorbing alloy, wherein the hydrogen absorbing alloy has a crystal phase having Gd.sub.2Co.sub.7 type crystal structure and contains calcium.

Claims

1. A nickel-metal hydride battery comprising a negative electrode, the negative electrode including an LaMgNi based hydrogen absorbing alloy, wherein said hydrogen absorbing alloy has a crystal phase having Gd.sub.2Co.sub.7 type crystal structure and said hydrogen absorbing alloy contains calcium; wherein said hydrogen absorbing alloy has a layered structure of a plurality of crystal phases layered in a c-axis direction of the crystal structure; wherein the content of the crystal phase having said Gd.sub.2Co.sub.7 type crystal structure is 76% by mass or higher; wherein the content of the magnesium in said hydrogen absorbing alloy is 3.3% by atom or higher and 5.6% by atom or lower; and wherein the content of said calcium in said hydrogen absorbing alloy is 0.7% by atom or higher and 9.5% by atom or lower.

2. A nickel-metal hydride battery comprising a negative electrode, the negative electrode including an RMgNi based hydrogen absorbing alloy, wherein R comprises a rare earth element; wherein said hydrogen absorbing alloy has a crystal phase having Gd.sub.2Co.sub.7 type crystal structure and said hydrogen absorbing alloy contains calcium; wherein said hydrogen absorbing alloy has a layered structure of a plurality of crystal phases layered in a c-axis direction of the crystal structure; wherein the content of the crystal phase having said Gd.sub.2Co.sub.7 type crystal structure is 76% by mass or higher; wherein the content of the magnesium in said hydrogen absorbing alloy is 3.3% by atom or higher and 5.6% by atom or lower; wherein the content of said calcium in said hydrogen absorbing alloy is 0.7% by atom or higher and 9.5% by atom or lower; and wherein a number of Ni atoms is at least 3 and at most 5 times as much as a sum of the numbers of R atoms, Mg atoms, and Ca atoms.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1: A drawing showing Gd.sub.2Co.sub.7 type crystal structure.

(2) FIG. 2: A graph formed by plotting the results of Examples and Comparative Examples, showing the content of Ca in the abscissa axis and capacity retention ratio in the ordinate axis.

(3) FIG. 3: A graph formed by plotting results of Examples and Comparative Examples, showing the content of Gd.sub.2Co.sub.7 phase in the abscissa axis and capacity retention ratio in the ordinate axis.

(4) FIG. 4: A graph formed by plotting results of Examples and Comparative Examples, showing the content of Ca in the abscissa axis and the content of Gd.sub.2Co.sub.7 phase in the ordinate axis.

BEST MODE FOR CARRYING OUT THE INVENTION

(5) The nickel-metal hydride battery of the present invention is a nickel-metal hydride battery having a negative electrode including an LaMgNi type hydrogen absorbing alloy, wherein the hydrogen absorbing alloy has a crystal phase having Gd.sub.2Co.sub.7 type crystal structure (hereinafter, simply referred to also as Gd.sub.2Co.sub.7 phase) and contains calcium.

(6) The Gd.sub.2Co.sub.7 type crystal structure is, as shown in FIG. 1, a crystal structure formed by inserting 2 units of AB.sub.5 unit between A.sub.2B.sub.4 units and belongs to a rhombohedral crystal system and has a R-3m space group.

(7) Herein, the A.sub.2B.sub.4 unit is a crystal lattice having a hexagonal MgZn.sub.2 type crystal structure (C14 structure) or a hexagonal MgCu.sub.2 type crystal structure (C15 structure) and the AB.sub.5 units is a crystal lattice having a hexagonal CaCu.sub.5 type crystal structure.

(8) Further, in general, A represents any element selected from the group consisting of rare earth elements and Mg and B represents any element selected from the group consisting of transition metal elements and Al.

(9) The content of the Gd.sub.2Co.sub.7 phase is preferably 3% by mass or higher, more preferably 5% by mass or higher, even preferably 20% by mass or higher, and particularly more preferably 70% by mass or higher in the hydrogen absorbing alloy.

(10) The cycle performance of the nickel-metal hydride battery can be further improved by adjusting the content of the crystal phase having Gd.sub.2Co.sub.7 type crystal structure to the above range.

(11) The hydrogen absorbing alloy may also have, as another crystal phase, a crystal phase having a hexagonal Pr.sub.5Co.sub.19 type crystal structure (hereinafter, simply referred to also as Pr.sub.5Co.sub.19 phase), a crystal phase having a rhombohedral Ce.sub.5Co.sub.19 type crystal structure (hereinafter, simply referred to also as Ce.sub.5Co.sub.19 phase), and a crystal phase having a hexagonal Ce.sub.2Ni.sub.7 type crystal structure (hereinafter, simply referred to also as Ce.sub.2Ni.sub.7 phase) and may preferably have the Pr.sub.5Co.sub.19 phase and the Ce.sub.5Co.sub.19 phase.

(12) Herein, the Pr.sub.5Co.sub.19 type crystal structure is a crystal structure formed by inserting 3 units of AB.sub.5 unit between A.sub.2B.sub.4 units; the Ce.sub.5Co.sub.19 type crystal structure is a crystal structure formed by inserting 3 units of AB.sub.5 unit between A.sub.2B.sub.4 units; and the Ce.sub.2Ni.sub.7 type crystal structure is a crystal structure formed by inserting 2 units of AB.sub.5 unit between A.sub.2B.sub.4 units.

(13) The crystal structures of the respective crystal phases having the crystal structures can be specified by, for example, carrying out X-ray diffractometry for pulverized alloy powders and analyzing the obtained X-ray diffraction pattern by the Rietveld method.

(14) Further, the content of the calcium contained in the hydrogen absorbing alloy is preferably adjusted to 0.7% by atom or higher and 9.5% by atom or lower, more preferably 1.1% by atom or higher and 4.4% by atom or lower, and particularly preferably 1.1% by atom or higher and 4.3% by atom or lower.

(15) The cycle performance of the nickel-metal hydride battery can be further improved by adjusting the content of the calcium in the hydrogen absorbing alloy in the above range.

(16) Moreover, from the viewpoint of an increase of the content of the crystal phase having Gd.sub.2Co.sub.7 type crystal structure, the amount of magnesium to be added is preferably adjusted to 1.1% by atom or higher, more preferably 2.2% by atom or higher, even preferably 3.3% by atom or higher, and particularly preferably 4.0% by atom or higher and from the same viewpoint, it is preferably adjusted to less than 5.8% by atom, more preferably 5.6% by atom or lower, even preferably 5.5% by atom or lower, and particularly preferably 5.0% by atom or lower.

(17) In general, an LaMgNi based hydrogen absorbing alloy means an alloy containing rare earth elements, Mg, and Ni and having the number of Ni atoms more than 3 times and less than 5 times as much as the total number of rare earth elements and Mg atoms; however in the present invention, since Ca is contained, the LaMgNi type hydrogen absorbing alloy is an alloy containing rare earth elements, Mg, and Ni and having the number of Ni atoms more than 3 times and less than 5 times as much as the total number of rare earth elements, Mg atoms, and Ca atoms added according to the present invention.

(18) The composition of the alloy is preferably an alloy represented by the following general formula (1):
R1.sub.vCa.sub.wMg.sub.xNi.sub.yR2.sub.z(1).

(19) In the above general formula, R1 is one or more elements selected from the group consisting of Y and rare earth elements and is preferably one or more elements selected from the group consisting of La, Ce, Pr, Nd, Sm, and Y.

(20) R2 is one or more elements selected from the group consisting of Co, Cu, Mn, Al, Cr, Fe, Zn, V, Nb, Ta, Ti, Zr, and Hf and is preferably one or more elements selected from the group consisting of Co and Al.

(21) Further, v, w, x, y, and z are numerals satisfying v+w+x+y+z=100; v is a numeral satisfying 6.7v17.9 and preferably a numeral satisfying 11.3v16.7; w is a numeral satisfying 0.7w9.5 and preferably a numeral satisfying 1.1w4.4; x is a numeral satisfying 1.1x5.6 and preferably a numeral satisfying 3.3x5.6; y is a numeral satisfying 73.3y78.7 and preferably a numeral satisfying 74.4y78.3; and z is a numeral satisfying 0z4.4 and preferably a numeral satisfying 0z3.3.

(22) Particularly, in the present invention, an alloy satisfying 3.3(y+z)/(v+w+z)3.7 in the above composition may be more preferably used. Use of the alloy with such composition can provide an effect such that hydrogen can be reversely absorbed and desorbed in around normal temperature and normal pressure and a high hydrogen absorbing capacity can be shown.

(23) Further, in the present invention, the LaMgNi based hydrogen absorbing alloy preferable has a layered structure of a plurality of crystal phases layered in the c-axis direction of the crystal structure. In the alloy with such a structure, the function effect of Ca addition as described above tends to be easily exhibited and the cycle performance of the nickel-metal hydride battery can be furthermore improved.

(24) Next, a method of producing the nickel-metal hydride battery of the present invention will be described.

(25) A method of producing a hydrogen absorbing alloy as one embodiment involves a melting step of melting alloy raw materials blended to give the prescribed composition ratio, a cooling step of quenching and solidifying the melted raw materials at a cooling rate of 1000 K/s or higher, and an annealing step of annealing the cooled alloy under inert gas atmosphere in pressurized state at the temperature of 860 C. or higher and 1000 C. or lower.

(26) The respective steps will be specifically described and first, prescribed amounts of raw material ingots (alloy raw materials) are weighed based on the chemical composition of an aimed hydrogen absorbing alloy.

(27) In the melting step, the alloy raw materials are put in a crucible and heated at, for example, 1200 C. or higher and 1600 C. or lower under inert gas atmosphere or in vacuum by using a high frequency melting furnace to melt the alloy raw materials.

(28) In the cooling step, the melted alloy raw materials are cooled and solidified. The cooling rate is preferably 1000 K/s or higher (also called as quenching). Quenching at 1000 K/s or higher is effective to make the alloy composition very fine and homogeneous. Further, the cooling rate may be set in a range of 1000000 K/s or lower.

(29) Further, in the cooling step, as the cooling rate becomes faster, the amount of CaCu.sub.5 phase to be produced in the solidified alloy is lessened and if the rate exceeds a certain rate, it tends to be constant. Since the discharge capacity is improved by lessening the amount of the CaCu.sub.5 phase to be produced, it is preferable to adjust the cooling rate capable of lessening the amount of the CaCu.sub.5 phase to be produced as described above, and particularly, it is preferable to adjust the cooling rate to the rate at which the amount to be produced tends to be constant.

(30) From such a viewpoint, as the cooling method, those so-called quenching, specifically, a melt spinning method or a gas atomization method may be employed, and particularly, a melt spinning method at a cooling rate of 100000 K/s or higher and a gas atomization method at a cooling rate of 10000 K/s are more preferably employed.

(31) In the annealing step, under inert gas atmosphere in pressurized state, heating to 860 C. or higher and 1000 C. or lower is carried out by using, for example, an electric furnace or the like. The pressurizing condition may be preferably 0.2 MPa (gauge pressure) or higher and 1.0 MPa (gauge pressure) or lower. The treatment time in the annealing step is preferably adjusted to 3 hours or longer and 50 hours or shorter.

(32) The hydrogen absorbing alloy obtained in such a manner tends to have a layered structure of a plurality of crystal phases layered in the c-axis direction of the crystal structure and particularly, use of the above alloy raw materials makes it possible to give the hydrogen absorbing alloy which tends to have a crystal phase having Gd.sub.2Co.sub.7 type crystal structure.

(33) The hydrogen absorbing alloy electrode of the present invention has, for example, the hydrogen absorbing alloy produced as described above as a hydrogen absorbing medium. At the time of using the hydrogen absorbing alloy as a hydrogen absorbing medium for an electrode, the hydrogen absorbing alloy is preferably used after pulverization.

(34) Pulverization of the hydrogen absorbing alloy at the time of electrode production may be carried out either before or after the annealing. However, since the surface area becomes large by pulverization, it is preferable to carry out pulverization after annealing from the viewpoint of prevention of surface oxidation of the alloy. The pulverization is preferably carried out under inert atmosphere in order to prevent oxidation of the alloy surface.

(35) For the pulverization, for example, mechanical pulverization or hydrogenation pulverization may be employed.

(36) The hydrogen absorbing alloy electrode can be produced by mixing the hydrogen absorbing alloy powders obtained in the above-mentioned manner with a binder such as a resin composition or a rubber composition and pressure-molding the obtained mixture in a prescribed shape. The nickel-metal hydride battery of the present invention can be produced by using the hydrogen absorbing alloy electrode as a negative electrode and an electrode made of nickel hydroxide separately produced as a positive electrode and packing an aqueous potassium hydroxide solution as an electrolyte solution.

EXAMPLES

(37) Hereinafter, the present invention will be more specifically described with reference to Examples and Comparative Examples. However, the present invention should not be limited to the following Examples.

Example 1

Production of LaMgNi Type Hydrogen Absorbing Alloy

(38) Prescribed amounts of raw material ingots to give chemical composition of La.sub.17.9Ca.sub.0.7Mg.sub.4.7Ni.sub.76.7 were weighed and the raw materials were put in a crucible and heated to 1500 C. under argon atmosphere in reduced pressure by using a high frequency melting furnace to melt the materials. After the melting, quenching was carried out by employing a melt spinning method to solidify an alloy.

(39) Next, after heated at 910 C. under argon atmosphere pressurized to 0.2 MPa (gauge pressure, the same applies hereinafter), the obtained hydrogen absorbing alloy was pulverized to obtain a hydrogen absorbing alloy powder with an average particle diameter (D50) of 20 m.

(40) Measurement of Crystal Structure and Calculation of Existence Ratio

(41) The obtained hydrogen absorbing alloy powder was subjected to a measurement under the condition of 40 kV and 100 mA (Cu bulb) by using an X-ray diffraction apparatus (manufactured by Bruker AXS, product number M06XCE). Further, analysis by Rietveld method (analysis soft: RIETAN2000) was carried out for structure analysis and the ratio of the crystal phases produced in each hydrogen absorbing alloy was calculated. The results are shown in Table 2.

(42) Measurement of Capacity Retention Ratio of Nickel-Metal Hydride Battery (Opened Type Cell)

(43) 1) Production of Electrodes

(44) An opened type nickel-metal hydride battery was produced by using the above-mentioned hydrogen absorbing alloy powder for a negative electrode. Specifically, a paste obtained by adding 3 parts by weight of a nickel powder (manufactured by INCO, #210) to 100 parts by weight of the hydrogen absorbing alloy powder obtained in the above-mentioned manner to be mixed, adding an aqueous solution in which a thickener (methyl cellulose) was dissolved, and further adding 1.5 parts by weight of a binder (styrene butadiene rubber) was applied to both surfaces of a punched steel plate with a thickness of 45 m (porosity 60%) and dried and thereafter pressed to the thickness of 0.36 mm to obtain a negative electrode. On the other hand, a sintered nickel hydroxide electrode in an excess capacity was employed as a positive electrode.

(45) 2) Production of Opened Type Cell

(46) The electrode produced in the above-mentioned manner was sandwiched with the positive electrode through a separator interposed therebetween and these electrodes were fixed with bolts in a manner of applying a pressure of 1 kgf/cm.sup.2 to the electrodes to assemble an opened type cell.

(47) A mixed solution of a 6.8 mol/L KOH solution and a 0.8 mol/L LiOH solution was used as an electrolyte solution.

(48) 3) Evaluation of Capacity Retention Ratio

(49) In a water tank at 20 C., 50 cycles each involving 150% charge at 0.1 ItA and discharge to give a cutoff voltage of 0.6 V (relatively to Hg/HgO) at 0.2 ItA were repeated. The discharge capacity at the 50th cycle to the maximum discharge capacity was calculated as the capacity retention ratio (%).

Examples 2 to 11 and Comparative Examples 1 to 10

(50) Nickel-metal hydride batteries of the following Examples and Comparative Examples were produced in the same manner as in Example 1, except that hydrogen absorbing alloys with different contents of Ca as shown in the following Table 1 or hydrogen absorbing alloys having different crystal phases were used and similarly, evaluations of the maximum discharge capacity and the capacity retention ratio were carried out. The ratio of the crystal phases of the obtained alloys and the evaluation results of the capacity retention ratio were shown in Table 2 and based on the data obtained from Table 2, a graph formed by plotting the obtained results is shown in FIG. 2, showing the content of Ca in the abscissa axis and capacity retention ratio in the ordinate axis.

(51) TABLE-US-00001 TABLE 1 Alloy composition (% by atom) La Ce Pr Nd Sm Y Ca Mg Ni Co Mn Al Example 1 17.9 0.0 0.0 0.0 0.0 0.0 0.7 4.7 76.7 0.0 0.0 0.0 Example 2 16.7 0.0 0.0 0.0 0.0 0.0 1.1 4.4 77.8 0.0 0.0 0.0 Example 3 16.3 0.0 0.0 0.0 0.0 0.0 2.3 4.7 76.7 0.0 0.0 0.0 Example 4 13.3 0.0 0.0 0.0 0.0 0.0 3.3 5.6 77.8 0.0 0.0 0.0 Example 5 11.1 2.2 0.0 0.0 0.0 0.0 4.3 3.7 78.7 0.0 0.0 0.0 Example 6 10.2 0.0 1.1 0.0 0.0 0.0 6.5 4.4 74.4 0.0 0.0 3.3 Example 7 7.2 0.0 1.1 0.0 0.0 0.0 9.5 4.4 77.8 0.0 0.0 0.0 Example 8 5.6 0.0 0.0 1.1 0.0 0.0 11.1 4.4 77.8 0.0 0.0 0.0 Example 9 9.4 0.0 0.0 0.0 4.3 0.0 1.5 4.3 76.1 0.0 0.0 4.3 Example 10 14.4 0.0 0.0 0.0 0.0 0.0 2.7 3.8 77.1 0.0 0.0 2.1 Example 11 7.9 0.0 0.0 0.0 0.0 0.0 8.8 5.8 77.5 0.0 0.0 0.0 Comparative 17.8 0.0 0.0 0.0 0.0 0.0 0.0 4.4 77.8 0.0 0.0 0.0 Example 1 Comparative 12.5 0.0 4.2 0.0 0.0 0.0 0.0 4.2 71.9 4.2 0.0 3.1 Example 2 Comparative 14.3 0.0 0.0 0.0 0.0 0.0 5.3 3.4 72.4 0.0 2.3 2.3 Example 3 Comparative 11.6 0.0 0.0 0.0 0.0 0.0 7.0 4.7 72.1 0.0 0.0 4.7 Example 4 Comparative 4.2 1.0 0.7 0.8 0.0 0.0 10.0 0.0 71.7 5.0 3.3 3.4 Example 5 Comparative 17.5 0.0 0.0 0.0 0.0 0.0 0.0 7.5 75.0 0.0 0.0 0.0 Example 6 Comparative 14.3 0.0 0.0 0.0 0.0 0.0 2.0 8.3 75.4 0.0 0.0 0.0 Example 7 Comparative 11.8 0.0 0.0 0.0 0.0 0.0 5.8 7.5 75.0 0.0 0.0 0.0 Example 8 Comparative 9.6 0.0 0.0 0.0 0.0 0.0 7.9 7.5 75.0 0.0 0.0 0.0 Example 9 Comparative 5.5 0.0 0.0 0.0 0.0 0.0 12.0 7.5 75.0 0.0 0.0 0.0 Example 10

(52) TABLE-US-00002 TABLE 2 Maximum Capacity discharge retention Ratio of crystal phases (% by mass) capacity ratio Gd.sub.2Co.sub.7 PuNi.sub.3 CaCu.sub.5 Ce.sub.2Ni.sub.7 Ce.sub.5Co.sub.19 [mAh/g] [%] Example 1 58 2 18 23 0 372 91 Example 2 55 0 2 0 43 382 94 Example 3 80 0 1 0 19 387 95 Example 4 76 2 0 0 22 392 95 Example 5 58 2 1 0 40 377 95 Example 6 35 3 5 11 47 382 92 Example 7 48 1 21 28 2 380 89 Example 8 45 1 18 36 1 375 87 Example 9 2 1 59 32 7 351 88 Example 10 1 0 55 41 3 367 86 Example 11 2 71 17 1 10 385 82 Comparative 45 1 17 34 3 360 87 Example 1 Comparative 1 5 38 35 21 344 88 Example 2 Comparative 0 0 51 39 10 374 85 Example 3 Comparative 0 0 48 47 5 382 82 Example 4 Comparative 0 0 100 0 0 355 80 Example 5 Comparative 0 56 31 0 13 377 85 Example 6 Comparative 0 60 27 0 13 381 84 Example 7 Comparative 0 62 19 2 17 384 83 Example 8 Comparative 0 84 15 1 0 390 82 Example 9 Comparative 0 68 29 3 0 389 81 Example 10

(53) As a result of measurement of the crystal structure, the hydrogen absorbing alloys obtained in Examples and Comparative Examples (except Comparative Example 5) were found all having a layered structure of a plurality of crystal phases layered in the c-axis direction of the crystal structure.

(54) Further, as shown in Table 2 and FIG. 2, Comparative Examples in which Ca atoms were added to hydrogen absorbing alloys scarcely containing Gd.sub.2Co.sub.7 phase were found having no improvement effect of the capacity retention ratio; and on the other hand, Examples in which Ca atoms were added to LaMgNi based hydrogen absorbing alloys containing the Gd.sub.2Co.sub.7 phase were found having improved capacity retention ratio and particularly, in the case of alloys containing 3% by mass or higher of Gd.sub.2Co.sub.7 phase or alloys having the amount of Ca to be added of 0.7% by atom or higher and 9.5% by atom or lower, it was found that the capacity retention ratio was remarkably improved.

(55) In addition, although the capacity retention ratios of Examples 9, 10, and 11 had low values as compared with those of other Examples, the capacity retention ratios were improved as compared with those in the case of the same conditions except that Gd2Co7 phase was less.

Examples 12 to 18 and Comparative Examples 11 and 12

(56) Nickel-metal hydride batteries of the following Examples and Comparative Examples were produced in the same manner as in Example 1, except that hydrogen absorbing alloys with different contents of mainly Gd.sub.2Co.sub.7 phase, as shown in the following Table 3 and Table 4, were used and similarly, the capacity retention ratio was evaluated. The evaluation results of the maximum discharge capacity and capacity retention ratio are shown in Table 4, and based on the data obtained from Table 4, a graph formed by plotting the obtained results is shown in FIG. 3, showing the content of Gd.sub.2Co.sub.7 phase in the abscissa axis and capacity retention ratio in the ordinate axis. Example 17 and Comparative Example 12 were the same experimental examples of Example 4 and Comparative Example 10, respectively. FIG. 3 together shows the data of Example 9.

(57) TABLE-US-00003 TABLE 3 Alloy composition (% by atom) La Ce Pr Nd Sm Y Ca Mg Ni Co Mn Al Example 12 13.4 0.0 0.0 3.3 0.0 0.0 1.1 3.9 78.3 0.0 0.0 0.0 Example 13 10.2 0.0 0.0 1.1 0.0 0.0 6.5 4.4 77.8 0.0 0.0 0.0 Example 14 11.1 0.0 0.0 0.0 2.2 0.0 4.4 4.4 73.3 1.8 0.0 2.6 Example 15 11.1 0.0 0.0 2.2 0.0 0.0 5.6 3.3 77.8 0.0 0.0 0.0 Example 16 11.1 0.0 0.0 0.0 0.0 2.2 4.4 4.4 74.4 0.0 0.0 3.3 Example 17(4) 11.1 0.0 2.2 0.0 0.0 0.0 3.3 5.6 77.8 0.0 0.0 0.0 Example 18 11.1 0.0 0.0 2.2 0.0 0.0 4.4 4.4 77.8 0.0 0.0 0.0 Comparative 15.5 0.0 0.0 0.0 0.0 0.0 3.6 2.1 78.7 0.0 0.0 0.0 Example 11 Comparative 5.5 0.0 0.0 0.0 0.0 0.0 12.0 7.5 75.0 0.0 0.0 0.0 Example 12(10)

(58) TABLE-US-00004 TABLE 4 Maximum Capacity discharge retention Ratio of crystal phases (% by mass) capacity ratio Gd.sub.2Co.sub.7 PuNi.sub.3 CaCu.sub.5 Ce.sub.2Ni.sub.7 Ce.sub.5Co.sub.19 [mAh/g] [%] Comparative 0 2 26 71 2 379 87 Example 11 Comparative 0 68 29 3 0 389 81 Example 12(10) Example 12 5 1 23 69 3 382 91 Example 13 8 1 3 0 88 390 92 Example 14 22 4 2 0 73 368 93 Example 15 31 1 12 2 54 378 94 Example 16 48 1 2 0 49 375 94 Example 17(4) 76 2 0 0 22 392 95 Example 18 83 0 0 0 17 383 95

(59) As a result of measurement of the crystal structure, the hydrogen absorbing alloys obtained in Examples and Comparative Examples were found all having a layered structure of a plurality of crystal phases layered in the c-axis direction of the crystal structure.

(60) Further, as shown in Table 4 and FIG. 3, it was found that the capacity retention ratio was also increased as the content ratio of Gd.sub.2Co.sub.7 phase was increased and specifically, if the Gd.sub.2Co.sub.7 phase was contained in 3% by mass or higher in the LaMgNi based hydrogen absorbing alloy, the capacity retention ratio exceeded 90%; if it was contained in 5% by mass or higher, the capacity retention ratio was 91% or higher; if it was contained in 20% by mass or higher, the capacity retention ratio exceeded about 93%; if it was contained in 22% by mass or higher, the capacity retention ratio was further heightened; if it was contained in 70% by mass or higher, the capacity retention ratio exceeded about 95%; and if it was contained in 76% by mass or higher, the capacity retention ratio was most excellent and thus it was found that a significant effect was exhibited.

Examples 19 to 26 and Comparative Examples 13 and 14

(61) Hydrogen absorbing alloy powders were produced in the same manner as in Example 1, except that Mg contents mainly differ as shown in the following Table 5 and the ratios of produced crystal phases were measured. Further, nickel-metal hydride batteries were produced in the same manner as in Example 1 and similarly, the capacity retention ratio was evaluated. The obtained evaluation results are shown in Table 6, and a graph formed by plotting the obtained results is shown in FIG. 4, showing the content of Mg in the abscissa axis and the content ratio of Gd.sub.2Co.sub.7 phase in the ordinate axis.

(62) TABLE-US-00005 TABLE 5 Alloy composition (% by atom) La Ce Pr Nd Sm Y Ca Mg Ni Co Mn Al Comparative 4.2 1.0 0.7 0.8 0.0 0.0 10.0 0.0 71.7 5.0 3.3 3.4 Example 13(5) Example 19 16.7 0.0 0.0 0.0 0.0 0.0 4.4 1.1 77.8 0.0 0.0 0.0 Example 20 15.6 0.0 0.0 0.0 0.0 0.0 4.4 2.2 77.8 0.0 0.0 0.0 Example 21(15) 11.1 0.0 0.0 2.2 0.0 0.0 5.6 3.3 77.8 0.0 0.0 0.0 Example 22(5) 11.1 2.2 0.0 0.0 0.0 0.0 4.3 3.7 78.7 0.0 0.0 0.0 Example 23(18) 11.1 0.0 0.0 2.2 0.0 0.0 4.4 4.4 77.8 0.0 0.0 0.0 Example 24 17.4 0.0 0.0 0.0 0.0 0.0 1.2 4.7 76.7 0.0 0.0 0.0 Example 25 14.4 0.0 0.0 0.0 0.0 0.0 2.2 5.6 77.8 0.0 0.0 0.0 Example 26(11) 7.9 0.0 0.0 0.0 0.0 0.0 8.8 5.8 77.5 0.0 0.0 0.0 Comparative 14.3 0.0 0.0 0.0 0.0 0.0 2.0 8.3 75.4 0.0 0.0 0.0 Example 14(7)

(63) TABLE-US-00006 TABLE 6 Maximum Capacity discharge retention Ratio of crystal phases (% by mass) capacity ratio Gd.sub.2Co.sub.7 PuNi.sub.3 CaCu.sub.5 Ce.sub.2Ni.sub.7 Ce.sub.5Co.sub.19 [mAh/g] [%] Comparative 0 0 100 0 0 355 80 Example 13(5) Example 19 3 8 15 52 22 315 71 Example 20 8 4 9 61 18 331 78 Example 21(15) 31 1 12 2 54 378 94 Example 22(5) 58 2 1 0 40 377 95 Example 23(18) 83 0 0 0 17 383 95 Example 24 76 0 2 1 21 385 94 Example 25 20 1 6 7 66 390 93 Example 26(11) 2 71 17 1 10 385 82 Comparative 0 60 27 0 13 381 84 Example 14(7)

(64) As a result of measurement of the crystal structure, the hydrogen absorbing alloys obtained in Examples and Comparative Examples (except Comparative Example 13) were found all having a layered structure of a plurality of crystal phases layered in the c-axis direction of the crystal structure.

(65) Further, as shown in Table 6 and FIG. 4, it was found that in a case where no Mg was contained or the content of Mg was 5.8% by atom or higher, the production ratio of Gd.sub.2Co.sub.7 phase was less than 3% by mass, and thus no hydrogen absorbing alloy to be used for the present invention could be obtained.

(66) In addition, although the capacity retention ratios of Examples 19 and 20 were low values as compared with those of other Examples, the capacity retention ratios were improved as compared with those in a case where the content of Mg was less than 3.3% by atom and the production ratio of Gd.sub.2Co.sub.7 phase was less.

Example 27

(67) A hydrogen absorbing alloy powder was produced in the same condition as that of Example 1, except that the melted raw materials were solidified by a gas atomization method and an opened type cell was assembled in the same procedure as that of Example 1. The ratio of crystal phases produced in the hydrogen absorbing alloy of Example 27 was substantially the same as that of Example 1. The maximum discharge capacity and the capacity retention ratio of the opened type cell of Example 27 were also substantially the same as those of Example 1.