Double row tapered roller bearing, bearing ring, and method for producing double row tapered roller bearing
10378076 ยท 2019-08-13
Assignee
Inventors
- Michio Hori (Kuwana, JP)
- Hideto Torisawa (Kuwana, JP)
- Hiroshi Yuki (Kuwana, JP)
- Chikara Ohki (Kuwana, JP)
- Kazuhiro Yagita (Kuwana, JP)
Cpc classification
F16C43/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49684
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C19/385
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/585
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2240/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/583
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/386
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2223/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C21D2221/10
CHEMISTRY; METALLURGY
F16C33/605
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/526
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C21D1/18
CHEMISTRY; METALLURGY
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C2360/31
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C43/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A double row tapered roller bearing includes: an outer ring having an annular shape; an inner ring disposed on an inner circumferential side of the outer ring and having an annular shape; and rollers. The inner ring has an outer circumferential surface facing the outer ring and having two rows of grooves having a bottom surface serving as a raceway surface. The rollers are tapered rollers disposed in the grooves in contact with the raceway surface of the inner ring and are also in contact with the outer ring. At outer circumferential surface of the inner ring, a region adjacent to the groove includes a hardened region extending from the inner peripheral surface of the groove to the region adjacent to the groove, and an unhardened region located at a position farther from the groove than the hardened region and being smaller in hardness than the hardened region.
Claims
1. A double row tapered roller bearing comprising: an outer ring serving as a bearing ring having an annular shape; an inner ring disposed on an inner circumferential side of the outer ring and serving as a bearing ring having an annular shape, the inner ring having an outer circumferential surface facing the outer ring and having two rows of grooves having a bottom surface serving as a raceway surface; and tapered rollers disposed in the grooves in contact with the raceway surface of the inner ring and being also in contact with the outer ring, at the outer circumferential surface of the inner ring, a region adjacent to the groove including a hardened region extending from an inner peripheral surface of the groove to the region adjacent to the groove, and an unhardened region located at a position farther from the groove than the hardened region and being smaller in hardness than the hardened region, the region adjacent to the groove being located outside of the groove, and forming a boundary between the hardened region and the unhardended region on the outer circumference surface.
2. The double row tapered roller bearing according to claim 1, wherein an angle that the raceway surface forms with a central axis of the inner ring is 40 or more and 50 or less.
3. A method for producing a bearing ring of a double row tapered roller bearing, comprising the steps of: preparing a formed body constituted of steel and having an outer circumferential surface having an annular groove having a bottom surface to serve as a raceway surface of the bearing ring; induction-heating the formed body to form a heated region including the bottom surface of the groove and heated to a temperature of at least an A.sub.1 point; simultaneously cooling a whole of the heated region to a temperature of not more than an M.sub.s point, in the step of preparing a formed body, the formed body including an excessive portion in which a region adjacent to the groove extends outwardly of a position which becomes an outer circumferential surface of the bearing ring; and removing the excessive portion from the formed body after the step of cooling.
4. The method for producing a bearing ring according to claim 3, wherein the formed body has an annular shape, and in the step of preparing a formed body, the excessive portion of the formed body is annularly arranged so as to sandwich the groove in a direction of a central axis of the formed body.
5. A method for producing a double row tapered roller bearing, comprising the steps of: preparing a bearing ring; preparing tapered rollers; and assembling a double row tapered roller bearing by combining the bearing ring and the rollers, the bearing ring being produced in the method for producing a bearing ring according to claim 4.
6. The method for producing a bearing ring according to claim 4, wherein in the step of preparing a formed body, an angle that the bottom surface of the groove of the formed body forms with the central axis is 40 or more and 50 or less.
7. A method for producing a double row tapered roller bearing, comprising the steps of: preparing a bearing ring; preparing tapered rollers; and assembling a double row tapered roller bearing by combining the bearing ring and the rollers, the bearing ring being produced in the method for producing a bearing ring according to claim 6.
8. A method for producing a double row tapered roller bearing, comprising the steps of: preparing a bearing ring; preparing tapered rollers; and assembling a double row tapered roller bearing by combining the bearing ring and the rollers, the bearing ring being produced in the method for producing a bearing ring according to claim 3.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
DESCRIPTION OF EMBODIMENTS
(11) Embodiments of the present invention are now described with reference to the drawings. In the figures, identical or corresponding components are identically denoted and will not be described redundantly.
(12) <Configuration of Double Row Tapered Roller Bearing>
(13) A structure of a double row tapered roller bearing according to an embodiment will be described with reference to
(14) The double row tapered roller bearing shown in
(15) Inner ring 5 includes two inner ring members 3a and 3b and an inner ring spacer 4. Two inner ring members 3a and 3b each have an annular shape. Inner ring spacer 4 has an annular shape and is disposed between inner ring members 3a and 3b. Inner ring spacer 4 may be dispensed with. Inner ring members 3a and 3b each have an outer circumferential surface 16 facing outer ring 2 and having a groove having a bottom surface serving as a raceway surface. That is, inner ring 5 has two rows of grooves 19. From another point of view, outer circumferential surface 16 means a surface portion of inner ring member 3a, 3b that extends along the central axis of roller 6. Rollers 6 are disposed in groove 19 in contact with the raceway surface of inner ring 5 and are also in contact with outer ring 2. Roller 6 is a tapered roller. At outer circumferential surface 16 of inner ring 5, a region adjacent to groove 19 includes inner ring hardened region 15b extending from the inner peripheral surface of groove 19 to the region adjacent to groove 19, and unhardened region 18 located at a position farther from groove 19 than inner ring hardened region 15b and being smaller in hardness than inner ring hardened region 15b. The region of outer circumferential surface 16 of inner ring 5 that is adjacent to groove 19 as shown in
(16) An angle that the bottom surface of groove 19 serving as the raceway surface forms with central axis 25 of inner ring 5 is at least 40 and not more than 50. Further, angle may be 45.
(17) <Function and Effect of Double Row Tapered Roller Bearing>
(18) In double row tapered roller bearing 1 shown in
(19) In double row tapered roller bearing 1, angle that the bottom surface of groove 19 serving as the raceway surface forms with central axis 25 of inner ring 5 is at least 40 and not more than 50, and double row tapered roller bearing 1 can alone provide a large action point distance. Accordingly, applying double row tapered roller bearing 1 as a bearing for a main shaft of a wind turbine generator allows a bearing portion for the main shaft of the wind power generator to be dimensionally smaller than applying a plurality of cylindrical roller bearings as a bearing for that main shaft does.
(20) <Configuration of Wind Turbine Generator with Double Row Tapered Roller Bearing Applied Thereto>
(21) With reference to
(22) With reference to
(23) A plurality of blades 30 are attached to a rotor head 20 connected to the upper end of main shaft 22. Main shaft 22 is supported inside nacelle 90. The rotation of main shaft 22 is transmitted to power generator 50 via speed up gear 40.
(24) Main shaft 22 enters nacelle 90 from rotor head 20 and is connected to the input shaft of speed up gear 40. Main shaft 22 is rotatably supported by main shaft bearing 60. And main shaft 22 transmits rotation torque that is generated by blade 30 receiving wind power to the input shaft of speed up gear 40. Blade 30 converts wind power into rotation torque, and transmits it to main shaft 22.
(25) Main shaft bearing 60 is disposed in nacelle 90 in a fixed manner and supports main shaft 22 rotatably. Main shaft bearing 60 is constituted by double row tapered roller bearing 1 shown in
(26) Speed up gear 40 is provided between main shaft 22 and power generator 50, accelerates the rotation speed of main shaft 22 and outputs it to power generator 50. As an example, speed up gear 40 is composed of a gear speed-up mechanism including a planetary gear, a countershaft, a high speed shaft, etc. Power generator 50 is connected to an output shaft 61 of speed up gear 40, and generates electric power by the rotation torque received from speed up gear 40. Power generator 50 is an induction generator, for example.
(27) The wind turbine generator is configured to be capable of performing a yaw motion to rotate nacelle 90 in accordance with the wind direction with respect to tower 100 fixed on the ground. Preferably, nacelle 90 is rotated so that the blade 30 side is positioned windward.
(28) Further, wind turbine generator 10 may be configured to obtain appropriate rotation by changing an angle (hereinafter referred to as a pitch) of blade 30 with respect to the wind direction depending on the strength of the wind force. Furthermore, wind turbine generator 10 may be configured to similarly control the blades' pitch when starting and stopping the wind turbine. Further, wind turbine generator 10 may also be configured so that each blade 30 swings by several degrees while main shaft 22 is rotated once. By doing so, an amount of energy that can be obtained from wind can be adjusted. For example, for strong wind, the blades have a wind receiving surface (also referred to as a wing surface) set parallel to the wind direction in order to suppress the rotation of the wind turbine.
(29) <Method for Producing Bearing Ring of Double Row Tapered Roller Bearing, and Double Row Tapered Roller Bearing>
(30) A method for producing a bearing ring of a double row tapered roller bearing and the double row tapered roller bearing will be described with reference to
(31) Referring to
(32) As shown in
(33) Then, a normalizing step is carried out as a step (S20). In this step (S20), the formed body prepared in the step (S10) is heated to a temperature of at least an A.sub.1 transformation point and thereafter cooled to a temperature of less than the A.sub.1 transformation point, whereby normalizing is performed. At this time, a cooling rate in the cooling in the normalizing may simply be a cooling rate at which the steel constituting the formed body does not transform into martensite, i.e., a cooling rate of less than a critical cooling rate. Hardness of the formed body after the normalizing becomes high when this cooling rate increases, and becomes low when the cooling rate decreases. Therefore, desired hardness can be imparted to the formed body by adjusting the cooling rate.
(34) Then, referring to
(35) Then, the formed body is rotated about the central axis, more specifically, in a direction of arrow , while a high-frequency current is supplied to coil 121 from a power source (not shown). Thus, a surface layer region of the formed body including raceway surface 11 is induction-heated to a temperature of at least the A.sub.1 point, and an annular heated region along raceway surface 11 is formed. At the time, the temperature of the surface of raceway surface 11 is measured with a thermometer 122 such as a radiation thermometer, and controlled.
(36) Then, in the step (S40), water as a cooling liquid, for example, is injected toward the whole of the formed body including the heated region formed in the step (S30), whereby the whole of the heated region is simultaneously cooled to a temperature of not more than the M.sub.s point. Thus, the heated region transforms into martensite, and a region including raceway surface 11 hardens. Through the aforementioned procedure, induction quenching is performed, and the quench hardening step is completed.
(37) Then, a tempering step is carried out as a step (S50). In this step (S50), the formed body quench-hardened in the steps (S30) and (S40) is charged into a furnace, for example, heated to a temperature of not more than the A.sub.1 point and retained for a prescribed time, whereby tempering is performed.
(38) Then, a finishing step is carried out as a step (S60). In this step (S60), as shown in
(39) Further, inner ring member 3a has excessive portions 12, 13 removed after a heat treatment to expose inner ring hardened region 15b and unhardened region 18 at a region of outer circumferential surface 16 adjacent to groove 19 (in
(40) Note that when excessive portions 12, 13 (see
(41) Furthermore, an assembling step is carried out as a step (S70). In this step (S70), inner ring member 3a produced as described above and inner ring member 3b and outer ring 2 produced in the same manner as inner ring member 3a are assembled together with rollers 6 (
(42) According to the present embodiment, coil 121 arranged to face part of raceway surface 11 of the formed body is relatively rotated along the circumferential direction of the formed body in the step (S30), whereby the heated region is formed on the formed body. Therefore, it is possible to employ coil 121 small with respect to the outer shape of the formed body, and the production cost for a quenching apparatus can be suppressed even in a case of quench-hardening a large-sized formed body. In the present embodiment, further, the whole of the heated region is simultaneously cooled to a temperature of not more than the M.sub.s point. Therefore, it becomes possible to form inner ring hardened region 15b which is an annular quench-hardened region homogeneous in the circumferential direction, and residual stress is prevented from concentrating on a partial region.
(43) In the step (S30), coil 121 having any shape can be applied in so far as it can heat the formed body by induction heating. For example, an annular coil may be used which covers raceway surface 11 of the formed body entirely.
(44) It should be noted that although the normalizing step performed in step (S20) is not an essential step in the method for producing a bearing ring according to the present invention, carrying out this step allows a formed body of steel to be adjusted in hardness while suppressing quench cracking.
(45) In this step (S20), hard particles may be sprayed to the formed body along with a gas to perform shot blasting while cooling the formed body. Thus, the shot blasting can be performed simultaneously with air-blast cooling at the time of the normalizing, and scales formed on a surface layer portion of the formed body are removed, and reduction of characteristics of inner ring member 3a resulting from formation of the scales, reduction of thermal conductivity resulting from formation of the scales, etc. are suppressed. As the hard particles (a projection material), metal particles made of steel, cast iron etc. can be employed, for example.
(46) <Function and Effect of the Above Production Method>
(47) The method for producing a bearing ring according to the present disclosure as shown in
(48) This allows induction heating to be performed to selectively quench a heated region including a bottom surface of groove 19 to serve as raceway surface 11 of inner ring member 3a constituting a bearing ring, and accordingly, allows the bearing ring to be produced through a process simpler than when performing a carburizing heat treatment accompanied by an anti-carburization treatment and can also reduce a period of time required for the process. This allows the bearing ring to be produced at a reduced cost.
(49) Furthermore, the quenching process performed in a state where excessive portions 12 and 13 are present adjacent to groove 19 to be heated can reduce a possibility of overheating or overcooling and thus quench-cracking an end of the opening of groove 19, that is, a (corner) portion connecting an inner peripheral surface of groove 19 and the outer circumferential surface of inner ring member 3a serving as a bearing ring, as would be in a case without excessive portions 12 and 13. That is, excessive portions 12 and 13 allow uniform heated and cooled states around groove 19 in the step of forming a heated region (S30) and the cooling step (S40). From a different point of view, excessive portions 12 and 13 can suppress uneven quenching resulting from a mass effect around groove 19.
(50) In the method for producing the bearing ring, as described above, the formed body may have an annular shape, as shown in
(51) In the method for producing the bearing ring, as described above, angle (see
(52) A method for producing a double row tapered roller bearing as shown in
(53) While an embodiment of the present invention has been described as above, the embodiment can be variously modified. Further, the present invention is not limited in scope to the above-described embodiment. The scope of the present invention is defined by the terms of the claims, and is intended to include any modifications within the meaning and scope equivalent to the terms of the claims.
INDUSTRIAL APPLICABILITY
(54) The present embodiment is advantageously applicable to a double row tapered roller bearing applied to a wind turbine generator, in particular.
REFERENCE SIGNS LIST
(55) 1: bearing; 20: outer ring; 3a, 3b: inner ring member; 4: inner ring spacer; 5: inner ring; 6: roller; 7: cage; 8: bolt hole; 9: raceway surface; 10: wind turbine generator; 11: raceway surface; 12, 13: excessive portion; 14: dotted line; 15a: outer ring hardened regions; 15b: inner ring hardened regions 15b; 16: outer circumferential surface 17: boundary portion; 18: unhardened region; 19: groove; 20: rotor head; 22: main shaft; 25: central axis; 30: blade; 40: speed up gear; 50: power generator; 60 main shaft bearing; 61: output shaft; 90: nacelle; 100: tower; 121: coil; 122: thermometer.