WO2017199941A1 - Traction speed reducer and electric motor–equipped speed reducer - Google Patents

Traction speed reducer and electric motor–equipped speed reducer Download PDF

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Publication number
WO2017199941A1
WO2017199941A1 PCT/JP2017/018327 JP2017018327W WO2017199941A1 WO 2017199941 A1 WO2017199941 A1 WO 2017199941A1 JP 2017018327 W JP2017018327 W JP 2017018327W WO 2017199941 A1 WO2017199941 A1 WO 2017199941A1
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WO
WIPO (PCT)
Prior art keywords
carrier
axial direction
traction
contact
internal ring
Prior art date
Application number
PCT/JP2017/018327
Other languages
French (fr)
Japanese (ja)
Inventor
正 今村
Original Assignee
日本電産シンポ株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP2016149242A external-priority patent/JP2017207193A/en
Application filed by 日本電産シンポ株式会社 filed Critical 日本電産シンポ株式会社
Priority to CN201780029857.8A priority Critical patent/CN109154367A/en
Publication of WO2017199941A1 publication Critical patent/WO2017199941A1/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H13/00Gearing for conveying rotary motion with constant gear ratio by friction between rotary members
    • F16H13/06Gearing for conveying rotary motion with constant gear ratio by friction between rotary members with members having orbital motion
    • F16H13/08Gearing for conveying rotary motion with constant gear ratio by friction between rotary members with members having orbital motion with balls or with rollers acting in a similar manner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H13/00Gearing for conveying rotary motion with constant gear ratio by friction between rotary members
    • F16H13/10Means for influencing the pressure between the members
    • F16H13/14Means for influencing the pressure between the members for automatically varying the pressure mechanically
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/10Structural association with clutches, brakes, gears, pulleys or mechanical starters

Definitions

  • the present invention relates to a traction speed reducer and a speed reducer with an electric motor.
  • a traction reducer that uses the traction (friction) generated between the sun roller and the planetary roller to reduce the rotational speed of the input shaft and rotate the output shaft.
  • a traction reducer is described in, for example, Japanese Patent Application Laid-Open No. 2009-138924.
  • the traction power transmission device described in the document includes a sun roller that is rotatable around a first central axis, and a plurality of second central axes that are arranged on a plurality of peripheral axes that are parallel to the first central axis.
  • the planetary roller is pressed against the circumferential surface of the sun roller by guiding the shaft member so as to be movable in the radial direction of the sun roller, and power transmission by traction is enabled between the sun roller and the planetary roller.
  • a pressing member is pressed against the circumferential surface of the sun roller by guiding the shaft member so as to be movable in the radial direction of the sun roller, and power transmission by traction is enabled between the sun roller and the planetary roller.
  • An object of the present invention is to provide a technology capable of reducing the number of parts and reducing the size of a traction reducer in a traction reducer.
  • An exemplary first invention of the present application is a traction speed reducer, which is a sun roller that rotates about a rotation axis, a plurality of planetary rollers arranged around the sun roller, and a contact with the plurality of planetary rollers.
  • a pair of annular internal rings and a carrier that rotates around the rotation axis while holding the planetary roller, and the plurality of planetary rollers are respectively the sun roller and the internal ring.
  • the carrier revolves around the rotation axis while rotating by receiving power from the sun roller while being in contact with both the carrier, the carrier has a contact surface facing the outer peripheral surface of the planetary roller, and the planet The outer peripheral surface of the roller and the contact surface are in contact with each other in the circumferential direction around the rotation axis.
  • a carrier pin that supports each planetary roller so as to rotate is not necessary. For this reason, the number of parts can be reduced and the traction speed reducer can be miniaturized.
  • FIG. 1 is a perspective view of a reduction gear with an electric motor according to the first embodiment.
  • FIG. 2 is a longitudinal sectional view of the reduction gear with an electric motor according to the first embodiment.
  • FIG. 3 is a cross-sectional view of the traction reducer according to the first embodiment.
  • FIG. 4 is a cross-sectional view of the traction reducer according to the first embodiment.
  • FIG. 5 is a cross-sectional view of the traction reducer according to the first embodiment.
  • FIG. 6 is a longitudinal sectional view of a reduction gear with an electric motor according to the second embodiment.
  • FIG. 7 is a cross-sectional view of the traction reducer according to the second embodiment.
  • FIG. 8 is a cross-sectional view of a traction reducer according to the second embodiment.
  • FIG. 9 is a partial longitudinal sectional view of a reduction gear with an electric motor according to the third embodiment.
  • the direction parallel to the rotation axis of the sun roller is “axial direction”
  • the direction orthogonal to the rotation axis is “radial direction”
  • the direction along the arc centered on the rotation axis is “circumferential direction”.
  • the above “parallel direction” includes a substantially parallel direction.
  • the above-mentioned “orthogonal direction” includes a substantially orthogonal direction.
  • the right side in FIG. 1 is referred to as “input side” and the left side in FIG. 1 is referred to as “output side”.
  • FIG. 1 is a perspective view of a reduction gear 10 with an electric motor including a traction reduction gear 1 according to the present embodiment.
  • FIG. 2 is a longitudinal sectional view of the reduction gear 10 with an electric motor including the traction reduction gear 1 according to the present embodiment.
  • the motor-equipped speed reducer 10 is a speed reducer that rotates the output shaft 90 by converting the rotational motion of the first rotational speed obtained from the motor 11 into the rotational motion of the second rotational speed lower than the first rotational speed. is there.
  • the traction reduction gear 1 and the reduction gear 10 with an electric motor of the present invention are used, for example, for precision parts of electrical appliances.
  • the speed reducer 10 with an electric motor includes a motor 11, a mounting plate 12, and a traction speed reducer 1.
  • the motor 11 is an electric motor that is a power source of the reduction gear 10 with an electric motor.
  • the motor 11 is connected to the sun roller 20 of the traction speed reducer 1 described later. When the motor 11 is driven, the sun roller 20 rotates around the rotation shaft 9.
  • the mounting plate 12 is a plate-like member for mounting the traction speed reducer 1 to the motor 11.
  • the mounting plate 12 is disposed substantially perpendicular to the rotation shaft 9.
  • the mounting plate 12 is fixed to a motor casing that is an outer frame of the motor 11.
  • the motor casing and the mounting plate 12 are fixed by a fixing tool such as a screw.
  • the motor casing and the mounting plate 12 may be fixed by other methods.
  • the traction speed reducer 1 is a device that decelerates the rotational motion of the motor 11 and transmits it to the output shaft 90.
  • the traction speed reducer 1 is a so-called traction type planetary that transmits power by rotating the outer circumferential surface of the sun roller 20 and the outer circumferential surfaces of the plurality of planetary rollers 30 in contact with each other without using gears. A reduction mechanism is used.
  • the traction speed reducer 1 includes one sun roller 20, a plurality of planetary rollers 30, an internal ring 40, a carrier 50, a carrier bearing 60, an elastic member 70, a housing 80, and an output shaft. 90.
  • the sun roller 20 is a columnar member arranged coaxially with the rotary shaft 9.
  • the sun roller 20 is connected to the motor 11 located on the input side in the axial direction.
  • the sun roller 20 rotates at the first rotation speed around the rotation shaft 9 by the power received from the motor 11.
  • the output shaft of the motor 11 is the sun roller 20.
  • a sun roller that rotates together with the output shaft may be provided separately from the output shaft of the motor 11.
  • FIG. 3 is a cross-sectional view of the traction reducer 1 taken along the line AA in FIG.
  • the plurality of planetary rollers 30 are arranged around the sun roller 20. As shown in FIG. 3, in the present embodiment, three planetary rollers 30 are arranged around the sun roller 20 at equal intervals in the circumferential direction.
  • Each of the plurality of planetary rollers 30 includes a disk portion 31 and a pair of shaft portions 32.
  • the disc portion 31 is arranged around the sun roller 20 so that a straight line connecting the center viewed from the axial input side and the center viewed from the axial output side is parallel to the rotation shaft 9. Is done.
  • the outer peripheral portion of the disc portion 31 is in contact with the outer peripheral portion of the sun roller 20.
  • the pair of shaft portions 32 extend in parallel with the rotation shaft 9 from the center of the disc portion 31 to the input side and output side in the axial direction.
  • the disc part 31 and a pair of axial part 32 are comprised by one member.
  • Each shaft portion 32 has an annular inclined surface 33 at the end opposite to the axial disk portion 31.
  • the inclined surface 33 is inclined with respect to the axial direction so as to decrease in diameter toward the tip of the shaft portion 32.
  • the disk portion 31 only needs to have a circular outer periphery when viewed from the axial direction, and the surface shape may be other than a plate shape.
  • the internal ring 40 is a pair of annular members that contact the plurality of planetary rollers 30.
  • the internal ring 40 according to this embodiment includes a fixed internal ring 41 and a movable internal ring 42.
  • the fixed internal ring 41 of the present embodiment is positioned on the input side in the axial direction with respect to the disc portion 31, and the position in the axial direction is fixed.
  • the movable internal ring 42 is positioned on the output side in the axial direction with respect to the disc portion 31 and is movable in the axial direction.
  • the movable internal ring 42 may be disposed on the input side in the axial direction with respect to the disc portion 31, and the fixed internal ring 41 may be disposed on the output side in the axial direction with respect to the disc portion 31.
  • FIG. 4 is a cross-sectional view of the traction reducer 1 taken along the line BB in FIG.
  • the plurality of planetary rollers 30 are rotatably supported around the sun roller 20 by the sun roller 20 and the internal ring 40. As shown in FIG. 4, the outer peripheral portions of the plurality of planetary rollers 30 are in contact with the inner peripheral portion of the internal ring 40.
  • the sun roller 20 rotates about the rotation shaft 9
  • the plurality of planetary rollers 30 receives power from the sun roller 20.
  • the plurality of planetary rollers 30 revolve around the rotating shaft 9 while rotating around the sun roller 20.
  • the internal ring 40 of the present embodiment is in contact with the inclined surface 33 of the shaft portion 32. Thereby, the internal ring 40 and the planetary roller 30 can be contacted, suppressing the radial width. Further, since the disk portion 31 and the shaft portion 32 of the planetary roller 30 are the same member, the internal ring 40 is not provided with a separate contact member between the internal ring 40 and the planetary roller 30. Can be transmitted directly to the planetary roller 30. As a result, the number of parts of the traction reduction gear 1 can be reduced.
  • FIG. 5 is a cross-sectional view taken along the line CC of FIG.
  • the carrier 50 rotates around the rotation shaft 9 while holding the plurality of planetary rollers 30.
  • the carrier 50 has a contact surface 54 that faces the outer peripheral surface of the shaft portion 32 of the planetary roller 30.
  • the contact surface 54 and at least a part of the outer peripheral surface of the shaft portion 32 are in contact with each other in the circumferential direction around the rotation shaft 9. Accordingly, each planetary roller 30 is supported around the sun roller 20 so as to be capable of rotating.
  • the shaft portion 32 that is a part of the planetary roller 30 is supported by the carrier 50. For this reason, it is not necessary to separately provide a member such as a carrier pin. As a result, the number of parts can be reduced and the traction speed reducer 1 can be downsized.
  • the carrier 50 of the present embodiment has a plurality of accommodating portions 56.
  • the plurality of accommodating portions 56 are arranged in the circumferential direction around the rotation shaft 9, and each of the accommodating portions 56 is open radially outward.
  • the shaft portions 32 of the plurality of planetary rollers 30 are accommodated in the accommodating portion 56.
  • the planetary roller 30 can be inserted into the accommodating portion 56 of the carrier 50 from the outside in the radial direction when the traction reduction gear 1 is manufactured. Thereby, the assembly of the traction reduction gear 1 becomes easy.
  • the carrier 50 of this embodiment is comprised with a single member. For this reason, the number of parts can be reduced as compared with the case where the carrier 50 is constituted by a plurality of members. Thereby, the traction reduction gear 1 can be further reduced in size. Moreover, the assembly of the traction speed reducer 1 becomes easier.
  • the carrier bearing 60 supports the carrier 50 so as to be rotatable about the rotary shaft 9. As shown in FIG. 2, the carrier bearing 60 of the present embodiment contacts at least a part of the outer peripheral surface of the carrier 50. Further, the carrier bearing 60 is in contact with the end face on the output side in the axial direction of the carrier 50. Thereby, the movement of the radial direction and the axial direction is regulated and the carrier 50 is stably held.
  • the elastic member 70 is a member that pressurizes the movable internal ring 42 toward the input side in the axial direction.
  • the elastic member 70 is an annular member that expands and contracts in the axial direction.
  • a wave spring is used for the elastic member 70.
  • the elastic member 70 is disposed between the carrier bearing 60 and the movable internal ring 42 in a state compressed in the axial direction rather than the natural length. For this reason, the movable internal ring 42 is pressurized to the input side by the repulsive force of the elastic member 70.
  • the fixed internal ring 41 and the movable internal ring 42 are in contact with the inclined surface 33 of the shaft portion 32 of the planetary roller 30. For this reason, when the movable internal ring 42 is pressurized toward the input side in the axial direction, the shaft portion 32 receives a pressing force toward the radially inner side via the inclined surface 33. That is, the plurality of planetary rollers 30 are pressed radially inward by the fixed internal ring 41 and the movable internal ring 42.
  • the elastic member 70 of the present embodiment is disposed in a space on the outer side in the radial direction of the carrier 50. Thereby, the dimension of the axial direction of the traction reduction gear 1 can be reduced rather than the case where the carrier 50 and the elastic member 70 are arrange
  • the housing 80 is a member that accommodates at least the sun roller 20, the plurality of planetary rollers 30, the pair of internal rings 40, the carrier 50, and the carrier bearing 60 therein.
  • the housing 80 has a cylindrical inner peripheral surface surrounding at least the outer periphery of the internal ring 40.
  • the housing 80 of the present embodiment has a claw portion 81 that extends radially inward.
  • the claw portion 81 is formed, for example, by caulking a part in the circumferential direction of the output side end edge of the housing 80.
  • the claw portion 81 contacts the carrier bearing 60 in the axial direction. Thereby, the axial positioning of the carrier bearing 60 with respect to the housing 80 can be easily performed. As a result, the traction speed reducer 1 can be easily assembled.
  • the claw portion 81 is in contact with the carrier bearing 60 and the circumferential direction around the rotation shaft 9. Thereby, relative rotation of the carrier bearing 60 with respect to the housing 80 can be easily prevented.
  • the internal ring 40 of the present embodiment has a plurality of first anti-rotation portions 43 that are recessed inward in the radial direction in a part of the outer peripheral surface and whose surface is a flat portion.
  • the housing 80 of the present embodiment has a plurality of second anti-rotation portions 82 that are convex inward in the radial direction and whose inner surface in the radial direction is a flat portion.
  • the plurality of first detent portions 43 are arranged at equal intervals in the circumferential direction around the rotation shaft 9.
  • the plurality of second anti-rotation portions 82 are arranged at equal intervals in the circumferential direction around the rotation shaft 9.
  • the first anti-rotation portion 43 is fitted into the second anti-rotation portion 82, and the flat portion of the first anti-rotation portion 43 and the flat portion of the second anti-rotation portion 82 are in contact with each other. Thereby, relative rotation of the internal ring 40 with respect to the housing 80 can be prevented. As a result, the rotation of the planetary roller 30 and the carrier 50 is stabilized.
  • the plurality of first detent portions 43 may be formed so that a part of the outer peripheral surface of the internal ring 40 is a non-perfect circle, and is not limited to the structure of FIG.
  • the plurality of second anti-rotation portions 82 may be formed so that a part of the inner peripheral surface of the housing 80 is a non-circular shape, and is not limited to the structure of FIG.
  • the output shaft 90 is a columnar member that extends to the output side in the axial direction along the rotation shaft 9.
  • the output shaft 90 is fixed, for example, by being press-fitted from an end on the output side in the axial direction of the carrier 50 into a recess 55 that is recessed on the input side in the axial direction.
  • other methods may be used for fixing the output shaft 90 and the carrier 50.
  • the output shaft 90 rotates around the rotation shaft 9 together with the carrier 50.
  • the plurality of planetary rollers 30 are always in contact with the sun roller 20, the fixed internal ring 41, and the movable internal ring 42, respectively.
  • a lubricant (not shown) is interposed between the sun roller 20 and the planetary roller 30. Thereby, traction is generated between the sun roller 20 and the planetary roller 30.
  • a lubricant (not shown) is interposed between the planetary roller 30 and the internal ring 40. As a result, traction is generated between the planetary roller 30 and the internal ring 40.
  • the sun roller 20 is rotated by the driving force of the motor 11
  • the plurality of planetary rollers 30 receive power from the sun roller 20 and rotate by traction with the sun roller 20.
  • the plurality of planetary rollers 30 revolve around the rotating shaft 9 along the internal ring 40 by traction with the internal ring 40. At this time, the revolution speed of the planetary roller 30 is a second rotational speed lower than the first rotational speed.
  • the carrier 50 When the plurality of planetary rollers 30 revolve at the second rotational speed after deceleration, the carrier 50 also rotates at the second rotational speed around the rotation shaft 9.
  • the output shaft 90 fixed to the carrier 50 is also rotated at the second rotation speed around the rotation shaft 9.
  • the rotational motion at the first rotational speed of the motor 11 is converted into the rotational motion at the second rotational speed that is lower than the first rotational speed, and is output to the output shaft 90.
  • FIG. 6 is a longitudinal sectional view of a reduction gear with an electric motor including a traction reduction gear 1A according to the second embodiment.
  • FIG. 7 is a DD cross-sectional view of FIG. 6 of the traction reducer 1A according to the second embodiment.
  • FIG. 8 is a cross-sectional view taken along the line EE of FIG. 6 of the traction reducer 1A according to the second embodiment.
  • this reduction gear with motor 10A rotates the rotation motion at the first rotation speed obtained from the motor 11A at the second rotation speed lower than the first rotation speed. It is a speed reducer that converts the motion to rotate the output shaft 90A.
  • the traction reduction gear 1A of this embodiment includes one sun roller 20A, a plurality of planetary rollers 30A, an internal ring 40A, a carrier 50A, a carrier bearing 60A, an elastic member 70A, a housing 80A, and an output shaft. 90A.
  • the sun roller 20A is a columnar member arranged coaxially with the rotating shaft 9A.
  • the sun roller 20A is connected to a motor 11A located on the input side in the axial direction. When the motor 11A is driven, the sun roller 20A rotates at the first rotation speed around the rotation shaft 9A by the power received from the motor 11A.
  • Each of the plurality of planetary rollers 30A has a disk portion 31A and a pair of shaft portions 32A.
  • the disc portion 31A is arranged around the sun roller 20A so that a straight line connecting the center viewed from the axial input side and the center viewed from the axial output side is parallel to the rotation shaft 9A. Is done.
  • the outer peripheral portion of the disc portion 31A is in contact with the outer peripheral portion of the sun roller 20A.
  • the pair of shaft portions 32A extends parallel to the rotation shaft 9A from the center of the disc portion 31A to the input side and output side in the axial direction.
  • Each shaft portion 32A has an annular inclined surface 33A at the end opposite to the axial disk portion 31A.
  • the inclined surface 33A is inclined with respect to the axial direction so as to decrease in diameter toward the tip of the shaft portion 32A.
  • the disk portion 31A only needs to have a circular outer periphery when viewed from the axial direction, and the surface shape may be other than a plate shape.
  • the internal ring 40A is a pair of annular members that are in contact with the plurality of planetary rollers 30A.
  • the internal ring 40A of the present embodiment includes a fixed internal ring 41A and a movable internal ring 42A.
  • the fixed internal ring 41A of the present embodiment is positioned on the output side in the axial direction from the disk portion 31A, and the position in the axial direction is fixed.
  • the movable internal ring 42A is positioned on the input side in the axial direction with respect to the disc portion 31A, and is movable in the axial direction.
  • the plurality of planetary rollers 30A are rotatably supported around the sun roller 20A by the sun roller 20A and the internal ring 40A. Further, the outer peripheral portions of the plurality of planetary rollers 30A are in contact with the inner peripheral portion of the internal ring 40A. For this reason, when the sun roller 20A rotates around the rotation shaft 9A, the plurality of planetary rollers 30A receive power from the sun roller 20A. The plurality of planetary rollers 30A revolve around the rotating shaft 9A while rotating around the sun roller 20A.
  • the internal ring 40A of this embodiment is in contact with the inclined surface 33A of the shaft portion 32A, as in the first embodiment.
  • the carrier 50A rotates around the rotation shaft 9A while holding the plurality of planetary rollers 30A.
  • the carrier 50A of the present embodiment has two first carrier members 511A and 512A, a second carrier member 52A, and a plurality of carrier poles 53A.
  • the first carrier member 51A is a disk-shaped member having a contact surface 54A. As shown in FIGS. 6 and 8, one of the two first carrier members 511A has at least part of the outer peripheral surface of the shaft portion 32A on the output side in the axial direction of the planetary roller 30A and the contact surface 54A. The contact is made in the circumferential direction around the rotating shaft 9A.
  • the other first carrier member 512A is arranged in the circumferential direction centering on the rotating shaft 9A via at least a part of the outer circumferential surface of the shaft portion 32A on the input side in the axial direction of the planetary roller 30A and the contact surface 54A. Contact. Thereby, each planetary roller 30A is supported so that it can rotate around the sun roller 20A.
  • the second carrier member 52A is disposed on the output side in the axial direction with respect to the first carrier members 511A and 512A and the planetary roller 30A.
  • the carrier pole 53A is a columnar member extending in the axial direction. As shown in FIG. 7, in this embodiment, three carrier poles 53A are arranged at equal intervals in the circumferential direction around the sun roller 20A and between the planetary rollers 30A. The end portion on the input side in the axial direction of the carrier pole 53A is fixed to the first carrier member 51A. Further, the end on the output side in the axial direction of the carrier pole 53A is fixed to the second carrier member 52A. As a result, the first carrier member 51A and the second carrier member 52A rotate around the rotation shaft 9A as the planetary roller 30A rotates.
  • the carrier bearing 60A supports the second carrier member 52A so as to be rotatable about the rotation shaft 9A. As shown in FIG. 6, the carrier bearing 60A of the present embodiment is in contact with at least a part of the outer peripheral surface of the carrier 50A. Furthermore, the carrier bearing 60A is in contact with the end face on the output side in the axial direction of the carrier 50A. Thereby, the carrier 50A is restricted from moving in the radial direction and the axial direction, and is stably held.
  • the elastic member 70A is a mechanism that pressurizes the movable internal ring 42A toward the output side in the axial direction.
  • the elastic member 70A is an annular member that expands and contracts in the axial direction.
  • a wave spring is used for the elastic member 70.
  • the elastic member 70A is disposed between the mounting plate 12A and the movable internal ring 42A in a state compressed in the axial direction rather than the natural length. For this reason, the movable internal ring 42A is pressurized toward the output side by the repulsive force of the elastic member 70A.
  • the shaft portion 32A When the movable internal ring 42A is pressurized toward the output side in the axial direction, the shaft portion 32A receives a pressing force toward the radially inner side via the inclined surface 33A. That is, the plurality of planetary rollers 30A are pressed radially inward by the fixed internal ring 41A and the movable internal ring 42A.
  • the housing 80A is a member that accommodates at least the sun roller 20A, the plurality of planetary rollers 30A, the pair of internal rings 40A, the carrier 50A, and the carrier bearing 60A.
  • the output shaft 90A is a columnar member that extends to the output side in the axial direction along the rotation shaft 9A.
  • the output shaft 90A is fixed, for example, by being press-fitted into a through hole 55A provided in the center of the second carrier member 52A.
  • the output shaft 90A rotates around the rotation shaft 9A together with the second carrier member 52A.
  • the internal ring 40 ⁇ / b> A of the present embodiment has a plurality of first detent portions 43 ⁇ / b> A that are non-circular on a part of the outer peripheral surface.
  • the housing 80A of the present embodiment has a plurality of second anti-rotation portions 82A that are non-circular on a part of the inner peripheral surface.
  • the plurality of first detent portions 43A are arranged at equal intervals in the circumferential direction around the rotation shaft 9A.
  • the plurality of second anti-rotation portions 82A are arranged at equal intervals in the circumferential direction around the rotation shaft 9A.
  • the first detent portion 43A comes into contact with the second detent portion 82A.
  • the circumferential positioning of the carrier 50A with respect to the housing 80A can be facilitated.
  • the traction reduction gear 1A can be easily assembled.
  • relative rotation of the internal ring 40A with respect to the housing 80A can be prevented.
  • the rotation of the planetary roller 30A and the carrier 50A is stabilized.
  • the plurality of planetary rollers 30A are always in contact with the sun roller 20A, the fixed internal ring 41A, and the movable internal ring 42A, respectively.
  • a lubricant (not shown) is interposed between the sun roller 20A and the planetary roller 30A. Thereby, traction is generated between the sun roller 20A and the planetary roller 30A.
  • a lubricant (not shown) is interposed between the planetary roller 30A and the internal ring 40A. As a result, traction is generated between the planetary roller 30 and the internal ring 40.
  • the plurality of planetary rollers 30A revolve around the rotating shaft 9A along the internal ring 40A by traction with the internal ring 40A. At this time, the revolution speed of the planetary roller 30 ⁇ / b> A is a second rotational speed lower than the first rotational speed.
  • the second carrier member 52A fixed to the carrier pole 53A together with the first carrier member 51A also has the second center around the rotation shaft 9A. Rotates at the number of revolutions.
  • the output shaft 90A fixed to the second carrier member 52A also rotates at the second rotation speed about the rotation shaft 9A. Thereby, the rotational motion at the first rotational speed of the motor is converted into the rotational motion at the second rotational speed lower than the first rotational speed, and is output to the output shaft 90A.
  • FIG. 9 is a partial longitudinal sectional view of a reduction gear 10B with an electric motor including a traction reduction gear 1B according to the third embodiment.
  • differences from the first embodiment will be mainly described, and redundant description of parts equivalent to those of the first embodiment will be omitted.
  • This reduction gear 10B with an electric motor performs a rotational motion at a first rotational speed obtained from a motor (not shown) in a second rotation lower than the first rotational speed.
  • the carrier bearing 60B of the traction reduction gear 1B has a plurality of radial bearing surfaces including a first radial bearing surface 110B and a second radial bearing surface 111B.
  • the first radial bearing surface 110B and the second radial bearing surface 111B each extend in an annular shape in the circumferential direction around the rotating shaft 9B, and are separated from each other in the axial direction.
  • the first radial bearing surface 110B is located on the input side in the axial direction and on the outer side in the radial direction than the second radial bearing surface 111B.
  • the carrier bearing 60B is in contact with the outer peripheral surface of the carrier 50B at the first radial bearing surface 110B and the second radial bearing surface 111B, and rotatably supports the carrier 50B.
  • the plurality of radial bearing surfaces may be composed of three or more radial bearing surfaces.
  • a space 120B is formed between the first radial bearing surface 110B and the second radial bearing surface 111B.
  • the space 120B plays a role of storing grease to be described later, thereby suppressing leakage of grease from the output shaft 90B side. Further, since the carrier 50B is supported by the first radial bearing surface 110B and the second radial bearing surface 111B that are axially separated from each other, the carrier 50B can be prevented from rotating in an inclined state.
  • the inner peripheral surface of the carrier bearing 60B has an annular bearing step surface 600B that extends perpendicularly or obliquely to the axial direction.
  • the outer peripheral surface of the carrier 50B has an annular carrier step surface 500B that extends perpendicularly or obliquely to the axial direction.
  • the bearing step surface 600B and the carrier step surface 500B are opposed in the axial direction at least in part.
  • the above-described space 120B is parallel to the bearing step surface 600B, the carrier step surface 500B, the annular surface extending in parallel to the axial direction on the inner peripheral surface of the carrier bearing 60B, and the axial direction on the outer peripheral surface of the carrier 50B. Formed by an expanding annular surface.
  • the first radial bearing surface 110B is positioned at least on the input side in the axial direction from the bearing step surface 600B and the carrier step surface 500B
  • the second radial bearing surface 111B is formed from at least the bearing step surface 600B and the carrier step surface 500B. Is also located on the axial output side. That is, the first radial bearing surface 110B and the second radial bearing surface 111B are located on the outer side in the axial direction from the bearing step surface 600B and the carrier step surface 500B.
  • the space 120B can be easily formed without excessively complicating the structures of the carrier 50B and the carrier bearing 60B.
  • the positional relationship in the axial direction between the first radial bearing surface 110B and the second radial bearing surface 111B may be reversed.
  • a first grease is sealed as a lubricant between the plurality of planetary rollers 30B and at least one of the sun roller (not shown) and the internal ring 40B.
  • a second grease having a viscosity higher than that of the first grease is enclosed in the space 120B (not shown).
  • the space 120B may be a space formed between at least two of the plurality of radial bearing surfaces, and is between the radial bearing surfaces different from the first radial bearing surface 110B and the second radial bearing surface 111B. It may be a space formed.
  • the reduction gear with motor and the traction reduction gear were used for precision parts of electrical appliances.
  • the traction reduction gear and the reduction gear with electric motor of the present invention may be used for other applications such as industrial machinery.
  • three planetary rollers are arranged at equal intervals in the circumferential direction around the sun roller.
  • the number of planetary rollers included in the traction reducer may be two or four or more.
  • the elastic member is an annular member that expands and contracts in the axial direction.
  • the elastic member only needs to generate a repulsive force in the axial direction.
  • a plurality of coil springs may be arranged at equal intervals in the circumferential direction, and may be constituted by other members. It may be.
  • three carrier poles are arranged at equal intervals in the circumferential direction around the sun roller and between the planetary rollers.
  • the number of carrier poles may be two or four or more.
  • a high-strength metal may be used as the material of each member constituting the wheel-in speed reducer.
  • the material of each member is not limited to metal as long as it can withstand the load during use.
  • a resin may be used as the material of some members.
  • the shape of the details of the traction reducer and the reduction gear with an electric motor may be different from the shapes shown in the drawings of the present application. Moreover, you may combine suitably each element which appeared in said embodiment and modification in the range which does not produce inconsistency.
  • the present invention can be used for a traction speed reducer and a speed reducer with an electric motor.

Abstract

This traction speed reducer is provided with: a sun roller that rotates about an axis of rotation; a plurality of planetary rollers that are disposed around the sun roller; a pair of annular internal rings that are in contact with the plurality of planetary rollers; and a carrier that holds the planetary rollers and rotates about the axis of rotation. The plurality of planetary rollers are each in contact with the sun roller and both of the internal rings, and by receiving motive power from the sun roller, orbit around the axis of rotation while rotating independently. The carrier has a contact surface facing the outer circumferential surface of the planetary rollers, and the contact surface and the outer circumferential surface of the planetary rollers are in contact in the circumferential direction about the axis of rotation. As a result, a carrier pin for rotatably supporting the planetary rollers is unnecessary. Thus, it is possible to reduce the number of components and decrease the size of the traction speed reducer.

Description

トラクション減速機および電動機付き減速機Traction reducer and reducer with electric motor
 本発明は、トラクション減速機および電動機付き減速機に関する。 The present invention relates to a traction speed reducer and a speed reducer with an electric motor.
 従来、太陽ローラと遊星ローラとの間に発生させたトラクション(摩擦)を利用して、入力軸の回転速度を減速させて出力軸を回転させる、トラクション減速機が知られている。このようなトラクション減速機については、例えば、特開2009-138924号公報に記載されている。 Conventionally, there is known a traction reducer that uses the traction (friction) generated between the sun roller and the planetary roller to reduce the rotational speed of the input shaft and rotate the output shaft. Such a traction reducer is described in, for example, Japanese Patent Application Laid-Open No. 2009-138924.
 当該文献に記載のトラクション動力伝達装置は、第1中心軸線回りに回転自在な太陽ローラと、第1中心軸線と平行な複数の周辺軸線上に第2中心軸線が合致するように配置される複数の軸部材と、軸部材に支持された状態で、太陽ローラの周面に沿って回転自在に設けられた複数の遊星ローラと、第1中心軸線と第2中心軸線との平行を保持したまま、軸部材を太陽ローラの径方向に移動自在に案内する案内部材と、太陽ローラの周面に対して遊星ローラを押し付け、太陽ローラと遊星ローラとの間にてトラクションによる動力伝達を可能にする押圧部材と、を備える。 The traction power transmission device described in the document includes a sun roller that is rotatable around a first central axis, and a plurality of second central axes that are arranged on a plurality of peripheral axes that are parallel to the first central axis. The shaft member, a plurality of planetary rollers rotatably provided along the peripheral surface of the sun roller while being supported by the shaft member, and the parallelism between the first central axis and the second central axis is maintained The planetary roller is pressed against the circumferential surface of the sun roller by guiding the shaft member so as to be movable in the radial direction of the sun roller, and power transmission by traction is enabled between the sun roller and the planetary roller. A pressing member.
 当該文献には、太陽ローラの径方向に遊星ローラの回転中心である軸部材が移動するため、遊星ローラを太陽ローラの周面に押し付ける力が作用すると、それによって太陽ローラと遊星ローラとの間にトラクションを発生させることができる旨が記載されている。さらに、遊星ローラが太陽ローラの径方向に移動しても、常に遊星ローラの回転中心が太陽ローラの回転中心と平行を保持しているため、軸方向で均等にトラクションを発生させることができる旨が記載されている(段落0007~0008等参照)。
特開2009-138924号公報
In this document, since the shaft member, which is the rotation center of the planetary roller, moves in the radial direction of the sun roller, a force that presses the planetary roller against the circumferential surface of the sun roller acts, thereby Describes that traction can be generated. Furthermore, even if the planetary roller moves in the radial direction of the sun roller, the rotation center of the planetary roller always keeps parallel to the rotation center of the sun roller, so that traction can be generated evenly in the axial direction. (See paragraphs 0007 to 0008, etc.).
JP 2009-138924 A
 しかしながら、特開2009-138924号公報に記載の構造では、押圧部による遊星歯車の押圧面を、軸部材よりも径方向外側に配置する必要がある。また、軸部材とは別に遊星ローラの押圧面を設ける必要がある。このため、トラクション減速機の径方向の小型化が困難となる。 However, in the structure described in Japanese Patent Application Laid-Open No. 2009-138924, it is necessary to dispose the pressing surface of the planetary gear by the pressing portion on the radially outer side than the shaft member. Further, it is necessary to provide a pressing surface of the planetary roller separately from the shaft member. For this reason, it is difficult to reduce the size of the traction reducer in the radial direction.
 本発明の目的は、トラクション減速機において、部品点数を減らしトラクション減速機を小型化できる技術を提供することである。 An object of the present invention is to provide a technology capable of reducing the number of parts and reducing the size of a traction reducer in a traction reducer.
 本願の例示的な第1発明は、トラクション減速機であって、回転軸を中心として回転する太陽ローラと、前記太陽ローラの周囲に配置された複数の遊星ローラと、前記複数の遊星ローラに接触する一対の円環状のインタナルリングと、前記遊星ローラを保持しつつ前記回転軸を中心として回転するキャリアと、を有し、前記複数の遊星ローラは、それぞれ、前記太陽ローラおよび前記インタナルリングの双方に接触しつつ、前記太陽ローラから動力を受けることによって、自転しながら前記回転軸を中心として公転し、前記キャリアは、前記遊星ローラの外周面に対向する接触面を有し、前記遊星ローラの外周面と、前記
接触面とが、前記回転軸を中心とする周方向に接触する。
An exemplary first invention of the present application is a traction speed reducer, which is a sun roller that rotates about a rotation axis, a plurality of planetary rollers arranged around the sun roller, and a contact with the plurality of planetary rollers. A pair of annular internal rings and a carrier that rotates around the rotation axis while holding the planetary roller, and the plurality of planetary rollers are respectively the sun roller and the internal ring. The carrier revolves around the rotation axis while rotating by receiving power from the sun roller while being in contact with both the carrier, the carrier has a contact surface facing the outer peripheral surface of the planetary roller, and the planet The outer peripheral surface of the roller and the contact surface are in contact with each other in the circumferential direction around the rotation axis.
 本願の例示的な第1発明によれば、各遊星ローラを自転可能に支持するキャリアピンが不要となる。このため、部品点数を減らして、トラクション減速機を小型化できる。 According to the first exemplary invention of the present application, a carrier pin that supports each planetary roller so as to rotate is not necessary. For this reason, the number of parts can be reduced and the traction speed reducer can be miniaturized.
図1は、第1実施形態に係る電動機付き減速機の斜視図である。FIG. 1 is a perspective view of a reduction gear with an electric motor according to the first embodiment. 図2は、第1実施形態に係る電動機付き減速機の縦断面図である。FIG. 2 is a longitudinal sectional view of the reduction gear with an electric motor according to the first embodiment. 図3は、第1実施形態に係るトラクション減速機の横断面図である。FIG. 3 is a cross-sectional view of the traction reducer according to the first embodiment. 図4は、第1実施形態に係るトラクション減速機の横断面図である。FIG. 4 is a cross-sectional view of the traction reducer according to the first embodiment. 図5は、第1実施形態に係るトラクション減速機の横断面図である。FIG. 5 is a cross-sectional view of the traction reducer according to the first embodiment. 図6は、第2実施形態に係る電動機付き減速機の縦断面図である。FIG. 6 is a longitudinal sectional view of a reduction gear with an electric motor according to the second embodiment. 図7は、第2実施形態に係るトラクション減速機の横断面図である。FIG. 7 is a cross-sectional view of the traction reducer according to the second embodiment. 図8は、第2実施形態に係るトラクション減速機の横断面図である。FIG. 8 is a cross-sectional view of a traction reducer according to the second embodiment. 図9は、第3実施形態に係る電動機付き減速機の部分縦断面図である。FIG. 9 is a partial longitudinal sectional view of a reduction gear with an electric motor according to the third embodiment.
 以下、本発明の例示的な実施形態について、図面を参照しながら説明する。なお、本願では、太陽ローラの回転軸と平行な方向を「軸方向」、回転軸に直交する方向を「径方向」、回転軸を中心とする円弧に沿う方向を「周方向」、とそれぞれ称する。ただし、上記の「平行な方向」は、略平行な方向も含む。また、上記の「直交する方向」は、略直交する方向も含む。また、以下では、説明の便宜上、図1中の右側を「入力側」、図1中の左側を「出力側」、とそれぞれ称する。 Hereinafter, exemplary embodiments of the present invention will be described with reference to the drawings. In the present application, the direction parallel to the rotation axis of the sun roller is “axial direction”, the direction orthogonal to the rotation axis is “radial direction”, and the direction along the arc centered on the rotation axis is “circumferential direction”. Called. However, the above “parallel direction” includes a substantially parallel direction. In addition, the above-mentioned “orthogonal direction” includes a substantially orthogonal direction. In the following, for convenience of explanation, the right side in FIG. 1 is referred to as “input side” and the left side in FIG. 1 is referred to as “output side”.
 図1は、本実施形態に係るトラクション減速機1を含む電動機付き減速機10の斜視図である。図2は、本実施形態に係るトラクション減速機1を含む電動機付き減速機10の縦断面図である。この電動機付き減速機10は、モータ11から得られる第1回転数の回転運動を、第1回転数よりも低い第2回転数の回転運動に変換して、出力軸90を回転させる減速機である。本発明のトラクション減速機1および電動機付き減速機10は、例えば、電化製品の精密部品等に使用される。 FIG. 1 is a perspective view of a reduction gear 10 with an electric motor including a traction reduction gear 1 according to the present embodiment. FIG. 2 is a longitudinal sectional view of the reduction gear 10 with an electric motor including the traction reduction gear 1 according to the present embodiment. The motor-equipped speed reducer 10 is a speed reducer that rotates the output shaft 90 by converting the rotational motion of the first rotational speed obtained from the motor 11 into the rotational motion of the second rotational speed lower than the first rotational speed. is there. The traction reduction gear 1 and the reduction gear 10 with an electric motor of the present invention are used, for example, for precision parts of electrical appliances.
 図1および図2に示すように、本実施形態の電動機付き減速機10は、モータ11と、取付板12と、トラクション減速機1とを有する。 As shown in FIGS. 1 and 2, the speed reducer 10 with an electric motor according to the present embodiment includes a motor 11, a mounting plate 12, and a traction speed reducer 1.
 モータ11は、電動機付き減速機10の動力源となる電動機である。モータ11は、後述するトラクション減速機1の太陽ローラ20と接続されている。モータ11を駆動させると、太陽ローラ20が回転軸9を中心に回転する。 The motor 11 is an electric motor that is a power source of the reduction gear 10 with an electric motor. The motor 11 is connected to the sun roller 20 of the traction speed reducer 1 described later. When the motor 11 is driven, the sun roller 20 rotates around the rotation shaft 9.
 取付板12は、モータ11にトラクション減速機1を取り付けるための板状の部材である。取付板12は、回転軸9に対して略垂直に配置されている。取付板12は、モータ11の外枠であるモータケーシングに固定される。モータケーシングと取付板12とは、ねじ等の固定具によって固定される。ただし、モータケーシングと取付板12とは、他の方法によって固定されてもよい。 The mounting plate 12 is a plate-like member for mounting the traction speed reducer 1 to the motor 11. The mounting plate 12 is disposed substantially perpendicular to the rotation shaft 9. The mounting plate 12 is fixed to a motor casing that is an outer frame of the motor 11. The motor casing and the mounting plate 12 are fixed by a fixing tool such as a screw. However, the motor casing and the mounting plate 12 may be fixed by other methods.
 トラクション減速機1は、モータ11の回転運動を、減速させて出力軸90に伝達する装置である。このトラクション減速機1には、歯車を用いることなく、太陽ローラ20の外周面と複数の遊星ローラ30の外周面とを、互いに接触させながら回転させることで動力を伝達する、いわゆるトラクション型の遊星減速機構が用いられている。 The traction speed reducer 1 is a device that decelerates the rotational motion of the motor 11 and transmits it to the output shaft 90. The traction speed reducer 1 is a so-called traction type planetary that transmits power by rotating the outer circumferential surface of the sun roller 20 and the outer circumferential surfaces of the plurality of planetary rollers 30 in contact with each other without using gears. A reduction mechanism is used.
 図2に示すように、本実施形態のトラクション減速機1は、1つの太陽ローラ20、複数の遊星ローラ30、インタナルリング40、キャリア50、キャリア軸受60、弾性部材70、ハウジング80および出力軸90を有する。 As shown in FIG. 2, the traction speed reducer 1 according to the present embodiment includes one sun roller 20, a plurality of planetary rollers 30, an internal ring 40, a carrier 50, a carrier bearing 60, an elastic member 70, a housing 80, and an output shaft. 90.
 太陽ローラ20は、回転軸9と同軸に配置された、円柱状の部材である。太陽ローラ20は、軸方向の入力側に位置するモータ11に連結される。モータ11を駆動させると、太陽ローラ20は、モータ11から受ける動力によって、回転軸9を中心として第1回転数で回転する。本実施形態では、モータ11の出力シャフトが、太陽ローラ20となっている。このように、モータ11の出力シャフトと太陽ローラ20とを、単一の部品とすれば、電動機付き減速機10の部品点数が減る。したがって、電動機付き減速機10を小型化しやすくなる。ただし、モータ11の出力シャフトとは別に、出力軸とともに回転する太陽ローラを設けてもよい。 The sun roller 20 is a columnar member arranged coaxially with the rotary shaft 9. The sun roller 20 is connected to the motor 11 located on the input side in the axial direction. When the motor 11 is driven, the sun roller 20 rotates at the first rotation speed around the rotation shaft 9 by the power received from the motor 11. In the present embodiment, the output shaft of the motor 11 is the sun roller 20. Thus, if the output shaft of the motor 11 and the sun roller 20 are made into a single part, the number of parts of the reduction gear 10 with an electric motor will reduce. Therefore, it becomes easy to miniaturize the reduction gear 10 with an electric motor. However, a sun roller that rotates together with the output shaft may be provided separately from the output shaft of the motor 11.
 図3は、トラクション減速機1の、図1のA-A断面図である。複数の遊星ローラ30は、太陽ローラ20の周囲に配置される。図3に示すように、本実施形態では、太陽ローラ20の周囲に、3個の遊星ローラ30が周方向に等間隔に配置されている。 FIG. 3 is a cross-sectional view of the traction reducer 1 taken along the line AA in FIG. The plurality of planetary rollers 30 are arranged around the sun roller 20. As shown in FIG. 3, in the present embodiment, three planetary rollers 30 are arranged around the sun roller 20 at equal intervals in the circumferential direction.
 複数の遊星ローラ30は、それぞれ円板部31と、一対の軸部32とを有する。円板部31は、太陽ローラ20の周囲に、軸方向の入力側から見た中心と軸方向の出力側から見た中心とを結ぶ直線が、回転軸9に対して平行となるように配置される。図2および図3に示すように、円板部31の外周部は、太陽ローラ20の外周部と接触する。一対の軸部32は、円板部31の中央から軸方向の入力側および出力側に、回転軸9と平行に延びる。本実施形態では、円板部31および一対の軸部32は一部材により構成されている。また、各軸部32は、軸方向の円板部31とは反対側の端部に、円環状の傾斜面33を有する。傾斜面33は、軸部32の先端へ向かうにつれて縮径するように、軸方向に対して傾斜する。なお、円板部31は、軸方向から見たときに外周が円形であればよく、表面形状は板状以外の形状であってもよい。 Each of the plurality of planetary rollers 30 includes a disk portion 31 and a pair of shaft portions 32. The disc portion 31 is arranged around the sun roller 20 so that a straight line connecting the center viewed from the axial input side and the center viewed from the axial output side is parallel to the rotation shaft 9. Is done. As shown in FIGS. 2 and 3, the outer peripheral portion of the disc portion 31 is in contact with the outer peripheral portion of the sun roller 20. The pair of shaft portions 32 extend in parallel with the rotation shaft 9 from the center of the disc portion 31 to the input side and output side in the axial direction. In this embodiment, the disc part 31 and a pair of axial part 32 are comprised by one member. Each shaft portion 32 has an annular inclined surface 33 at the end opposite to the axial disk portion 31. The inclined surface 33 is inclined with respect to the axial direction so as to decrease in diameter toward the tip of the shaft portion 32. The disk portion 31 only needs to have a circular outer periphery when viewed from the axial direction, and the surface shape may be other than a plate shape.
 インタナルリング40は、複数の遊星ローラ30に接触する一対の円環状の部材である。本実施形態のインタナルリング40は、固定インタナルリング41および可動インタナルリング42によって構成される。図2に示すように、本実施形態の固定インタナルリング41は、円板部31よりも軸方向の入力側に位置し、軸方向の位置が固定されている。また、可動インタナルリング42は、円板部31よりも軸方向の出力側に位置し、軸方向に移動可能となっている。ただし、可動インタナルリング42が円板部31よりも軸方向の入力側に配置され、固定インタナルリング41が円板部31よりも軸方向の出力側に配置されていてもよい。 The internal ring 40 is a pair of annular members that contact the plurality of planetary rollers 30. The internal ring 40 according to this embodiment includes a fixed internal ring 41 and a movable internal ring 42. As shown in FIG. 2, the fixed internal ring 41 of the present embodiment is positioned on the input side in the axial direction with respect to the disc portion 31, and the position in the axial direction is fixed. The movable internal ring 42 is positioned on the output side in the axial direction with respect to the disc portion 31 and is movable in the axial direction. However, the movable internal ring 42 may be disposed on the input side in the axial direction with respect to the disc portion 31, and the fixed internal ring 41 may be disposed on the output side in the axial direction with respect to the disc portion 31.
 図4は、トラクション減速機1の、図1のB-B断面図である。複数の遊星ローラ30は、太陽ローラ20およびインタナルリング40によって、太陽ローラ20の周囲で回動自在に支持される。図4に示すように、複数の遊星ローラ30の外周部は、インタナルリング40の内周部と接触する。太陽ローラ20が回転軸9を中心に回転すると、複数の遊星ローラ30は、太陽ローラ20から動力を受ける。そして、複数の遊星ローラ30は、太陽ローラ20の周囲で、自転しながら回転軸9を中心として公転する。 FIG. 4 is a cross-sectional view of the traction reducer 1 taken along the line BB in FIG. The plurality of planetary rollers 30 are rotatably supported around the sun roller 20 by the sun roller 20 and the internal ring 40. As shown in FIG. 4, the outer peripheral portions of the plurality of planetary rollers 30 are in contact with the inner peripheral portion of the internal ring 40. When the sun roller 20 rotates about the rotation shaft 9, the plurality of planetary rollers 30 receives power from the sun roller 20. The plurality of planetary rollers 30 revolve around the rotating shaft 9 while rotating around the sun roller 20.
 また、図2に示すように、本実施形態のインタナルリング40は、軸部32の傾斜面33と接触する。これにより、径方向の幅を抑えつつ、インタナルリング40と遊星ローラ30とを接触させることができる。また、遊星ローラ30の円板部31と軸部32とは、同一部材であることから、インタナルリング40と遊星ローラ30との間に、別途の接触部材を設けることなく、インタナルリング40の圧力を、遊星ローラ30に直接伝えることができる。その結果、トラクション減速機1の部品点数を低減できる。 Further, as shown in FIG. 2, the internal ring 40 of the present embodiment is in contact with the inclined surface 33 of the shaft portion 32. Thereby, the internal ring 40 and the planetary roller 30 can be contacted, suppressing the radial width. Further, since the disk portion 31 and the shaft portion 32 of the planetary roller 30 are the same member, the internal ring 40 is not provided with a separate contact member between the internal ring 40 and the planetary roller 30. Can be transmitted directly to the planetary roller 30. As a result, the number of parts of the traction reduction gear 1 can be reduced.
 図5は、トラクション減速機1の、図1のC-C断面図である。キャリア50は、複数の遊星ローラ30を保持しつつ回転軸9を中心として回転する。図5に示すように、キャリア50は、遊星ローラ30の軸部32の外周面と対向する接触面54を有する。軸部32の外周面のうち、遊星ローラ30の公転の回転方向前側に位置する面の少なくとも一部と、接触面54とは、周方向に接触する。すなわち、接触面54と、軸部32の外周面の少なくとも一部とは、回転軸9を中心とする周方向に接触する。これにより、各遊星ローラ30は、太陽ローラ20の周囲で、自転可能に支持される。このように、遊星ローラ30の一部である軸部32が、キャリア50によって支持される。このため、キャリアピンのような部材を別途設ける必要がなくなる。その結果、部品点数を減らして、トラクション減速機1を小型化できる。 FIG. 5 is a cross-sectional view taken along the line CC of FIG. The carrier 50 rotates around the rotation shaft 9 while holding the plurality of planetary rollers 30. As shown in FIG. 5, the carrier 50 has a contact surface 54 that faces the outer peripheral surface of the shaft portion 32 of the planetary roller 30. Of the outer peripheral surface of the shaft portion 32, at least a part of the surface located on the front side in the rotational direction of the revolution of the planetary roller 30 and the contact surface 54 are in contact in the circumferential direction. That is, the contact surface 54 and at least a part of the outer peripheral surface of the shaft portion 32 are in contact with each other in the circumferential direction around the rotation shaft 9. Accordingly, each planetary roller 30 is supported around the sun roller 20 so as to be capable of rotating. Thus, the shaft portion 32 that is a part of the planetary roller 30 is supported by the carrier 50. For this reason, it is not necessary to separately provide a member such as a carrier pin. As a result, the number of parts can be reduced and the traction speed reducer 1 can be downsized.
 また、図2、図4および図5に示すように、本実施形態のキャリア50は、複数の収容部56を有する。複数の収容部56は、回転軸9を中心とする周方向に配列され、各々が径方向外側へ向けて開いている。そして、複数の遊星ローラ30の軸部32は、収容部56に収容される。このため、トラクション減速機1の製造時に、遊星ローラ30をキャリア50の収容部56に対して径方向外側から挿入できる。これにより、トラクション減速機1の組み立てが容易となる。 Further, as shown in FIGS. 2, 4, and 5, the carrier 50 of the present embodiment has a plurality of accommodating portions 56. The plurality of accommodating portions 56 are arranged in the circumferential direction around the rotation shaft 9, and each of the accommodating portions 56 is open radially outward. The shaft portions 32 of the plurality of planetary rollers 30 are accommodated in the accommodating portion 56. For this reason, the planetary roller 30 can be inserted into the accommodating portion 56 of the carrier 50 from the outside in the radial direction when the traction reduction gear 1 is manufactured. Thereby, the assembly of the traction reduction gear 1 becomes easy.
 なお、本実施形態のキャリア50は、単一の部材により構成される。このため、キャリア50が複数の部材で構成される場合よりも、部品数を低減できる。これにより、トラクション減速機1をより小型化できる。また、トラクション減速機1の組み立てがより容易となる。 In addition, the carrier 50 of this embodiment is comprised with a single member. For this reason, the number of parts can be reduced as compared with the case where the carrier 50 is constituted by a plurality of members. Thereby, the traction reduction gear 1 can be further reduced in size. Moreover, the assembly of the traction speed reducer 1 becomes easier.
 キャリア軸受60は、キャリア50を回転軸9を中心に回転可能に支持する。図2に示すように、本実施形態のキャリア軸受60は、キャリア50の外周面の少なくとも一部と接触する。さらに、キャリア軸受60は、キャリア50の軸方向の出力側の端面と接触する。これにより、キャリア50は、径方向および軸方向の移動が規制され、安定的に保持される。 The carrier bearing 60 supports the carrier 50 so as to be rotatable about the rotary shaft 9. As shown in FIG. 2, the carrier bearing 60 of the present embodiment contacts at least a part of the outer peripheral surface of the carrier 50. Further, the carrier bearing 60 is in contact with the end face on the output side in the axial direction of the carrier 50. Thereby, the movement of the radial direction and the axial direction is regulated and the carrier 50 is stably held.
 弾性部材70は、可動インタナルリング42を軸方向の入力側へ加圧する部材である。弾性部材70は、軸方向に伸縮する円環状の部材である。弾性部材70には、例えば、ウェーブばねが用いられる。弾性部材70は、キャリア軸受60と可動インタナルリング42との間に、自然長よりも軸方向に圧縮された状態で配置される。このため、弾性部材70の反発力によって、可動インタナルリング42が、入力側へ加圧される。 The elastic member 70 is a member that pressurizes the movable internal ring 42 toward the input side in the axial direction. The elastic member 70 is an annular member that expands and contracts in the axial direction. For the elastic member 70, for example, a wave spring is used. The elastic member 70 is disposed between the carrier bearing 60 and the movable internal ring 42 in a state compressed in the axial direction rather than the natural length. For this reason, the movable internal ring 42 is pressurized to the input side by the repulsive force of the elastic member 70.
 上述したように、固定インタナルリング41および可動インタナルリング42は、遊星ローラ30の軸部32の傾斜面33と接触する。このため、可動インタナルリング42が軸方向の入力側へ加圧されると、軸部32は傾斜面33を介して、径方向内側に向けて押圧力を受ける。すなわち、複数の遊星ローラ30は、固定インタナルリング41および可動インタナルリング42によって、径方向内側に加圧される。 As described above, the fixed internal ring 41 and the movable internal ring 42 are in contact with the inclined surface 33 of the shaft portion 32 of the planetary roller 30. For this reason, when the movable internal ring 42 is pressurized toward the input side in the axial direction, the shaft portion 32 receives a pressing force toward the radially inner side via the inclined surface 33. That is, the plurality of planetary rollers 30 are pressed radially inward by the fixed internal ring 41 and the movable internal ring 42.
 また、本実施形態の弾性部材70は、キャリア50の径方向外側のスペースに配置される。これにより、キャリア50と弾性部材70とを、異なる軸方向位置に配置する場合よりも、トラクション減速機1の軸方向の寸法を低減できる。その結果、トラクション減速機1をより小型化できる。 Further, the elastic member 70 of the present embodiment is disposed in a space on the outer side in the radial direction of the carrier 50. Thereby, the dimension of the axial direction of the traction reduction gear 1 can be reduced rather than the case where the carrier 50 and the elastic member 70 are arrange | positioned in a different axial direction position. As a result, the traction speed reducer 1 can be further downsized.
 ハウジング80は、少なくとも、太陽ローラ20、複数の遊星ローラ30、一対のインタナルリング40、キャリア50およびキャリア軸受60を内部に収容する部材である。ハウジング80は、少なくともインタナルリング40の外周を取り囲む円筒状の内周面を有する。 The housing 80 is a member that accommodates at least the sun roller 20, the plurality of planetary rollers 30, the pair of internal rings 40, the carrier 50, and the carrier bearing 60 therein. The housing 80 has a cylindrical inner peripheral surface surrounding at least the outer periphery of the internal ring 40.
 図2に示すように、本実施形態のハウジング80は、径方向内側に向けて延びる爪部81を有する。爪部81は、例えば、ハウジング80の出力側の端縁の周方向の一部分を、かしめることにより形成される。爪部81は、キャリア軸受60と軸方向に接触する。これにより、ハウジング80に対するキャリア軸受60の軸方向の位置決めを容易に行うことができる。その結果、トラクション減速機1を容易に組み立てることができる。また、爪部81は、キャリア軸受60と回転軸9を中心とする周方向に接触する。これにより、ハウジング80に対するキャリア軸受60の相対回転を、容易に防止できる。 As shown in FIG. 2, the housing 80 of the present embodiment has a claw portion 81 that extends radially inward. The claw portion 81 is formed, for example, by caulking a part in the circumferential direction of the output side end edge of the housing 80. The claw portion 81 contacts the carrier bearing 60 in the axial direction. Thereby, the axial positioning of the carrier bearing 60 with respect to the housing 80 can be easily performed. As a result, the traction speed reducer 1 can be easily assembled. Further, the claw portion 81 is in contact with the carrier bearing 60 and the circumferential direction around the rotation shaft 9. Thereby, relative rotation of the carrier bearing 60 with respect to the housing 80 can be easily prevented.
 また、図4に示すように、本実施形態のインタナルリング40は、外周面の一部分に径方向内側に凹み、表面が平面部である、複数の第1回り止め部43を有する。また、本実施形態のハウジング80は、径方向内側に凸となり、径方向内側の面が平面部である複数の第2回り止め部82を有する。複数の第1回り止め部43は、回転軸9を中心とする周方向に等間隔に配置される。複数の第2回り止め部82は、回転軸9を中心とする周方向に等間隔に配置される。第1回り止め部43は、第2回り止め部82に嵌まり、第1回り止め部43の平面部と、第2回り止め部82の平面部とが接触する。これにより、ハウジング80に対するインタナルリング40の相対回転を防止できる。その結果、遊星ローラ30およびキャリア50の回転が安定する。 Further, as shown in FIG. 4, the internal ring 40 of the present embodiment has a plurality of first anti-rotation portions 43 that are recessed inward in the radial direction in a part of the outer peripheral surface and whose surface is a flat portion. Further, the housing 80 of the present embodiment has a plurality of second anti-rotation portions 82 that are convex inward in the radial direction and whose inner surface in the radial direction is a flat portion. The plurality of first detent portions 43 are arranged at equal intervals in the circumferential direction around the rotation shaft 9. The plurality of second anti-rotation portions 82 are arranged at equal intervals in the circumferential direction around the rotation shaft 9. The first anti-rotation portion 43 is fitted into the second anti-rotation portion 82, and the flat portion of the first anti-rotation portion 43 and the flat portion of the second anti-rotation portion 82 are in contact with each other. Thereby, relative rotation of the internal ring 40 with respect to the housing 80 can be prevented. As a result, the rotation of the planetary roller 30 and the carrier 50 is stabilized.
 なお、複数の第1回り止め部43は、インタナルリング40の外周面の一部分が非真円となるように形成されればよく、図4の構造に限定されない。また、複数の第2回り止め部82は、ハウジング80の内周面の一部分が非真円となるように形成されればよく、図4の構造に限定されない。 Note that the plurality of first detent portions 43 may be formed so that a part of the outer peripheral surface of the internal ring 40 is a non-perfect circle, and is not limited to the structure of FIG. Further, the plurality of second anti-rotation portions 82 may be formed so that a part of the inner peripheral surface of the housing 80 is a non-circular shape, and is not limited to the structure of FIG.
 出力軸90は、回転軸9に沿って軸方向の出力側に延びる円柱状の部材である。出力軸90は、キャリア50の軸方向の出力側の端部から、軸方向の入力側に凹む凹部55に、例えば、圧入されることで固定される。ただし、出力軸90とキャリア50との固定方法は、他の方法を用いてもよい。出力軸90は、キャリア50とともに回転軸9を中心に回転する。 The output shaft 90 is a columnar member that extends to the output side in the axial direction along the rotation shaft 9. The output shaft 90 is fixed, for example, by being press-fitted from an end on the output side in the axial direction of the carrier 50 into a recess 55 that is recessed on the input side in the axial direction. However, other methods may be used for fixing the output shaft 90 and the carrier 50. The output shaft 90 rotates around the rotation shaft 9 together with the carrier 50.
 複数の遊星ローラ30は、それぞれ、太陽ローラ20、固定インタナルリング41および可動インタナルリング42と、常に接触する。そして、太陽ローラ20と遊星ローラ30との間には図示を省略した潤滑剤が介在する。これにより、太陽ローラ20と遊星ローラ30との間にはトラクションが発生する。また、遊星ローラ30とインタナルリング40との間には図示を省略した潤滑剤が介在する。これにより、遊星ローラ30とインタナルリング40との間にはトラクションが発生する。モータ11の駆動力により、太陽ローラ20が回転すると、複数の遊星ローラ30は、太陽ローラ20からの動力を受け、太陽ローラ20との間のトラクションによって自転する。また、複数の遊星ローラ30は、インタナルリング40との間のトラクションにより、インタナルリング40に沿って、回転軸9の周囲を公転する。このとき、遊星ローラ30の公転の回転数は、第1回転数よりも低い第2回転数となる。 The plurality of planetary rollers 30 are always in contact with the sun roller 20, the fixed internal ring 41, and the movable internal ring 42, respectively. A lubricant (not shown) is interposed between the sun roller 20 and the planetary roller 30. Thereby, traction is generated between the sun roller 20 and the planetary roller 30. A lubricant (not shown) is interposed between the planetary roller 30 and the internal ring 40. As a result, traction is generated between the planetary roller 30 and the internal ring 40. When the sun roller 20 is rotated by the driving force of the motor 11, the plurality of planetary rollers 30 receive power from the sun roller 20 and rotate by traction with the sun roller 20. Further, the plurality of planetary rollers 30 revolve around the rotating shaft 9 along the internal ring 40 by traction with the internal ring 40. At this time, the revolution speed of the planetary roller 30 is a second rotational speed lower than the first rotational speed.
 複数の遊星ローラ30が減速後の第2回転数で公転すると、それに伴い、キャリア50も、回転軸9を中心として、第2回転数で回転する。また、キャリア50が回転すると、キャリア50に固定された出力軸90も、回転軸9を中心として、第2回転数で回転する。これにより、モータ11の第1回転数の回転運動は、第1回転数よりも低い第2回転数の回転運動に変換されて、出力軸90に出力される。 When the plurality of planetary rollers 30 revolve at the second rotational speed after deceleration, the carrier 50 also rotates at the second rotational speed around the rotation shaft 9. When the carrier 50 is rotated, the output shaft 90 fixed to the carrier 50 is also rotated at the second rotation speed around the rotation shaft 9. Thereby, the rotational motion at the first rotational speed of the motor 11 is converted into the rotational motion at the second rotational speed that is lower than the first rotational speed, and is output to the output shaft 90.
 次に、第2実施形態に係る電動機付き減速機10Aおよびトラクション減速機1Aについて説明する。図6は、第2実施形態に係るトラクション減速機1Aを含む電動機付き減速機の縦断面図である。図7は、第2実施形態に係るトラクション減速機1Aの、図6のD-D断面図である。図8は、第2実施形態に係るトラクション減速機1Aの、図6のE-E断面図である。 Next, a reduction gear 10A with an electric motor and a traction reduction gear 1A according to a second embodiment will be described. FIG. 6 is a longitudinal sectional view of a reduction gear with an electric motor including a traction reduction gear 1A according to the second embodiment. FIG. 7 is a DD cross-sectional view of FIG. 6 of the traction reducer 1A according to the second embodiment. FIG. 8 is a cross-sectional view taken along the line EE of FIG. 6 of the traction reducer 1A according to the second embodiment.
 この電動機付き減速機10Aは、第1実施形態に係る電動機付き減速機10と同様に、モータ11Aから得られる第1回転数の回転運動を、第1回転数よりも低い第2回転数の回転運動に変換して、出力軸90Aを回転させる減速機である。 Similar to the reduction gear with motor 10 according to the first embodiment, this reduction gear with motor 10A rotates the rotation motion at the first rotation speed obtained from the motor 11A at the second rotation speed lower than the first rotation speed. It is a speed reducer that converts the motion to rotate the output shaft 90A.
 図6に示すように、本実施形態のトラクション減速機1Aは、1つの太陽ローラ20A、複数の遊星ローラ30A、インタナルリング40A、キャリア50A、キャリア軸受60A、弾性部材70A、ハウジング80Aおよび出力軸90Aを有する。 As shown in FIG. 6, the traction reduction gear 1A of this embodiment includes one sun roller 20A, a plurality of planetary rollers 30A, an internal ring 40A, a carrier 50A, a carrier bearing 60A, an elastic member 70A, a housing 80A, and an output shaft. 90A.
 太陽ローラ20Aは、回転軸9Aと同軸に配置された、円柱状の部材である。太陽ローラ20Aは、軸方向の入力側に位置するモータ11Aに連結される。モータ11Aを駆動させると、太陽ローラ20Aは、モータ11Aから受ける動力によって、回転軸9Aを中心として第1回転数で回転する。 The sun roller 20A is a columnar member arranged coaxially with the rotating shaft 9A. The sun roller 20A is connected to a motor 11A located on the input side in the axial direction. When the motor 11A is driven, the sun roller 20A rotates at the first rotation speed around the rotation shaft 9A by the power received from the motor 11A.
 複数の遊星ローラ30Aは、それぞれ円板部31Aと、一対の軸部32Aとを有する。円板部31Aは、太陽ローラ20Aの周囲に、軸方向の入力側から見た中心と軸方向の出力側から見た中心とを結ぶ直線が、回転軸9Aに対して平行となるように配置される。図6および図7に示すように、円板部31Aの外周部は、太陽ローラ20Aの外周部と接触する。一対の軸部32Aは、円板部31Aの中央から軸方向の入力側および出力側に回転軸9Aと平行に延びる。各軸部32Aは、軸方向の円板部31Aとは反対側の端部に、円環状の傾斜面33Aを有する。傾斜面33Aは、軸部32Aの先端へ向かうにつれて縮径するように、軸方向に対して傾斜する。なお、円板部31Aは、軸方向から見たときに外周が円形であればよく、表面形状は板状以外の形状であってもよい。 Each of the plurality of planetary rollers 30A has a disk portion 31A and a pair of shaft portions 32A. The disc portion 31A is arranged around the sun roller 20A so that a straight line connecting the center viewed from the axial input side and the center viewed from the axial output side is parallel to the rotation shaft 9A. Is done. As shown in FIGS. 6 and 7, the outer peripheral portion of the disc portion 31A is in contact with the outer peripheral portion of the sun roller 20A. The pair of shaft portions 32A extends parallel to the rotation shaft 9A from the center of the disc portion 31A to the input side and output side in the axial direction. Each shaft portion 32A has an annular inclined surface 33A at the end opposite to the axial disk portion 31A. The inclined surface 33A is inclined with respect to the axial direction so as to decrease in diameter toward the tip of the shaft portion 32A. The disk portion 31A only needs to have a circular outer periphery when viewed from the axial direction, and the surface shape may be other than a plate shape.
 インタナルリング40Aは、複数の遊星ローラ30Aに接触する一対の円環状の部材である。本実施形態のインタナルリング40Aは、固定インタナルリング41Aおよび可動インタナルリング42Aによって構成される。図6に示すように、本実施形態の固定インタナルリング41Aは、円板部31Aよりも軸方向の出力側に位置し、軸方向の位置が固定されている。また、可動インタナルリング42Aは、円板部31Aよりも軸方向の入力側に位置し、軸方向に移動可能となっている。 The internal ring 40A is a pair of annular members that are in contact with the plurality of planetary rollers 30A. The internal ring 40A of the present embodiment includes a fixed internal ring 41A and a movable internal ring 42A. As shown in FIG. 6, the fixed internal ring 41A of the present embodiment is positioned on the output side in the axial direction from the disk portion 31A, and the position in the axial direction is fixed. The movable internal ring 42A is positioned on the input side in the axial direction with respect to the disc portion 31A, and is movable in the axial direction.
 複数の遊星ローラ30Aは、太陽ローラ20Aおよびインタナルリング40Aによって、太陽ローラ20Aの周囲で回動自在に支持される。また、複数の遊星ローラ30Aの外周部は、インタナルリング40Aの内周部と接触する。このため、太陽ローラ20Aが回転軸9Aを中心に回転すると、複数の遊星ローラ30Aは、太陽ローラ20Aから動力を受ける。そして、複数の遊星ローラ30Aは、太陽ローラ20Aの周囲で、自転しながら回転軸9Aを中心として公転する。本実施形態のインタナルリング40Aは、第1実施形態と同様に、軸部32Aの傾斜面33Aと接触する。 The plurality of planetary rollers 30A are rotatably supported around the sun roller 20A by the sun roller 20A and the internal ring 40A. Further, the outer peripheral portions of the plurality of planetary rollers 30A are in contact with the inner peripheral portion of the internal ring 40A. For this reason, when the sun roller 20A rotates around the rotation shaft 9A, the plurality of planetary rollers 30A receive power from the sun roller 20A. The plurality of planetary rollers 30A revolve around the rotating shaft 9A while rotating around the sun roller 20A. The internal ring 40A of this embodiment is in contact with the inclined surface 33A of the shaft portion 32A, as in the first embodiment.
 キャリア50Aは、複数の遊星ローラ30Aを保持しつつ回転軸9Aを中心として回転する。本実施形態のキャリア50Aは、二つの第1キャリア部材511A,512A、第2キャリア部材52Aおよび複数のキャリアポール53Aを有する。 The carrier 50A rotates around the rotation shaft 9A while holding the plurality of planetary rollers 30A. The carrier 50A of the present embodiment has two first carrier members 511A and 512A, a second carrier member 52A, and a plurality of carrier poles 53A.
 第1キャリア部材51Aは、接触面54Aを有する円板状の部材である。図6および図8に示すように、二つのうち一方の第1キャリア部材511Aは、遊星ローラ30Aの軸方向の出力側の軸部32Aの外周面の少なくとも一部と、接触面54Aを介して、回転軸9Aを中心とする周方向に接触する。また、他方の第1キャリア部材512Aは、遊星ローラ30Aの軸方向の入力側の軸部32Aの外周面の少なくとも一部と、接触面54Aを介して、回転軸9Aを中心とする周方向に接触する。これにより、各遊星ローラ30Aは、太陽ローラ20Aの周囲で、自転可能に支持される。第2キャリア部材52Aは、第1キャリア部材511A,512A、および遊星ローラ30Aよりも軸方向の出力側に配置される。 The first carrier member 51A is a disk-shaped member having a contact surface 54A. As shown in FIGS. 6 and 8, one of the two first carrier members 511A has at least part of the outer peripheral surface of the shaft portion 32A on the output side in the axial direction of the planetary roller 30A and the contact surface 54A. The contact is made in the circumferential direction around the rotating shaft 9A. The other first carrier member 512A is arranged in the circumferential direction centering on the rotating shaft 9A via at least a part of the outer circumferential surface of the shaft portion 32A on the input side in the axial direction of the planetary roller 30A and the contact surface 54A. Contact. Thereby, each planetary roller 30A is supported so that it can rotate around the sun roller 20A. The second carrier member 52A is disposed on the output side in the axial direction with respect to the first carrier members 511A and 512A and the planetary roller 30A.
 キャリアポール53Aは、軸方向に延びる円柱状の部材である。図7に示すように、本実施形態では、3個のキャリアポール53Aが、太陽ローラ20Aの周囲かつ遊星ローラ30Aの間に、周方向に等間隔に配置されている。キャリアポール53Aの軸方向の入力側の端部は、第1キャリア部材51Aに固定される。また、キャリアポール53Aの軸方向の出力側の端部は、第2キャリア部材52Aに固定される。これにより、第1キャリア部材51Aおよび第2キャリア部材52Aは、遊星ローラ30Aの回転に伴い、回転軸9Aを中心として回転する。 The carrier pole 53A is a columnar member extending in the axial direction. As shown in FIG. 7, in this embodiment, three carrier poles 53A are arranged at equal intervals in the circumferential direction around the sun roller 20A and between the planetary rollers 30A. The end portion on the input side in the axial direction of the carrier pole 53A is fixed to the first carrier member 51A. Further, the end on the output side in the axial direction of the carrier pole 53A is fixed to the second carrier member 52A. As a result, the first carrier member 51A and the second carrier member 52A rotate around the rotation shaft 9A as the planetary roller 30A rotates.
 キャリア軸受60Aは、第2キャリア部材52Aを、回転軸9Aを中心に回転可能に支持する。図6に示すように、本実施形態のキャリア軸受60Aは、キャリア50Aの外周面の少なくとも一部と接触する。さらに、キャリア軸受60Aは、キャリア50Aの軸方向の出力側の端面と接触する。これにより、キャリア50Aは、径方向および軸方向の移動が規制され、安定的に保持される。 The carrier bearing 60A supports the second carrier member 52A so as to be rotatable about the rotation shaft 9A. As shown in FIG. 6, the carrier bearing 60A of the present embodiment is in contact with at least a part of the outer peripheral surface of the carrier 50A. Furthermore, the carrier bearing 60A is in contact with the end face on the output side in the axial direction of the carrier 50A. Thereby, the carrier 50A is restricted from moving in the radial direction and the axial direction, and is stably held.
 弾性部材70Aは、可動インタナルリング42Aを軸方向の出力側へ加圧する機構である。弾性部材70Aは、軸方向に伸縮する円環状の部材である。弾性部材70には、例えば、ウェーブばねが用いられる。弾性部材70Aは、取付板12Aと可動インタナルリング42Aとの間に、自然長よりも軸方向に圧縮された状態で配置される。このため、弾性部材70Aの反発力によって、可動インタナルリング42Aが、出力側へ加圧される。可動インタナルリング42Aが軸方向の出力側へ加圧されると、軸部32Aは傾斜面33Aを介して、径方向内側に向けて押圧力を受ける。すなわち、複数の遊星ローラ30Aは、固定インタナルリング41Aおよび可動インタナルリング42Aによって、径方向内側に加圧される。 The elastic member 70A is a mechanism that pressurizes the movable internal ring 42A toward the output side in the axial direction. The elastic member 70A is an annular member that expands and contracts in the axial direction. For the elastic member 70, for example, a wave spring is used. The elastic member 70A is disposed between the mounting plate 12A and the movable internal ring 42A in a state compressed in the axial direction rather than the natural length. For this reason, the movable internal ring 42A is pressurized toward the output side by the repulsive force of the elastic member 70A. When the movable internal ring 42A is pressurized toward the output side in the axial direction, the shaft portion 32A receives a pressing force toward the radially inner side via the inclined surface 33A. That is, the plurality of planetary rollers 30A are pressed radially inward by the fixed internal ring 41A and the movable internal ring 42A.
 ハウジング80Aは、少なくとも、太陽ローラ20A、複数の遊星ローラ30A、一対のインタナルリング40A、キャリア50Aおよびキャリア軸受60Aを内部に収容する部材である。 The housing 80A is a member that accommodates at least the sun roller 20A, the plurality of planetary rollers 30A, the pair of internal rings 40A, the carrier 50A, and the carrier bearing 60A.
 出力軸90Aは、回転軸9Aに沿って軸方向の出力側に延びる円柱状の部材である。出力軸90Aは、第2キャリア部材52Aの中央に設けられた貫通孔55Aに、例えば、圧入されることで固定される。出力軸90Aは、第2キャリア部材52Aとともに回転軸9Aを中心に回転する。 The output shaft 90A is a columnar member that extends to the output side in the axial direction along the rotation shaft 9A. The output shaft 90A is fixed, for example, by being press-fitted into a through hole 55A provided in the center of the second carrier member 52A. The output shaft 90A rotates around the rotation shaft 9A together with the second carrier member 52A.
 図6に示すように、本実施形態のインタナルリング40Aは、外周面の一部分に非真円である複数の第1回り止め部43Aを有する。また、本実施形態のハウジング80Aは、内周面の一部分に非真円である複数の第2回り止め部82Aを有する。複数の第1回り止め部43Aは、回転軸9Aを中心とする周方向に等間隔に配置される。複数の第2回り止め部82Aは、回転軸9Aを中心とする周方向に等間隔に配置される。そして、第1回り止め部43Aは、第2回り止め部82Aと接触する。これにより、ハウジング80Aに対するキャリア50Aの周方向の位置決めを容易にできる。その結果、トラクション減速機1Aを容易に組み立てることができる。また、ハウジング80Aに対するインタナルリング40Aの相対回転を防止できる。その結果、遊星ローラ30Aおよびキャリア50Aの回転が安定する。 As shown in FIG. 6, the internal ring 40 </ b> A of the present embodiment has a plurality of first detent portions 43 </ b> A that are non-circular on a part of the outer peripheral surface. Further, the housing 80A of the present embodiment has a plurality of second anti-rotation portions 82A that are non-circular on a part of the inner peripheral surface. The plurality of first detent portions 43A are arranged at equal intervals in the circumferential direction around the rotation shaft 9A. The plurality of second anti-rotation portions 82A are arranged at equal intervals in the circumferential direction around the rotation shaft 9A. The first detent portion 43A comes into contact with the second detent portion 82A. Thereby, the circumferential positioning of the carrier 50A with respect to the housing 80A can be facilitated. As a result, the traction reduction gear 1A can be easily assembled. Further, relative rotation of the internal ring 40A with respect to the housing 80A can be prevented. As a result, the rotation of the planetary roller 30A and the carrier 50A is stabilized.
 複数の遊星ローラ30Aは、それぞれ、太陽ローラ20A、固定インタナルリング41Aおよび可動インタナルリング42Aと、常に接触する。そして、太陽ローラ20Aと遊星ローラ30Aとの間には図示を省略した潤滑剤が介在する。これにより、太陽ローラ20Aと遊星ローラ30Aとの間にはトラクションが発生する。また、遊星ローラ30Aとインタナルリング40Aとの間には図示を省略した潤滑剤が介在する。これにより、遊星ローラ30とインタナルリング40との間にはトラクションが発生する。モータ11Aの駆動力により、太陽ローラ20Aが回転すると、複数の遊星ローラ30Aは、太陽ローラ20Aからの動力を受け、太陽ローラ20Aとの間のトラクションによって自転する。また、複数の遊星ローラ30Aは、インタナルリング40Aとの間のトラクションにより、インタナルリング40Aに沿って、回転軸9Aの周囲を公転する。このとき、遊星ローラ30Aの公転の回転数は、第1回転数よりも低い第2回転数となる。 The plurality of planetary rollers 30A are always in contact with the sun roller 20A, the fixed internal ring 41A, and the movable internal ring 42A, respectively. A lubricant (not shown) is interposed between the sun roller 20A and the planetary roller 30A. Thereby, traction is generated between the sun roller 20A and the planetary roller 30A. A lubricant (not shown) is interposed between the planetary roller 30A and the internal ring 40A. As a result, traction is generated between the planetary roller 30 and the internal ring 40. When the sun roller 20A is rotated by the driving force of the motor 11A, the plurality of planetary rollers 30A receives power from the sun roller 20A and rotates by traction with the sun roller 20A. The plurality of planetary rollers 30A revolve around the rotating shaft 9A along the internal ring 40A by traction with the internal ring 40A. At this time, the revolution speed of the planetary roller 30 </ b> A is a second rotational speed lower than the first rotational speed.
 複数の遊星ローラ30Aが減速後の第2回転数で公転すると、それに伴い、第1キャリア部材51Aとともに、キャリアポール53Aに固定された第2キャリア部材52Aも、回転軸9Aを中心として、第2回転数で回転する。そして、第2キャリア部材52Aに固定された出力軸90Aも、回転軸9Aを中心として、第2回転数で回転する。これにより、モータの第1回転数の回転運動は、第1回転数よりも低い第2回転数の回転運動に変換されて、出力軸90Aに出力される。 When the plurality of planetary rollers 30A revolves at the second rotational speed after deceleration, the second carrier member 52A fixed to the carrier pole 53A together with the first carrier member 51A also has the second center around the rotation shaft 9A. Rotates at the number of revolutions. The output shaft 90A fixed to the second carrier member 52A also rotates at the second rotation speed about the rotation shaft 9A. Thereby, the rotational motion at the first rotational speed of the motor is converted into the rotational motion at the second rotational speed lower than the first rotational speed, and is output to the output shaft 90A.
 次に、第3実施形態に係る電動機付き減速機10Bおよびトラクション減速機1Bについて説明する。図9は、第3実施形態に係るトラクション減速機1Bを含む電動機付き減速機10Bの部分縦断面図である。なお、以下では、第1実施形態との相違点を中心に説明し、第1実施形態と同等の部分については、重複説明を省略する。 Next, a reduction gear 10B with an electric motor and a traction reduction gear 1B according to a third embodiment will be described. FIG. 9 is a partial longitudinal sectional view of a reduction gear 10B with an electric motor including a traction reduction gear 1B according to the third embodiment. In the following description, differences from the first embodiment will be mainly described, and redundant description of parts equivalent to those of the first embodiment will be omitted.
 この電動機付き減速機10Bは、第1実施形態に係る電動機付き減速機10と同様に、モータ(図示省略)から得られる第1回転数の回転運動を、第1回転数よりも低い第2回転数の回転運動に変換して、出力軸90Bを回転させる減速機である。 This reduction gear 10B with an electric motor, like the reduction gear 10 with an electric motor according to the first embodiment, performs a rotational motion at a first rotational speed obtained from a motor (not shown) in a second rotation lower than the first rotational speed. This is a speed reducer that converts the rotational motion into a number and rotates the output shaft 90B.
 図9に示すように、本実施形態のトラクション減速機1Bのキャリア軸受60Bは、第1ラジアル軸受面110Bおよび第2ラジアル軸受面111Bを含む複数のラジアル軸受面を有している。第1ラジアル軸受面110Bおよび第2ラジアル軸受面111Bは、各々回転軸9Bを中心とした周方向に円環状に広がり、互いに軸方向に離れている。第1ラジアル軸受面110Bは、第2ラジアル軸受面111Bよりも、軸方向の入力側かつ径方向外側に位置する。キャリア軸受60Bは、当該第1ラジアル軸受面110Bおよび第2ラジアル軸受面111Bにおいてキャリア50Bの外周面に接触し、キャリア50Bを回転可能に支持する。なお、複数のラジアル軸受面は3つ以上のラジアル軸受面から構成されてもよい。 As shown in FIG. 9, the carrier bearing 60B of the traction reduction gear 1B according to the present embodiment has a plurality of radial bearing surfaces including a first radial bearing surface 110B and a second radial bearing surface 111B. The first radial bearing surface 110B and the second radial bearing surface 111B each extend in an annular shape in the circumferential direction around the rotating shaft 9B, and are separated from each other in the axial direction. The first radial bearing surface 110B is located on the input side in the axial direction and on the outer side in the radial direction than the second radial bearing surface 111B. The carrier bearing 60B is in contact with the outer peripheral surface of the carrier 50B at the first radial bearing surface 110B and the second radial bearing surface 111B, and rotatably supports the carrier 50B. The plurality of radial bearing surfaces may be composed of three or more radial bearing surfaces.
 第1ラジアル軸受面110Bと第2ラジアル軸受面111Bとの間には、空間120Bが形成される。空間120Bは、後述するグリースを溜める役割を果たし、これにより、出力軸90B側からのグリースの漏れが抑制される。また、互いに軸方向に離れた第1ラジアル軸受面110Bと第2ラジアル軸受面111Bとでキャリア50Bを支持するので、キャリア50Bが、傾いた状態で回転することを防止できる。 A space 120B is formed between the first radial bearing surface 110B and the second radial bearing surface 111B. The space 120B plays a role of storing grease to be described later, thereby suppressing leakage of grease from the output shaft 90B side. Further, since the carrier 50B is supported by the first radial bearing surface 110B and the second radial bearing surface 111B that are axially separated from each other, the carrier 50B can be prevented from rotating in an inclined state.
 なお、キャリア軸受60Bの内周面は、軸方向に対して垂直または斜めに拡がる環状の軸受段差面600Bを有する。また、キャリア50Bの外周面は、軸方向に対して垂直または斜めに拡がる環状のキャリア段差面500Bを有する。軸受段差面600Bとキャリア段差面500Bとは、少なくとも一部において軸方向に対向する。上述の空間120Bは、軸受段差面600B、キャリア段差面500B、キャリア軸受60Bの内周面における軸方向に対して平行に広がる環状の面、およびキャリア50Bの外周面における軸方向に対して平行に広がる環状の面によって形成される。 The inner peripheral surface of the carrier bearing 60B has an annular bearing step surface 600B that extends perpendicularly or obliquely to the axial direction. In addition, the outer peripheral surface of the carrier 50B has an annular carrier step surface 500B that extends perpendicularly or obliquely to the axial direction. The bearing step surface 600B and the carrier step surface 500B are opposed in the axial direction at least in part. The above-described space 120B is parallel to the bearing step surface 600B, the carrier step surface 500B, the annular surface extending in parallel to the axial direction on the inner peripheral surface of the carrier bearing 60B, and the axial direction on the outer peripheral surface of the carrier 50B. Formed by an expanding annular surface.
 さらに、第1ラジアル軸受面110Bは、少なくとも軸受段差面600Bとキャリア段差面500Bよりも軸方向の入力側に位置し、第2ラジアル軸受面111Bは、少なくとも軸受段差面600Bとキャリア段差面500Bよりも軸方向の出力側に位置する。すなわち、第1ラジアル軸受面110Bと第2ラジアル軸受面111Bとは、軸受段差面600Bとキャリア段差面500Bよりも軸方向の外側に位置する。これにより、キャリア50Bおよびキャリア軸受60Bの構造を、過剰に複雑化することなく、空間120Bを容易に形成することができる。ただし、第1ラジアル軸受面110Bと第2ラジアル軸受面111Bとの軸方向における位置関係は、逆であってもよい。 Furthermore, the first radial bearing surface 110B is positioned at least on the input side in the axial direction from the bearing step surface 600B and the carrier step surface 500B, and the second radial bearing surface 111B is formed from at least the bearing step surface 600B and the carrier step surface 500B. Is also located on the axial output side. That is, the first radial bearing surface 110B and the second radial bearing surface 111B are located on the outer side in the axial direction from the bearing step surface 600B and the carrier step surface 500B. Thereby, the space 120B can be easily formed without excessively complicating the structures of the carrier 50B and the carrier bearing 60B. However, the positional relationship in the axial direction between the first radial bearing surface 110B and the second radial bearing surface 111B may be reversed.
 複数の遊星ローラ30Bと、太陽ローラ(図示省略)およびインタナルリング40Bの少なくとも1つとの間には、潤滑剤として第1のグリースが封入されていることが望ましい。この場合、空間120Bには第1のグリースの粘度よりも高い粘度の第2のグリースが封入されていること望ましい(図示省略)。これにより、トラクション減速機1B内の第1のグリースが出力軸90B側に流動して漏出することを、第2のグリースにより防止できる。なお、空間120Bは、複数のラジアル軸受面のうちの少なくとも2つの間に形成される空間であればよく、第1ラジアル軸受面110Bと第2ラジアル軸受面111Bとは別のラジアル軸受面の間に形成される空間であってもよい。 It is desirable that a first grease is sealed as a lubricant between the plurality of planetary rollers 30B and at least one of the sun roller (not shown) and the internal ring 40B. In this case, it is desirable that a second grease having a viscosity higher than that of the first grease is enclosed in the space 120B (not shown). Thereby, it is possible to prevent the first grease in the traction reduction gear 1B from flowing and leaking to the output shaft 90B side by the second grease. Note that the space 120B may be a space formed between at least two of the plurality of radial bearing surfaces, and is between the radial bearing surfaces different from the first radial bearing surface 110B and the second radial bearing surface 111B. It may be a space formed.
 以上、本発明の例示的な実施形態について説明したが、本発明は上記の実施形態には限定されない。 The exemplary embodiments of the present invention have been described above, but the present invention is not limited to the above embodiments.
 上記の実施形態の、電動機付き減速機およびトラクション減速機は、電化製品の精密部品に使用されるものであった。しかしながら、本発明のトラクション減速機および電動機付き減速機は、産業用機械等の他の用途に使用されるものであってもよい。 In the above embodiment, the reduction gear with motor and the traction reduction gear were used for precision parts of electrical appliances. However, the traction reduction gear and the reduction gear with electric motor of the present invention may be used for other applications such as industrial machinery.
 また、上記の実施形態では、太陽ローラの周囲に、3個の遊星ローラが周方向に等間隔に配置されていた。しかしながら、トラクション減速機が有する遊星ローラの数は、2個であってもよく、4個以上であってもよい。 In the above embodiment, three planetary rollers are arranged at equal intervals in the circumferential direction around the sun roller. However, the number of planetary rollers included in the traction reducer may be two or four or more.
 また、上記の実施形態では、弾性部材は、軸方向に伸縮する円環状の部材であった。しかしながら、弾性部材は、軸方向に反発力を発生させるものであればよく、例えば、複数のコイルばねを周方向に等間隔に配列したものであってもよく、他の部材により構成されるものであってもよい。 In the above embodiment, the elastic member is an annular member that expands and contracts in the axial direction. However, the elastic member only needs to generate a repulsive force in the axial direction. For example, a plurality of coil springs may be arranged at equal intervals in the circumferential direction, and may be constituted by other members. It may be.
 また、上記の第2実施形態では、3個のキャリアポールが、太陽ローラの周囲かつ遊星ローラの間に、周方向に等間隔に配置されていた。しかしながら、キャリアポールの数は、2個であってもよく、4個以上であってもよい。 In the second embodiment, three carrier poles are arranged at equal intervals in the circumferential direction around the sun roller and between the planetary rollers. However, the number of carrier poles may be two or four or more.
 ホイールイン減速装置を構成する各部材の材料には、例えば、高強度の金属を用いればよい。ただし、各部材の材料は、使用時の負荷に耐え得る材料であればよく、必ずしも金属には限定されない。軽量化のために、一部の部材の材料に樹脂を用いてもよい。 For example, a high-strength metal may be used as the material of each member constituting the wheel-in speed reducer. However, the material of each member is not limited to metal as long as it can withstand the load during use. In order to reduce the weight, a resin may be used as the material of some members.
 また、トラクション減速機および電動機付き減速機の細部の形状については、本願の各図に示された形状と相違していてもよい。また、上記の実施形態および変形例に登場した各要素を、矛盾が生じない範囲で、適宜に組み合わせてもよい。 Further, the shape of the details of the traction reducer and the reduction gear with an electric motor may be different from the shapes shown in the drawings of the present application. Moreover, you may combine suitably each element which appeared in said embodiment and modification in the range which does not produce inconsistency.
 本発明は、トラクション減速機および電動機付き減速機に利用できる。 The present invention can be used for a traction speed reducer and a speed reducer with an electric motor.
1,1A,1B トラクション減速機
9,9A,9B 回転軸
10,10A,10B 電動機付き減速機
11,11A モータ
12,12A 取付板
20,20A 太陽ローラ
30,30A,30B 遊星ローラ
31,31A 円板部
32,32A 軸部
33,33A 傾斜面
40,40A,40B インタナルリング
41,41A 固定インタナルリング
42,42A 可動インタナルリング
43,43A 第1回り止め部
50,50A,50B キャリア
511A,512A 第1キャリア部材
52A 第2キャリア部材
53A キャリアポール
54,54A 接触面
55 凹部
55A 貫通孔
56 収容部
60,60A,60B キャリア軸受
70,70A 弾性部材
80,80A ハウジング
81 爪部
82,82A 第2回り止め部
90,90A,90B 出力軸
110B 第1ラジアル軸受面
111B 第2ラジアル軸受面
120B 空間
500B キャリア段差面
600B 軸受段差面
1, 1A, 1B Traction reducer 9, 9A, 9B Rotating shaft 10, 10A, 10B Motor-equipped reducer 11, 11A Motor 12, 12A Mounting plate 20, 20A Sun rollers 30, 30A, 30B Planetary rollers 31, 31A Disc Portions 32, 32A Shaft portions 33, 33A Inclined surfaces 40, 40A, 40B Internal rings 41, 41A Fixed internal rings 42, 42A Movable internal rings 43, 43A First detent portions 50, 50A, 50B Carriers 511A, 512A First carrier member 52A Second carrier member 53A Carrier pole 54, 54A Contact surface 55 Recess 55A Through hole 56 Housing portion 60, 60A, 60B Carrier bearing 70, 70A Elastic member 80, 80A Housing 81 Claw portion 82, 82A Second rotation Stop part 90, 90A, 90B Output shaft 110B First radial bearing surface 111B Second radial bearing surface 120B Space 500B Carrier step surface 600B Bearing step surface

Claims (18)

  1.  トラクション減速機であって、
     回転軸を中心として回転する太陽ローラと、
     前記太陽ローラの周囲に配置された複数の遊星ローラと、
     前記複数の遊星ローラに接触する一対の円環状のインタナルリングと、
     前記遊星ローラを保持しつつ前記回転軸を中心として回転するキャリアと、
    を有し、
     前記複数の遊星ローラは、それぞれ、前記太陽ローラおよび前記インタナルリングの双方に接触しつつ、前記太陽ローラから動力を受けることによって、自転しながら前記回転軸を中心として公転し、
     前記キャリアは、前記遊星ローラの外周面に対向する接触面を有し、
     前記遊星ローラの外周面と、前記接触面とが、前記回転軸を中心とする周方向に接触する。
    A traction reducer,
    A sun roller that rotates about a rotation axis;
    A plurality of planetary rollers disposed around the sun roller;
    A pair of annular internal rings in contact with the plurality of planetary rollers;
    A carrier that rotates about the rotation axis while holding the planetary roller;
    Have
    Each of the plurality of planetary rollers revolves around the rotation axis while rotating by receiving power from the sun roller while contacting both the sun roller and the internal ring.
    The carrier has a contact surface facing the outer peripheral surface of the planetary roller;
    The outer peripheral surface of the planetary roller and the contact surface are in contact with each other in the circumferential direction about the rotation axis.
  2.  請求項1に記載のトラクション減速機であって、
     前記遊星ローラは、
      前記太陽ローラに接触する円板部と、
      前記円板部の中央から軸方向の両側に延びる軸部と、
    を有し、
     前記キャリアの前記接触面は、前記軸部の外周面と周方向に接触する。
    The traction reducer according to claim 1,
    The planetary roller is
    A disk portion in contact with the sun roller;
    A shaft portion extending from the center of the disc portion to both sides in the axial direction;
    Have
    The contact surface of the carrier is in contact with the outer peripheral surface of the shaft portion in the circumferential direction.
  3.  請求項2に記載のトラクション減速機であって、
     前記軸部は、軸方向の前記円板部とは反対側の端部に、軸方向に対して傾斜した円環状の傾斜面を有し、
     前記インタナルリングは、前記傾斜面に接触する。
    The traction reducer according to claim 2,
    The shaft portion has an annular inclined surface inclined with respect to the axial direction at an end opposite to the disk portion in the axial direction,
    The internal ring contacts the inclined surface.
  4.  請求項2または請求項3に記載のトラクション減速機であって、
     前記キャリアは、前記回転軸を中心とする周方向に配列され、各々が径方向外側へ向けて開いた複数の収容部を有し、
     前記収容部に、前記軸部が収容される。
    The traction reducer according to claim 2 or claim 3,
    The carrier is arranged in a circumferential direction centering on the rotation axis, and each of the carriers has a plurality of accommodating portions that are opened outward in the radial direction.
    The shaft portion is housed in the housing portion.
  5.  請求項2に記載のトラクション減速機であって、
     軸方向に伸縮する弾性部材をさらに有し、
     前記軸部は、軸方向に対して傾斜した円環状の傾斜面を有し、
     前記一対のインタナルリングは、
      前記円板部よりも軸方向一方側に位置し、軸方向の位置が固定された固定インタナルリングと、
      前記円板部よりも軸方向他方側に位置し、軸方向に移動可能な可動インタナルリングと、
    を有し、
     前記弾性部材は、前記可動インタナルリングを軸方向一方側に押圧し、
     前記一対のインタナルリングが、前記遊星ローラを径方向内側へ加圧する。
    The traction reducer according to claim 2,
    It further has an elastic member that expands and contracts in the axial direction,
    The shaft portion has an annular inclined surface inclined with respect to the axial direction,
    The pair of internal rings is:
    A fixed internal ring that is positioned on one side in the axial direction from the disk portion and in which the position in the axial direction is fixed;
    A movable internal ring that is located on the other side in the axial direction than the disc part and is movable in the axial direction;
    Have
    The elastic member presses the movable internal ring in one axial direction,
    The pair of internal rings pressurize the planetary roller radially inward.
  6.  請求項5に記載のトラクション減速機であって、
     前記弾性部材は、前記キャリアの径方向外側に位置する。
    The traction reducer according to claim 5,
    The elastic member is located on the radially outer side of the carrier.
  7.  請求項1から請求項6までのいずれか1項に記載のトラクション減速機であって、
     前記太陽ローラは、軸方向の入力側から動力を受け、
     前記キャリアに固定され、前記回転軸に沿って軸方向の前記入力側とは反対の出力側に延びる出力軸をさらに有する。
    The traction reducer according to any one of claims 1 to 6,
    The sun roller receives power from the axial input side,
    It further has an output shaft fixed to the carrier and extending to the output side opposite to the input side in the axial direction along the rotation axis.
  8.  請求項1から請求項7までのいずれか1項に記載のトラクション減速機であって、
     前記キャリアを回転可能に支持するキャリア軸受をさらに有し、
     前記キャリア軸受は、前記キャリアの外周面および軸方向の端面に接触する。
    The traction reducer according to any one of claims 1 to 7,
    A carrier bearing rotatably supporting the carrier;
    The carrier bearing contacts the outer peripheral surface and the axial end surface of the carrier.
  9.  請求項8に記載のトラクション減速機であって、
     前記キャリア軸受は、
      互いに軸方向に離れた、各々が円環状の複数のラジアル軸受面
    を有し、
     前記キャリア軸受は、前記複数のラジアル軸受面において前記キャリアの外周面に接触する。
    The traction reducer according to claim 8,
    The carrier bearing is
    A plurality of radial bearing surfaces, each axially spaced apart, each having an annular shape,
    The carrier bearing is in contact with the outer peripheral surface of the carrier at the plurality of radial bearing surfaces.
  10.  請求項9に記載のトラクション減速機であって、
     前記キャリア軸受は、軸方向に対して垂直または斜めに拡がる環状の軸受段差面を有し、
     前記キャリアは、軸方向に対して垂直または斜めに拡がる環状のキャリア段差面を有し、
     前記軸受段差面と前記キャリア段差面とは、少なくとも一部において軸方向に対向し、
     前記複数のラジアル軸受面は、少なくとも、前記軸受段差面と前記キャリア段差面よりも軸方向一方側、および前記軸受段差面と前記キャリア段差面よりも軸方向他方側に位置する。
    The traction reducer according to claim 9,
    The carrier bearing has an annular bearing step surface that extends perpendicularly or obliquely to the axial direction,
    The carrier has an annular carrier step surface extending perpendicularly or obliquely to the axial direction,
    The bearing step surface and the carrier step surface are at least partially opposed in the axial direction,
    The plurality of radial bearing surfaces are positioned at least on one axial side of the bearing step surface and the carrier step surface and on the other axial side of the bearing step surface and the carrier step surface.
  11.  請求項9または請求項10に記載のトラクション減速機であって、
     前記複数の遊星ローラと、前記太陽ローラおよび前記インタナルリングの少なくとも1つとの間に、第1のグリースを有し、
     前記複数のラジアル軸受面の少なくとも2つの間に形成される空間に、第2のグリースを有し、
     前記第2のグリースの粘度は、前記第1のグリースの粘度よりも高い。
    A traction reducer according to claim 9 or claim 10, wherein
    A first grease between the plurality of planetary rollers and at least one of the sun roller and the internal ring;
    A second grease is provided in a space formed between at least two of the plurality of radial bearing surfaces;
    The viscosity of the second grease is higher than the viscosity of the first grease.
  12.  請求項8に記載のトラクション減速機であって、
     前記インタナルリングを取り囲む円筒状の内周面をもつハウジングをさらに有し、
     前記ハウジングは、径方向内側へ向けて延びる爪部を有し、
     前記爪部は、前記キャリア軸受と軸方向に接触する。
    The traction reducer according to claim 8,
    A housing having a cylindrical inner peripheral surface surrounding the internal ring;
    The housing has a claw portion extending radially inward,
    The claw portion is in axial contact with the carrier bearing.
  13.  請求項12に記載のトラクション減速機であって、
     前記爪部と前記キャリア軸受とが、前記回転軸を中心とする周方向に接触する。
    The traction reducer according to claim 12,
    The claw portion and the carrier bearing are in contact with each other in the circumferential direction around the rotation axis.
  14.  請求項1から請求項8までのいずれか1項に記載のトラクション減速機であって、
     前記インタナルリングを取り囲む円筒状の内周面をもつハウジングをさらに有し、
     前記インタナルリングは、外周面の一部分に非真円の第1回り止め部を有し、
     前記ハウジングは、前記内周面の一部分に非真円の第2回り止め部を有し、
     前記第1回り止め部と前記第2回り止め部とが接触する。
    The traction reducer according to any one of claims 1 to 8,
    A housing having a cylindrical inner peripheral surface surrounding the internal ring;
    The internal ring has a first non-circular first detent on a part of the outer peripheral surface;
    The housing has a non-circular second detent on a part of the inner peripheral surface,
    The first detent portion and the second detent portion come into contact with each other.
  15.  請求項14に記載のトラクション減速機であって、
     前記インタナルリングは、前記回転軸を中心とする周方向に等間隔に配置された複数の前記第1回り止め部を有し、
     前記ハウジングは、前記回転軸を中心とする周方向に等間隔に配置された複数の前記第2回り止め部を有する。
    The traction reducer according to claim 14,
    The internal ring has a plurality of the first detent portions arranged at equal intervals in the circumferential direction around the rotation axis,
    The housing has a plurality of the second detent portions arranged at equal intervals in the circumferential direction around the rotation shaft.
  16.  請求項1から請求項15までのいずれか1項に記載のトラクション減速機であって、
     前記キャリアは、単一の部材である。
    A traction reducer according to any one of claims 1 to 15,
    The carrier is a single member.
  17.  請求項1から請求項15までのいずれか1項に記載のトラクション減速機であって、
     前記キャリアは、
      前記接触面を有する円板状の第1キャリア部材と、
      前記第1キャリア部材とは異なる軸方向位置に配置された第2キャリア部材と、
      軸方向に延びるキャリアポールと、
    を有し、
     前記キャリアポールの軸方向の一端は、前記第1キャリア部材に固定され、
     前記キャリアポールの軸方向の他端は、前記第2キャリア部材に固定される。
    A traction reducer according to any one of claims 1 to 15,
    The carrier is
    A disc-shaped first carrier member having the contact surface;
    A second carrier member disposed at an axial position different from the first carrier member;
    A carrier pole extending in the axial direction;
    Have
    One end of the carrier pole in the axial direction is fixed to the first carrier member,
    The other end of the carrier pole in the axial direction is fixed to the second carrier member.
  18.  請求項1から請求項17までのいずれか1項に記載のトラクション減速機と、
     前記回転軸を中心として前記太陽ローラを回転させる電動機と、
    を有する、電動機付き減速機。
    A traction reducer according to any one of claims 1 to 17,
    An electric motor that rotates the sun roller around the rotation axis;
    A reduction gear with an electric motor.
PCT/JP2017/018327 2016-05-16 2017-05-16 Traction speed reducer and electric motor–equipped speed reducer WO2017199941A1 (en)

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JPS5941631Y2 (en) * 1976-10-06 1984-12-01 日本無線株式会社 Dial device with display panel
JPS6237561A (en) * 1985-08-09 1987-02-18 Matsushita Electric Works Ltd Reduction gear
JP2000065165A (en) * 1998-08-20 2000-03-03 Namiki Precision Jewel Co Ltd Planetary gear speed reducer and assembling method therefor
JP2000130529A (en) * 1998-10-28 2000-05-12 Ntn Corp Friction type multistage roller transmission
JP2002171721A (en) * 2000-12-01 2002-06-14 Nidec-Shimpo Corp Rotating drive unit
JP2016034223A (en) * 2014-07-31 2016-03-10 日本電産シンポ株式会社 Traction power transmission reduction gear and motor with reduction gear

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5941631Y2 (en) * 1976-10-06 1984-12-01 日本無線株式会社 Dial device with display panel
JPS54140153U (en) * 1978-03-24 1979-09-28
JPS6237561A (en) * 1985-08-09 1987-02-18 Matsushita Electric Works Ltd Reduction gear
JP2000065165A (en) * 1998-08-20 2000-03-03 Namiki Precision Jewel Co Ltd Planetary gear speed reducer and assembling method therefor
JP2000130529A (en) * 1998-10-28 2000-05-12 Ntn Corp Friction type multistage roller transmission
JP2002171721A (en) * 2000-12-01 2002-06-14 Nidec-Shimpo Corp Rotating drive unit
JP2016034223A (en) * 2014-07-31 2016-03-10 日本電産シンポ株式会社 Traction power transmission reduction gear and motor with reduction gear

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