HUB UNIT BEARING AND METHOD FOR MANUFACTURING SAME
20220325751 · 2022-10-13
Inventors
Cpc classification
F16C43/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2226/52
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2326/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/063
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/186
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21K25/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
F16C25/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An amount of decrease ΔC in an axial clearance of a hub unit bearing is found based on an amount of expansion ΔD of an inner ring of the hub unit bearing, which is the difference between the outer-diameter dimension D1 of the inner ring after the inner ring is externally fitted with a tubular fitting portion of a hub spindle of the hub unit bearing and after formation of a swaged portion of the hub spindle, the inner ring being held between the swaged portion and a stepped surface of the hub spindle, and an outer-diameter dimension D0 of the inner ring before the inner ring is externally fitted with the tubular fitting portion.
Claims
1. A method for manufacturing a hub bearing unit; the hub bearing unit comprising: an outer ring supported by and fastened to a suspension device so as not to rotate, and having double-row outer-raceways around an inner-circumferential surface thereof; a hub to which a wheel is fastened and that rotates together with the wheel, and having double-row inner-raceways around an outer-circumferential surface thereof; a plurality of rolling bodies arranged between the double-row outer-raceways and the double-row inner-raceways, and to which a preload is applied; the hub comprising: an inner ring having an inner-raceway on an axially inner side of the double-row inner-raceways around an outer-circumferential surface thereof; and a hub spindle having an inner-raceway on an axially outboard side of the double-row inner-raceways around an outer-circumferential surface at an axially intermediate section thereof; and the inner ring and the hub spindle, in a state in which the inner ring is externally fitted with a tubular fitting portion positioned further on the axially inboard side than the inner-raceway of the hub spindle that is on the axially outboard side, being joined and fastened together by pushing an end surface on the axially inboard side of the inner ring by a swaged portion formed by plastically deforming a tubular portion of the hub spindle that protrudes further toward the axially inboard side than an end surface on the axially inboard side of the inner ring outward in a radial direction; the method for manufacturing the hub unit bearing comprising: a pre-fitting step of measuring an outer-diameter dimension of the inner ring before externally fitting the inner ring with the tubular fitting portion; an arranging step of arranging the outer ring and the rolling bodies around the hub spindle; an external fitting step of externally fitting the inner ring with the tubular fitting portion; a swaging step of forming the swaged portion by plastically deforming the tubular portion outward in the radial direction; and a post-swaging step of measuring an outer-diameter dimension of the inner ring after formation of the swaged portion; then, finding an amount of decrease in an axial clearance that is decreased by the external fitting step and the swaging step based on an amount of expansion of the inner ring that is a difference between the outer-diameter dimension of the inner ring after formation of the swaged portion and the outer-diameter dimension of the inner ring before being externally fitted with the tubular fitting portion; and controlling the preload based on the amount of decrease in the axial clearance.
2. The method for manufacturing the hub unit bearing according to claim 1, wherein an axial clearance of the hub unit bearing in a state after formation of the swaged portion is calculated by subtracting the amount of decrease in the axial clearance from an initial axial clearance, which is an axial clearance of the hub unit bearing in a state before formation of the swaged portion, and the preload is found in a completed state of the hub unit bearing based on the axial clearance.
3. The method for manufacturing the hub bearing unit according to claim 2, wherein the preload is set within a specified range by using the preload in the completed state of the hub unit bearing that is found based on the axial clearance.
4. A hub unit bearing, comprising: an outer ring supported by and fastened to a suspension device so as not to rotate, and having double-row outer-raceways around an inner-circumferential surface thereof; a hub to which a wheel is fastened and that rotates together with the wheel, and having double-row inner-raceways around an outer-circumferential surface thereof; a plurality of rolling bodies arranged between the double-row outer-raceways and the double-row inner-raceways, and to which a preload is applied; the hub comprising: an inner ring having an inner-raceway on an axially inner side of the double-row inner-raceways around an outer-circumferential surface thereof; and a hub spindle having an inner-raceway on an axially outboard side of the double-row inner-raceways around an outer-circumferential surface at an axially intermediate section thereof; and the inner ring and the hub spindle, in a state in which the inner ring is externally fitted with a tubular fitting portion positioned further on the axially inboard side than the inner-raceway of the hub spindle that is on the axially outboard side, being joined and fastened together by pushing an end surface on the axially inboard side of the inner ring by a swaged portion formed by plastically deforming a tubular portion of the hub spindle that protrudes further toward the axially inboard side than an end surface on the axially inboard side of the inner ring outward in a radial direction; wherein the preload is controlled based on an amount of decrease in an axial clearance found from an amount of expansion of the inner ring, which is the difference between an outer-diameter dimension of the inner ring after formation of the swaged portion and an outer-diameter dimension of the inner ring before being externally fitted with the tubular fitting portion.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0027]
[0028]
[0029]
[0030]
[0031]
[0032]
[0033]
[0034]
DESCRIPTION OF THE EMBODIMENTS
[0035] An example of an embodiment of the present invention will be described referring
[0036] <Structure of Hub Unit Bearing>
[0037] A hub unit bearing 1 that is the object of this embodiment includes an outer ring 2, a hub 3, and rolling bodies 4a, 4b.
[0038] The outer ring 2 is made of a hard metal such as medium carbon steel or the like. The outer ring 2 has double-row outer-raceways 5a, 5b around the inner-circumferential surface, and has a stationary flange 6 at an axially intermediate section that protrudes toward the radially outer side. The stationary flange 6 has support holes 7 that penetrate in the axial direction at a plurality of locations in the circumferential direction of a radially intermediate section. The outer ring 2 is supported by and fastened to a suspension device by support bolts that are inserted through the support holes 7 of the stationary flange 6, and does not rotate even when a wheel rotates.
[0039] The hub 3 has double-row inner-raceways 8a, 8b around the outer-circumferential surface, and is coaxially arranged with the outer ring 2 on the radially inner side of the outer ring 2. The hub 3 has a rotating flange 9 located at a portion further on the axially outboard side than an end section on the axially outboard side of the outer ring 2 and protrudes toward the radially outer side, and has a cylindrical pilot section 10 at an end section on the other side in the axial direction. The rotating flange 9 has installation holes 11 that penetrate in the axial direction at a plurality of locations in the circumferential direction of a radially intermediate section. A stud 12 is press fitted (serration fit) in each of the installation holes 11. In other words, in this example, each installation hole 11 is composed of a press fitting hole.
[0040] Note that the “axially outboard side” is the outer side of the vehicle in a state in which the hub unit bearing 1 is assembled in the automobile, and is the left side in
[0041] A brake rotating body such as a disc, drum or the like, and wheel are fixed to the rotating flange 9 by inserting the pilot section 10 through a center hole that penetrates in the axial direction of a center section thereof, and inserting the studs 12 through through holes that axially penetrate at a plurality of locations in the circumferential direction of the radially intermediate section and screwing hub nuts on the tip-end sections of the studs 12.
[0042] Note that the installation holes of the rotating flange may be composed of female screw holes. In this case, the brake rotating body and wheel are joined and fastened to the rotating flange by screwing hub bolts that are inserted through through holes provided in the brake rotating body and through through holes provided in the wheel into the installation holes.
[0043] The hub 3 of this embodiment includes an inner ring 13 and a hub spindle 14.
[0044] The inner ring 13 is made of a hard metal such as bearing steel or the like. The inner ring 13 has an inner-raceway 8a on the axially inboard side of the double-row inner-raceways 8a, 8b at an axially intermediate section of the outer-circumferential surface. Furthermore, the inner ring 13 has an inner-ring shoulder section 15 at a portion of the outer-circumferential surface adjacent to the axially inboard side of the inner-raceway 8a on the axially inboard side, and has a chamfered section 16 having an arc-shaped cross section at a connecting section of the end surface on the axially inboard side and the inner-ring shoulder section 15. The inner-ring shoulder section 15 is composed of a cylindrical surface of which the outer-diameter dimension does not change along the axial direction.
[0045] The hub spindle 14 is made of a hard metal such as medium carbon steel or the like. The hub spindle 14 has an inner-raceway 8b on the axially outboard side of the double-row inner-raceways 8a, 8b at an axially intermediate section of the outer-circumferential surface. The hub spindle 14 has the rotating flange 9 that is located at a portion further on the axially outboard side than the inner-raceway 8b on the axially outboard side and that protrudes toward the radially outer side, and has the cylindrical shaped pilot section 10 at an end section on the axially outboard side.
[0046] The hub spindle 14 has a tubular fitting portion 17 that is located at a portion further on the axially inboard side than the inner-raceway 8b on the axially outboard side, the outer diameter of the tubular fitting portion 17 is smaller than that of a portion adjacent to the axially outboard side, and the inner ring 13 externally fits with the tubular fitting portion 17. Furthermore, the hub spindle 14 has a stepped surface 18 that faces toward the axially inboard side and to which the end surface on the axially outboard side of the inner ring 13 comes in contact, and has a swaged portion 19 that is bent toward the radially outer side of the end section on the axially inboard side of the tubular fitting portion 17 and that pushes the end surface on the axially inboard side of the inner ring 13. That is, the hub 3 of this embodiment is such that the inner ring 13 externally fits with the tubular fitting portion 17 of the hub spindle 14 with a press fit, and the swaged portion 19 pushes the end surface on the axially inboard side of the inner ring 13. In other words, the inner ring 13 is held on both sides in the axial direction between the stepped surface 18 and the swaged portion 19. As a result, the hub 3 is configured by joining and fastening the inner ring 13 and the hub spindle 14.
[0047] Each of the rolling bodies 4a, 4b is made of a hard metal such as bearing steel or the like, or is made of ceramic. The rolling bodies 4a, 4b are respectively arranged between the double-row outer-raceways 5a, 5b and the double-row inner-raceways 8a, 8b, and are respectively held by retainers 20a, 20b so as to be able to roll freely. As a result, the hub 3 is rotatably supported on the radially inner side of the outer ring 2. Moreover, a preload is applied to the rolling bodies 4a, 4b due to a force (axial force) that is applied toward the axially outboard side from the inner ring 13.
[0048] In this embodiment, balls are used as the rolling bodies 4a, 4b; however, it is also possible to use tapered rollers instead of balls. Furthermore, in this embodiment, the diameter of the pitch circle of the rolling bodies 4a, 4b in the row on the axially inboard side and the diameter of the pitch circle of the rolling bodies 4a, 4b in the row on the axially outboard side are the same as each other; however, the present invention can also be applied to an asymmetric type hub unit bearing in which the diameter of the pitch circle of the rolling bodies in the row on the axially inboard side and the diameter of the pitch circle of the rolling bodies in the row on the axially outboard side differ from each other.
[0049] The hub unit bearing 1 further includes seal devices 22a, 22b that are located between the inner-circumferential surface of the outer ring 2 and the outer-circumferential surface of the hub 3, and that cover opening sections on both sides in the axial direction of a cylindrical rolling body installation space 21 where the rolling bodies 4a, 4b are arranged.
[0050] Of the seal devices 22a, 22b, the seal device 22a on the axially inboard side includes a slinger 23 that is externally fastened to the inner-ring shoulder section 15 of the inner ring 13, and a seal ring 24 having seal lips that come in sliding contact with the surface of the slinger 23 around the entire circumference. In other words, in this embodiment, the seal device 22a on the axially inboard side is composed of a combination seal ring.
[0051] Note that a seal device on the axially inboard side for covering the opening section on the axially inboard side of the rolling body installation space could also be configured by a bottomed cylindrical shaped cover that is internally fixed to the outer ring. In this case, it is possible to externally fix an encoder for detecting the number of rotations (rotational speed) of the wheel to the inner-ring shoulder section of the inner ring as necessary.
[0052] Of the seal devices 22a, 22b, the seal device 22b on the axially outboard side has seal lips that come in sliding contact with the outer-circumferential surface of the hub 3 or the surface on the axially inboard side of the rotating flange 9 around the entire circumference. In other words, in this embodiment, the seal device 22b on the axially outboard side is composed of a seal ring.
[0053] <Method for Manufacturing Hub Unit Bearing>
[0054] When manufacturing the hub unit bearing 1, as illustrated in
[0055] Next, as illustrated going from
[0056] The method for forming the swaged portion 19 is not particularly limited. The swaged portion 19 could also be formed for example by pushing a die that is supported so as to be able to rotate around a rotation axis that is inclined with respect to the center axis of the hub spindle 14 against the end section on the axially inboard side of the tubular portion 25 while at the same time oscillating the die around the center axis of the hub spindle 14. Alternatively, the swaged portion 19 could be formed by stamping (deburring press) in which a die pushes the end section of the axially inboard side of the tubular portion 25 in the axial direction.
[0057] In the manufacturing method of this embodiment, in order to control the preload that is applied to the rolling bodies 4a, 4b in the completed state of the hub unit bearing 1, the outer-diameter dimension D.sub.0 of the inner ring 13 as a single body before being externally fitted with the tubular fitting portion 17 of the hub spindle 14 is measured. More specifically, the outer-diameter dimension D.sub.0 of the inner-ring shoulder section 15 of the inner ring 13 is measured. The inner-ring shoulder section 15 is composed of a cylindrical surface having good shape accuracy to which the slinger 23 of the seal device 22a, which is a combination seal ring, or an encoder is externally fitted. The position in the axial direction of the portion of the inner-ring shoulder section 15 where the outer-diameter dimension D.sub.0 is measured is not particularly limited. However, from the aspect of maintaining a large difference between the outer-diameter dimension D.sub.0 of the inner ring 13 before being externally fitted with the hub spindle 14, and the outer-diameter dimension D.sub.1 of the inner ring 13 after formation of the swaged portion 19, preferably the outer-diameter dimension D.sub.0 of the inner-ring shoulder section 15 is measured within a range located further on the axially outboard side than the chamfered section 16 and located as much as possible on the axially inboard side.
[0058] In the manufacturing method of this embodiment, the outer-diameter dimension D.sub.1 of the inner ring 13 is measured after the swaged portion 19 is formed and before the seal device 22a on the axially inboard side is installed. The position in the axial direction of the portion where the outer-diameter dimension D.sub.1 of the inner ring 13 is measured is the same as the position in the axial direction of the portion where the outer-diameter dimension D.sub.0 of the inner ring 13 before being externally fitted with the tubular fitting portion 17 of the hub spindle 14 is measured.
[0059] An amount of decrease ΔC in the axial space is found based on the amount of expansion ΔD of the inner ring 13, which is the difference (D.sub.1−D.sub.0) between the outer-diameter dimension D.sub.1 of the inner ring 13 after the swaged portion 19 is formed (swaged state) and the outer-diameter dimension D.sub.0 of the inner ring 13 before being externally fitted with the tubular fitting portion 17 of the hub spindle 14. The amount of decrease ΔC in the axial clearance represents the amount of decrease in the axial clearance of the hub unit bearing 1 that occurs when the swaged portion 19 is formed. The relation between the amount of expansion ΔD of the inner ring 13 and the amount of decrease ΔC in the axial clearance is found beforehand through experimentation and simulation, and is stored as a map or formula in memory of a computing device. In other words, the amount of expansion ΔD of the inner ring 13 is inputted to the computing device, and the amount of decrease ΔC in the axial clearance is found using the map or formula.
[0060] In this embodiment, the preload applied to the rolling bodies 4a, 4b is controlled based on the amount of decrease ΔC in the axial clearance that is found in this way. More specifically, determining whether or not the preload applied to the rolling bodies 4a, 4b is within a proper range, or setting the preload to be applied to the rolling bodies 4a, 4b to a proper range is performed based on the amount of decrease ΔC in the axial clearance.
[0061] As described above, in the method for manufacturing a hub unit bearing of this embodiment, the amount of decrease ΔC in the axial clearance of the hub unit bearing 1 is found based on the amount of expansion ΔD, which is the difference between the outer-diameter dimension D.sub.1 of the inner ring 13 in the swaged state and the outer-diameter dimension D.sub.0 of the inner ring 13 as a single body before being externally fitted with the tubular fitting portion 17 of the hub spindle 14. In other words, in this embodiment, the effect that not only the amount of expansion of the inner ring 13 due to the formation of the swaged portion 19 (the amount of expansion of the inner ring 13 from the state illustrated in
[0062] The reason for this will be described using
[0063] Here, in a case where the interference of the inner ring 13 with respect to the tubular fitting portion 17 is large, the friction force acting between the outer-circumferential surface of the tubular fitting portion 17 and the inner-circumferential surface of the inner ring 13 will become large. Therefore, when the interference of the inner ring 13 with respect to the tubular fitting portion 17 is large, the amount of movement of the end surface on the axially inboard side of the inner ring 13 toward the axially outboard side decreases, and the amount of expansion of the inner ring 13 also decreases as the swaged portion 19 is formed. In other words, when the interference of the inner ring 13 with respect to the tubular fitting portion 17 is large, the amount of decrease in the axial clearance due to formation of the swaged portion 19 decreases.
[0064] Conversely, in a case where the interference of the inner ring 13 with respect to the tubular fitting portion 17 is small, the friction force acting between the outer-circumferential surface of the tubular fitting portion 17 and the inner-circumferential surface of the inner ring 13 will become small. Therefore, when the interference of the inner ring 13 with respect to the tubular fitting portion 17 is small, the amount of movement of the end surface on the axially inboard side of the inner ring 13 toward the axially outboard side increases, and the amount of expansion of the inner ring 13 also increases as the swaged portion 19 is formed. In other words, when the interference of the inner ring 13 with respect to the tubular fitting portion 17 is small, the amount of decrease in the axial clearance due to formation of the swaged portion 19 increases.
[0065] Therefore, in a case where the processing load for forming the swaged portion 19 is the same for a specific size, as illustrated in
[0066] In the method described in JP 2003-013979A, only the amount of expansion of the inner ring before and after formation of the swaged portion (portion indicated by the mat pattern in
[0067] Note that in the manufacturing method of this embodiment, it is also possible to additionally find the initial axial clearance C.sub.0, which is the axial clearance of the hub unit bearing 1a in the state before formation of the swaged portion 19 (state illustrated in
[0068] In order to find the initial axial clearance C.sub.0, as illustrated in
[0069] The first dimension d.sub.1 and the second dimension d.sub.2 can be measured, for example, by using a dedicated measuring device that includes a curved surface section having a radius of curvature that is the same as ½ the diameter of the rolling bodies 4a, 4b (ball diameter), and a measuring element that is capable of moving toward or away from the curved surface section. In other words, in the single body state of the hub spindle 14, the first dimension d.sub.1 is obtained by bringing the curved surface section in contact with the inner-raceway 8b on the axially outboard side, and bringing the measuring element in contact with the stepped surface 18, and then measuring the interval in the axial direction between the center of curvature of the curved surface section and the stepped surface 18. Moreover, in the single body state of the inner ring 13, the second dimension d.sub.2 is obtained by bringing the curved surface section of the measuring device in contact with the inner-raceway 8a on the axially inboard side, and bringing the measuring element in contact with the end surface on the axially outboard side of the inner ring 13, and then measuring the interval in the axial direction between the center of curvature of the curved surface section and the end surface on the axially outboard side of the inner ring 13. Furthermore, a second dimension d.sub.2′ is obtained by correcting the second dimension d.sub.2 in consideration of the interference of the inner ring 13 with respect to the tubular fitting portion 17. In other words, the corrected second dimension d.sub.2′ is obtained by reducing the second dimension d.sub.2 by the amount that the center of the rolling bodies 4a of the row on the axially inboard side move toward the axially outboard side due to expansion of the inner-raceway 8a on the axially inboard side as the inner ring 13 is press fitted with the tubular fitting portion 17.
[0070] By finding the sum of the first dimension d.sub.1 and the corrected second dimension d.sub.2′ (d.sub.1+d.sub.2′), an inner-raceway distance d.sub.in, which is the distance between the double-row inner-raceways 8a, 8b in a state in which no axial force is applied by the swaged portion 19, is obtained.
[0071] Moreover, in the single body state of the outer ring 2, an outer-raceway distance clout, which is the distance in the axial direction between the center O.sub.outa of the rolling bodies 4a of the row on the axially inboard side and the center O.sub.outb of the rolling bodies 4b of the row on the axially outboard side, is measured for a case in which it is presumed that the rolling bodies 4a, 4b are in rolling contact with the double-row outer-raceways 5a, 5b of the outer ring 2.
[0072] The outer-raceway distance d.sub.out can be measured, for example, using a dedicated measuring device that includes a pair of curved surface sections having a radius of curvature that is the same as ½ the diameter of the rolling bodies 4a, 4b (ball diameter), and that are capable of moving toward or away from each other. In other words, in the single body state of the outer ring 2, the outer-raceway distance d.sub.out is obtained by bringing the pair of curved surface sections in contact with the double-row outer-raceways 5a, 5b and measuring the distance in the axial direction between the centers of curvature of the pair of curved surface sections.
[0073] The initial axial clearance C.sub.0 in the state before formation of the swaged portion 19 is obtained by finding the difference (d.sub.out−d.sub.in) between the outer-raceway distance d.sub.out and the inner-raceway distance d.sub.in.
[0074] Note that in a case where tapered rollers are used as the rolling bodies, the center of the rolling bodies that is specified for measuring the first dimension, the second dimension, and the outer-raceway distance can be set at any arbitrary position on the center axis of the rolling bodies. More specifically, of the center axis of the rolling bodies, an axially central position of the rolling bodies can be set as the center of the rolling bodies.
[0075] The axial clearance C.sub.1 of the hub unit bearing 1b in the swaged state is found by subtracting the amount of decrease ΔC in the axial clearance from the initial axial clearance C.sub.0.
[0076] Then, based on the axial clearance C.sub.1, it is possible to calculate the preload applied to the rolling bodies 4a, 4b in the completed state of the hub unit bearing 1, and to determine whether or not the calculated preload is within a proper range. Note that in this case, for the initial axial clearance C.sub.0 for finding the axial clearance C.sub.1 of the hub unit bearing 1b in the swaged state, it is possible to use a design value instead of finding the value through measurement.
[0077] Alternatively, it is possible to set the preload to be applied to the rolling bodies 4a, 4b to a proper specified range by calculating the preload applied to the rolling bodies 4a, 4b in the completed state of the hub unit bearing 1 based on the axial clearance C.sub.1, and using the calculated preload as feedback. More specifically, it is possible to select from among a plurality of outer rings 2, inner rings 13, and hub spindle 14, a combination of an outer ring 2, an inner ring 13, and a hub spindle 14 for which the initial axial clearance C.sub.0 will be proper, and it is possible to adjust the processing load when forming the swaged portion 19.
[0078] In any case, the relation between the axial clearance C.sub.1 and the preload applied to the rolling bodies 4a, 4b in the completed state of the hub unit bearing 1 can be found beforehand by experimentation, simulation or the like.
[0079] In this embodiment, a case is described of using a so-called third-generation hub unit bearing 1 that includes a hub 3 formed by joining and fixing one inner ring 13 to the hub spindle 14 as the object; however, in the present invention, it is also possible to use a so-called 2.5-generation hub unit bearing that includes a hub formed by joining and fixing a pair of inner rings to a shaft member as the object. In the 2.5-generation hub unit bearing, a hub spindle is composed of a shaft member, and an inner ring on the axially outboard side of a pair of inner rings.
[0080] Moreover, in this embodiment, a case is described of a hub unit bearing 1 for a non-driven wheel in which the hub 3 (hub spindle 14) has a solid structure; however, in the present invention, it is also possible to use a hub unit bearing for a driven wheel in which the hub has an engagement hole in the center section for engaging with a drive shaft so as to be able to transmit torque.
EXAMPLES
[0081] Experimentation that was performed in order to confirm the effect of the present invention will be described. This experimentation was performed using a hub unit bearing 1 such as illustrated in
[0082] <Specifications of the Hub Unit Bearing 1> [0083] Diameter of the rolling bodies 4a, 4b (ball diameter): 11.906 [mm] [0084] Pitch circle diameter of the rolling bodies 4a, 4b: 61 [mm] [0085] Material of the rolling bodies 4a, 4b: SUJ2 (bearing steel) [0086] Material of the inner ring 13: SUJ2 (bearing steel) [0087] Material of the hub spindle 14: S53C (medium carbon steel) [0088] Outer diameter of the inner-ring shoulder section 15 (in the single body state): 60 [mm]
[0089] Note that it is difficult to accurately measure the preload applied to the rolling bodies 4a, 4b, and thus in this experimentation, even after formation of the swaged portion 19, the initial axial clearance C.sub.0 was set to be larger than that of an actual product so that the axial clearance of the hub unit bearing 1 would be positive.
[0090] The swaged portion 19 was formed by using a die that is supported so as to be able to rotate about a rotation axis that is inclined with respect to the center axis of the hub spindle 14 to push and swage the end section on the axially inboard side of the tubular portion 25 with a load of 10.8 [kN] while oscillating the die about the center axis of the hub spindle 14 with a rotating motion (revolving motion) at rotating speed of 5 [s.sub.−1].
[0091] The initial axial clearance C.sub.0 of the hub unit bearing 1 used in this experimentation was found by measuring the amount of displacement in the axial direction of the hub 3 while restricting the axial displacement of the outer ring 2 in the state illustrated in
[0092] The axial clearance C.sub.1 of the hub unit bearing 1 in the completed state was found by measuring the amount of axial displacement of the hub 3 while restricting the axial displacement of the outer ring 2 in the state illustrated in
[0093] The amount of decrease ΔC in the axial clearance was calculated by finding the difference (C.sub.0−C.sub.1) between the initial axial clearance C.sub.0 and axial clearance C.sub.1 in the complete state.
[0094] In the Example, the amount of expansion ΔD of the inner ring 13 was found by measuring the outer-diameter dimension D.sub.0 of the inner ring 13 (inner-ring shoulder section 15) before being externally fitted with the tubular fitting portion 17, and the outer-diameter dimension D.sub.1 of the inner ring 13 after formation of the swaged portion 19, and calculating the difference (D.sub.1−D.sub.0) of these for fourteen hub unit bearings 1. The amount of expansion ΔD of the inner ring 13 found in this way, and the amount of decrease ΔC in the axial clearance are plotted in
[0095] In the Comparative Example, the outer-diameter dimension Do′ of the inner ring 13 after being fitted with the tubular fitting portion 17 and before formation of the swaged portion 19 was measured for fourteen hub unit bearings 1 in the same way as in the Example. Then, the amount of expansion ΔD′ of the inner ring was found by calculating the difference (D.sub.1−D.sub.0′) with the outer-diameter dimension D.sub.1 of the inner ring 13 after formation of the swaged portion 19. The amount of expansion ΔD′ of the inner ring 13 found in this way, and the amount of decrease ΔC in the axial clearance are plotted in
[0096] In the Comparative Example, a correlation coefficient between the amount of expansion ΔD′ of the inner ring 13 and the amount of decrease ΔC in the axial clearance was found to be 0.75; however, in the Example, a correlation coefficient between the amount of expansion ΔD of the inner ring 13 and the amount of decrease ΔC in the axial clearance was found to be 0.81. In other words, it was learned that the amount of expansion ΔD of the inner ring 13 from the single body state before being externally fitted with the tubular fitting portion 17 of the hub spindle 14 has a stronger correlation with the amount of decrease ΔC in the axial clearance than the amount of expansion ΔD′ of the inner ring 13 from the state of being externally fitted with the tubular fitting portion 17 and before formation of the swaged portion 19, and thus consequently, has a stronger correlation with the preload applied to the rolling bodies 4a, 4b.
REFERENCE SIGNS LIST
[0097] 1, 1a, 1b Hub unit bearing [0098] 2 Outer ring [0099] 3 Hub [0100] 4 Rolling body [0101] 5a, 5b Outer-raceway [0102] 6 Stationary flange [0103] 7 Support hole [0104] 8a, 8b Inner-raceway [0105] 9 Rotating flange [0106] 10 Pilot section [0107] 11 Installation hole [0108] 12 Stud [0109] 13 Inner ring [0110] 14 Hub spindle [0111] 15 Inner-ring shoulder section [0112] 16 Chamfered section [0113] 17 Tubular fitting portion [0114] 18 Stepped surface [0115] 19 Swaged portion [0116] 20a, 20b Retainer [0117] 21 Rolling body installation space [0118] 22a, 22b Seal device [0119] 23 Slinger [0120] 24 Seal ring [0121] 25 Tubular portion