JP2018109427A - Bearing component and manufacturing method thereof - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a bearing component capable of suppressing a crack or the like resulting from hoop stress, and a manufacturing method thereof.SOLUTION: A bearing component includes a steel-based ring-shaped member having an inner diameter surface and an outer diameter surface. The ring-shaped member has a quench-hardened layer on only one of the inner diameter surface side and outer diameter surface side. For the bearing component, a crack or the like resulting from hoop stress can be suppressed.SELECTED DRAWING: Figure 1

Description

  The present invention relates to a bearing component and a manufacturing method thereof.

  A rolling bearing has a bearing ring and a rolling element. The race ring is composed of an inner ring and an outer ring. The inner ring is disposed on the inner diameter side of the outer ring. The rolling element is disposed between the inner ring and the outer ring.

  In addition, although the prior art about this invention was demonstrated based on the general technical information which the applicant acquired, the information which should be disclosed as prior art document information before filing in the range which an applicant memorize | stores The applicant does not have

  A hoop stress (tensile stress in the circumferential direction of the inner ring) may occur in the race (for example, the inner ring). If excessive hoop stress acts on the race, it will cause cracks in the race. In order to suppress cracking due to excessive hoop stress, it is effective to apply compressive residual stress to the raceway surface in advance.

  In principle, it is possible to impart compressive residual stress to the raceway surface by performing surface quenching (quenching only on the surface). However, when a thin ring is used, quenching is likely to occur not only on the heated surface but also on the surface opposite to the heated surface, and it is difficult to achieve surface quenching. Therefore, generally, the compressive residual stress is not applied to the inner ring surface. This is because, conventionally, appropriate conditions for performing surface quenching have not been clarified.

  The present invention has been made in view of the above-mentioned problems of the prior art. More specifically, the present invention provides a bearing component capable of suppressing cracks and the like due to hoop stress and a method for manufacturing the same.

  A bearing component according to an aspect of the present invention includes a steel ring-shaped member having an inner diameter surface and an outer diameter surface. The ring-shaped member has a hardened and hardened layer only on either the inner diameter surface side or the outer diameter surface side.

A bearing component manufacturing method according to an aspect of the present invention provides a steel ring-shaped member having an inner diameter surface, an outer diameter surface, and a wall thickness that is a distance between the inner diameter surface and the outer diameter surface. A preparatory step, and a heat treatment step of locally heating one of the inner diameter surface and the outer diameter surface to the heat treatment temperature, and then performing a heat treatment for cooling, and the average heating rate during heating is S (unit: ° C) / Second), and when the wall thickness is W (unit: mm), S ≧ 930 / (0.3477W ² -1.594W-0.804) is satisfied.

  According to the bearing component and the manufacturing method thereof according to one embodiment of the present invention, cracks and the like due to hoop stress can be suppressed.

It is a top view of the bearing component which concerns on 1st Embodiment. It is sectional drawing in II-II of FIG. It is a flowchart for demonstrating the manufacturing method of the bearing components which concern on 1st Embodiment. It is a flowchart for demonstrating the manufacturing method of the bearing components which concern on 2nd Embodiment. It is a graph which shows the relationship between the carbide area rate after a heat processing process, and the heat processing temperature. It is a graph which shows an example of the heat pattern in the heat treatment process in the manufacturing method of the bearing component concerning a 2nd embodiment. It is a graph which shows the other example of the heat pattern in the heat processing process in the manufacturing method of the bearing components which concerns on 2nd Embodiment.

  Hereinafter, embodiments 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 the description thereof will not be repeated.

(First embodiment)
Below, the structure of the bearing component which concerns on 1st Embodiment is demonstrated. FIG. 1 is a plan view of a bearing component according to the first embodiment. 2 is a cross-sectional view taken along the line II-II in FIG. As shown in FIGS. 1 and 2, the bearing component according to the first embodiment is, for example, an inner ring of a rolling bearing. However, the bearing component according to the first embodiment is not limited to this. The bearing component according to the first embodiment may be an outer ring of a rolling bearing.

  The bearing component according to the first embodiment has a ring-shaped member 1. The ring-shaped member 1 is made of steel. The steel constituting the ring-shaped member 1 is, for example, high carbon chrome bearing steel. High carbon chromium bearing steel is a steel type specified in JIS 4805: 2008.

  The ring-shaped member 1 has an outer diameter surface 11, an inner diameter surface 12, an upper surface 13, and a bottom surface 14. The outer diameter surface 11 is a surface on the outer diameter side of the ring-shaped member 1. The inner diameter surface 12 is a surface on the inner diameter side of the ring-shaped member 1. The upper surface 13 is one surface perpendicular to the axial direction of the ring-shaped member 1. The bottom surface 14 is the opposite surface of the top surface 13.

  The ring-shaped member 1 has an outer diameter D and an inner diameter d. The outer diameter D is measured at a position where the distance between the outer diameter surface 11 and the inner diameter surface 12 is closest. The ring-shaped member 1 has a wall thickness W and a width T. The wall thickness W is the minimum value of the distance between the outer diameter surface 11 and the inner diameter surface 12. From another viewpoint, the wall thickness W has a value obtained by dividing the difference between the outer diameter D and the inner diameter d by two. The width T is the distance between the top surface 13 and the bottom surface 14.

  The wall thickness W is preferably 5 mm or more. On the other hand, the wall thickness W is preferably 100 mm or less.

  The ring-shaped member 1 has a quench hardened layer 15. The quench hardening layer 15 is formed only on one of the outer diameter surface 11 and the inner diameter surface 12 of the ring-shaped member 1 and is not formed on the other. When the bearing component according to the first embodiment is an inner ring of a rolling bearing, the hardened hardened layer 15 is formed only on the outer diameter surface 11 side of the ring-shaped member 1 and formed on the inner diameter surface 12 side. It has not been.

  The quench hardened layer 15 is a layer in which the steel constituting the ring-shaped member 1 is martensite. Whether or not the quench hardened layer 15 is formed can be determined by observation of the structure. The carbide area ratio in the quench hardened layer 15 is preferably 8% or more and 12% or less. The carbide area ratio is measured by performing image processing on an image photographed with a microscope.

  Below, the manufacturing method of the bearing component which concerns on 1st Embodiment is demonstrated. FIG. 3 is a flowchart for explaining the method for manufacturing the bearing component according to the first embodiment. As shown in FIG. 3, the bearing component manufacturing method according to the first embodiment includes a material preparation step S10 and a heat treatment step S20. The manufacturing method of the bearing component according to the first embodiment may further include a post-processing step S30. The bearing component manufacturing method according to the first embodiment may further include an assembly step S40.

  In the bearing component manufacturing method according to the first embodiment, a material preparation step S10 is first performed. In the material preparation step S10, a steel workpiece is prepared. This object to be processed is a steel member that serves as a bearing component such as an outer ring or inner ring of a bearing. This object to be processed is a ring-shaped member 1. The steel used for this workpiece is, for example, high carbon chrome bearing steel.

  Next, a heat treatment step S20 is performed. The heat treatment step S20 includes a heating step S21 and a cooling step S22. In the heat treatment step S20, a heating step S21 is first performed. In the heat treatment step S20, the cooling step S22 is performed after the heating step S21. The heat treatment step S20 may further include a tempering step S23. The tempering step S23 is performed after the cooling step S22.

  In the heat treatment step S20, the ring-shaped member 1 is heated. The ring-shaped member 1 is heated locally. The ring-shaped member 1 is heated from either one of the outer diameter surface 11 and the inner diameter surface 12. For example, when the bearing component manufactured according to the manufacturing method of the bearing component according to the first embodiment is an inner ring of a rolling bearing, heating is performed from the outer diameter surface 11 side.

  The heating of the ring-shaped member 1 locally means that only the vicinity of the surface of the ring-shaped member 1 is a heating region. For the local heating, any conventionally known method can be used. For the local heating, for example, induction heating, laser irradiation, energization heating, or the like can be used. Local heating is preferably performed by induction heating.

The temperature in the heating region is called the heat treatment temperature. The heat treatment temperature is the surface temperature of the heated part in the ring-shaped member 1. The heat treatment temperature can be measured using, for example, a radiation thermometer. Heat treatment temperature may be a temperature of more than ₁ point A. The heat treatment temperature may be a temperature of more than _three points A. The heat treatment temperature is preferably 900 ° C. or higher and 1000 ° C. or lower.

Here, the _point A, the steel is a temperature for starting the austenitizing, the _three points A, is the temperature at which austenitization of the steel is completely performed.

Heating is performed at an average temperature increase rate S. The average rate of temperature increase S is a value obtained by dividing the heat treatment temperature by the time required to reach the heat treatment temperature from room temperature. The average heating rate S can be controlled using, for example, a means for measuring the temperature of the object to be heated and a PLC (Programmable Logic Controller). The average heating rate S (unit: ° C.) and the thickness W (unit: mm) of the ring-shaped member 1 satisfy the relationship of S ≧ 930 / (0.3477W ² -1.594W-0.804). doing. The relationship between the average temperature increase rate S and the thickness W of the ring-shaped member 1 is derived by electromagnetic field heat conduction analysis.

  In the heat treatment step S20, after reaching the heat treatment temperature, holding for a predetermined time is performed (hereinafter referred to as soaking time). The soaking time is preferably the time required for the carbide area ratio on the outer diameter surface 11 side of the ring-shaped member 1 to be 8% or more and 12% or less. Specifically, the soaking time is preferably 2 seconds or more and 200 seconds or less.

  In the cooling step S22, the ring-shaped member 1 is cooled. The ring-shaped member 1 is cooled using any conventionally known refrigerant. The refrigerant used for cooling the ring-shaped member 1 is, for example, oil or water.

In the cooling step S22, the ring-shaped member 1 may be cooled to a temperature equal to or lower than the _MS point, for example. The M _S point, when the austenitization and steel is cooled, the temperature to start martensite. Thereby, the hardening hardening layer 15 is formed on the surface of the ring-shaped member 1 on the heating region side.

On the other hand the average heating rate S (unit: ° C.) and the ring-shaped member 1 thick W (unit: mm) and ^{is, S ≧ 930 / (0.3477W 2} -1.594W-0.804) and the relationship Is satisfied, the hardened and hardened layer 15 is not formed on the surface opposite to the surface on the heating region side.

In the tempering step S23, the ring-shaped member 1 is tempered. Tempering is performed by a conventionally known method. That is, tempering heats the ring-shaped member 1 to a predetermined temperature of A ₁ point or less (hereinafter referred to as tempering temperature) and at the tempering temperature for a certain time (hereinafter referred to as tempering holding time). .) It is done by holding.

  Subsequently, a post-processing step S30 is performed. In post-processing process S30, the post-processing with respect to the ring-shaped member 1 is performed. In the post-processing step S30, for example, cleaning of the ring-shaped member 1, machining such as grinding and polishing for the ring-shaped member 1, and the like are performed. Thereby, the bearing component which concerns on 1st Embodiment is manufactured.

  Further, an assembly process S40 is performed. In the assembly step S40, the assembly of the bearing component according to the first embodiment is performed. More specifically, the bearing is manufactured by assembling the bearing component according to the first embodiment.

  Below, the test result which evaluated the relationship between the average temperature increase rate S, the thickness W of the ring-shaped member 1, and the realization of surface quenching is demonstrated.

(1) Sample The sample used in this test is a ring-shaped member 1 made of SUJ2 defined in JIS 4805: 2008. In the ring-shaped member 1 used for this test, the outer diameter D is 76 mm, the inner diameter d is 60 mm, the width T is 15 mm, and the wall thickness W is 8 mm.

(2) Heat treatment conditions As the heat treatment conditions, the first heat treatment condition and the second heat treatment condition were used. In the first heat treatment condition and the second heat treatment condition, the heating method, the heat treatment temperature, and the soaking time are common.

  More specifically, the heating was performed by induction heating. This induction heating was performed from the outer diameter surface 11 side of the ring-shaped member 1. The current frequency in induction heating was 80 Hz. The heat treatment temperature was 950 ° C. Holding at the heat treatment temperature was performed until the carbide area ratio on the outer diameter surface 11 side of the ring-shaped member 1 reached about 9%. Specifically, the soaking time was 9 seconds.

  However, in the first heat treatment condition and the second heat treatment condition, different conditions were applied with respect to the average heating rate S. Specifically, the average temperature increase rate S was 160 ° C./second under the first heat treatment condition. Under the second heat treatment condition, the average rate of temperature increase S was set to 70 ° C./second.

  In this test, the thickness W of the ring-shaped member 1 is 8 mm as described above. Therefore, when the relational expression between the average heating rate S and the wall thickness W is applied, the first heat treatment condition is expressed by this relational expression. The second heat treatment condition is satisfied, and this relational expression is not satisfied.

(3) Test result As a test result, the presence or absence of the hardening hardening layer 15 in the inner diameter surface 12 side of the ring-shaped member 1 was evaluated. The presence or absence of the quench hardened layer 15 was evaluated by observation of the structure. When the first heat treatment condition was applied, the hardened and hardened layer 15 was not formed on the inner diameter surface 12 side of the ring-shaped member 1. That is, surface quenching was realized.

  On the other hand, when the second heat treatment condition was applied, the hardened and hardened layer 15 was formed on the inner diameter surface 12 side of the ring-shaped member 1. That is, surface quenching was not realized. From such test results, the surface quenching of the ring-shaped member 1 is realized when the relational expression between the average heating rate S and the wall thickness W is satisfied, and otherwise the surface of the ring-shaped member 1 is achieved. It was experimentally confirmed that quenching was not realized.

  Below, the effect of the bearing component which concerns on 1st Embodiment, and its manufacturing method is demonstrated. In the bearing component according to the first embodiment, the hardened hardened layer 15 is formed only on either the outer diameter surface 11 or the inner diameter surface 12 of the ring-shaped member 1. By forming the quench hardened layer 15, the volume of the portion tends to expand. However, the expansion is constrained by the portion where the hardened and hardened layer 15 is not formed. As a result, compressive residual stress acts on the quench hardened layer 15. Therefore, according to the bearing component according to the first embodiment, cracks and the like due to the hoop stress can be suppressed by the compressive residual stress acting on the hardened hardened layer 15.

  According to the method for manufacturing a bearing component according to the first embodiment, the hardened hardened layer 15 is formed only on either the outer diameter surface 11 or the inner diameter surface 12 of the ring-shaped member 1. Therefore, according to the method for manufacturing a bearing component according to the first embodiment, it is possible to manufacture a bearing component in which cracks due to hoop stress are suppressed.

(Second Embodiment)
Below, the bearing component which concerns on 2nd Embodiment, and its manufacturing method are demonstrated. In the following, differences from the first embodiment will be mainly described, and the same description will not be repeated.

  FIG. 4 is a flowchart showing a method for manufacturing a bearing component according to the second embodiment. As shown in FIG. 4, the manufacturing method of the bearing component according to the second embodiment includes a material preparation step S10 and a heat treatment step S20. The bearing component manufacturing method according to the second embodiment may further include a post-processing step S30. The bearing component manufacturing method according to the second embodiment may further include an assembly step S40. In these respects, the bearing component manufacturing method according to the second embodiment is the same as the bearing component manufacturing method according to the first embodiment.

  However, as described below, the bearing component manufacturing method according to the second embodiment differs from the bearing component manufacturing method according to the first embodiment in the details of the heat treatment conditions of the heat treatment step S20.

  In the heat treatment step S20, the following formulas 1 and 2 are satisfied when the carbide area ratio in the workpiece to be processed after the heat treatment step S20 is Y (unit:%) and the heat treatment temperature is X (unit: ° C.). As such, the conditions for the heat treatment are determined.

Formula 1: 6.600 × 10 ⁻⁴ X ² −1.205X + 5.539 × 10 ² <Y
Formula 2: 1.160 × 10 ⁻³ X ² −2.094X + 9.472 × 10 ² <Y
FIG. 5 is a graph showing the relationship between the carbide area ratio and the heat treatment temperature after the heat treatment step S20. In FIG. 5, the horizontal axis represents the heat treatment temperature (unit: ° C.). In FIG. 5, the vertical axis represents the carbide area ratio (unit:%).

Drawing graphs 5, the solid line of the graph formula ^{1 (6.600 × 10 -4 X 2} -1.205X + 5.539 × 10 2 = Y) shows the dotted line of the graph formula 2 (1.160 × 10 ^{- 3} X ² -2.094X + 9.472 × 10 ² = Y). The above relationship indicates a region above the solid line indicating Expression 1 and the dotted line indicating Expression 2 in FIG.

  Specifically, in the region where the heat treatment temperature is 900 ° C. or more and 950 ° C. or less, it is above the solid line graph (formula 1), and in the region where the heat treatment temperature is 950 ° C. or more and 1000 ° C. or less, the dotted line graph (formula 2 The region above the graph) is a region that satisfies the above relationship. Further, as the above relationship, a relationship between the carbide area ratio and the heat treatment temperature of 900 ° C. ≦ X ≦ 950 ° C. and 8% ≦ Y ≦ 12% may be adopted. This relationship is shown as a shaded portion in FIG.

  In the heating step S <b> 21, any method can be used as long as it is a means for locally heating the ring-shaped member 1, as in the bearing component manufacturing method according to the first embodiment. For example, induction heating can be used as a means for locally heating the ring-shaped member 1.

  In the heating step S21, the heat treatment temperature and the soaking time (the time during which the temperature of the ring-shaped member 1 is maintained in a certain temperature range including the heat treatment temperature) are determined so as to satisfy the above relationship. About the average temperature increase rate S, it sets so that the relational expression demonstrated in 1st Embodiment may be satisfied.

  When the temperature of the ring-shaped member 1 is maintained within a certain temperature range as described above before the ring-shaped member 1 is cooled, the heat treatment temperature is maintained within the certain temperature range. It may be an average value of the surface temperature of the ring-shaped member 1 during a certain period (for example, a period from 60 seconds before the start of cooling to the start of cooling, or a period from 30 seconds before the start of cooling to the start of cooling). When the surface temperature of the ring-shaped member 1 has changed to some extent before the ring-shaped member 1 is cooled (for example, the surface temperature gradually increases), the heat treatment temperature is constant before the cooling starts. (For example, the period from 60 seconds before the start of cooling to the start of cooling, or the period from 30 seconds before the start of cooling to the start of cooling). May be.

  The soaking time is, for example, within a predetermined temperature range including the heat treatment temperature (for example, a temperature range of ± 30 ° C. heat treatment) after the surface temperature of the portion heated in the ring-shaped member 1 becomes equal to or higher than the heat treatment temperature. This is the time that is maintained (more preferably, the time that is maintained in a predetermined temperature range equal to or higher than the heat treatment temperature). Practically, as the soaking time, the time from when the surface temperature of the heated part of the ring-shaped member 1 becomes equal to or higher than the heat treatment temperature until the cooling of the ring-shaped member 1 can be used. .

  FIG. 6 is a graph showing an example of a heat pattern in the heating step S21 in the method for manufacturing a bearing component according to the second embodiment. FIG. 7 is a graph showing another example of the heat pattern in the heating step S21 in the method for manufacturing the bearing component according to the second embodiment. 6 and 7, the horizontal axis indicates time (unit: second), and the vertical axis indicates the heat treatment temperature (unit: ° C.). FIG. 6 shows a case where the heat treatment temperature is 900 ° C. and the soaking time is about 60 seconds. FIG. 6 shows a case where the heat treatment temperature during the soaking time is almost as set. FIG. 7 shows a case where the soaking time is about 30 seconds and the heat treatment temperature during the soaking time varies to some extent.

The cooling step S22 in the bearing component manufacturing method according to the second embodiment is the same as the bearing component manufacturing method according to the first embodiment. That is, in the bearing component manufacturing method according to the second embodiment, the ring-shaped member 1 is cooled in the cooling step S22. The ring-shaped member 1 is cooled using any conventionally known refrigerant. For example, the ring-shaped member 1 may be cooled to a temperature equal to or lower than the _MS point.

  In the induction heating, the heating device can be easily started up and down. Therefore, induction heating is suitable for manufacturing bearing parts in a small lot. Therefore, in the method for manufacturing a bearing component according to the second embodiment, when induction heating is used as a means for locally heating the ring-shaped member 1, a bearing component having a quality equal to or higher than that when using atmospheric furnace heat treatment is used. Can be easily manufactured in a small lot.

  In the method for manufacturing a bearing part according to the second embodiment, the steel constituting the part to be processed may be a high carbon chromium bearing steel. In this case, the quality after the heat treatment equivalent to or higher than that in the case of using the atmospheric furnace heat treatment can be ensured for the bearing component made of the high carbon chromium bearing steel.

In the bearing component manufacturing method according to the second embodiment, in the heat treatment step S20,
900 ℃ ≦ X ≦ 950 ℃
8% ≦ Y ≦ 12%
The conditions for the heat treatment may be determined so as to satisfy the relationship. In this case, the quality of the ring-shaped member 1 after the heat treatment can be made equal to or higher than that when the atmosphere furnace heat treatment is reliably used.

<Basic concept for derivation of heat treatment conditions>
According to the study of the present inventor, there are two differences that are considered to affect the bearing characteristics among the differences in the heat treatment method that performs local heating such as induction heating with respect to the atmospheric furnace heat treatment. The first difference is that induction heating is high-temperature and short-time heating. The second difference is that, in principle, it is difficult for induction heating to make the carbon penetration constant within the part, and the carbon penetration (carbon solid dissolution) varies within the part. is there.

  Variations in the amount of carbon dissolved in bearing parts are expected to affect the aging stability, static load capacity, and crushing value of bearing parts. Therefore, if the upper and lower limits of the carbon solid solution amount in which the values of these characteristics are equal to or higher than those of the atmosphere furnace heat treated product are investigated, it can be regarded as the allowable carbon solid solution concentration range inside the bearing part.

  Heat treatment temperature is also expected to affect the above properties. Therefore, the allowable range of the heat treatment temperature is determined by investigating the range of the heat treatment temperature at which these characteristic values are equal to or higher than those of the atmosphere furnace heat treatment product.

  Then, by using the above-described range of the carbon solid solution amount and the range of the heating temperature, when the entire bearing component is included in the range, it can be determined that the quality is equal to or higher than that of the atmosphere furnace heat treatment product. . Therefore, the effects of the carbon solid solution amount and the heat treatment temperature on the bearing characteristics were investigated, and the conditions for obtaining the same quality as the atmosphere furnace heat treatment product were obtained by the following tests.

  It is difficult to directly measure the amount of carbon solid solution. Therefore, the carbide area ratio in the ring-shaped member 1 (bearing part) after heat treatment was used as an alternative index. It is possible to calculate an approximate amount of carbon solid solution from the carbide area ratio.

<Samples used to derive heat treatment conditions>
(1) Sample The chemical composition of the sample material used in the test is shown in the table.

Assuming that all the carbides are composed of Fe ₃ C in the material of the chemical component described above, the carbide area ratio before the heat treatment is calculated from the above-described carbon concentration to be 15.1%.

(2) Heat treatment method In the samples used in the following tests, the carbide area ratio test levels were 4%, 8%, and 12%. Moreover, the test level of heating temperature was 900 degreeC, 950 degreeC, and 1000 degreeC. In addition, the heat treatment time (soaking time) at each heating temperature for setting the carbide area ratio to 4%, 8%, and 12% in the above materials is as shown in Table 2 below.

  Table 2 shows the heat treatment time (unit: seconds) required to obtain a predetermined carbide area ratio when each heating temperature is employed. For example, as shown in Table 2, when the heating temperature is 900 ° C., the heat treatment time necessary for setting the carbide area ratio to 4% is 316 seconds.

  In the sample used for the test, the following heat treatment was performed in order to realize the above-described carbide area ratio. As a sample used for the test, a ring-shaped member 1 made of SUJ2 defined in JIS 4805: 2008 was used. The ring-shaped member 1 has an outer diameter D of 60.3 mm, an inner diameter d of 53.7 mm, a width T of 15.3 mm, and a wall thickness W of 3.3 mm.

  The heating step S21 was performed by induction heating using a single turn coil. The output of the power supply (to supply power to the single turn coil) connected to the single turn coil is controlled by feeding back the measured temperature of the steel ring surface (the surface of the part that is inductively heated by the single turn coil). It was. The surface temperature of the steel ring was raised from room temperature to a predetermined temperature (specifically, 900 ° C., 950 ° C. or 1000 ° C.). In addition, it took about 5 seconds until the temperature of the steel ring surface rose to the predetermined temperature described above from the start of the heat treatment.

  After the surface of the steel ring was heated to a predetermined temperature, the power supplied to the single turn coil was controlled so that the ring was held at the predetermined temperature for a specific time (heat treatment time) (soaking).

  Then, cooling process S22 was performed and the steel ring was cooled. As a cooling method, the steel ring was cooled by immersing the steel ring in oil at a temperature of 70 ° C. (quenching treatment). As the heat pattern of such heat treatment, for example, the heat pattern shown in FIG. 6 can be adopted.

  A tempering step S23 was performed after the cooling step S22. The tempering conditions were a standard condition of a tempering temperature of 180 ° C. and a tempering holding time of 2 hours.

<Aged dimensional stability test>
The bearings change in size as the retained austenite decomposes during use. Since the dimensional change reduces the accuracy of the bearing, it is required to be below a certain standard.

(1) Sample After the heat treatment step S20 described above, the sample was polished to prepare a ring-shaped sample having an outer diameter of 60 mm, an inner diameter of 54 mm, and an axial width of 15 mm. As shown in Table 2, nine types of samples were prepared by combining the heating temperature (900 ° C., 950 ° C., 1000 ° C.) and the carbide area ratio in the heat treatment described above.

(2) Test and Results For the nine types of samples described above, changes in the external dimensions before and after treatment under the conditions of a heating temperature of 230 ° C. and a holding time of 2 hours were measured. The results are shown in Table 3.

Here, the dimensional change rate is (the absolute value of D ₁ −D ₀ ) / D ₀ when the outer diameter of the sample before the treatment is D ₀ and the outer diameter of the sample after the treatment is D _1. Is defined. The measurement position of the outer diameter of the sample was the same before and after holding at high temperature. The measurement of the outer diameter was evaluated in two directions intersecting 90 ° when viewed from the center of the ring-shaped sample. In addition, n = 3 for each level.

In Table 3, a dimensional change rate of less than 70 × 10 ⁻⁵ was regarded as being equivalent to or higher than that of the atmosphere furnace heat treated product, and was determined to be acceptable (OK determination). In Table 3, a dimensional change rate of 70 × 10 ⁻⁵ or more was regarded as unacceptable (NG judgment). As can be seen from Table 3, from this result, the samples capable of securing aged dimensional stability equal to or higher than that of the atmosphere furnace heat treated product have a carbide area ratio of 8% and 12% when the heat treatment temperatures are 900 ° C. and 950 ° C. This is a sample whose carbide area ratio is 12% when the heat treatment temperature is 1000 ° C.

Further, when an approximate function is obtained from the test data described above and the condition that the dimensional change rate is less than 70 × 10 ⁻⁵ is obtained, when the heat treatment temperature is 900 ° C., the carbide area ratio is 4.0% or more and the heat treatment temperature is In the case of 950 ° C., the carbide area ratio is 4.8% or more, and in the case where the heat treatment temperature is 1000 ° C., the carbide area ratio is 8.9% or more.

<Static load capacity test>
When a large load is applied to the bearing, plastic deformation occurs. However, in order for the rolling element of the bearing to roll smoothly, the amount of plastic deformation of the rolling element is required to be 1 / 10,000 or less of the diameter of the rolling element.

(1) Sample A sample having a size of 6 mm long × 15 mm wide × 3 mm thick was obtained by polishing and wire cutting the ring after the heat treatment step S20 described above. A 6 mm × 15 mm surface of the sample was mirror-polished. Nine types of samples were prepared by combining the heating temperature and the carbide area ratio in the same manner as in the aged dimensional stability test described above.

  For comparison, a sample (comparative example sample) having the same size was prepared by performing an atmosphere furnace heat treatment as a heat treatment on a sample having the same composition and then performing machining.

(2) Test and Results A 3/8 inch ceramic ball was pressed against the mirror-polished surface of the sample with a constant test load. And the depth of the indentation produced by the plastic deformation in the said surface was evaluated. The test load was 471 N corresponding to Pmax 4 GPa in Hertz contact. In addition, n = 3 for each level. The results are shown in Table 4.

  The column of indentation depth in Table 4 shows an average value of indentation depths measured for each sample. The column of standard deviation in Table 4 shows the standard deviation of the indentation depth data. And in the column of judgment of Table 4, the thing which is hard to make an indentation from the sample of atmosphere furnace heat treatment with a significance level of 95% is displayed as pass (OK), and the thing which is easy to make an indentation is displayed as failure (NG). In addition, "-" is displayed in the judgment column for items that do not meet the above criteria.

  From this result, it can be seen that the sample in which the display in the judgment column is OK and “−” shows a static load capacity equal to or higher than that of the atmosphere furnace heat treatment product. Specifically, when the heat treatment temperatures are 900 ° C. and 950 ° C., the samples having a carbide area ratio of 8% and 12% show a static load capacity equal to or higher than that of the atmospheric furnace heat treatment product.

  In addition, when an approximate function is obtained from the test data described above and a standard deviation is set to 0.015 μm and a range that can ensure a quality equivalent to or better than that of an atmosphere furnace heat treatment product is calculated, when the heat treatment temperature is 900 ° C., the carbide area ratio When the heat treatment temperature is 950 ° C., the carbide area ratio is 4.8% or more, and when the heat treatment temperature is 1000 ° C., the carbide area ratio is 13.2% or more.

<Crush strength test>
The crushing strength may be required for the bearing, and the following tests were conducted.

(1) Sample A ring-shaped sample having an outer diameter of 60 mm, an inner diameter of 54 mm, and an axial width of 15 mm was prepared by polishing the sample after the heat treatment step S20 described above. As shown in Table 2, nine types of samples were prepared by combining the heating temperature (900 ° C., 950 ° C., 1000 ° C.) and the carbide area ratio in the heat treatment described above. In addition, n = 3 for each level.

  For comparison, a sample (comparative example sample) having the same size was prepared by performing an atmosphere furnace heat treatment as a heat treatment on a sample having the same composition and then performing machining.

(2) Test and Results For each sample, a load was applied at a constant speed with a material sandwiched from the radial direction, and the load that resulted in crushing was measured. Moreover, the fracture stress was calculated from the load. The results are shown in Table 5.

  In the judgment column of Table 5, those having a crushing strength lower than that of the atmosphere furnace heat treated product even if the standard deviation is taken into consideration are displayed as “NG” (NG). “−” Is indicated for the material that can secure the crushing strength.

  From this result, it can be seen that the sample in which the display in the judgment column is “−” can show a crushing strength equivalent to or higher than that of the atmosphere furnace heat treatment product. Specifically, when the heat treatment temperatures are 900 ° C. and 950 ° C., a sample with a carbide area ratio of 8% or 12% can exhibit a crushing strength equal to or higher than that of the atmosphere furnace heat treatment product.

  Further, when an approximate function is obtained from the test data described above and a range in which a quality equivalent to or better than that of the atmospheric furnace heat treatment product can be secured when the standard deviation is 150 MPa, the carbide area ratio is 4 when the heat treatment temperature is 900 ° C. When the heat treatment temperature is 950 ° C., the carbide area ratio is 5.4% or more, and when the heat treatment temperature is 1000 ° C., the carbide area ratio is 9.3% or more.

<Examination of heat treatment conditions>
From the above results, when high temperature short time heating means such as induction heating is used for quenching of high carbon chrome bearing steel such as SUJ2 as defined in JIS 4805: 2008, performance equal to or better than that of atmosphere furnace heat treated products is obtained. This can be reliably realized when the heat treatment temperatures are 900 ° C. and 950 ° C. and the carbide area ratio is 8% and 12%.

  Looking at each data, all the test results are monotonously increasing or monotonically decreasing with respect to the heat treatment temperature and carbide area ratio. Therefore, it is considered that the quality equivalent to or higher than that of the atmosphere furnace heat-treated product can be realized even by the heat treatment conditions corresponding to the region surrounded by the four points obtained this time (the region indicated by hatching in FIG. 3).

  Therefore, it is in the region where the heat treatment temperature is 900 ° C. or more and 950 ° C. or less and the carbide area ratio is 8% or more and 12% or less that can ensure the same or better quality as the atmosphere furnace heat treatment product.

  Table 6 shows the range of the carbide area ratio obtained from the approximate function of each test result and having a quality equivalent to or better than that of the atmosphere furnace heat-treated product.

When an approximate function is obtained for the relationship between the carbide area ratio range and the heat treatment temperature shown in Table 6 (in the following conditional expressions, Y is the carbide area ratio (%), and X is the heat treatment temperature (° C.)). is there),
Aged dimensions:
6.600 × 10 ⁻⁴ X ² −1.205X + 5.539 × 10 ² <Y (conditional expression 1)
Static load capacity:
1.160 × 10 ⁻³ X ² −2.094X + 9.472 × 10 ² <Y (Condition 2)
Crush test:
5.000 × 10 ⁻⁴ X ² −8.970 × 10 ⁻¹ X + 4.063 × 10 ² <Y (conditional expression 3)
It becomes.

  And the range which can ensure the quality equivalent to or better than the atmosphere furnace heat treated product is the case where the carbide area ratio Y satisfies the above conditional expressions 1 to 3 in the heat treatment temperature X range of 900 ° C. or higher and 1000 ° C. or lower.

  Here, in the range of the heat treatment temperature of 900 ° C. or higher and 1000 ° C. or lower, X satisfying conditional expression 1 always satisfies conditional expression 3. Therefore, conditional expression 3 need not be considered. For this reason, the range which can ensure the quality equivalent to or better than the atmosphere furnace heat treated product is a case where the carbide area ratio Y satisfies the conditional expression 1 and the conditional expression 2 in the heat treatment temperature range of 900 ° C. to 1000 ° C.

  Although the embodiment of the present invention has been described above, the above-described embodiment can be variously modified. Further, the scope of the present invention is not limited to the above-described embodiment. The scope of the present invention is defined by the terms of the claims, and is intended to include any modifications within the scope and meaning equivalent to the terms of the claims.

  The above embodiments are particularly advantageously applied to bearing parts using induction heating and their manufacture.

  DESCRIPTION OF SYMBOLS 1 Ring-shaped member, 11 Outer surface, 12 Inner surface, 13 Upper surface, 14 Bottom surface, S10 Material preparation process, S20 Heat treatment process, S21 Heating process, S22 Cooling process, S23 Tempering process, S30 Post-processing process, S40 Assembly process , D outer diameter, d inner diameter, T width, W thickness, S average heating rate, X heat treatment temperature, Y carbide area ratio.

Claims (7)

Preparing a ring-shaped member made of steel having an inner diameter surface, an outer diameter surface, and a wall thickness that is a distance between the inner diameter surface and the outer diameter surface;
A heat treatment step of locally heating one of the inner diameter surface and the outer diameter surface to a heat treatment temperature and then performing a heat treatment for cooling, and
When an average rate of temperature increase obtained by dividing the heat treatment temperature by the time from room temperature to the heat treatment temperature is S (unit: ° C./second) and the thickness is W (unit: mm), S ≧ 930 / (0.3477W < ² > -1.594W-0.804) The manufacturing method of a bearing component. The heat treatment temperature is 900 ° C. or higher and 1000 ° C. or lower,
In the heat treatment step, when the carbide area ratio of the ring-shaped member after the heat treatment step is Y (unit:%) and the heat treatment temperature is X (unit: ° C.),
6.600 × 10 ⁻⁴ X ² −1.205X + 5.539 × 10 ² <Y
1.160 × 10 ⁻³ X ² −2.094X + 9.472 × 10 ² <Y
The method for manufacturing a bearing component according to claim 1, wherein the conditions for the heat treatment are determined so as to satisfy the relationship. In the heat treatment step,
900 ℃ ≦ X ≦ 950 ℃
8% ≦ Y ≦ 12%
The method for manufacturing a bearing part according to claim 2, wherein the conditions for the heat treatment are determined so as to satisfy the relationship.   The method for manufacturing a bearing component according to claim 1, wherein in the heat treatment step, the ring-shaped member is heated by induction heating.   The said steel which comprises the said ring-shaped member is a manufacturing method of the bearing components of any one of Claims 1-4 which is high carbon chromium bearing steel.   The said thickness is a manufacturing method of the bearing components of any one of Claims 1-5 which are 5 mm or more and 100 mm or less. A steel ring-shaped member having an inner diameter surface and an outer diameter surface;
The wall thickness that is the distance between the inner diameter surface and the outer diameter surface is 5 mm or more and 100 mm or less,
The ring-shaped member is a bearing component having a hardened and hardened layer only on one of the inner diameter surface side and the outer diameter surface side.

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