transaxle

The transaxle design addresses oil splashing issues by using guide protrusions and oil holes to efficiently lubricate pinion gears, ensuring consistent lubrication and preventing oil shortages.

JP7729282B2Active Publication Date: 2025-08-26TOYOTA JIDOSHA KK
View PDF 7 Cites 0 Cited by

Patent Information

Application Number
JP2022123997
Authority / Receiving Office
JP · JP
Patent Type
Patents
Current Assignee / Owner
Filing Date
2022-08-03
Publication Date
2025-08-26
Estimated Expiration
2042-08-03

AI Technical Summary

Technical Problem

The rotation of components in a transaxle causes oil inside the axle case to splash, leading to a shortage of lubrication in certain areas, particularly around the support holes of the pinion gears.

Method used

A transaxle design featuring a carrier with guide protrusions and oil holes that collect and direct splashed oil to the pinion gears using centrifugal force, ensuring efficient lubrication.

Benefits of technology

The solution effectively guides oil to the pinion gears, maintaining adequate lubrication and preventing oil shortages, thereby enhancing the transaxle's operational efficiency.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure 0007729282000001
    Figure 0007729282000001
  • Figure 0007729282000002
    Figure 0007729282000002
Patent Text Reader

Abstract

To efficiently guide oil to a pinion gear.SOLUTION: A transaxle 100 comprises a sun gear, a plurality of pinion gears, a ring gear, a carrier 70, and an axle case. The carrier 70 comprises a carrier body 72 and guide protrusions 75. Further, the carrier body 72 comprises support holes and oil holes 72B. The support holes extend in a direction along the rotation axis 100Z and support a portion of the pinion gear including the right end. The oil hole 72B extends from the support hole to the right. The guide protrusion 75 protrudes from the right end surface of the carrier body 72. The guide protrusion 75 comprises a recess 77. The oil hole 72B is open at a location connected to an inner edge 77A of the recess 77. When viewed from the direction along the rotational axis 100Z, the inner edge 77A has a distance from the rotational axis 100Z, which becomes larger as the inner edge approaches the oil hole 72B.SELECTED DRAWING: Figure 2
Need to check novelty before this filing date? Find Prior Art

Description

[Technical Field]

[0001] The present invention relates to a transaxle. [Background technology]

[0002] The transaxle of Patent Document 1 includes a sun gear, multiple pinion gears, a ring gear, a carrier, a differential gear, and an axle case. The sun gear is rotatable. The pinion gear meshes with both the sun gear and the ring gear. The pinion gear is capable of revolving around the sun gear. The carrier includes multiple support holes. Each support hole penetrates the carrier in a direction along the rotation axis of the carrier. The carrier supports the pinion gear inside the support hole. The pinion gear is rotatable within the support hole. The carrier is rotatable coaxially with the sun gear as the pinion gear revolves. The differential gear is connected to the carrier. The differential gear is rotatable together with the carrier. The axle case houses the sun gear, multiple pinion gears, the ring gear, the carrier, and the differential gear. The axle case also stores oil. [Prior art documents] [Patent documents]

[0003] [Patent Document 1] Patent Publication No. 2021-110374 Summary of the Invention [Problem to be solved by the invention]

[0004] In a transaxle such as that described in Patent Document 1, the rotation of the carrier and other components causes oil inside the axle case to splash. When some of the splashed oil reaches the support hole, it lubricates the area between the inner circumferential surface of the support hole and the outer circumferential surface of the pinion gear, for example. However, if oil splashes as the carrier and other components rotate, it can lead to a shortage of oil in certain locations inside the axle case. Therefore, a structure is needed that can efficiently guide the oil circulating and splashing inside the axle case to gears that require lubrication. [Means for solving the problem]

[0005] A transaxle for solving the above problem includes a sun gear that rotates about a rotation axis, a plurality of pinion gears that mesh with the sun gear and revolve around the sun gear, a ring gear that meshes with the pinion gears, a carrier that rotatably supports the pinion gears and rotates coaxially with the sun gear in accordance with the revolution of the pinion gears, and an axle case that houses the sun gear, the pinion gears, the ring gear, and the carrier, wherein the carrier includes a carrier body that supports a portion including an end of the pinion gear. and a guide protrusion protruding from the carrier body on the side opposite to the pinion gear, the carrier body having a support hole extending in a direction along the rotation axis and supporting a portion including the end of the pinion gear, and an oil hole extending from the support hole on the side opposite to the pinion gear, when viewed in a direction along the rotation axis, if the edge of the guide protrusion on the rotation axis side is considered to be the inner edge, the oil hole opens at a point connected to the inner edge, and when viewed in a direction along the rotation axis, the distance from the rotation axis of the inner edge increases as the inner edge approaches the oil hole.

[0006] With this configuration, some of the oil scattered by the rotation of the carrier or the like strikes the guide protrusion and is collected by the guide protrusion. Then, due to the centrifugal force of the rotating carrier, the oil collected by the guide protrusion flows along the inner edge of the guide protrusion toward the side farther from the rotation axis. The oil collected by the guide protrusion then reaches the support hole via the oil hole. This allows oil to be efficiently guided to the pinion gear that requires lubrication. [Brief explanation of the drawings]

[0007] [Figure 1] FIG. 2 is a cross-sectional view showing the overall configuration of the transaxle. [Figure 2] FIG. 2 is a cross-sectional view taken along line 2-2 in FIG. DETAILED DESCRIPTION OF THE INVENTION

[0008] <Overall transaxle configuration> An embodiment of the present invention will be described below with reference to Figures 1 and 2. First, the overall configuration of a transaxle 100 applied to a vehicle will be described. Note that the following description will be based on the top and bottom, front and rear, and left and right of the vehicle.

[0009] 1, transaxle 100 includes an axle case 10, a motor-generator 20, a planetary gear mechanism 30, a differential 80, and a plurality of drive shafts 90. Transaxle 100 also includes a plurality of bearings 95 and a plurality of needle bearings 98.

[0010] The axle case 10 includes a case body 11 and a partition wall 12. The case body 11 is generally cylindrical with an internal space. The partition wall 12 divides the internal space of the case body 11 into a motor chamber 10A and a gear chamber 10B. The axle case 10 houses a motor generator 20 in the motor chamber 10A. The axle case 10 also houses a planetary gear mechanism 30 and a differential device 80 in the gear chamber 10B. Furthermore, the axle case 10 can store oil in the gear chamber 10B to lubricate the planetary gear mechanism 30 and the differential device 80.

[0011] The motor generator 20 includes a stator 21, a rotor 22, and a rotating shaft 23. The stator 21 is fixed to the case body 11 of the axle case 10. The rotor 22 is rotatable relative to the stator 21. The rotational axis of the rotor 22 coincides with the rotational axis 100Z of the transaxle 100. The rotational axis 100Z extends to the left and right of the vehicle. The rotating shaft 23 is fixed to the rotor 22. The rotating shaft 23 is substantially cylindrical. The partition wall 12 of the axle case 10 supports the rotating shaft 23 via a bearing 95. A portion of the rotating shaft 23, including its right end, penetrates the partition wall 12 and is located in the gear chamber 10B. The motor generator 20 can transmit driving force to the left and right drive shafts 90 via the planetary gear mechanism 30 and the differential device 80.

[0012] The planetary gear mechanism 30 includes a sun gear 40, multiple pinion gears 50, a ring gear 60, and a carrier 70. The sun gear 40 protrudes from a portion of the outer circumferential surface of the rotating shaft 23 of the motor generator 20, including the right end thereof. The sun gear 40 has an annular shape with external teeth. The sun gear 40 rotates integrally with the rotating shaft 23 about a rotation axis 100Z.

[0013] The ring gear 60 protrudes from the inner peripheral surface of the case body 11 of the axle case 10. In other words, the ring gear 60 is fixed to the axle case 10. The ring gear 60 has an annular shape with internal teeth. The central axis of the ring gear 60 coincides with the rotation axis 100Z. The ring gear 60 is located to the right of the vehicle relative to the sun gear 40.

[0014] The pinion gear 50 includes a pinion shaft 51, a large diameter gear 52, and a small diameter gear 53. That is, the pinion gear 50 is a so-called stepped pinion. The pinion shaft 51 has a substantially cylindrical shape. The central axis of the pinion shaft 51 is parallel to the rotation axis 100Z. The large diameter gear 52 protrudes from the outer peripheral surface of the pinion shaft 51. The large diameter gear 52 meshes with the sun gear 40. The small diameter gear 53 protrudes from a portion of the outer peripheral surface of the pinion shaft 51 that is to the right of the large diameter gear 52. The outer diameter of the small diameter gear 53 is smaller than the outer diameter of the large diameter gear 52. The small diameter gear 53 meshes with the ring gear 60. In this embodiment, the planetary gear mechanism 30 includes three pinion gears 50. In FIG. 1 , only one pinion gear 50 is shown as a representative.

[0015] The carrier 70 includes a first carrier 71 and a second carrier 79. The first carrier 71 includes a carrier body 72. The carrier body 72 is located near the right end of the pinion gear 50. The carrier body 72 is generally disk-shaped. The carrier body 72 includes three support holes 72A. The support holes 72A are recessed rightward from the left end face of the carrier body 72. In other words, the support holes 72A extend in a direction along the rotation axis 100Z. The support holes 72A are located at positions spaced a fixed distance from the rotation axis 100Z in a direction perpendicular to the rotation axis 100Z. The three support holes 72A are located every 120 degrees on a circumference centered on the rotation axis 100Z. The carrier body 72 supports a portion of the pinion gear 50, including its right end, via a needle bearing 98 at the support holes 72A. Therefore, the pinion gear 50 is rotatable relative to the carrier 70. In other words, the pinion gear 50 is rotatable on its axis. Furthermore, the axle case 10 supports the carrier body 72 via a bearing 95. Therefore, the carrier body 72 is rotatable relative to the axle case 10. The rotation axis of the carrier body 72 coincides with the rotation axis 100Z. As a result, the pinion gear 50 is able to revolve around the sun gear 40. Furthermore, the carrier body 72 is able to rotate coaxially with the sun gear 40 in accordance with the revolution of the pinion gear 50.

[0016] The carrier body 72 has three oil holes 72B. The oil holes 72B extend from the bottom surface of the support hole 72A to the right end surface of the carrier body 72 in the direction along the rotation axis 100Z. In other words, the oil holes 72B extend from the bottom surface of the support hole 72A to the side opposite the pinion gear 50. In this embodiment, the inner diameter of the oil holes 72B is smaller than the inner diameter of the support hole 72A.

[0017] The second carrier 79 is located near the left end of the pinion gear 50. The second carrier 79 is generally annular in shape. The central axis of the second carrier 79 coincides with the rotation axis 100Z. The second carrier 79 is fixed to the carrier body 72 of the first carrier 71 via bolts or the like (not shown). Therefore, the first carrier 71 and the second carrier 79 can rotate together.

[0018] The second carrier 79 has three support holes 79A and three oil holes 79B. The support holes 79A and oil holes 79B in the second carrier 79 are symmetrical in shape to the support holes 72A and oil holes 72B in the first carrier 71 with respect to a plane perpendicular to the rotation axis 100Z. The second carrier 79 supports a portion of the pinion gear 50, including its left end, in the support hole 79A via a needle bearing 98.

[0019] The differential device 80 includes a differential case 81, a differential pinion shaft 82, a plurality of differential pinion gears 83, and a plurality of differential side gears 84. The differential case 81 is located between the carrier body 72 of the first carrier 71 and the second carrier 79. The differential case 81 protrudes from the center portion of the left end surface of the carrier body 72. In this embodiment, the differential case 81 is molded integrally with the carrier body 72 by casting. Therefore, when the carrier 70 rotates, the differential case 81 rotates. The rotation of the differential case 81 rotates the left and right drive shafts 90 via the differential pinion shaft 82, the differential pinion gears 83, and the differential side gears 84. The above-mentioned gears allow the differential device 80 to allow a difference in rotational speed between the left and right drive shafts 90.

[0020] <Career-related components> As shown in FIG. 1, the first carrier 71 includes, in addition to a carrier body 72, three guide protrusions 75 and three covers 78. The guide protrusions 75 protrude from the right end face of the carrier body 72. As shown in FIG. 2, the guide protrusions 75 are substantially arc-shaped. The guide protrusions 75 extend along the outer periphery of the right end face of the carrier body 72. When viewed from a direction along the rotation axis 100Z, the guide protrusions 75 are located at positions overlapping with the pinion gear 50. In this embodiment, the guide protrusions 75 are molded integrally with the carrier body 72 by casting.

[0021] 1, the guide protrusion 75 includes a connection hole 76 and a recess 77. The connection hole 76 extends rightward from the right end of the oil hole 72B of the carrier body 72 in the direction along the rotation axis 100Z. The right end of the connection hole 76 is located in the center of the guide protrusion 75 in the direction along the rotation axis 100Z. In this embodiment, the inner diameter of the connection hole 76 is approximately the same as the inner diameter of the oil hole 72B.

[0022] 1, recess 77 is recessed from the end face of guide protrusion 75 closer to rotation axis 100Z toward the end face farther from it. In other words, recess 77 is recessed from the inner surface of arc-shaped guide protrusion 75 toward the outside. Recess 77 is connected to oil hole 72B via connection hole 76. Recess 77 extends from the left end to the right end of guide protrusion 75 in the direction along rotation axis 100Z.

[0023] As shown in FIG. 2, when viewed from the direction along the rotation axis 100Z, the bottom edge of the recess 77 has a substantially arc-shaped configuration. Here, the bottom edge of the recess 77 is defined as an inner edge 77A, which is the edge closer to the rotation axis 100Z. The central axis of the arc-shaped inner edge 77A is defined as an inner edge center 77B. Furthermore, a virtual line that is perpendicular to the rotation axis 100Z and passes through the central axis of the oil hole 72B and the rotation axis 100Z is defined as a virtual line 70Z. In this case, when viewed from the direction along the rotation axis 100Z, the connection hole 76 and the oil hole 72B open at the locations where they connect to the inner edge 77A. Furthermore, the inner edge center 77B is located between the central axis of the oil hole 72B and the rotation axis 100Z in the direction along the virtual line 70Z. The closer the inner edge 77A is to the oil hole 72B, the greater the distance from the rotation axis 100Z.

[0024] As shown in FIG. 2, when viewed from a direction along the rotation axis 100Z, the inner edge center 77B is offset from the imaginary line 70Z. Specifically, the inner edge center 77B corresponding to the inner edge 77A located forward of the imaginary line 70Z is located slightly forward of the imaginary line 70Z. Specifically, the distance between the inner edge center 77B of the front inner edge 77A and the imaginary line 70Z is the same as the radius of the oil hole 72B. Furthermore, when viewed from a direction along the rotation axis 100Z, the inner edge center 77B corresponding to the inner edge 77A located rearward of the imaginary line 70Z is located slightly rearward of the imaginary line 70Z. Specifically, the distance between the inner edge center 77B of the rear inner edge 77A and the imaginary line 70Z is the same as the radius of the oil hole 72B. In this embodiment, the recess 77 is formed by cutting.

[0025] 1, the cover 78 is fixed to the right end surface of the guide protrusion 75. The cover 78 covers the right side of the recess 77. In this embodiment, the cover 78 is molded integrally with the guide protrusion 75 and the carrier body 72 by casting.

[0026] As shown in FIG. 1, the axle case 10 has a plurality of protruding ribs 13. The protruding ribs 13 protrude from the inner wall surface of the case body 11. The protruding ribs 13 are located to the right of the carrier body 72. The protruding ribs 13 are also located at a predetermined distance from the rotation axis 100Z in a direction perpendicular to the rotation axis 100Z. The plurality of protruding ribs 13 are located at predetermined angular intervals on a circumference centered on the rotation axis 100Z. The protruding ribs 13 are located closer to the rotation axis 100Z than the guide protrusions 75. The protruding end faces of the protruding ribs 13 extend in a direction perpendicular to the rotation axis 100Z.

[0027] <Operation of this embodiment> In the transaxle 100, when the carrier 70 rotates, oil located near the lower end of the carrier 70 in the gear chamber 10B is scattered. Some of the oil scattered in the gear chamber 10B flows along the inner wall surface of the axle case 10 and reaches the vicinity of the center of the carrier 70. As shown by the dashed arrow in FIG. 1, the rotation of the carrier 70 causes the oil that has reached the vicinity of the center of the carrier 70 to be scattered. At this time, some of the scattered oil hits the guide protrusion 75 and is collected in the recess 77 of the guide protrusion 75. As shown by the dashed arrow in FIG. 2, centrifugal force acts on the oil rotating with the rotating carrier 70, causing the oil collected in the recess 77 of the guide protrusion 75 to flow along the inner edge 77A toward the side farther from the rotation axis 100Z. The oil in the recess 77 of the guide protrusion 75 then reaches the support hole 72A via the connection hole 76 and the oil hole 72B.

[0028] <Effects of this embodiment> (1) As described above, oil collected in recess 77 of guide projection 75 reaches support hole 72A via oil hole 72B, and therefore a large amount of oil is supplied to support hole 72A. As a result, the oil supplied to support hole 72A lubricates, for example, the area between the inner circumferential surface of support hole 72A and the outer circumferential surface of pinion shaft 51 of pinion gear 50. Therefore, in transaxle 100, oil can be efficiently guided to pinion gear 50, which requires lubrication.

[0029] (2) As shown in Figure 2, when viewed from the direction along the rotation axis 100Z, the inner edge center 77B corresponding to the inner edge 77A located forward with respect to the imaginary line 70Z is located slightly forward with respect to the imaginary line 70Z. Therefore, the opening of the recess 77 is larger than when, for example, the inner edge center 77B corresponding to the forward-located inner edge 77A is located on the imaginary line 70Z. This allows the amount of oil collected in the recess 77 of the guide protrusion 75 to be increased.

[0030] (3) As shown in FIG. 1 , the axle case 10 includes a protruding rib 13. The protruding end surface of the protruding rib 13 extends in a direction perpendicular to the rotation axis 100Z. In other words, the protruding end surface of the protruding rib 13 extends from the center of the carrier 70 toward the recessed portion 77 of the guide protrusion 75. Therefore, oil from near the center of the carrier 70 splashes along the protruding end surface of the protruding rib 13, and is likely to flow toward the recessed portion 77 of the guide protrusion 75. As a result, regardless of the shape of the inner wall surface of the axle case 10, for example, the protruding rib 13 can guide oil splashed from near the center of the carrier 70 toward the recessed portion 77 of the guide protrusion 75.

[0031] (4) Cover 78 covers the right side of recess 77. This prevents oil collected in recess 77 of guide projection 75 from leaking out from the right end of recess 77. As a result, oil collected in recess 77 of guide projection 75 can be more reliably supplied to oil hole 72B.

[0032] (5) The guide protrusions 75 are molded integrally with the carrier body 72 by casting. This makes it possible to prevent the number of parts of the carrier 70 from increasing when the guide protrusions 75 are employed.

[0033] <Example of change> This embodiment can be modified as follows: This embodiment and the following modifications can be combined and implemented within the scope of technical compatibility.

[0034] In the above embodiment, the shape of the guide protrusion 75 may be changed. For example, the position of the inner edge center 77B of the recess 77 may be changed. As a specific example, if the amount of oil collected in the recess 77 is sufficiently large, the inner edge center 77B corresponding to the inner edge 77A located forward of the imaginary line 70Z in FIG. 2 may be located on the imaginary line 70Z. Similarly, the inner edge center 77B corresponding to the inner edge 77A located rearward of the imaginary line 70Z may be located on the imaginary line 70Z.

[0035] For example, the shape of inner edge 77A of recess 77 may be changed. As a specific example, inner edge 77A of recess 77 may be linear when viewed from the direction along rotation axis 100Z. Even with this configuration, if the distance from rotation axis 100Z of inner edge 77A increases as it approaches oil hole 72B, oil collected in recess 77 will more easily flow to oil hole 72B.

[0036] In the above embodiment, the configuration of the carrier 70 may be changed. For example, the guide protrusion 75 does not necessarily have to be integrally formed with the carrier body 72. Even in this configuration, the technology relating to the guide protrusion 75 of the present invention can be applied.

[0037] For example, the cover 78 does not have to be molded integrally with the guide projection 75. Also, for example, if the amount of oil collected in the recess 77 of the guide projection 75 is sufficiently large, the cover 78 may be omitted.

[0038] For example, the guide protrusion 75 may protrude from the left end surface of the second carrier 79. In other words, the technology relating to the guide protrusion 75 of the present invention may be applied to the oil hole 79B of the second carrier 79 in addition to or instead of the oil hole 72B of the first carrier 71.

[0039] In the above embodiment, the configuration of the axle case 10 may be changed. For example, if the amount of oil scattered from the vicinity of the central portion of the carrier 70 that is collected by the recessed portion 77 of the guide projection 75 is sufficiently large, the protruding rib 13 may be omitted. [Explanation of symbols]

[0040] 10...Axle case 20...Motor generator 30...Planetary gear mechanism 40...Sun gear 50...Pinion gear 60…Ring gear 70...Career 70Z...imaginary line 71...First career 72...Carrier body 72A…Support hole 72B...Oil hole 75...Guide protrusion 76...Connection hole 77...recess 77A...Common-law marriage 77B...Center of inner edge 78...Cover 79...Second career 80…Differential device 81...Differential case 82...Differential pinion shaft 83...Differential pinion gear 84...Differential side gear 90...Drive shaft 100...Transaxle 100Z...rotation axis

Claims

[Claim 1] a sun gear that rotates around a rotation axis; a plurality of pinion gears meshing with the sun gear and revolving around the sun gear; a ring gear that meshes with the pinion gear; a carrier that rotatably supports the pinion gear and rotates coaxially with the sun gear in accordance with the revolution of the pinion gear; an axle case that houses the sun gear, the pinion gear, the ring gear, and the carrier; A transaxle comprising: the carrier includes a carrier body that supports a portion including an end of the pinion gear, and a guide protrusion that protrudes from the carrier body to a side opposite to the pinion gear, the carrier body includes a support hole extending in a direction along the rotation axis and supporting a portion of the pinion gear including an end thereof, and an oil hole extending from the support hole to a side opposite to the pinion gear, When viewed from a direction along the rotation axis, when the edge of the guide protrusion that is closer to the rotation axis is defined as an inner edge, The oil hole is open at a location connected to the inner edge, When viewed from a direction along the rotation axis, the distance of the inner edge from the rotation axis increases as the inner edge approaches the oil hole, The portion of the inner edge that is farthest from the rotation axis is located closer to the rotation axis than the portion of the oil hole that is farthest from the rotation axis. Transaxle.

Citation Information

Patent Citations

  • Lubricating mechanism of planetary gear train supporting bearing in wind power gearbox

    CN106594250A

  • Oil lubricating structure of automatic transmission

    JP1998038058A

  • Lubricating structure of planetary gear device

    JP2004270736A

  • Lubricating structure of planetary gearing mechanism

    JP2010156413A

  • Lubrication structure of planetary gear mechanism

    JP2014052065A