Double-row self-aligning roller bearing

Abstract

A double-row self-aligning roller bearing has rollers interposed, in two rows aligned in a bearing width direction, between an inner ring and an outer ring. The outer ring has a spherical raceway surface. Each of the rollers has an outer circumferential surface having a cross-sectional shape that matches the raceway surface of the outer ring. The rollers have lengths equal to each other and maximum diameters equal to each other, and have different distances from centers of the roller lengths to positions at which the maximum diameters are obtained.

Claims

1. A double-row self-aligning roller bearing comprising: an inner ring; an outer ring having a spherical raceway surface; and rollers in two rows juxtaposed to each other in a bearing width direction and interposed between the inner ring and the outer ring, each of the rollers in the two rows having an outer circumferential surface having a cross-sectional shape that matches the raceway surface of the outer ring, wherein the rollers in the two rows have lengths equal to each other and maximum diameters equal to each other, and have different distances from centers of the roller lengths to positions at which the maximum diameters are obtained.

2. The double-row self-aligning roller bearing as claimed in claim 1, wherein, in the rollers in either row of the rollers in the two rows, the position at which the maximum diameter is obtained is shifted to an inner side in the bearing width direction with respect to the center of the roller length.

3. The double-row self-aligning roller bearing as claimed in claim 1, wherein, of the rollers in the two rows, the rollers having the longer distance from the center of the roller length to the position at which the maximum diameter is obtained have a larger contact angle than the rollers having the shorter distance.

4. The double-row self-aligning roller bearing as claimed in claim 1, wherein the double-row self-aligning roller bearing is used for supporting a main shaft of a wind power generator.

5. The double-row self-aligning roller bearing as claimed in claim 1, further comprising retainers configured to retain the rollers in the respective rows, wherein each retainer includes an annular portion that has an annular shape and is configured to guide axially inner end faces of the rollers in the row, and a plurality of pillar portions that extend in an axial direction from the annular portion and that are provided at predetermined intervals along a circumferential direction, pockets configured to retain the rollers are provided between those pillar portions, and one of the retainers configured to retain the rollers having the longer distance from the center of the roller length to the position at which the maximum diameter is obtained has an inclination angle by which a radially outer surface of each pillar portion is inclined radially inward from a proximal end side toward a distal end side.

6. The double-row self-aligning roller bearing as claimed in claim 1, wherein each of the rollers has a DLC coating on a roller rolling surface thereof.

7. The double-row self-aligning roller bearing as claimed in claim 1, wherein each of the rollers has a crowning at an end portion of a roller rolling surface thereof.

8. The double-row self-aligning roller bearing as claimed in claim 1, wherein the inner ring includes an intermediate flange that is provided on an outer circumferential surface of the inner ring between the rollers in the two rows and configured to guide the rollers in the two rows, and small flanges that are provided at opposite ends of the outer circumferential surface, respectively, and that face axially outer end faces of the rollers in the respective rows, and one small flange of the respective small flanges of the inner ring, that faces the axially outer end faces of the rollers having the longer distance from the center of the roller length to the position at which the maximum diameter is obtained has an insertion slot for inserting the rollers into the bearing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In any event, the present invention will become more clearly understood from the following description of preferred embodiments thereof, when taken in conjunction with the accompanying drawings. However, the embodiments and the drawings are given only for the purpose of illustration and explanation, and are not to be taken as limiting the scope of the present invention in any way whatsoever, which scope is to be determined by the appended claims. In the accompanying drawings, like reference numerals are used to denote like parts throughout the several views, and:

(2) FIG. 1 is a cross-sectional view of a double-row self-aligning roller bearing according to a first embodiment of the present invention;

(3) FIG. 2 is an explanatory diagram exaggeratedly representing the shapes of rollers of the double-row self-aligning roller bearing;

(4) FIG. 3 is an explanatory diagram exaggeratedly representing the cross-sectional shape of the rolling surface of the roller of the double-row self-aligning roller bearing;

(5) FIG. 4 is a cross-sectional view of a double-row self-aligning roller bearing according to a second embodiment of the present invention;

(6) FIG. 5 is an enlarged cross-sectional view showing crownings, etc., of a roller of a double-row self-aligning roller bearing according to a third embodiment of the present invention;

(7) FIG. 6 is a diagram showing a relationship between a straight length and a PV value of the roller;

(8) FIG. 7 is a diagram showing a relationship between the straight length of the roller and bearing life;

(9) FIG. 8 is an enlarged cross-sectional view of a DLC coating of a roller, etc., of a double-row self-aligning roller bearing according to a fourth embodiment of the present invention;

(10) FIG. 9 is an enlarged cross-sectional view showing an insertion slot of an inner ring, etc., of a double-row self-aligning roller bearing according to a fifth embodiment of the present invention;

(11) FIG. 10 is an end view of the insertion slot of the inner ring, etc., as seen from an axial direction;

(12) FIG. 11 is a cross-sectional view of a double-row self-aligning roller bearing according to a sixth embodiment of the present invention;

(13) FIG. 12 is a partially cutaway perspective view of an example of a main shaft supporting device of a wind power generator;

(14) FIG. 13 is a cutaway side view of the main shaft supporting device;

(15) FIG. 14 is a cross-sectional view of a conventional general double-row self-aligning roller bearing;

(16) FIG. 15 is a cross-sectional view of a double-row self-aligning roller bearing of a first proposed example; and

(17) FIG. 16 is a cross-sectional view of a double-row self-aligning roller bearing of a second proposed example.

DESCRIPTION OF EMBODIMENTS

(18) A first embodiment of the present invention will be described with reference to FIG. 1.

(19) In a double-row self-aligning roller bearing 1, rollers 4 and 5 in left and right two rows juxtaposed to each other in a bearing width direction are interposed between an inner ring 2 and an outer ring 3. The outer ring 3 has a spherical raceway surface 3a, and the rollers 4 and 5 in the left and right rows each have an outer circumferential surface having a cross-sectional shape that matches the raceway surface 3a of the outer ring 3. In other words, the outer circumferential surfaces of the rollers 4 and 5 are rotation curved surfaces obtained by rotating, about center lines C1 and C2, a circular arc extending along the raceway surface 3a of the outer ring 3. On the inner ring 2, raceway surfaces 2a and 2b in double rows having cross-sectional shapes along the outer circumferential surfaces of the rollers 4 and 5 in the respective left and right rows are formed. Flanges (small flanges) 6 and 7 are provided at opposite ends of the outer circumferential surface of the inner ring 2, respectively. An intermediate flange 8 is provided on a center portion of the outer circumferential surface of the inner ring 2, that is, between the rollers 4 in the left row and the rollers 5 in the right row. The rollers 4 and 5 in the respective left and right rows are retained by retainers 11 and 12, respectively.

(20) The retainer 11 for the left row includes: an annular portion 11a that has an annular shape and guides the axially inner end faces of the rollers 4 in the left row; and a plurality of pillar portions 11b that extend in the axial direction from the annular portion 11a and are provided at predetermined intervals along the circumferential direction. Pockets Pt for retaining the rollers 4 are provided between those pillar portions. The retainer 12 for the right row includes: an annular portion 12a that has an annular shape and guides the axially inner end faces of the rollers 5 in the right row; and a plurality of pillar portions 12b that extend in the axial direction from the annular portion 12a and are provided at predetermined intervals along the circumferential direction. Pockets Pt for retaining the rollers 5 are provided between those pillar portions.

(21) The rollers 4 in the left row and the rollers 5 in the right row have lengths L1 and L2, along the center lines C1 and C2, equal to each other, and also have maximum diameters D1max and D2max equal to each other. However, both the rollers 4 and 5 in the respective left and right rows are asymmetrical rollers. The asymmetrical rollers are rollers having asymmetrical shapes in which positions A1 and A2 at which the maximum diameters D1max and D2max are obtained are shifted from centers B1 and B2 of the roller lengths as exaggeratedly shown in FIG. 2. In the case of this embodiment, the position A1 at which the maximum diameter D1max of the rollers 4 in the left row is obtained is at the right side, that is, at the inner side in the bearing width direction, with respect to the center B1 of the roller length, and the position A2 at which the maximum diameter D2max of the rollers 5 in the right row is obtained is at the left side, that is, at the inner side in the bearing width direction, with respect to the center B2 of the roller length.

(22) Since the rollers 4 and 5 are the asymmetrical rollers as described above, the contact angles 1 and 2 can be changed without changing the positions or the lengths of the rollers 4 and 5, in contrast to symmetrical rollers (not shown) in each of which the position at which the maximum diameter is obtained is at the center of the roller length. By adjusting distances K1 and K2 from the centers B1 and B2 of the roller lengths to the positions A1 and A2 at which the maximum diameters D1max and D2max are obtained, optimum contact angles 1 and 2 can be set.

(23) When the positions A1 and A2 at which the maximum diameters D1max and D2max of the rollers 4 and 5 in the respective left and right rows are obtained are located at the inner side in the bearing width direction with respect to the centers B1 and B2 of the roller lengths as in this embodiment, the contact angles 1 and 2 are smaller than those in the case where each roller is a symmetrical roller. By shifting the positions A1 and A2, at which the maximum diameters of the rollers 4 and 5 in the respective rows are obtained, to the inner side in the bearing width direction with respect to the centers B1 and B2 of the roller lengths, a load toward the intermediate flange 8 is generated when a load is applied to the rollers 4 and 5. Thus, the end faces of the rollers 4 and 5 are assuredly guided by the intermediate flange 8, and the rollers 4 and 5 can stably rotate.

(24) Moreover, in this embodiment, the contact angle 2 of the rollers 5 having the distance K2 that is larger when the distances K1 and K2 from the centers B1 and 132 of the roller lengths to the positions A1 and A2 at which the maximum diameters are obtained are compared to each other, is set so as to be larger than the contact angle 1 of the rollers 4 having the smaller distance K1. Thus, when a load is applied to the respective rollers 4 and 5, a greater load toward the intermediate flange 8 is generated at the rollers 5 having the larger contact angle 2, than at the rollers 4 having the smaller contact angle 1. A roller having a larger contact angle tends to unstably rotate. However, by causing a greater load to be generated toward the intermediate flange 8 as described above, rotation of the rollers 5 having the larger contact angle 2 can be stabilized.

(25) In FIG. 1, lines of action S1 and S2 which define the contact angles 1 and 2 of the rollers 4 and 5 in the respective rows intersect each other at a point P on a bearing central axis O. Thus, it is possible for the inner ring 2 and the rollers 4 and 5 to make an aligning operation along the raceway surface 3a of the outer ring 3. The position in the bearing width direction of the point P is shifted to the side at which the rollers 4 having a smaller contact angle 1 are present, with respect to a center position Q in the bearing width direction of the intermediate flange 8. The lines of action S1, S2 are defined as lines along which a resultant force of forces acting on contact portions between the rollers 4, 5 and the inner and outer rings 2, 3 acts.

(26) As shown in FIG. 3, crownings may be provided on the rolling surfaces 13 of either of the rollers 4 or 5 in the left or right rows or the rolling surfaces 13 of both rollers 4 and 5. By providing the crownings, the radii of curvature of both end portions 13b and 13c of each rolling surface 13 are made smaller than that of a center portion 13a of the rolling surface 13. The shape of each crowning is, for example, a logarithmic curve. The shape of each crowning may be a straight line, a single circular arc, or a shape obtained by combining a plurality of circular arcs, other than the logarithmic curve. By providing crownings at opposite ends of the rolling surfaces 13 of the rollers 4 and 5 as described above, surface pressures on both end portions 13b and 13c of the rolling surfaces 13 of the rollers 4 and 5 at which a sliding velocity is high are decreased, and the absolute value of a PV value (surface pressuresliding velocity) is reduced, so that friction can be reduced. In particular, crownings are preferably provided to the rollers 5 in the right row in FIG. 1 which receives an axial load.

(27) The double-row self-aligning roller bearing 1 having this configuration is used in a usage in which an axial load and a radial load are received and loads having magnitudes different from each other act on left and right roller rows, for example, as a bearing for supporting a main shaft of a wind power generator. In this case, the double-row self-aligning roller bearing 1 is mounted such that the rollers 4 in the left row are located at the side closer to revolving blades (the front side) and the rollers 5 in the right row are located at the side farther from the revolving blades (the rear side). Thus, the rollers 5 in the right row having the larger contact angle 2 bear substantially the entirety of an axial load and part of a radial load, and the rollers 4 in the left row having the smaller contact angle 1 bear the rest of the radial load.

(28) By appropriately setting the contact angles 1 and 2 of the rollers 4 and 5, the load can be shared at a ratio corresponding to the load capacities of the rollers 4 and 5 in the respective left and right rows. As a result, the surface pressures on the rollers 4 and 5 in the respective left and right rows become equal to each other. Accordingly, a high load capacity can be ensured in the entire bearing, and the substantial life of the entire bearing can also be improved. Since the rollers 4 and 5 are the asymmetrical rollers, optimum contact angles 1 and 2 can be easily set without changing the positions or the lengths of the rollers 4 and 5.

(29) Other embodiments will be described.

(30) In the following description, in each embodiment, portions corresponding to the matters described in the previously described embodiments are designated by the same reference numerals, and the redundant description thereof is omitted. When only a part of a configuration is described, the remaining part of the configuration is the same as that of the previously described embodiment unless otherwise specified. The same advantageous effects are achieved by the same configuration. In addition to the combinations of portions described specifically in each embodiment, it is also possible to partially combine the embodiments unless any problem is particularly posed due to the combination.

Retainer 12A with Inclination Angle

(31) A double-row self-aligning roller bearing according to a second embodiment will be described with reference to FIG. 4.

(32) The double-row self-aligning roller bearing 1 includes a retainer 12A with an inclination angle. The retainer 12A for the right row shown in FIG. 4 is a retainer for retaining the rollers 5 having the larger distance K2 from the center B2 of the roller length to the position A2 at which the maximum diameter is obtained. The retainer 12A has an inclination angle at which a radially outer surface 12D of each pillar portion 12Ab is inclined radially inward from a proximal end side toward a distal end side. The inclination angle is an angle relative to the bearing central axis O. The inclination angle of the retainer 12A is set within a range of greater than zero and not greater than a maximum diameter angle 2 of the rollers 5 having the larger distance K2 (0<2). The maximum diameter angle 2 is an inclination angle, relative to a plane perpendicular to the bearing central axis O, at the position A2 at which the maximum diameter D2max of the rollers 5 in the right row is obtained.

(33) The radially inner surface of each pillar portion 12Ab in the retainer 12A for the right row in this example has an inclined surface portion 12da and a flat surface portion 12db connected to the inclined surface portion 12da. The inclined surface portion 12da extends from the proximal end side of the radially inner surface of the pillar portion 12Ab to a position near the middle in the axial direction of the radially inner surface, and has an inclination angle at Which the inclined surface portion 35Ab is inclined radially inward from the proximal end side to the position near the middle in the axial direction. The inclination angle is also an angle relative to the bearing central axis O, and is set so as to be not less than the inclination angle (). In this example, the inclination angle is set so as to be greater than the inclination angle by several degrees. However, the relationship between these inclination angles is not limited to this relationship (). The flat surface portion 12db is a flat surface that extends in the axial direction from the distal edge of the inclined surface portion 12da and is parallel to the bearing central axis O. In the retainer 11 for the left row, the radially outer surfaces and the radially inner surfaces of the pillar portions 11b do not have any inclination angle, that is, are parallel to the bearing central axis O.

(34) Since the retainer 12A for the right row has the above-described inclination angle , the pocket surfaces of the retainer 12A can hold the maximum diameter positions of the rollers 5. Thus, the attitude stability of the rollers 5 in the right row is not deteriorated, and it is also possible to easily fit the rollers 5.

Crowning Cw

(35) In a double-row self-aligning roller bearing according to a third embodiment, as shown in FIG. 5, the rollers 4 and 5 in the respective left and right rows may each have crownings Cw at the end portions 13b and 13c of the roller rolling surface 13 thereof. As each crowning Cw in this example, a complex R crowning that increases a drop amount by making the end portion 13b or 13c of the roller rolling surface 13 smaller than a reference R of the roller rolling surface 13 is used. A length Ls of a roller center portion 13a at which no crowning Cw is provided (hereinafter, referred to as straight length) may be 50% to 70% and preferably 60% of a roller overall length L1 (L2).

(36) FIG. 6 is a diagram showing a relationship between a straight length and a PV value (surface pressuresliding velocity) when an average wind load is applied to a double-row self-aligning roller bearing for supporting a windmill main shaft. FIG. 7 is a diagram showing a relationship between the straight length and bearing life. From FIG. 6, it is understood that the shorter the straight length is, the lower the PV value is. From FIG. 7, it is understood that, when the straight length is less than 60% of the roller overall length, the life reduction rate exceeds 5% as compared to the case where no crowning is provided (straight length=100%). Therefore, the straight length is preferably 60% of the roller overall length.

(37) In the case where the rollers 4 and 5 in the respective rows have such crownings Cw (FIG. 5), edge stress can be relaxed. Instead of the complex R crowning, a logarithmic crowning in which the end portion 13b or 13c of the roller rolling surface 13 is represented by a logarithmic curve may be used.

DLC Coating

(38) In a double-row self-aligning roller bearing according to a fourth embodiment, as shown in FIG. 8, the rollers 4 and 5 in the respective rows may each have a DLC coating 14 on the roller rolling surface 13 thereof. In the DLC coating 14 in this example, a multi-layer structure having high adhesion to the roller 4 or 5, which is a base, is used. The DLC coating 14 has a surface layer 16, an intermediate layer 17, and a stress relaxation layer 18. The surface layer 16 is a film in which only graphite that is a solid target is used as a carbon supply source and which is mainly formed of DLC in which an amount of hydrogen mixed is reduced. The intermediate layer 17 is a layer that is formed between the surface layer 16 and the base and is mainly formed of at least Cr or W. The stress relaxation layer 18 is formed between the intermediate layer 17 and the surface layer 16.

(39) The intermediate layer 17 has a structure including a plurality of layers having different compositions, and a three-layer structure of 17a to 17c is shown in FIG. 8. For example, a layer 17c mainly formed of Cr is formed on the surface of the base, a layer 17b mainly formed of W is formed on the layer 17c, and a layer 17a mainly formed of W and C is formed on the layer 17b. In FIG. 8, the three-layer structure is shown, but, as necessary, the intermediate layer 17 may include layers whose number is less than or greater than three.

(40) By the layer 17a adjacent to the stress relaxation layer 18 being mainly formed of carbon and a metal that is the metal of which the layer 17b adjacent to the layer 17a at the other side is mainly composed, the adhesion between the intermediate layer 17 and the stress relaxation layer 18 can be improved. For example, in the case where the layer 17a is mainly formed of W and C, further improvement of the adhesion can be achieved by decreasing the contained amount of W and increasing the contained amount of C from the side at which the intermediate layer 17b mainly formed of W is present, toward the side at which the stress relaxation layer 18 mainly formed of C is present (composition gradient).

(41) The stress relaxation layer 18 is a gradient layer that is mainly formed of C and in which the hardness thereof increases in a continuous or stepwise manner from the intermediate layer 17 side to the surface layer 16 side. Specifically, the stress relaxation layer 18 is a DLC gradient layer that is obtained by using a graphite target in a DBMS method and forming a film while increasing a bias voltage to the base in a continuous or stepwise manner. The reason why the hardness increases in a continuous or stepwise manner is that the distribution ratio of a graphite structure (SP2) and a diamond structure (SP3) in a DLC structure becomes biased due to the increase of the bias voltage such that the latter is increased.

(42) The surface layer 16 is a film that is formed by extension of the stress relaxation layer 18 and mainly formed of DLC, particularly, a DLC film in which a contained amount of hydrogen in the structure thereof is reduced. Since the contained amount of hydrogen is reduced, the wear resistance is improved. To form such a DLC film, a method, in which, for example, a UBMS method is used and a raw material to be used in sputtering, hydrogen, and a compound containing hydrogen are not mixed in sputtering gas, is used.

(43) Regarding the film forming method for the stress relaxation layer 18 and the surface layer 16, the case of using the DBMS method has been described, but any other publicly known film forming method can be adopted as long as it is a film forming method that allows the hardness to be changed in a continuous or stepwise manner. The sum of the film thicknesses of the multiple layers including the intermediate layer 17, the stress relaxation layer 18, and the surface layer 16 is preferably 0.5 m to 3.0 m. If the sum of the film thicknesses is less than 0.5 m, the wear resistance and the mechanical strength are poor, and if the sum of the film thicknesses exceeds 3.0 m, these layers are easily peeled off. Thus, such cases are not preferable.

(44) In this example, the DLC coating 14 is provided only on the outer circumferential surface of each of the rollers 4 and 5, but a DLC coating 14 may be further provided on each end face of each of the rollers 4 and 5. In particular, in the case where a DLC coating 14 is provided on one end face of each of the rollers 4 and 5 guided by the intermediate flange 8 (FIG. 4), the one end face of each of the rollers 4 and 5 is hardly worn, so that the wear resistance of the rollers 4 and 5 can be further enhanced.

Insertion Slot 15

(45) In a double-row self-aligning roller bearing according to a fifth embodiment, as shown in FIG. 9, of the respective small flanges 6 and 7 (FIG. 4) of the inner ring 2, the small flange 7 that faces the axially outer end faces of the rollers 5 having the longer distance K2 from the center B2 of the roller length to the position A2 at which the maximum diameter is obtained may have an insertion slot 15 for inserting the rollers 5 into the bearing. As shown in FIG. 10, an insertion slot 15 having a circular arc shape is provided at one location in the circumferential direction on the small flange 7 of the inner ring 2. The radius of curvature of a circular arc 15a of the insertion slot 15 is set as appropriate in accordance with the maximum diameter of the rollers 5 (FIG. 9) to be inserted. In the case where such an insertion slot 15 is provided to the inner ring 2, fittability of the rollers 5 in the right row into the bearing can be further improved.

(46) In the double-row self-aligning roller bearing according to the sixth embodiment, as shown in FIG. 11, the inclination angle of the radially outer surface 12D of each pillar portion 12Ab in the retainer 12A for the right row may be set within a range of greater than zero and not greater than the maximum diameter angle 2 of the rollers 5 in the right row, and the inclination angle of the radially inner surface 12d of each pillar portion 12Ab may be set so as to be equal to the inclination angle of the radially outer surface. The inclination angle in this example is set to an angle that is not greater than the maximum diameter angle 2 and substantially close to the maximum diameter angle 2. In addition, the radially inner surface of the pillar portion 12Ab is formed of only an inclined surface portion, and the above-described flat surface portion is not provided therein.

(47) According to the configuration in FIG. 11, since the retainer 12A has the above-described inclination angle , the pocket Pt surfaces of the retainer 12A are more assuredly maintained around the position of the pitch circle diameter of the rollers 5, so that the pocket Pt surfaces of the retainer 12A can smoothly and assuredly hold the maximum diameter positions of the rollers 5 during operation of the bearing. In addition, fitting of the longer rollers 5 in the right row can also be performed more easily.

(48) FIG. 12 and FIG. 13 show an example of a main shaft supporting device of a wind power generator. A casing 23a of a nacelle 23 is provided on a support stand 21 via a slewing ring bearing 22 (FIG. 13) so as to be horizontally slewable. A main shaft 26 is rotatably provided within the casing 23a of the nacelle 23 via main shaft supporting bearings 25 provided in bearing housings 24. Blades 27 as a swirler are mounted on a portion of the main shaft 26 that projects outside the casing 23a. The other end of the main shaft 26 is connected to a speed increaser 28, and an output shaft of the speed increaser 28 is connected to a rotor shaft of a generator 29. The nacelle 23 is slowed at an arbitrary angle via a speed reducer 31 by a slewing motor 30.

(49) There are two main shaft supporting bearings 25 that are aligned in the illustrated example, but the number of main shaft supporting bearings 25 may be one. The double-row self-aligning roller bearing 1 of any of the embodiments described above is used as each main shaft supporting bearing 25. In this case, both a radial load and an axial load act on the row farther from the blades 27, and thus the rollers 5 having the larger contact angle 2 are used as the rollers in the row farther from the blades 27. Only the radial load mainly acts on the row closer to the blades 27, and thus the rollers 4 having the smaller contact angle 1 are used as the rollers in the row closer to the blades 27.

(50) The present invention is not limited to the above-described embodiments, and various additions, changes, or deletions can be made without departing from the gist of the present invention. Therefore, these are construed as included within the scope of the present invention.

REFERENCE NUMERALS

(51) 1 . . . Double-row self-aligning roller bearing 2 . . . Inner ring 3 . . . Outer ring 3a . . . Raceway surface 4, 5 . . . Roller 6, 7 . . . Small flange 8 . . . Intermediate flange 11, 12, 12A . . . Retainer 11a, 12a . . . Annular portion 11b, 12b, 12Ab . . . Pillar portion 13 . . . Roller rolling surface 14 . . . DLC coating 15 . . . Insertion slot 26 . . . Main shaft A1, A2 . . . Position at which maximum diameter of roller is obtained B1, B2 . . . Center of roller length Cw . . . Crowning D1max, D2max . . . Maximum diameter of roller K1, K2 . . . Distance from center of roller length to position at which maximum diameter of roller is obtained L1, L2 . . . Roller length 1, 2 . . . Contact angle