JP5588214B2 - Rolling bearing - Google Patents

Description

  The present invention relates to a rolling bearing, and more specifically to a rolling bearing provided with a cage made of a magnesium alloy.

  As a cage for holding rolling elements of a rolling bearing, a metal cage made of steel or brass may be used. Such a metal cage is excellent in strength, but has a problem of high cost when processed into a complicated shape. Further, since the mass increases due to the high specific gravity of the material, there is also a problem that it is disadvantageous for bearings for high-speed rotation applications and transportation equipment applications that require weight reduction.

  On the other hand, a resin cage that is easy to mold and can achieve weight reduction is known. In addition, a resin-made cage that has been reinforced by including fibers in the resin has been proposed (see, for example, Patent Documents 1 to 4). As a result, it is possible to provide a cage that achieves low-cost processing and weight reduction to a desired shape while ensuring a certain level of strength.

  Furthermore, there is also a proposal that a cage manufactured by semi-melt molding of a magnesium alloy can be applied to an application that requires lighter weight and higher strength. Thereby, it is said that a cage suitable for high-speed rotation can be provided because of excellent moldability, high strength, and light weight (see, for example, Patent Document 5).

JP 2005-127493 A JP 2005-140269 A Japanese Patent Laid-Open No. 2005-163997 JP 2007-78118 A JP 2000-213544 A

  The resin cage is generally formed by injection molding. Further, in a resin cage, a reinforcing material having a large aspect ratio such as fiber is often added for the purpose of securing a desired strength. Therefore, the amount of molding shrinkage and the anisotropy of mechanical properties associated with flow orientation become problems. In addition, since the longitudinal direction of the reinforcing material tends to be aligned along the weld line in the weld portion formed by injection molding, the reinforcing effect of the reinforcing material does not reach the weld portion, and as a result, the strength of the weld portion can be ensured. There is also the problem that it is difficult.

  On the other hand, in a cage made of a magnesium alloy, since the reinforcing material having a large aspect ratio is usually not used, the above-mentioned anisotropy problem due to the addition of the reinforcing material does not occur. However, when a cage made of a magnesium alloy is actually formed by injection molding, there is a problem that high strength and fatigue characteristics that should be originally obtained cannot be sufficiently obtained.

  Accordingly, an object of the present invention is to provide a rolling bearing provided with a magnesium alloy cage that is lightweight and has high strength.

  A rolling bearing according to the present invention includes a race member, a plurality of rolling elements arranged in contact with the race member, and a cage that holds the rolling elements in a freely rollable manner. The cage is made of a magnesium alloy and is formed by injection molding. In the injection molding, a joining region, which is a region containing voids formed by joining the magnesium alloy containing the liquid phase, flows out of the cage. Furthermore, when the cross section of the cage is observed, the proportion of the α phase having a particle diameter of 20 μm or more in the magnesium alloy is less than 15%.

  The present inventor has investigated the cause of the high strength and fatigue characteristics that cannot be obtained sufficiently in a magnesium alloy cage formed by injection molding and countermeasures thereof. As a result, the following knowledge was obtained and the present invention was conceived.

  That is, when producing a magnesium alloy cage by injection molding, the magnesium alloy containing the liquid phase flows and fills the inside of the mold (cavity part). At this time, due to the shape of the cage and the number of gates, a region where the magnesium alloy containing the liquid phase merges is formed. Here, the magnesium alloy when the injection molding is performed is supplied into the mold in a state in which the viscosity is significantly smaller than that of a general resin. In addition, compared with general resins, magnesium alloys have a low specific heat and excellent thermal conductivity, so that the solidification rate is fast. In order to cope with such characteristics of the magnesium alloy, the magnesium alloy is filled in the mold at a high speed several times to ten times as high as that in the case of general resin injection molding. Therefore, the magnesium alloy tends to be turbulent, and it is easy to entrain gas (such as air) in the mold. As a result, the gas is confined in the region where the magnesium alloy is merged, thereby forming a merged region that is a region containing voids. As described above, in the cage made of magnesium alloy, there is a problem that high strength and fatigue characteristics that should be originally obtained cannot be sufficiently obtained due to insufficient strength due to voids in the merging region.

  On the other hand, in the cage constituting the rolling bearing of the present invention, a merged region, which is a region containing voids formed by the joining of magnesium alloys including a liquid phase, flows out of the cage. As a result, according to the rolling bearing of the present invention, it is possible to provide a rolling bearing provided with a magnesium alloy cage that is lightweight and has high strength.

  Furthermore, in the cage constituting the rolling bearing of the present invention, when the cross section of the cage is observed, the proportion of the α phase having a particle diameter of 20 μm or more in the magnesium alloy is less than 15%. The α phase (solid phase made of pure magnesium) having a particle size of 20 μm or more in the magnesium alloy becomes a factor for reducing the strength of the cage. Therefore, by reducing the proportion of the α phase having a particle diameter of 20 μm or more in the magnesium alloy constituting the cage, the strength at the weld and other portions than the weld is improved. More specifically, when the cross section of the cage is observed, the strength of the cage can be effectively improved by setting the proportion of the α phase having a particle diameter of 20 μm or more in the magnesium alloy to less than 15%.

  Further, the cage is heated to a temperature range equal to or higher than the melting point, and a magnesium alloy controlled only in a liquid phase (a state that does not include an α phase; a completely molten state) is injected into a mold. It is preferable that it is manufactured by this. Thereby, the cage made from a magnesium alloy which is excellent in fatigue strength than the precipitation of the coarsened alpha phase (alpha phase crystal grain) can be provided. The coarse α phase as used herein means a crystal grain size of 20 μm or more, and sometimes exceeds 100 μm. Such a coarsened α phase is formed by coarsening an approximately spherical α phase generated in an injection molding cylinder in the course of cooling and solidification from injection during molding.

  The rolling bearing according to the present invention may be a bearing that is used to rotatably support a main shaft of a machine tool with respect to a member that is disposed so as to face the main shaft.

  Since the main spindle of a machine tool rotates at an extremely high rotational speed, a cage for a bearing (rolling bearing for machine tool) that supports the spindle is required to have high strength and light weight. In addition, when the rigidity is insufficient with respect to the centrifugal force caused by the high rotational speed of the rolling bearing for machine tools, the cage is deformed and the rotational accuracy of the bearing is reduced (NRRO (Non-Repeatable Run-Out); asynchronous runout). Rise) and heat generation at the bearing increases. On the other hand, the rolling bearing of the present invention provided with a cage made of a magnesium alloy having not only high strength and light weight but also high specific rigidity is suitable as a rolling bearing for machine tools.

  In the above rolling bearing, more preferably, when the cross section of the cage is observed, the proportion of the α phase having a particle diameter of 20 μm or more in the magnesium alloy is less than 5%. In the above rolling bearing, more preferably, when the cross section of the cage is observed, the magnesium alloy does not contain an α phase having a particle diameter of 20 μm or more.

By setting the proportion of the α phase having a particle size of 20 μm or more to less than 5%, the strength of the cage can be further improved. Moreover, the intensity | strength of a holder | retainer can be improved further by making the ratio of alpha phase with a particle size of 20 micrometers or more less than 2%. Moreover, the strength of the cage is further improved by preventing the α phase having a particle size of 20 μm or more from being included. Here, the state in which the α phase having a particle size of 20 μm or more is not included refers to a state in which the magnesium alloy does not substantially include an α phase having a particle size of 20 μm or more. Specifically, in the cross section of the cage, when four or more regions of 10 mm ² or more are randomly observed and α phase having a particle size of 20 μm or more is not confirmed, the magnesium alloy constituting the cage has substantially no grain. It can be determined that an α phase having a diameter of 20 μm or more is not included.

  In the rolling bearing, preferably, the magnesium alloy contains aluminum, zinc, and manganese. A magnesium alloy containing aluminum, zinc, and manganese is suitable for injection molding. By employing such a magnesium alloy, a cage constituting the rolling bearing of the present invention can be easily manufactured. Here, as a magnesium alloy containing aluminum, zinc, and manganese, ASTM standard AZ91D can be mentioned, for example.

  The cage may have a comb shape. A comb-shaped cage having a comb shape including an annular portion having an annular shape and a plurality of column portions protruding in the axial direction from the annular portion is easily deflected, and high specific rigidity is required. Therefore, the cage having a high specific rigidity by being made of a magnesium alloy is suitable for application to a comb cage.

  In the cage constituting the rolling bearing, the ratio of the tensile strength in the weld portion formed in the region where the magnesium alloy is joined in the injection molding to the tensile strength in the portion other than the weld portion is preferably 0.8 or more.

  The cage made of magnesium alloy manufactured by injection molding is basically high strength, but the strength of the weld part is lower than other areas, and the strength in the weld part is insufficient. May be damaged. On the other hand, by setting the ratio to 0.8 or more, breakage of the cage due to insufficient strength of the weld portion can be suppressed.

  In the cage constituting the rolling bearing, an anodized layer (modified layer) having a thickness of 15 μm or less may be formed on the surface. Corrosion resistance and wear resistance can be improved by forming the anodized layer. On the other hand, when the thickness of the anodized layer is increased, the shape change such as the growth of recesses (increase in surface roughness) and volume expansion accompanying modification is increased. May be adversely affected. Therefore, the thickness of the anodized layer (modified layer) is preferably 15 μm or less. Further, from the viewpoint of ensuring the smoothness of the surface required for the cage, the thickness is particularly preferably 10 μm or less.

  Further, in the cage constituting the rolling bearing, a nickel plating film may be formed on the surface. By forming the nickel plating film, the wear resistance can be particularly improved. The thickness of the nickel plating film may be determined as needed from the viewpoint of wear resistance and corrosion resistance, and the corrosion resistance improves as the thickness increases. On the other hand, when the thickness of the nickel plating film exceeds 15 μm, the plating film thickness is likely to vary in each part, and wear powder due to one-side contact may occur between the rolling elements, the inner ring, the outer ring and the like. As a result, there is a risk that the deterioration of the lubricant may be accelerated by the deterioration of the rotation accuracy, the occurrence of vibration, and the wear and vibration generated in some cases. Therefore, the thickness of the nickel plating film is preferably 15 μm or less. On the other hand, if the thickness of the nickel plating film is less than 5 μm, the corrosion resistance may be insufficient and the wear resistance may be insufficient. Therefore, the thickness of the nickel plating film is preferably 5 μm or more.

  Furthermore, in the cage constituting the rolling bearing, a cationic electrodeposition coating layer having a thickness of 15 μm or less may be formed on the surface. By forming the cationic electrodeposition coating layer, corrosion resistance and lubricity can be improved. On the other hand, even if the thickness of the cationic electrodeposition coating layer exceeds 15 μm, the corrosion resistance and lubricity are not greatly improved. Therefore, the thickness of the cationic electrodeposition coating layer is preferably 15 μm or less.

  In the rolling bearing, the average crystal grain size of the magnesium alloy constituting the cage is preferably 10 μm or less, and more preferably 5 μm or less. Thus, the strength of the cage can be improved by reducing the average crystal grain size in the base of the magnesium alloy.

  In the above rolling bearing, the magnesium alloy constituting the cage may be age hardened. Thereby, the intensity | strength of a holder | retainer can be improved.

  As is apparent from the above description, according to the rolling bearing of the present invention, it is possible to provide a rolling bearing including a magnesium alloy cage that is lightweight and has high strength.

It is a schematic sectional drawing which shows the structure of the spindle vicinity of the machine tool provided with the rolling bearing for machine tools. It is a general | schematic fragmentary sectional view which shows the structure of a double row cylindrical roller bearing. It is the schematic which shows the structure of the holder | retainer of a double row cylindrical roller bearing. It is a general | schematic fragmentary sectional view which shows the structure of an angular contact ball bearing. It is the schematic which shows the structure of an injection molding apparatus. FIG. 3 is a schematic diagram showing a configuration of a mold in the first embodiment. It is a flowchart which shows the outline of the manufacturing process of a holder | retainer. It is a general | schematic fragmentary sectional view which shows the structure of a holder | retainer. FIG. 6 is a schematic diagram showing a configuration of a mold in a second embodiment. It is a schematic sectional drawing which shows the structure of the jig | tool for experiment. 6 is a schematic cross-sectional view for explaining a method for manufacturing a test piece in Example 2. FIG. 2 is an optical micrograph showing the structure of Example E. 2 is an optical micrograph showing the structure of Example F. 2 is an optical micrograph showing the structure of Example G. 2 is an optical micrograph showing the structure of Example H. 4 is a SEM photograph showing the structure of Example E. 3 is a SEM photograph showing the structure of Example H.

  Hereinafter, embodiments of the present invention will be described with reference to the drawings. In the following drawings, the same or corresponding parts are denoted by the same reference numerals, and description thereof will not be repeated.

(Embodiment 1)
First, Embodiment 1 which is one embodiment of the present invention will be described. Referring to FIG. 1, machine tool 90 in the present embodiment includes a main shaft 91 having a cylindrical shape, a housing 92 that surrounds the outer peripheral surface of main shaft 91, and outer peripheral surfaces of outer ring 11 and outer ring 21. For the machine tool disposed between the main shaft 91 and the housing 92 so that each of the inner peripheral surfaces of the inner ring 12 and the inner ring 22 is in contact with the outer peripheral surface 91A of the main shaft 91. A double row cylindrical roller bearing 1 (rear bearing) and an angular ball bearing 2 (front bearing) as rolling bearings are provided. Thus, the main shaft 91 is supported so as to be rotatable about the axis with respect to the housing 92.

  In addition, a motor rotor 93B is installed on the main shaft 91 so as to surround a part of the outer peripheral surface 91A. A motor stator 93A is installed on the inner wall 92A of the housing 92 at a position facing the motor rotor 93B. The motor stator 93A and the motor rotor 93B constitute a motor 93 (built-in motor). Thus, the main shaft 91 can be rotated relative to the housing 92 by the power of the motor 93.

  That is, the double-row cylindrical roller bearing 1 and the angular ball bearing 2 are machine tool rollings that rotatably support the main shaft 91 of the machine tool 90 with respect to a housing 92 that is a member disposed so as to face the main shaft 91. It is a bearing.

  Next, the operation of the machine tool 90 will be described. Referring to FIG. 1, when power is supplied from a power source (not shown) to motor stator 93A of motor 93, a driving force for rotating motor rotor 93B around the axis is generated. Thus, the main shaft 91 rotatably supported by the angular ball bearing 2 and the double row cylindrical roller bearing 1 with respect to the housing 92 rotates relative to the housing 92 together with the motor rotor 93B. Thus, by rotating the main shaft 91, a tool (not shown) attached to the tip 91B of the main shaft 91 can cut and grind the workpiece, thereby processing the workpiece.

  Next, the double row cylindrical roller bearing 1 will be described. Referring to FIG. 2, a double row cylindrical roller bearing 1 includes an outer ring 11 as a first race member, an inner ring 12 as a second race member, a cylindrical roller 13 as a plurality of rolling elements, and a cage 14. It has. On the inner peripheral surface of the outer ring 11, outer ring rolling surfaces 11A as first annular rolling surfaces are formed in double rows (two rows). On the outer peripheral surface of the inner ring 12, inner ring rolling surfaces 12 </ b> A are formed in a double row (two rows) as an annular second rolling surface facing each of the double row (two rows) outer ring rolling surfaces 11 </ b> A. ing. The plurality of cylindrical rollers 13 are formed with a roller contact surface 13A (an outer peripheral surface of the cylindrical roller 13) as a rolling element contact surface. The cylindrical roller 13 comes into contact with each of the outer ring rolling surface 11A and the inner ring rolling surface 12A at the roller contact surface 13A, and is arranged at a predetermined pitch in the circumferential direction by an annular retainer 14. It is rotatably held on an annular orbit of the row. Thereby, the outer ring | wheel 11 and the inner ring | wheel 12 can rotate relatively mutually.

  Here, referring to FIG. 3, the retainer 14 is a comb retainer including an annular portion 14 </ b> A having an annular shape and a plurality of column portions 14 </ b> B protruding in the axial direction from the annular portion 14 </ b> A. As shown in FIG. 2, in the double row cylindrical roller bearing 1, the opposite surfaces of the annular portion 14 </ b> A from the side from which the column portion 14 </ b> B protrudes face each other, and the central axes thereof coincide with each other. Two cages 14 are incorporated.

  And the holder | retainer 14 consists of magnesium alloys, such as AZ91D, and is shape | molded by injection molding. In this cage 14, the joining region, which is a region including voids formed by joining magnesium alloys in injection molding, is pushed out of the cage 14, so that the joining region is excluded from the cage 14. Yes. Thereby, the retainer 14 is a magnesium alloy retainer that is lightweight and has high strength. The retainer 14 is a comb retainer in which the column portion 14B is easily bent and requires a high specific rigidity. However, since the retainer 14 is made of a magnesium alloy, a sufficient specific rigidity is ensured.

  Furthermore, the double-row cylindrical roller bearing 1 is provided with a cage 14 and is a highly reliable rolling bearing suitable for high-speed rotation required for a rolling bearing for machine tools.

  Here, in this Embodiment, it enumerates about the advantage which employ | adopts the cage 14 made from a magnesium alloy formed by injection molding. Since the cage 14 is made of a magnesium alloy and has a specific gravity smaller and lighter than a brass cage having the same shape, the energy loss due to the cage under intermittent operation is, for example, 30% or less. Can be reduced. Further, since the cage 14 is formed by injection molding, it is excellent in mass productivity as compared with a general metal cage manufactured by machining such as cutting.

  Furthermore, the double-row cylindrical roller bearing 1 employs a magnesium alloy cage having excellent specific rigidity, so that it is used as a bearing used under high-speed rotation where a large centrifugal force is generated, such as a rolling bearing for machine tools. However, there is little deformation of the cage. The specific rigidity (value obtained by dividing the elastic modulus by the specific gravity) of the magnesium alloy is 2.5 times or more that of high-strength brass and 1.5 times or more that of fiber-reinforced resin such as carbon fiber-reinforced PEEK resin. In general, fiber reinforced resin is excellent in specific strength (value obtained by dividing strength by specific gravity), but the specific strength of magnesium alloy is equal to or higher than that of fiber reinforced resin, and is 2.5 times higher than that of high-strength brass. is there.

  Furthermore, unlike a resin or the like to which fibers are added, the magnesium alloy has no molding anisotropy or is very small, so that sink marks and deformation due to the molding anisotropy are suppressed, and the resin material In comparison, the linear expansion coefficient is small. Therefore, a highly accurate cage can be manufactured by injection molding.

  Thus, excellent specific rotation accuracy (low NRRO) can be achieved by high specific rigidity and molding accuracy. Furthermore, since the magnesium alloy is also excellent in vibration absorption, it can be expected that the operating noise of the bearing will be reduced (noise reduction).

  Further, since the magnesium alloy has a higher thermal conductivity than the resin, it has excellent heat dissipation. As a result, temperature rise during the operation of the bearing can be suppressed and deterioration of the lubricant due to heat can be reduced, so that the life of the rolling bearing can be extended.

  Furthermore, in the case of a cage made of fiber reinforced resin, if a recycled material such as a pulverized material obtained by pulverizing a molded product or a so-called repellet material granulated again by a melt kneader or the like is used as a raw material, There may be a problem that the physical properties are reduced due to breakage or the base material strength is reduced due to thermal deterioration. On the other hand, in the case of a cage made of magnesium alloy, not only does the strength decrease due to recycling, but the energy required for recycling is about 5% as compared with the case of newly manufacturing (smelting). . In general injection molding, regardless of whether a resin material or a magnesium alloy is used as a raw material, waste materials such as solidified portions are generated in the sprue portion and runner portion of the mold. Here, when a magnesium alloy is adopted as a material of the cage, since it is excellent in recyclability as described above, no substantial waste is generated and the environmental load is reduced. Furthermore, the material cost can be reduced and the reliability in terms of strength can be ensured. Therefore, it is preferable to employ a magnesium alloy chip manufactured from a recycled material as a raw material of the cage 14 in the present embodiment.

  Here, referring to FIG. 3, surface treatment layer 14 </ b> C having a thickness of 15 μm or less is formed on the surface of cage 14 in the present embodiment. The surface treatment layer 14C is not an essential component in the cage of the present invention, but by forming this, it is possible to improve corrosion resistance, wear resistance, and the like. The surface treatment layer 14C may be, for example, an anodization layer (modified layer) formed by anodization, a nickel plating film formed by nickel plating, or a resin formed by cationic electrodeposition coating or the like It may be a membrane.

  Next, the angular ball bearing 2 will be described. 4 and 2, the angular ball bearing 2 and the double row cylindrical roller bearing 1 basically have the same configuration and have the same effects. However, the angular ball bearing 2 is different from the double-row cylindrical roller bearing 1 in the shape of the race and rolling elements.

  That is, the angular ball bearing 2 includes an outer ring 21 as a first race member, an inner ring 22 as a second race member, balls 23 as a plurality of rolling elements, and a cage 24. On the inner peripheral surface of the outer ring 21, an outer ring rolling surface 21A as an annular first rolling surface is formed. An inner ring rolling surface 22A as an annular second rolling surface facing the outer ring rolling surface 21A is formed on the outer peripheral surface of the inner ring 22. In addition, a plurality of balls 23 are formed with a ball contact surface 23A (a surface of the ball 23) as a rolling element contact surface. The balls 23 are in contact with each of the outer ring rolling surface 21A and the inner ring rolling surface 22A at the ball contact surface 23A, and are arranged at a predetermined pitch in the circumferential direction by an annular cage 24, thereby forming an annular shape. It is held so that it can roll on the track. Thereby, the outer ring | wheel 21 and the inner ring | wheel 22 can rotate relatively mutually.

  Here, in the angular ball bearing 2, a straight line connecting a contact point between the ball 23 and the outer ring 21 and a contact point between the ball 23 and the inner ring 22 is a radial direction (a direction perpendicular to the rotation axis of the angular ball bearing 2). ). Therefore, it is possible to receive not only the radial load but also the axial load, and when the radial load is applied, the axial direction (the direction of the rotation axis of the angular ball bearing 2) is reduced. Power is generated. Referring to FIG. 1, in machine tool 90 of the present embodiment, two angular ball bearings 2 in the same direction are arranged on the front side (tip 91B side of main shaft 91) and on the rear side (motor rotor 93B side). Has two angular ball bearings 2 opposite to the front side to cancel the component force.

  And the holder | retainer 24 consists of magnesium alloys, such as AZ91D, and is shape | molded by injection molding. In this cage 24, the merged region, which is a region including voids formed by joining magnesium alloys in injection molding, is pushed out of the cage 24, so that the merged region is excluded from the cage 24. Has been. As a result, the cage 24 is a lightweight and high strength magnesium alloy cage.

  Here, in the cages 14 and 24, when the cages 14 and 24 are cut and the cross section is observed, the proportion of the α phase having a particle size of 20 μm or more in the magnesium alloy constituting the cages 14 and 24 is 15%. Is less than. The proportion of the α phase is more preferably less than 5%. Further, in the cages 14 and 24, when the cages 14 and 24 are cut and the cross section is observed, it is preferable that the magnesium alloy does not contain an α phase having a particle size of 20 μm or more. Thereby, the intensity | strength of a holder | retainer can be improved further.

  Furthermore, it is desirable that the ratio of the tensile strength in the welded portion of the cage formed in the region where the magnesium alloy is joined in the injection molding to the tensile strength in the portion other than the welded portion is 0.8 or more. Thereby, breakage of the cages 14 and 24 due to insufficient strength of the weld portion can be suppressed. Such suppression of insufficient strength of the weld portion can be achieved, for example, by manufacturing the retainers 14 and 24 by the manufacturing method described below.

  Next, a method for manufacturing the cage in the present embodiment will be described. First, an injection molding apparatus used in the present embodiment will be described. Referring to FIG. 5, injection molding apparatus 70 in the present embodiment includes an injection unit 50 and a mold 60. The injection part 50 is fitted into the hollow part of the cylinder 51 having a cylindrical hollow part, the supply part 52 connected to the hollow part of the cylinder 51 and supplying the magnesium alloy chip 41 to the hollow part, A screw 53 having a spiral groove formed on the outer peripheral surface and a heater 56 arranged so as to surround the cylinder 51 are provided. The cylinder 51 has a nozzle 55 formed at one end thereof and connected to the mold 60. In addition, a storage portion 54, which is a region surrounded by the tip side of the screw 53 (an end portion close to the mold 60) and the cylinder 51, is formed on one end side of the screw 53. The storage unit 54 is connected to the mold 60 through the nozzle 55.

  5 and 6, the mold 60 includes a sprue portion 63 that is a hollow region connected to the hollow region of the nozzle 55 of the cylinder 51, and a cavity portion 61 that is a hollow region corresponding to the shape of the cage. And a runner portion 62 extending radially from the sprue portion 63 and connected to the cavity portion 61. The runner part 62 includes a gate part 62 </ b> A. In the gate part 62 </ b> A, the runner part 62 is connected to the cavity part 61. The cavity portion 61 includes a weld region 65 that is a region where magnesium alloys supplied from the runner portion 62 to the cavity portion 61 merge. The mold 60 further includes an overflow portion 66 that is connected to the weld region 65 and stores the magnesium alloy that reaches the weld region 65 and overflows from the cavity portion 61. The overflow part 66 has a discharge part 66A connected to the weld region 65 and a holding part 66B connected to the discharge part 66A.

  Next, with reference to FIGS. 5-7, the manufacturing method of the holder | retainer using the said injection molding apparatus 70 is demonstrated. Referring to FIG. 7, in the method for manufacturing a cage in the present embodiment, a raw material chip supply step is first performed as a step (S10). In this step (S <b> 10), referring to FIG. 5, the magnesium alloy chip 41 manufactured from the recycled material is supplied into the cylinder 51 from the supply unit 52 of the injection unit 50.

  Next, a heating step is performed as a step (S20). In this step (S20), the screw 53 rotates around the axis, so that the magnesium alloy chip 41 supplied into the cylinder 51 in the step (S10) follows the spiral groove formed on the outer peripheral surface of the screw 53. The heater 56 is heated to the melting point or higher while moving. Then, the molten magnesium alloy 42 in a molten state is stored in the storage portion 54. At this time, the molten magnesium alloy 42 may be in a completely molten state only in a liquid phase in which no solid phase exists, or in a semi-molten state in which magnesium (α phase) as a solid phase is dispersed in the liquid phase. Also good. However, in the semi-molten state, it is preferable that the ratio of the solid phase is small. Specifically, when the cross section of the magnesium alloy after solidification is observed, the ratio of the α phase is less than 15% in area ratio. Adjusted. The area ratio of the α phase is preferably less than 5%. As a result, a coarse α phase having a particle size of 20 μm or more becomes a stress concentration source in the completed cage, and it is possible to suppress a decrease in fatigue strength and the like of the cage. Moreover, the fall of the fatigue strength etc. of a holder | retainer can be further suppressed by making the ratio of the alpha phase with a particle size of 20 micrometers or more into an area rate less than 2%.

  Next, an injection process is performed as a process (S30). In this step (S 30), the molten magnesium alloy 42 stored in the storage portion 54 in the step (S 20) is injected into the mold 60 by advancing the screw 53 toward the mold 60. Referring to FIG. 6, molten magnesium alloy 42 injected into mold 60 is first supplied to sprue portion 63, then branched into a plurality of runner portions 62 and injected into cavity portion 61. At this time, in the cage shape of FIG. 6 in which an even number of pockets for holding rolling elements are formed, for example, two pockets are arranged between adjacent runner portions 62, that is, every other cavity portion 61 is arranged. The molten magnesium alloy 42 is injected into the cavity portion 61A. Here, the adjacent cavity portions 61 (the cavity portion 61A and the cavity portion 61B) in FIG. 6 are connected to each other in the front-rear direction (the front side and the back side of the paper surface) in the axial direction. Therefore, the molten magnesium alloy 42 injected from the runner 62 into the two cavities 61A joins in the weld region 65 formed in the cavity 61B sandwiched between the two cavities 61A, as indicated by the dashed arrow α. To do. When the molten magnesium alloy 42 is further injected into the two cavities 61A, the molten magnesium alloy 42 overflows from the cavities, flows into the overflow portion 66, and is stored.

  Next, an extraction step is performed as a step (S40). In this step (S40), the cage produced by being injected into the mold 60 and solidifying in the step (S30) is taken out from the mold 60.

  Further, a separation step is performed as a step (S50). A magnesium alloy solidified in the runner portion 62 and the overflow portion 66 is connected to the cage taken out in the step (S40). In this step (S50), the magnesium alloy in the region other than the cage is separated from the cage. Thereby, for example, referring to FIG. 8, the cage 24 is obtained.

  Here, in the present embodiment, referring to FIG. 6, in runner portion 62, the cross-sectional area of the gate portion boundary surface that is the boundary surface with cavity portion 61 is the gate in the region adjacent to the gate portion boundary surface. This is smaller than the cross-sectional area parallel to the boundary surface. More specifically, as the runner portion 62 approaches the cavity portion 61, the cross-sectional area in the cross section perpendicular to the longitudinal direction becomes smaller, and the cross-sectional area becomes the smallest at the boundary surface of the gate portion. Furthermore, in the overflow part 66, the cross-sectional area of the discharge part boundary surface which is a boundary surface with the cavity part 61 is smaller than the cross-sectional area parallel to the discharge part boundary surface in the region adjacent to the discharge part boundary surface. . That is, as with the runner portion 62, the overflow portion 66 has a cross-sectional area that is perpendicular to the longitudinal direction as it approaches the cavity portion 61, and the cross-sectional area that is the smallest at the discharge portion boundary surface. Therefore, the magnesium alloy solidified in the cavity portion 61 (retainer) and the magnesium alloy solidified in the runner portion 62 are easily separated at the gate portion boundary surface, and the magnesium alloy solidified in the cavity portion 61 (retainer) ) And the magnesium alloy solidified in the overflow portion 66 can be easily separated at the discharge portion interface. As a result, in the present embodiment, when the step (S40) and the step (S50) are performed simultaneously, that is, when the cage is taken out from the mold 60, the magnesium alloy in the region other than the cage is separated from the cage. It is possible to do.

  Next, a polishing step is performed as a step (S60). In this step (S60), polishing such as barrel polishing is performed on the cage separated in step (S50). As a result, the surface of the cage is smoothed.

  Next, a surface treatment step is performed as a step (S70). In this step (S70), for example, surface treatment such as anodizing is performed on the cage. This step (S70) is not an essential step in the method for manufacturing a cage of the present invention, but by performing this, the corrosion resistance and wear resistance of the cage are improved.

  Further, a finishing step is performed as a step (S80). In this step (S80), polishing treatment such as barrel polishing, sealing (sealing) treatment, overcoat treatment, etc. that are carried out when the surface irregularities are increased by the surface treatment in step (S70) are required. Will be implemented accordingly. Through the above steps, the cage 14 and the cage 24 in the present embodiment are completed.

  In the method for manufacturing a cage in the present embodiment, the molten magnesium alloy 42 merges in the step (S30) as described above, whereby a merged region including voids is formed in the weld region 65 of the cavity portion 61B. . However, this merged region is pushed out of the cage (cavity portion 61) when the molten magnesium alloy 42 overflows from the cavity portion 61B and flows into the overflow portion 66. As a result, the merging area is excluded from the cage, and the merging area containing voids remains in the cage and the strength is suppressed from being lowered. Therefore, according to the cage manufacturing method using the injection molding apparatus 70 in the present embodiment, a lightweight and high strength magnesium alloy cage 24 is manufactured with reference to FIG. Can do. In addition, it can confirm that the said joining area | region flowed out of the cavity part 61, for example by investigating the surface and cross section of the weld part 24D of the holder 24 of a finished product. Specifically, the weld portion 24D generated between adjacent gates or in the vicinity of the rolling element holding portion of the cage 24 has a characteristic appearance usually called a weld line. In the cage 24 manufactured by the manufacturing method according to the present invention, a weld line is not present, or traces of hot water flowing from the inside of the cage 24 to the outside and traces of removal of overflow portions are observed. Also, depending on the molding conditions, due to the difference in the cooling rate within the mold, the presence of coarse α phase with a particle size of 20 μm or more tends to be smaller in the vicinity of the discharge part than in the vicinity of the gate part. Therefore, it may be confirmed by tissue observation.

  Further, according to the method for manufacturing the cage 24 in the present embodiment, the joining region is excluded from the cage 24 as described above, and the strength reduction in the weld portion 24D is suppressed. Therefore, the ratio of the tensile strength in the weld portion 24D of the cage 24 to the tensile strength in a portion other than the weld portion 24D can be 0.8 or more.

(Embodiment 2)
Next, Embodiment 2 which is another embodiment of the present invention will be described. The cage and the rolling bearing according to the second embodiment have the same configuration as that of the first embodiment, and can produce the same effect as well. However, the cage in the first embodiment has an even number of pockets for holding rolling elements, whereas the cage in the second embodiment has an odd number of pockets. As a result, the configuration of the mold used in the injection molding is different from the first embodiment and the second embodiment.

  Referring to FIG. 9, in the cage shape in the second embodiment in which an odd number of pockets for holding rolling elements are formed, for example, three pockets are sandwiched from adjacent runner portions 62, that is, in cavity portion 61. Molten magnesium alloy 42 is injected into every other cavity portion 61A. Here, the adjacent cavity portions 61 in FIG. 9 are connected to each other in the longitudinal direction (front side and back side of the sheet). Therefore, the molten magnesium alloy 42 injected from the runner 62 into the two cavities 61A flows into the two cavities 61B sandwiched between the two cavities 61A, as indicated by the broken line arrow α, and the 2 They merge at the weld region 65 formed at the center (front side or back side) of the two cavity portions 61B. When the molten magnesium alloy 42 is further injected into the two cavities 61A, the molten magnesium alloy 42 overflows from the cavities, flows into the overflow portion 66, and is stored.

  Also in the present embodiment, as in the case of the first embodiment, the molten magnesium alloy 42 merges in the step (S30), whereby a merge region including voids is formed in the weld region 65. In the second embodiment, the weld region 65 is located in the central portion of the pocket (the central portion in the circumferential direction of the cage), which is a thin region of the cage. For this reason, if a merge region including voids remains in the region, the strength of the cage tends to be insufficient compared to the case of the first embodiment. However, the merged region is pushed out of the cavity portion 61 when the molten magnesium alloy 42 overflows from the cavity portion 61 and flows into the overflow portion 66. As a result, the merging area is excluded from the cage, and the merging area containing voids remains in the cage and the strength is suppressed from being lowered. As described above, the application of the present invention is particularly effective when the merge region is formed in the thin region of the cage.

  In the above embodiment, the ASTM standard AZ91D is exemplified as a magnesium alloy applicable to the present invention, but the magnesium alloy applicable to the present invention is not limited to this, and various magnesium alloys for die casting are applied. be able to. Examples of magnesium alloys that can be used in the present invention include alloys in which aluminum (Al), zinc (Zn), manganese (Mn), silicon (Si), and the like are added to magnesium (Mg), which is the main component. Can do. In addition, calcium (Ca), gadolinium (Gd), copper (Cu), iron (Fe), nickel (Ni), zirconium (Zr) may be used for the purpose of improving flame retardancy, heat resistance and toughness. ), Rare earth elements and the like may be added. Specific examples include Mg-Al-Zn alloys such as ASTM standards AZ91D, AZ61A, and AZ31B, Mg-Al alloys such as AM60B, and Mg-Al-Si alloys such as AS41A.

  Further, the volume (volume) of the overflow portion 66 is not particularly limited, but is preferably 5% or more of the volume of the cavity portion 61 from the viewpoint of reliably removing the merging portion from the cage (product), In order to more reliably exclude the merged portion, the content is preferably set to 10% or more. On the other hand, from the viewpoint of material yield, it is preferable that the amount of the waste material portion to be removed is small, and the volume (volume) of the overflow portion 66 is preferably 30% or less of the volume of the cavity portion 61.

  Furthermore, separation (removal) of the magnesium alloy solidified in the runner portion 62 and the overflow portion 66 performed in the step (S50) from the cage can be performed by various methods. As a specific method, for example, machining such as trimming by a press machine, barrel machining, and cutting can be exemplified.

  Further, a so-called hot nozzle or hot runner method capable of reducing the amount of magnesium alloy solidified in the sprue portion 63 or the runner portion 62, or a molding method using an in-mold gate cut method in which gate cutting is performed in a mold is also suitable. Can be used for In addition, the magnesium alloy solidified in the overflow part 66 by the in-mold processing can be removed together with the magnesium alloy solidified in the sprue part 63 and the runner part 62.

  Moreover, you may implement one or both of a solution treatment and an age hardening process with respect to the shape | molded cage | baskets 14 and 24 as needed.

  Furthermore, the surface treatment can be performed before or after the removal of the solidified magnesium alloy in the sprue portion 63, the runner portion 62, and the overflow portion 66, but is preferably performed after the removal. Specific examples of the surface treatment include plating treatment using a metal having excellent corrosion resistance, resin coating such as cationic electrodeposition coating, chemical conversion treatment or anodizing treatment for modifying the surface to magnesium hydroxide or magnesium oxide. . Among these, it is particularly preferable to employ an anodizing treatment that is excellent in corrosion resistance and wear resistance, and a cationic electrodeposition coating that is excellent in corrosion resistance and self-lubricating property without worrying about adhesion at the interface. In addition, since surface roughness often increases when anodizing is performed, polishing treatment such as barrel polishing after surface treatment, sealing with resin material (sealing), steam treatment, boiling water as necessary You may perform a process, sealing (sealing) by chemical | medical solution processes, such as a heated nickel acetate solution, or an overcoat process. The amount of polishing when the polishing treatment is performed can be made not more than the thickness of the modified layer in order to leave the modified layer formed by the surface treatment. If the thickness of the denatured layer is about 3 μm or more, there will be no major functional problem, but since the cage has a sliding part that contacts the rolling elements and the raceway, the thickness should be 5 μm or more. Is preferable. The thicker the modified layer is, the better the abrasion resistance and corrosion resistance is. However, the shape change such as recess growth (increase in surface roughness) and volume expansion accompanying modification becomes large, so that it is 15 μm or less. Preferably, the thickness is 10 μm or less.

  Moreover, when performing a plating process as surface treatment, it is preferable to employ | adopt nickel plating, such as various chromium plating, electroless nickel plating, electric nickel plating, for example.

  In addition, as the shape of the cage constituting the rolling bearing of the present invention, various types such as a crown type cage, a cage-type cage, a comb type cage, and a cage type cage can be adopted. Although there is no restriction | limiting in a shape, the rolling bearing of this invention can be suitably employ | adopted for the rolling bearing provided with the comb type | mold and crown type holder | retainer in which high rigidity is calculated | required especially. Furthermore, the rolling bearing of the present invention can be applied to various types of rolling bearings such as radial ball bearings, radial roller bearings, thrust ball bearings, thrust roller bearings, angular contact ball bearings, and is not particularly limited to the types of rolling bearings. Can be adopted. Also, the guide type of the cage is not particularly limited, and can be applied to any guide type such as rolling element guide, outer ring guide, and inner ring guide.

  Embodiment 1 of the present invention will be described below. A cage that constitutes the rolling bearing of the present invention was actually manufactured, and an experiment was performed in which the characteristics were compared with those of a conventional cage. The experimental procedure is as follows.

  First, the cage described in the above embodiment was manufactured by the same manufacturing method as in the above embodiment. As shown in FIGS. 1 and 2, the shape of the cage is a comb type cage that can be used for a bearing model number NN3020 (JIS nominal number). More specifically, the inner diameter is 120 mm, the outer diameter is 132 mm, the height is 10.5 mm, the thickness of the annular portion 14A (see FIG. 2) is 2.3 mm, the PCD (Pitch Circle Diameter) is 126 mm, and the number of columns is 28. did. The cage was manufactured by performing steps (S10) to (S60) in the manufacturing method (see FIG. 7) described in the above embodiment. In the step (S10), a magnesium alloy chip made of AZ91D was adopted as a raw material chip. In the steps (S20) and (S30), the conditions of a nozzle temperature of 610 ° C., a mold temperature of 250 ° C., an injection speed of 1200 mm / s, a holding pressure of 15 MPa, and a cooling time of 10 s were adopted. In the step (S50), the magnesium alloy solidified in the overflow portion 66 was removed by press molding. Furthermore, barrel polishing was performed in the step (S60). Thereafter, an age hardening treatment was performed as a post-treatment at 216 ° C. for 10 hours (JIS standard T5) (Example A).

  On the other hand, the same shape and manufacturing process as those in Example A were adopted, and the age hardening treatment was omitted and a process (S70) was added. In the step (S70), anodization was performed to form a modified layer having a thickness of 8 μm. When the surface roughness after the anodizing treatment was adjusted to 1.0 μm according to JIS standard Ra, the surface roughness became 0.9 μm in Ra (Example B).

  Further, the same shape and manufacturing process as in Example B above were adopted, and an electroless nickel plating (film thickness: 10 μm, base treatment: etching treatment) was performed instead of anodizing treatment in the step (S70). (Example C).

  In addition, the same shape and manufacturing process as in Example B above was adopted, and in the step (S70), a cation electrodeposition coating (film thickness: 10 μm, base treatment: chemical conversion treatment) was performed instead of anodizing treatment. (Example D).

  On the other hand, a resin cage (Comparative Example A) and a high-strength brass cage (Comparative Example B) having the same shape as the above examples were also prepared for the purpose of comparison with the above Examples of the present invention. In Comparative Example A, a cage was produced by injection molding a resin (PEEK450CA30 manufactured by Victrex) in which a CF (carbon fiber) material was added to a PEEK (Poly Ether Ether Keton) material. Specifically, injection molding was performed under the conditions of a nozzle temperature of 400 ° C., a mold temperature of 180 ° C., an injection speed of 50 mm / s, a holding pressure of 120 MPa, and a cooling time of 30 s, and further heated to 200 ° C. as a post-treatment for 3 hours. A holding annealing treatment was performed. Further, in Comparative Example B, high strength brass CAC301 was adopted as a material, and a cage was manufactured by processing into the above shape by cutting.

  Next, experimental items and experimental results will be described. First, an experiment for actually assembling the NN3020 bearing using the cages of Examples A to D was performed. Specifically, an inner ring and an outer ring made of JIS standard SUJ2 material and rolling elements made of silicon nitride were prepared, and two bearings were assembled back to back to assemble a bearing (see FIG. 1). As a result, any of the cages of Examples A to D could be assembled without any problem. In addition, no troubles such as peeling occurred in the altered layer, the nickel plating layer, and the cationic electrodeposition coating layer formed in the cages of Examples B to D.

Next, the cage mass, cage strength, column deflection amount, and friction coefficient of the JIS standard SUJ2 material were measured for the cages of the examples and comparative examples. The strength of the cage was measured by recording the load when the cage was pulled by breaking the cage by applying forces opposite to each other in the diameter direction of the cage from the inner diameter side of the cage. With respect to the amount of column deflection, the cage is placed on a flat surface so that the annular portion side of the cage faces down, and the jig shown in FIG. 10 is moved from the small diameter side (diameter φ ₂ side) to the inside diameter side of the cage. The amount of column collapse (the amount of change in the outer diameter) was measured when pushed in with a constant load. Here, referring to FIG. 10, jig 80 has a first flat surface 82 having a circular shape with a diameter φ ₁ (132 mm) and a circular shape with a diameter φ ₂ (115.5 mm) parallel to first plane 82. And a side surface 83 which is a spherical surface having a curvature radius of 66 mm. The thickness t, that is, the distance between the first plane 82 and the second plane 81 is 32 mm. Moreover, the friction coefficient with respect to SUJ2 material prepared the member which consists of SUJ2, and measured the friction coefficient with respect to the said member under mineral oil (VG2) spraying.

  Table 1 shows the experimental results. In Table 1, the cage mass is a mass ratio when Comparative Example B is set to 1, and the cage strength and the column deflection amount are expressed as a strength ratio and a column deflection amount ratio when Comparative Example A is 1, respectively. Has been.

  With reference to Table 1, the mass of Example AD is 1/5 of the comparative example B which is a high strength brass cage. It is confirmed that the cage of the present invention achieves a weight reduction comparable to that of Comparative Example A, which is a resin cage. Moreover, the intensity | strength of Examples AD exceeds the comparative example A which is a resin-made cage. Furthermore, the amount of column deflection in Examples A to D is greatly suppressed as compared with Comparative Example A, which is a resin cage, and is comparable to Comparative Example B, which is a cage made of high-strength brass. ing. Moreover, the friction coefficient with respect to SUJ2 of Examples A to D is smaller than the friction coefficient with respect to SUJ2 of Comparative Example B. In particular, the friction coefficient for SUJ2 of Examples C and D is a value comparable to the friction coefficient for SUJ2 of Comparative Example B, which is a resin cage.

  From the above experimental results, the cage constituting the rolling bearing of the present invention can be manufactured not only by injection molding with excellent mass productivity, but also light weight, high strength and rigidity, and friction against SUJ2, which is a bearing steel. It was confirmed that the cage has a suppressed coefficient.

  Embodiment 2 of the present invention will be described below. An experiment was conducted to confirm the effect of improving the strength by the method of manufacturing the cage constituting the rolling bearing of the present invention. The experimental procedure is as follows.

  First, No. 1 test piece (tensile test piece) defined in JIS standard K7113 was produced using the mold 60 shown in FIG. 11, and an experiment for confirming the tensile strength of the weld portion was performed. Specifically, referring to FIG. 11, a mold 60 includes a sprue portion 63 that is a hollow region connected to a nozzle for injecting a material, a cavity portion 61 corresponding to the shape of the No. 1 test piece, The sprue part 63 and the runner part 62 which connects each of the axial direction both ends of the cavity part 61 are provided. The runner part 62 includes a gate part 62 </ b> A that is a film gate, and the runner part 62 is connected to the cavity part 61 in two gate parts 62 </ b> A provided at both ends in the axial direction of the cavity part 61. . The cavity portion 61 includes a weld region 65 that is a region where magnesium alloys supplied from the runner portion 62 to the cavity portion 61 merge. The mold 60 further includes an overflow portion 66 that is connected to the weld region 65 and stores the magnesium alloy that reaches the weld region 65 and overflows from the cavity portion 61. The overflow part 66 has a discharge part 66A connected to the weld region 65 and a holding part 66B connected to the discharge part 66A.

  And AZ91D which is a material was inject | emitted to the metal mold | die 60 on the conditions shown in the following Table 2, and the test piece by which the weld part was formed in the small diameter part (weld area | region 65) of the test piece was produced (Example EH). ). In addition, about Example G, the age hardening process was implemented by hold | maintaining at 150 degreeC for 24 hours (JIS specification T5). On the other hand, for comparison, test pieces were similarly prepared under the conditions shown in Table 2 below using a resin (a PEEK material added with a CF material; PEEK450CA30 manufactured by Victrex) under the conditions shown in Table 2 below (Comparative Example C). In Comparative Example C, an annealing treatment was performed as a post-treatment, which was held at a temperature of 200 ° C. for 3 hours. Then, a tensile test was performed according to JIS standard K7113 which is a plastic tensile test method, and the tensile strength at the weld portion (corresponding to “weld strength” in Table 2) was investigated. The test speed was 10 mm / min.

  On the other hand, for the purpose of investigating the tensile strength other than the weld portion, a tensile test was performed under the conditions shown in Table 2 using a die in which the gate portion 62A was formed only at one end in the axial direction of the die 60. A piece was prepared and examined for tensile strength (corresponding to “tensile strength” in Table 2).

  Further, after cutting the central portion of the obtained tensile test piece and polishing the cross section, the cross section was etched with a 3% nital corrosive solution (nitric alcohol solution), and the cross section after etching was optical microscope (100 Times). Then, the image obtained as a result of the observation was binarized, and the area ratio of the coarse α phase having a particle diameter of 20 μm or more in the visual field (corresponding to “Coarse α solid phase ratio” in Table 2) was calculated. Optical micrographs of the cross sections of Examples E, F, G, and H after etching are shown in FIGS. 12, 13, 14, and 15, respectively. In Examples E and H, a region where a coarse α phase is not observed, such as region A in FIG. 12 and region B in FIG. 15, is observed with a scanning electron microscope (SEM) (1000 ×). (FIGS. 16 and 17). Table 2 shows the experimental conditions and experimental results.

  Next, experimental results will be described with reference to Table 2 and FIGS. In Table 2, the tensile strength and weld strength are shown as a ratio (relative value) where the weld strength of Comparative Example C is 1.

  Referring to Table 2, the weld strengths of Examples E to H are 60% or more higher than the weld strength of Comparative Example C. In addition, the ratio between the weld strength and the tensile strength is 0.8 or more, which is close to 1. Here, a weld portion is necessarily formed in a cage produced by a multi-point gate type injection molding method using a mold having a plurality of gates. And according to the cage which comprises the rolling bearing of this invention, unlike the cage | basket which consists of a fiber reinforced resin material represented by the comparative example C, the fall of the strength in a weld part is suppressed significantly. . Therefore, even when the multi-point gate type injection molding is adopted, according to the cage constituting the rolling bearing of the present invention, a cage having high strength can be provided. In addition, since a decrease in strength in the weld portion is suppressed, for example, it is possible to provide the weld portion in a portion other than the thick pillar portion, so that the degree of freedom in design is widened. Specifically, for example, the multi-point gate injection molding method is applied not only to the cage that holds an even number of rolling elements but also to the cage that holds an odd number of rolling elements without any design restrictions. It becomes possible to do.

  Furthermore, referring to Table 2, compared to Example G, in Examples E, F and H, the α solid phase ratio was kept low and less than 5% (Examples E and F were less than 2%). It has become. With reference to FIGS. 12-15, the white area | region in an optical micrograph respond | corresponds to the alpha phase which became coarse. As a result, the tensile strength of Examples E, F, and H is higher than that of Example G and is improved by 10% or more compared to Comparative Example C. Therefore, by reducing the α solid phase ratio to less than 5% (here, less than 2%), the cage can be further thinned and light weight can be achieved. Therefore, the cage of the present invention in which the α solid phase ratio is reduced to less than 5%, more preferably less than 2%, is applied to machine tool bearings that are required to cope with high-speed rotation by reducing the weight. In particular, it can be suitably used for a bearing retainer for office equipment where reduction of power consumption is strongly required.

  In addition, referring to FIGS. 16 and 17, the structure of the substrate in Example H is finer than that in Example E. More specifically, the average crystal grain size of the substrate of Example E is 6 μm, whereas the average crystal grain size of Example H is 2 μm. As a result, the tensile strength and weld strength of Example H are significantly higher than Example E. From this, in the cage constituting the rolling bearing of the present invention, it can be said that it is preferable to reduce the average crystal grain size of the magnesium alloy constituting the cage. More specifically, the average crystal grain size of the magnesium alloy constituting the cage is preferably 5 μm or less, and more preferably 2 μm or less.

  The embodiments and examples disclosed herein are illustrative in all respects and should not be construed as being restrictive. The scope of the present invention is defined by the terms of the claims, rather than the description above, and is intended to include any modifications within the scope and meaning equivalent to the terms of the claims.

  The rolling bearing of the present invention can be applied particularly advantageously to a rolling bearing that is required to have a cage that is lightweight and has high strength.

  DESCRIPTION OF SYMBOLS 1 Double row cylindrical roller bearing, 2 Angular contact ball bearing, 11, 21 Outer ring, 11A, 21A Outer ring rolling surface, 12, 22 Inner ring, 12A, 22A Inner ring rolling surface, 13 Cylindrical roller, 13A Roller contact surface, 14, 24 Cage, 14A annular portion, 14B pillar portion, 14C surface treatment layer, 23 balls, 23A ball contact surface, 24D weld portion, 41 magnesium alloy tip, 42 molten magnesium alloy, 50 injection portion, 51 cylinder, 52 supply portion, 53 Screw, 54 storage part, 55 nozzle, 56 heater, 60 mold, 61, 61A, 61B cavity part, 62 runner part, 62A gate part, 63 sprue part, 65 weld area, 66 overflow part, 66A discharge part, 66B holding Part, 70 injection molding device, 80 jig, 81 second plane, 82 first plane 83 side, 90 the machine tool, 91 spindle, 91A outer peripheral surface, 91B tip, 92 housing, 92A the inner wall, 93 motor, 93A motor stator, 93B motor rotor.

Claims (13)

A track member;
A plurality of rolling elements arranged in contact with the raceway member;
A cage for holding the rolling element so as to roll freely,
The cage is
Made of magnesium alloy,
Molded by injection molding,
In the injection molding, a joining region that is a region containing voids formed by joining the magnesium alloy containing the liquid phase controlled to a completely molten state flows out of the cage,
When the cross section of the cage is observed, the proportion of α phase having a particle size of 20 μm or more in the magnesium alloy is less than 15%,
The injection mold includes a cavity portion that is a hollow region corresponding to the shape of the cage, a runner portion that is connected to the cavity portion and supplies the magnesium alloy to the cavity portion, and the cavity portion includes the Connected to a weld region that is a region where the magnesium alloy supplied from the runner unit is joined, and an overflow unit that reaches the weld region and stores the magnesium alloy overflowed from the cavity,
As the runner part approaches the cavity part, the cross-sectional area in the cross section perpendicular to the longitudinal direction is reduced, and the cross-sectional area is the smallest in the gate part interface that is the interface with the cavity part,
The overflow part has a smaller cross-sectional area in a cross section perpendicular to the longitudinal direction as it approaches the cavity part, and the cross-sectional area is the smallest in the discharge part boundary surface that is a boundary surface with the cavity part,
A rolling bearing in which a portion where the magnesium alloy solidified in the runner portion and the overflow portion is separated from the cage is formed on the radially inner side of the annular shape of the cage.   The rolling bearing according to claim 1, wherein the rolling bearing is used to rotatably support a main shaft of a machine tool with respect to a member arranged so as to face the main shaft.   The rolling bearing according to claim 1 or 2, wherein a ratio of an α phase having a particle diameter of 20 µm or more in the magnesium alloy is less than 5% when a cross section of the cage is observed.   The rolling bearing according to claim 1 or 2, wherein when the cross section of the cage is observed, the magnesium alloy does not contain an α phase having a particle diameter of 20 µm or more.   The rolling bearing according to claim 1, wherein the magnesium alloy contains aluminum, zinc, and manganese.   The rolling bearing according to any one of claims 1 to 5, wherein the cage has a comb shape.   In the cage, a ratio of a tensile strength in a weld portion formed in a region where the magnesium alloy merges in the injection molding to a tensile strength in a portion other than the weld portion is 0.8 or more. The rolling bearing according to any one of -6.   The rolling bearing according to any one of claims 1 to 7, wherein an anodized layer having a thickness of 15 µm or less is formed on a surface of the cage.   The rolling bearing according to claim 1, wherein a nickel plating film is formed on a surface of the cage.   The rolling bearing according to claim 1, wherein a cationic electrodeposition coating layer having a thickness of 15 μm or less is formed on the surface of the cage.   The rolling bearing according to any one of claims 1 to 10, wherein an average crystal grain size of the magnesium alloy constituting the cage is 10 µm or less.   The rolling bearing according to any one of claims 1 to 10, wherein an average crystal grain size of the magnesium alloy constituting the cage is 5 µm or less.   The rolling bearing according to claim 1, wherein the magnesium alloy constituting the cage is age-hardened.