TUBULAR ROTARY COMPONENT, MANUFACTURING METHOD THEREFOR, AND MOLD THEREFOR

Abstract

Provided is a method for manufacturing a tubular rotary component from a donut-shaped metal disc, wherein the generation of wrinkles or cracks due to a drawing process can be suppressed. This method for manufacturing a tubular rotary component 100B includes: an intermediate molding step in which the entirety of both surfaces of a donut-shaped metal disc 100 having a prescribed inner diameter D.sub.1 and outer diameter D.sub.2 are pressed by the respective tapered surfaces of a punch 10A and a die 20A provided with a prescribed taper to carry out bore-expansion drawing, thereby obtaining a frustoconical intermediate molded article 100A; and a final molding step in which the intermediate molded article 100A is pressed by a punch 10B and a die 20B having a desired shape to carry out bore-expansion drawing again, thereby obtaining a tubular rotary component 100B.

Claims

1. A method for manufacturing a tubular rotary component from a metal disc with a hole formed in a central portion thereof, the metal disc having a predetermined inside diameter and a predetermined outside diameter, the method comprising: an intermediate molding step comprising subjecting the metal disc to a reaming-drawing process in which both surfaces of the metal disc are pressed in entirety by a tapered surface of a punch having a predetermined taper and a tapered surface of a die having a predetermined taper, thereby producing an intermediate molded article having a frustoconical shape; and a final molding step comprising subjecting the intermediate molded article to a further reaming-drawing process in which the intermediate molded article is pressed by a punch and a die having a smaller taper angle than the punch and the die for use in the intermediate molding step, respectively, thereby manufacturing the tubular rotary component.

2. The method according to claim 1, wherein the processes are performed under a condition that a stretch flange rate λ is 90% or less, the stretch flange rate λ being given by λ=(D.sub.1′−D.sub.1)/D.sub.1×100 where D.sub.1 represents the inside diameter of the metal disc before undergoing the processes, and D.sub.1′ represents an inside diameter of the tubular rotary component manufactured through the final molding step.

3. The method according to claim 1, wherein in the intermediate molding step, an angle formed between the tapered surface of the punch and a processing direction and an angle formed between the tapered surface of the die and the processing direction are each set to 30 degrees or greater.

4. The method according to claim 1, wherein in the intermediate molding step, the reaming-drawing process is performed two or more times while an angle between the tapered surface of the punch and a processing direction and an angle between the tapered surface of the die and the processing direction are varied.

5. The method according to claim 1, wherein the metal disc is made of a metal plate as a material, the metal plate containing inclusions that are unevenly distributed such that a quantity of the inclusions increases toward a midpoint of a plate thickness of the metal plate, wherein the method further comprises a cutting process step comprising subjecting the tubular rotary component obtained through the final molding step to a cutting process, wherein the tubular rotary component has a thickness in which a partial thickness from a midpoint of the thickness to an inside diameter-side surface of the tubular rotary component is defined as an inside diameter-side thickness, while a partial thickness from the midpoint of the thickness to an outside diameter-side surface of the tubular rotary component is defined as an outside diameter-side thickness, and wherein the cutting process is performed such that an inside diameter-side residue ratio becomes 0.37 or greater and an outside diameter-side residue ratio becomes 0.49 or greater, the inside diameter-side residue ratio being a ratio of the inside diameter-side thickness after the cutting process to the inside diameter-side thickness before the cutting process, and the outside diameter-side residue ratio being a ratio of the outside diameter-side thickness after the cutting process to the outside diameter-side thickness before the cutting process.

6. The method according to claim 5, further comprising a heat treatment step comprising subjecting the tubular rotary component obtained through the final molding step to hardening and tempering.

7. A mold for use in the method according to claim 1, the mold comprising: a punch with a predetermined taper and a die with a predetermined taper that are for use in the intermediate molding step; and a punch and a die that have a smaller taper angle than the punch and the die for use in the intermediate molding step, respectively.

8. A tubular rotary component manufactured by the method according to claim 5, the tubular rotary component having a thickness in which a partial thickness from a midpoint of the thickness to an inside diameter-side surface of the tubular rotary component is defined as an inside diameter-side thickness, while a partial thickness from the midpoint of the thickness to an outside diameter-side surface of the tubular rotary component is defined as the outside diameter-side thickness, and wherein an inside diameter-side residue ratio is 0.37 or greater and an outside diameter-side residue ratio is 0.49 or greater, the inside diameter-side residue ratio being a ratio of the inside diameter-side thickness after the cutting process to the inside diameter-side thickness before the cutting process, and the outside diameter-side residue ratio being a ratio of the outside diameter-side thickness after the cutting process to the outside diameter-side thickness before the cutting process.

9. A tubular rotary component having a distribution of inclusions in a plate thickness of the tubular rotary component, wherein when a quantity of the inclusions present in an inside diameter-side surface layer is defined as d (inside diameter) and a quantity of the inclusions present at a midpoint of the plate thickness is defined as d (plate thickness midpoint), the distribution satisfies a relationship expressed as d (plate thickness midpoint)>d (inside diameter).

10. The tubular rotary component according to claim 9, wherein the inclusions contain at least one selected from the group consisting of MnS, SiO.sub.2, Al.sub.2O.sub.3, and TiN.

11. The tubular rotary component according to claim 9, wherein the inclusions comprise at least one of MnS, SiO.sub.2, Al.sub.2O.sub.3, or TiN.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] FIG. 1 illustrates steps of a method for manufacturing a tubular rotary component according to an embodiment of the present invention;

[0026] FIG. 2 illustrates steps of a method for manufacturing a tubular rotary component according to a modification of the embodiment of the present invention;

[0027] FIG. 3 illustrates Example 1 of the present invention;

[0028] FIG. 4 is a photograph showing the external appearance of tubular rotary components produced in Example 1-1 of the present invention;

[0029] FIG. 5 illustrates Example 2 of the present invention;

[0030] FIG. 6 illustrates Comparative Example 1 of the present invention;

[0031] FIG. 7 is a photograph showing the external appearance of a tubular rotary component produced in Comparative Example 1 of the present invention;

[0032] FIG. 8 illustrates Comparative Example 2-1 in which the mold disclosed in Patent Document 1 was used;

[0033] FIG. 9 illustrates Comparative Example 2-2 in which the mold disclosed in Patent Document 2 was used;

[0034] FIG. 10 illustrates a residual ratio of an inside diameter-side thickness and that of an outside diameter-side thickness;

[0035] FIG. 11 shows optical micrographs of examples of inclusions;

[0036] FIG. 12 illustrates a method for determining a quantity of inclusions;

[0037] FIG. 13 illustrates results of measurement of quantities of inclusions;

[0038] FIG. 14A schematically illustrates a configuration of a rolling fatigue tester for testing an inner surface;

[0039] FIG. 14B schematically illustrates a configuration of a rolling fatigue tester for testing an outer surface;

[0040] FIG. 15A illustrates results of rolling fatigue tests on the inner surface of Example 4-1 and the inner surface of Comparative Example 6 (a tubular rotary component made from a seamless tube);

[0041] FIG. 15B illustrates results of rolling fatigue tests on the outer surface of Example 5-1 and the outer surface of Comparative Example 6 (the tubular rotary component made from the seamless tube);

[0042] FIG. 16A illustrates the manufacturing method disclosed in Patent Document 1;

[0043] FIG. 16B illustrates a crack caused by a tensile force generated in the manufacturing method of FIG. 16A;

[0044] FIG. 16C illustrates a crack caused by a bend occurring in the manufacturing method of FIG. 16A;

[0045] FIG. 17A illustrates the manufacturing method disclosed in Patent Document 2; and

[0046] FIG. 17B illustrates a crack caused by wrinkles generated in the manufacturing method of FIG. 17A.

PREFERRED MODE FOR CARRYING OUT THE INVENTION

[0047] Preferred embodiments of a method and a device for manufacturing a tubular rotary component of the present invention will be described with reference to the drawings. The tubular rotary component of the present invention is for use as a bearing ring of a rolling bearing, a bearing ring for a roller, and a gear component, and is required to have superior rolling fatigue characteristics.

Embodiment

[0048] FIG. 1 illustrates steps included in the method for manufacturing the tubular rotary component according to the present embodiment. According to the method of the present embodiment, a doughnut-shaped metal disc 100 having a predetermined inside diameter D.sub.1, a predetermined outside diameter D.sub.2, a predetermined plate thickness H, and a hole formed in a central portion is molded by a reaming-drawing process. The reaming-drawing process of the present embodiment is a molding process for molding a metal plate having a hole formed in a central portion thereof into a tubular rotary component, by concurrently subjecting an outer peripheral portion and an inner peripheral portion of the metal plate to shrink flange deformation and stretch flange deformation, respectively.

[0049] The shape of the metal disc 100 can be suitably determined by setting the inside diameter D.sub.1, the outside diameter D.sub.2, and the plate thickness H from a volume of a desired tubular rotary component 100B having a final shape.

[0050] Examples of a material for the metal disc 100 include metal plates such as a rolled steel plate. A rolled steel plate contains inclusions that are unevenly distributed in such a manner that a quantity of the inclusions increases toward a midpoint of the plate thickness of the rolled steel plate. Therefore, superior rolling fatigue characteristics can be obtained by way of a drawing process performed on the rolled steel plate so that a surface of the rolled steel plate is formed into a load-bearing surface. In this way, sufficient rolling fatigue characteristics can be obtained without using a rolled steel plate having a high index of cleanliness.

[0051] As illustrated in FIG. 1, the manufacturing method according to the present embodiment includes steps that are roughly grouped into (a) an intermediate molding step and (b) a final molding step. According to the known art, only one type of mold is used to perform a reaming-drawing process on a metal disc to mold the metal disc into a desired shape (see FIGS. 16A and 17A). In contrast, the manufacturing method according to the present embodiment uses two different types of molds, so that a frustoconical intermediate molded article 100A that is different in shape from a desired final shape is produced in the intermediate molding step, and thereafter, the intermediate molded article 100A undergoes a further reaming-drawing process in the final molding step. As a result, a tubular rotary component having the desired shape is molded.

[0052] As illustrated in (a) in FIG. 1, the intermediate molding step is carried out using a mold including a punch 10A with a predetermined taper and a die 20A with a predetermined taper that are for use in the intermediate molding step. The metal disc 100 is subjected to the reaming-drawing process in which both surfaces of the metal disc 100 are pressed in their entirety with the mold, so that the intermediate molded article 100A is produced. As can be seen, the tapered surface of the punch 10A and that of the die 20A sandwich therebetween both surfaces of the metal disc 100 in their entirety. This feature makes it possible to reduce occurrence of cracks that can be caused by tension and bending, in comparison with the conventional case where a metal disc is subjected to the drawing process while the rim of the metal disc is held with a holding plate (see FIG. 16B). Further, this feature can reduce occurrence of wrinkles and occurrence of cracks that can be caused by the wrinkles, in comparison with the conventional case (FIG. 17B) where a metal disc is subjected to the drawing process without using a holding plate for holding the rim of the metal disc.

[0053] The tapered surface of the punch 10A and that of the die 20A form an angle θ.sub.p and an angle θ.sub.d with a processing direction, respectively. In the present embodiment, the angles are set to satisfy the relationship expressed as θ.sub.p=θ.sub.d in order to make the produced tubular rotary component have a uniform thickness.

[0054] Setting the angle θ.sub.p of the punch 10A and the angle θ.sub.d of the die 20A to 25 degrees or greater makes it possible to produce the intermediate molded article 100A while reducing occurrence of cracks. Setting the angles θ.sub.p and θ.sub.d to 30 degrees or greater makes it possible to produce the intermediate molded article 100A while reducing occurrence of minute wrinkles.

[0055] As illustrated in (b) in FIG. 1, the final molding step is carried out using a mold including a punch 10B and a die 20B that are for use in the final molding step and are configured to mold the tubular rotary component having a desired shape. The intermediate molded article 100A is subjected to a further drawing process using the mold, so that the tubular rotary component 100B is produced. The punch 10B and the die 20B for use in this step have taper angles (θ.sub.p and θ.sub.d) smaller than those of the punch and the die for use in the intermediate molding step. In the present embodiment, to produce the tubular rotary component having an inside diameter D.sub.1′ and an outside diameter D.sub.2′, the punch 10B is designed to have a circular column shape with an outside diameter D.sub.1′ while the die 20B is designed to have an annular shape with an inside diameter D.sub.2′ (where angles θ.sub.p and θ.sub.d are both 0 degree).

[0056] Note that the “intermediate molding step” as used herein refers to subjecting the metal disc or the intermediate molded article to the reaming-drawing process, while both surfaces of the metal disc or the intermediate molded article are pressed in their entirety by the tapered surfaces. The “final molding step” as used herein refers to a step in which the intermediate molded article is subjected to the reaming-drawing process while both surfaces of the intermediate molded article are pressed in their entirety, but not by tapered surfaces.

[0057] Next, a stretch flange rate λ in the process in which the metal disc 100 is molded into the tubular rotary component 100B will be described.

[0058] Based on the inside diameter D.sub.1 of the metal disc 100 before the reaming-drawing process and the inside diameter D.sub.1′ of the tubular rotary component produced through the final molding step, the stretch flange rate λ is given by λ (%)=(D.sub.1′−D.sub.1)D.sub.1×100. If the inside diameter D.sub.1′ resulting from the final molding step is excessively large with respect to the inside diameter D.sub.1 before the reaming-drawing process, the risk of cracks arises. Therefore, it is preferable to set the shape of the metal disc 100 such that the stretch flange rate λ will be 90% or less.

[0059] The above-described method for manufacturing the tubular rotary component according to the present embodiment produces the following effects.

[0060] (1) The method is for manufacturing the tubular rotary component 100B from the doughnut-shaped metal disc 100 having the predetermined inside diameter D.sub.1 and the predetermined outside diameter D.sub.2. The method includes: the intermediate molding step including subjecting the metal disc 100 to the reaming-drawing process in which both surfaces of the metal disc 100 are pressed in their entirety by the tapered surfaces of the punch 10A with the predetermined taper and the die 20A with the predetermined taper, thereby producing the intermediate molded article 100A having a frustoconical shape; and the final molding step including subjecting the intermediate molded article 100A to the further reaming-drawing process in which the intermediate molded article 100A is pressed by the punch 10B and the die 20B that have a desired shape, thereby producing the tubular rotary component 100B. This feature makes it possible to mold the metal disc 100 into the tubular rotary component 100B, while reducing occurrence of cracks and wrinkles during the reaming-drawing processes. In the case of using a steel plate as the material for the metal disc, the tubular rotary component 100B can be made to have sufficient rolling fatigue characteristics.

[0061] (2) According to the manufacturing method of the present invention, the processes are carried out under the conditions that the stretch flange rate λ is 90% or less, the stretch flange rate λ being given by λ=(D.sub.1′−D.sub.1)/D.sub.1×100 where D.sub.1 represents the inside diameter of the metal disc 100 before undergoing the processes and D.sub.1′ represents the inside diameter of the tubular rotary component 100B produced through the final molding step. This feature makes it possible to produce the tubular rotary component 100B, while reducing occurrence of cracks.

[0062] (3) In the intermediate molding step, the angle θ.sub.p formed between the tapered surface of the punch 10A and the processing direction and the angle θ.sub.d formed between the tapered surface of the die 20A and the processing direction are each set to 30 degrees or greater. This feature makes it possible to produce the tubular rotary component 100B, while reducing occurrence of minute wrinkles.

<Modifications>

[0063] Next, a modification of the present embodiment will be described with reference to FIG. 2. This modification differs from the embodiment illustrated in FIG. 1 in that in the intermediate molding step of the modification, the reaming-drawing process is performed two or more times, while the angle between the tapered surface of the punch and the processing direction and the angle between the tapered surface of the die and the processing direction are varied. Dividing the intermediate molding step into two or more steps in this manner allows the reaming-drawing process to be performed further suitably.

[0064] As illustrated in (a) in FIG. 2, in the intermediate molding step, the metal disc 100 is subjected to a first reaming-drawing process in which both surfaces of the metal disc 100 are pressed in their entirety using a mold including a punch 10A1 with a predetermined taper and a die 20A1 with a predetermined taper, thereby producing an intermediate molded article 100A1.

[0065] A tapered surface of the punch 10A1 and that of the die 20A1 form an angle θ.sub.p1 and an angle θ.sub.d1 with a processing direction, respectively. In the present modification, the angles are set to satisfy a relationship expressed as θ.sub.p1=θ.sub.d1 in order to make the produced tubular rotary component have a uniform thickness.

[0066] As illustrated in (b) in FIG. 2, in the intermediate molding step, the intermediate molded article 100A1 is subjected to a second reaming-drawing process in which both surfaces of the intermediate molded article 100A1 are pressed in their entirety using a mold including a punch 10A2 with a predetermined taper and a die 20A2 with a predetermined taper, thereby producing an intermediate molded article 100A2.

[0067] A tapered surface of the punch 10A2 and that of the die 20A2 form an angle θ.sub.p2 and an angle θ.sub.d2 with the processing direction, respectively. In the present modification, the angles are set to satisfy a relationship expressed as θ.sub.p2=θ.sub.d2 in order to make the produced tubular rotary component have a uniform thickness. The angles θ.sub.p2 and θ.sub.d2 formed between the processing direction and the tapered surfaces of the punch 10A2 and the die 20A2 for use in the second reaming-drawing process are smaller than the angles θ.sub.p1 and θ.sub.d1 formed between the processing direction and the tapered surfaces of the punch 10A1 and the die 20A1 for use in the first reaming-drawing process.

[0068] As illustrated in (c) in FIG. 2, in the final molding step, the intermediate molded article 100A2 is subjected to a further drawing process using a mold including a punch 10B and a die 20B that are configured to mold the tubular rotary component having a desired shape. As a result, a tubular rotary component 100B is produced. In the present embodiment, to produce the tubular rotary component having an inside diameter D.sub.1′ and an outside diameter D.sub.2′, the punch 10B is designed to have a circular column shape with an outside diameter D.sub.1′ while the die 20B is designed to have an annular shape with an inside diameter D.sub.2′.

[0069] The method for manufacturing the tubular rotary component according to the present modification produces the following effects.

[0070] (4) In the intermediate molding step, the reaming-drawing process is performed two or more times, while the angle between the tapered surface of the punch and the processing direction and the angle between the tapered surface of the die and the processing direction are varied. This feature makes it possible to carry out the intermediate molding step further suitably, in comparison with the case where the intermediate molding step includes performing the reaming-drawing process once.

EXAMPLES

[0071] Next, with reference to FIGS. 3 to 15B, Examples in which tubular rotary components 100B were produced by the manufacturing method of the present invention and Comparative Examples in which tubular rotary components were produced by the conventional methods will be described.

[0072] A SUJ2 steel plate having a plate thickness of 6 mm was used as the material for each metal disc 100. The reaming-drawing process of the intermediate molding step and that of the final molding step were performed under the drawing process conditions shown in Table 1.

TABLE-US-00001 TABLE 1 Pressing Apparatus Mechanical Press (product of AMADA CO., LTD.) Machining Speed 20 SPM Lubricating Oil G-3456 (product of Nihon Kohsakuyu Co., Ltd.)

[0073] The tubular rotary components of the Examples and Comparative Examples were produced with different values of the stretch flange rate A. The tubular rotary components of Examples 1-1 to 1-3 were produced using the molds illustrated in FIG. 3 under the condition that λ=0%. The tubular rotary components of Examples 2-1 to 2-3 were produced using the molds illustrated in FIG. 5 under the condition that λ=85%. The tubular rotary component of Comparative Example 1 illustrated in FIG. 6 was produced under the condition that λ=100%.

[0074] The tubular rotary components of Examples 1-1′ to 1-3′ and Examples 2-1′ to 2-3′ were produced using the molds illustrated in FIG. 1. Examples 1-1′ to 1-3′ correspond to Examples 1-1 to 1-3, respectively. Examples 2-1′ to 2-3′ correspond to Examples 2-1 to 2-3, respectively.

[0075] FIG. 4 is a photograph showing the external appearance of the tubular rotary components of Example 1-1. FIG. 7 is a photograph showing the external appearance of the tubular rotary component of Comparative Example 1.

[0076] For the purpose of comparison with the conventional manufacturing methods, the tubular rotary component of Comparative Example 2 was produced using the mold disclosed in Patent Document 1, as illustrated in FIG. 8, and the tubular rotary component of Comparative Example 3 was produced using the mold disclosed in Patent Document 2, as illustrated in FIG. 9.

[0077] Table 2 shows the specifics of the shapes of the metal discs 100 used in Examples and Comparative Examples. Table 3 summarizes the results of the drawing process tests.

TABLE-US-00002 TABLE 2 Inside Outside Diameter Diameter Thickness D.sub.1(mm) D.sub.2(mm) H(mm) Remarks 10.0 30.0 6.0 Example 1 5.4 28.8 6.0 Example 2 Comparative Examples 2, 3 5.0 28.7 6.0 Comparative Example 1

TABLE-US-00003 TABLE 3 Intermediate Intermediate Stretch Molding Step Molding Step Flange First Second Final Rate θ.sub.p1, θ.sub.d1 θ.sub.p2, θ.sub.d2 Molding λ (%) (Degrees)/Evaluation (Degrees)/Evaluation Step Example 1-1 0 45/OK 20/OK OK Example 1-1′ 0 45/OK — OK Example 1-2 0 30/OK 20/OK OK Example 1-2′ 0 30/OK — OK(Minute Wrinkle) Example 1-3 0 25/OK(Minute 20/OK(Minute OK(Minute Wrinkle) Wrinkle) Wrinkle) Example 1-3′ 0 25/OK(Minute — OK(Minute Wrinkle) Wrinkle) Example 2-1 85 45/OK 20/OK OK Example 2-1′ 85 45/OK — OK Example 2-2 85 30/OK 20/OK OK Example 2-2′ 85 30/OK — OK(Minute Wrinkle) Example 2-3 85 25/OK(Minute 20/OK(Minute OK(Minute Wrinkle) Wrinkle) Wrinkle) Example 1-3′ 85 25/OK(Minute — OK(Minute Wrinkle) Wrinkle) Comparative 100 45/OK 20/OK NG(Crack) Example1 Comparative 85 — — NG(Crack) Example2-1 (Mold of Patent Document 1) Comparative 85 — — NG(Crack) Example2-2 (Mold of Patent Document 2)

[0078] As shown in Table 3, a comparison between the stretch flange rates of Examples 1-1 to 2-3 and Comparative Example 1 demonstrates the following. Examples 1-1 to 2-3 of which the stretch flange rate λ was 90% or less allowed the reaming-drawing processes to be performed, with the absence of cracks, as shown in FIG. 4. Comparative Example 1 of which the stretch flange rate λ was 100% experienced a crack in the final molding step, as shown in FIG. 7. It was confirmed that if the first reaming-drawing process in the intermediate molding step is performed in a state where the angles θ.sub.p1 and θ.sub.d1 of the tapered surfaces are 25 degrees or greater, the drawing process can be performed suitably although minute wrinkles are observed after the final molding step. It was also confirmed that if the first reaming-drawing process is performed in a state where the angles θ.sub.p1 and θ.sub.d1 of the tapered surfaces are 30 degrees or greater, the drawing process can be performed without allowing minute wrinkles to form. The minute wrinkles can be eliminated by a cutting process performed in a later step, and do not affect the shape and strength of the finished products.

[0079] Regarding Examples 1-1′ to 1-3′ and Examples 2-1′ to 2-3′ in which the intermediate molding step is carried out once and is followed by the final molding step, it was confirmed that if the reaming-drawing process is performed in a state where the angles θ.sub.p1 and θ.sub.d1 of the tapered surfaces are 25 degrees or greater, the drawing process can be performed suitably although minute wrinkles are observed after the final molding step. It was also confirmed that if the reaming-drawing process is performed in a state where the angles θ.sub.p1 and θ.sub.d1 of the tapered surfaces are 40 degrees or greater, the reaming-drawing process can be performed without allowing minute wrinkles to form.

[0080] In Comparative Examples 2-1 and 2-2, the same metal discs 100 as those of Examples 2-1 to 2-3 were used. That is, under the same condition that the stretch flange rate λ is 85%, the reaming-drawing process of the final molding step was performed using the conventional mold, while the intermediate molding step was omitted. Comparative Examples 2-1 and 2-2 experienced cracks, making it impossible to produce tubular rotary components.

[0081] Next, with reference to a case where a tubular rotary component produced through the reaming-drawing process is subjected to a cutting process, an effect exerted on the rolling fatigue characteristics by a cutting volume will be described.

[0082] With reference to FIG. 10, a residual ratio of an inside diameter-side thickness and that of an outside diameter-side thickness will be described. The residual ratio is an index indicating a volume cut off from an inner surface of the tubular rotary component or a volume cut off from an outer surface of the tubular rotary component.

[0083] FIG. 10 is a schematic diagram illustrating the tubular rotary component 100B that has been subjected to the reaming-drawing process, as viewed in an axial direction of the tubular shape. A plate thickness after the drawing process is denoted by t.sub.m. A partial thickness to the midpoint of the plate thickness (thickness midpoint) is denoted by t.sub.mc (t.sub.mc=t.sub.m/2). An inside diameter after the drawing process is denoted by D.sub.1′. An outside diameter after the drawing process is denoted by D.sub.2′. An inside diameter after the cutting process is denoted by D.sub.1c′. An outside diameter after the cutting process is denoted by D.sub.2c. Accordingly, an inside diameter-side cut thickness t.sub.mc1 is expressed as t.sub.mc1=(D.sub.1c′−D.sub.1′)/2. An outside diameter-side cut thickness t.sub.mc2 is expressed as t.sub.mc2=(D.sub.2′−D.sub.2c′)/2. Thus, an inside diameter-side partial thickness t.sub.1 after the cutting process is expressed as t.sub.1=t.sub.mc−t.sub.mc1, whereas an outside diameter-side partial thickness t.sub.2 after the cutting process is expressed as t.sub.2=t.sub.mc−t.sub.mc2. Hence, the residual ratio of the inside diameter-side thickness is given by t.sub.1/t.sub.mc, and the residual ratio of the outside diameter-side thickness is given by t.sub.2/t.sub.mc.

[0084] FIG. 11 shows examples of inclusions present in the steel plate as the material for the metal disc 100, as observed with an optical microscope. In FIG. 11, blackish particles are the inclusions, such as Al.sub.2O.sub.3, MnS, and TiN.

[0085] In the case of the metal disc made of steel, the inclusions generally contain three types of inclusion: namely, A type inclusions, which have undergone viscous deformation due to a process; B type inclusions, which form groups of particles arranged discontinuously in the processing direction; and C type inclusions, which have not undergone viscous deformation and are irregularly dispersed. Known representative non-metallic inclusions of A type inclusions include, for example, MnS as a sulfide having an elongated shape and SiO.sub.2 as silicate. Known representative non-metallic inclusions of B type inclusions include, for example, Al.sub.2O.sub.3. Known representative non-metallic inclusions of C type inclusions include, for example, oxide particles.

[0086] These non-metallic inclusions can be counted by microscopic observation in accordance with JIS G0555 “Microscopic testing method for the non-metallic inclusions in steel”. For example, the number of inclusions can be counted in the following manner. A specimen is cut off from a target, polished to be provided with mirror finish without etching, and observed with an optical microscope at 400×.

[0087] Next, with reference to FIG. 12, a process for determining a quantity of inclusions present in the tubular rotary component will be described. As illustrated in (a) in FIG. 12, a cuboid portion in a size of 2 mm×12 mm×3 mm is cut from the tubular rotary component. The cuboid portion is then further cut into six pieces as illustrated in (b) in FIG. 12, thereby preparing six cuboid specimens in a size of 2 mm×12 mm×0.5 mm. At this time, the specimens are cut such that the boundary between the third and fourth specimens coincides with the midpoint of the plate thickness (thickness midpoint). While the midpoint of the plate thickness is defined as 0 mm, a measurement position located toward the inner surface with respect to the midpoint is denoted by a negative numeral and a measurement position located toward the outer surface with respect to the midpoint is denoted by a positive numeral. The inclusions appearing on a surface of the specimen are counted using an optical microscope.

[0088] The count is then converted to the number per area of 1 mm.sup.2. The inclusions are counted on only one of the outer surface and the inner surface of each specimen. The number of the inclusions is divided by the area of the specimen, i.e., 2 mm×12 mm, whereby the number is converted to the number per area of 1 mm.sup.2. In the present embodiment, the inclusions appearing on the outer surface of each specimen was counted.

[0089] Quantities of the inclusions were measured by the foregoing process. FIG. 13 illustrates the results of the measurement. Example 3 is the tubular rotary component produced by the method of the present invention. A seamless tube of SUJ2 steel (having an inside diameter of 10 mm, an outside diameter 22 mm, and a wall thickness of 6 mm) produced by the Mannesmann piercing method was cut into a piece having a length of 13 mm along an axis of the tube, thereby producing a tubular rotary component as Comparative Example 3. The tubular rotary component of Example 3 corresponds to the tubular rotary component of Example 1-1 shown in Table 3. The tubular rotary component of Example 3 and that of Comparative Example 3 were each subjected to a cutting process to have an inside diameter of 11.9 mm, an outside diameter 20.1 mm, and a height of 12.1 mm.

[0090] The results shown in FIG. 13 demonstrate that the tubular rotary component of Example 3 includes many inclusions present near the midpoint of the plate thickness, and the quantity of inclusions decreases toward the inner surface and toward the outer surface. That is, when the quantity of inclusions present in an inside diameter-side surface layer is defined as d (inside diameter) and the quantity of inclusions present at the midpoint of the plate thickness is defined as d (plate thickness midpoint), the distribution of the quantity of the inclusions in the plate thickness of the tubular rotary component satisfies a relationship expressed as d (plate thickness midpoint)>d (inside diameter). Further, when the quantity of inclusions present in an outside diameter-side surface layer is defined as d (outside diameter), the distribution of the quantity of the inclusions satisfies a relationship expressed as d (plate thickness midpoint)>d (outside diameter). On the other hand, it was confirmed that in Comparative Example 3 made of the seamless steel tube, the quantity of inclusions increases toward the inner surface while decreasing toward the outer surface.

[0091] Next, to study an effect exerted on the rolling fatigue characteristics by the residual ratio of the inside diameter-side thickness and that of the outside diameter-side thickness, test pieces having different residual ratios of the inside diameter-side and outside diameter-side thicknesses were prepared.

[0092] Rolling fatigue testers will be described with reference to FIGS. 14A and 14B.

[0093] FIG. 14A illustrates a rolling fatigue test for the inner surface. In this test, a shaft S1 is brought into contact with the outer surface of the test piece of the tubular rotary component, and a steel ball B is brought into contact with the inner surface of the test piece (see (a) in FIG. 14A). The steel ball B is fitted to a shaft S2 (see (b) in FIG. 14A). In the illustrated configuration, when the shaft S1 under a load is maintained in contact with the test piece while rotating in the direction indicated in FIG. 14A, the test piece is rotated and the steel ball B rolls.

[0094] FIG. 14B illustrates a rolling fatigue test for the outer surface. In this test, a shaft S4 is brought into contact with the inner surface of the test piece of the tubular rotary component, and a steel ball B is brought into contact with the outer surface of the test piece (see (a) in FIG. 14B). The steel ball B is fitted to a shaft S3 (see (b) in FIG. 14B). In the illustrated configuration, while the shaft S4 is rotated in the direction indicated in FIG. 14B, a load is applied via the shaft S3 such that the shaft S4 is brought into contact with the test piece. Consequently, the test piece is rotated and the steel ball B rolls while being in contact with the outer surface.

[0095] Tubular rotary components of Examples and Comparative Examples were produced to have different residual ratios of the inside diameter-side and outside diameter-side thicknesses. The produced tubular rotary components were subjected to heat treatment under the heat treatment conditions shown in Table 4 and a fine finishing process, whereby the following tubular rotary components were prepared: tubular rotary components of Examples 4-1 to 4-3 and Comparative Example 4 (having different residues ratio of the inside diameter-side thickness); and tubular rotary components of Examples 5-1 to 5-3, Comparative Examples 5-1 and 5-2 (having different residue ratios of the outside diameter-side thickness). The cutting process after the reaming-drawing process was performed so that a finishing allowance of 0.1 mm was left with respect to a desired shape. The fine finishing process after the heat treatment was performed to grind the tubular rotary component by about 0.1 mm, thereby achieving the desired shape.

[0096] The tubular rotary components of these Examples and Comparative Examples were subjected to rolling fatigue tests under the test conditions shown in Table 5. Table 6 shows a relationship between the residue ratio of the inside diameter-side thickness and the rolling fatigue characteristics. Table 7 shows a relationship between the residue ratio of the outside diameter-side thickness and the rolling fatigue characteristics. The tubular rotary components of Examples and Comparative Examples shown in Table 7 all have a height of 12 mm. The rolling fatigue test results are evaluated and indicated as follows.

[0097] Under the conditions shown in Table 5, a cumulative fracture probability of the tests in which n=16 was calculated. The tubular rotary component having the characteristics equivalent or superior to those of a tubular rotary component made of a seamless steel tube was evaluated as good, and is marked with circle symbol (○). The tubular rotary component having the characteristics inferior to those of the tubular rotary component made of a seamless steel tube was evaluated as poor, and is marked with cross symbol (×).

TABLE-US-00004 TABLE 4 Hardening Tempering Temperature (° C.) 820 160 Time (Min.) 30 60 Cooling Method Oil Cooling Air Cooling

TABLE-US-00005 TABLE 5 Steel Ball Made of SUJ2, φ3 Maximum Contact Stress 4903 N/mm .sup.2 Number of Revolutions 1800 cpm Lubricating Oil Turbine #68 Maximum Number of 108 times Repetitions n (number) 16

TABLE-US-00006 TABLE 6 Residual Inside Ratio of Diameter- Inside Rolling Outside Inside Side Diameter- Fatigue Diameter Diameter Thickness Side Test (mm) (mm) (mm) Thickness Result Before Finishing 21.5 9.8 2.925 1 — Process(Example 3) Example 4-1 20 11 2.32 0.79 ∘ Example 4-2 20 12 1.82 0.62 ∘ Example 4-3 20 13 1.32 0.45 ∘ Example 4-4 20 13.5 1.07 0.37 ∘ Comparative 20 14 0.825 0.28 x Example4

TABLE-US-00007 TABLE 7 Residual Outside Ratio of Diameter- Outside Rolling Outside Inside Side Diameter- Fatigue Diameter Diameter Thickness Side Test (mm) (mm) (mm) Thickness Result Before Finishing 21.5 9.8 2.925 1 — Process(Example 3) Example 5-1 20 12 2.23 0.76 ∘ Example 5-2 19 12 1.68 0.57 ∘ Example 5-3 18.5 12 1.43 0.49 ∘ Comparative 18 12 1.18 0.40 x Example5-1 Comparative 17 12 0.68 0.23 x Example5-2

[0098] As shown in Table 6, in the cases of the tubular rotary components manufactured by the method including the cutting process step, if the residue ratio of the inside diameter-side thickness was equal to or greater than 0.37, good rolling fatigue characteristics were obtained. As shown in Table 7, if the residue ratio of the outside diameter-side thickness was equal to or greater than 0.49, good rolling fatigue characteristics were obtained.

[0099] Next, the following tubular rotary components were subjected to the rolling fatigue tests: the tubular rotary component of Example 4-1 (Table 6), the inside diameter side of which was subjected to the cutting process; the tubular rotary component of Example 5-1 (Table 7), the outside diameter side of which was subjected to the cutting process; and the tubular rotary component of Comparative Example 6 made from a seamless steel tube.

[0100] The tubular rotary component of Comparative Example 6 was made from a seamless tube of SUJ2 steel produced by the Mannesmann piercing method and having an outside diameter of 22 mm, an inside diameter of 10 mm, and a wall thickness of 6 mm. The seamless tube was subjected to a tube-drawing process to be formed into a shape with an outside diameter of 21.5 mm and an inside diameter of 9.8 mm. Subsequently, like Examples 4-1 and 5-1, the tubular rotary component of Comparative Example 6 underwent heat treatment and the finishing process to be formed into a shape with an outside diameter of 20 mm and an inside diameter of 12 mm. Thus, Comparative Example 6 has the residual ratio of the inside diameter-side thickness identical to that of Example 4-1, and the residual ratio of the outside diameter-side identical to that of Example 5-1.

[0101] The results of the rolling fatigue tests are illustrated in FIGS. 15A and 15B. FIG. 15A illustrates the results of the tests on the inner surfaces, while FIG. 15B illustrates the results of the tests on the outer surfaces.

[0102] The inner surfaces of the tubular rotary components of Examples 4-1 and 5-1 have better rolling fatigue characteristics than the inner surface of the seamless steel tube of Comparative Example 6. The outer surfaces of the tubular rotary components of Examples 4-1 and 5-1 have rolling fatigue characteristics equivalent to those of the outer surface of the seamless steel tube of Comparative Example 6.

[0103] Thus, in comparison with the case of producing a tubular rotary component from a seamless steel tube as a materiel, the manufacturing method of the present invention eliminates the need to cut off a considerable volume from the inner surface, improves material yield, and shortens time required for the cutting, thereby enabling an increase in productivity. Further, the manufacturing method of the present invention allows little difference in the rolling fatigue characteristics between the inner surface and the outer surface. Thus, the tubular rotary component of the present invention is suitable for inner and outer rings of a radial bearing.

[0104] In the foregoing, embodiments, modifications, and examples of the method for manufacturing the tubular rotary component according to the present invention have been described. However, the above-described embodiments, modifications, and examples are not intended to limit the present invention, and appropriate variations can be made to the present invention.

[0105] For example, in the above examples, the reaming-drawing process was performed once or twice. However, this is a non-limiting example. The reaming-drawing process may be performed more times, as necessary.

EXPLANATION OF REFERENCE NUMERALS

[0106] 10A, 10A1, 10A2, 10B: Punch [0107] 20A, 20A1, 20A2, 20B: Die [0108] 100: Metal Disc [0109] 100A, 100A1, 100A2: Intermediate Molded Article [0110] 100B: Tubular Rotary Component