WO2021117573A1 - 油路構造 - Google Patents
油路構造 Download PDFInfo
- Publication number
- WO2021117573A1 WO2021117573A1 PCT/JP2020/044848 JP2020044848W WO2021117573A1 WO 2021117573 A1 WO2021117573 A1 WO 2021117573A1 JP 2020044848 W JP2020044848 W JP 2020044848W WO 2021117573 A1 WO2021117573 A1 WO 2021117573A1
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- WO
- WIPO (PCT)
- Prior art keywords
- wall portion
- support wall
- tubular member
- oil passage
- oil
- Prior art date
- Legal status (The legal status 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 status listed.)
- Ceased
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H41/00—Rotary fluid gearing of the hydrokinetic type
- F16H41/24—Details
- F16H41/30—Details relating to venting, lubrication, cooling, circulation of the cooling medium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H41/00—Rotary fluid gearing of the hydrokinetic type
- F16H41/24—Details
- F16H41/28—Details with respect to manufacture, e.g. blade attachment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/02—Gearboxes; Mounting gearing therein
- F16H57/03—Gearboxes; Mounting gearing therein characterised by means for reinforcing gearboxes, e.g. ribs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/18—Sealings between relatively-moving surfaces with stuffing-boxes for elastic or plastic packings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/40—Sealings between relatively-moving surfaces by means of fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/46—Sealings with packing ring expanded or pressed into place by fluid pressure, e.g. inflatable packings
- F16J15/48—Sealings with packing ring expanded or pressed into place by fluid pressure, e.g. inflatable packings influenced by the pressure within the member to be sealed
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
- F16H2045/0215—Details of oil circulation
Definitions
- the present invention relates to an oil passage structure.
- JP2014-020299A discloses an oil pump cover in which an oil passage is formed.
- a dummy cover (a dummy cover) that divides the internal space of the transmission case and the internal space of the converter housing between the transmission case accommodating the transmission mechanism and the converter housing accommodating the torque converter. Cover member) is provided.
- An oil passage is formed inside the cover member as well as the oil pump cover, and the oil supplied from the hydraulic control circuit is supplied to the transmission mechanism side through the oil passage in the cover member to shift gears. It is used to drive and lubricate mechanical parts.
- a through hole through which the output shaft of the torque converter penetrates and a cylindrical support wall portion surrounding the through hole are provided in the central portion of the cover member.
- the output shaft is a shaft involved in torque transmission from the torque converter to the transmission mechanism portion, and the support wall portion is formed with a thickness in the radial direction in order to secure the support rigidity of the shaft.
- the support wall that surrounds the shaft insertion hole A first tubular member that fits outside the support wall It has a second tubular member that fits inside the support wall and supports the outer circumference of the shaft.
- An oil passage along the rotation axis direction of the shaft is provided between the support wall portion and the first tubular member, and at least one of the support wall portion and the second tubular portion.
- An oil channel structure is provided.
- the weight can be reduced while ensuring the support rigidity of the shaft.
- FIG. 1 is a diagram illustrating an automatic transmission adopting an oil passage structure.
- FIG. 2 is a plan view of the cover member.
- FIG. 3 is an enlarged view of a main part of the automatic transmission.
- FIG. 4 is a diagram illustrating an oil supply route to the oil chamber.
- FIG. 5A is a diagram showing a state before the gap between the inner circumference of the inner wall portion of the clutch drum and the outer circumference of the tubular member is sealed by the seal ring.
- FIG. 5B is an enlarged view of the region A in FIG. 5A.
- FIG. 5C is an enlarged view of the region B in FIG. 5A.
- FIG. 5A is a diagram showing a state before the gap between the inner circumference of the inner wall portion of the clutch drum and the outer circumference of the tubular member is sealed by the seal ring.
- FIG. 5B is an enlarged view of the region A in FIG. 5A.
- FIG. 5C is an enlarged view of the region B in FIG. 5
- FIG. 5D is a diagram showing a state in which the gap between the inner circumference of the inner wall portion of the clutch drum and the outer circumference of the tubular member is sealed with a seal ring.
- FIG. 5E is an enlarged view of the region C in FIG. 5D.
- FIG. 5F is a diagram illustrating a seal ring according to a comparative example.
- FIG. 6A is an enlarged view of a support wall portion provided with an oil passage.
- FIG. 6B is a diagram showing a support wall portion according to a comparative example.
- FIG. 7A is a cross-sectional view taken along the line VIIa-VIIa in FIG.
- FIG. 7B is a perspective view schematically showing a cross section of the cover member cut along the center line CL in FIG. 7A.
- FIG. 8A is a diagram illustrating an oil passage structure according to a modified example.
- FIG. 8B is a diagram illustrating an oil passage structure according to another modification.
- FIG. 1 is an enlarged view of a main part of the automatic transmission 1 adopting the oil passage structure 10.
- FIG. 2 is a plan view of the cover member 6 as viewed from the forward / backward switching mechanism 3 side.
- FIG. 3 is an enlarged view of a main part of the automatic transmission 1 and is an enlarged view of the circumference of the support wall portion 62 of the cover member 6.
- a cover member 6 (dummy cover) is provided between the torque converter 2 and the forward / backward switching mechanism 3 which is a component of the transmission mechanism.
- the cover member 6 has a partition wall portion 61 having a plate shape in a cross-sectional view.
- the partition wall portion 61 is provided in a direction orthogonal to the rotation axis X.
- the partition wall portion 61 of the cover member 6 is bolted to a transmission case (not shown) to seal the opening on the torque converter 2 side in the transmission case.
- a plurality of oil passages are provided inside the partition wall portion 61 (see FIG. 2, virtual line). Oil is supplied to each of the oil passages from a hydraulic control circuit (not shown). The oil supplied to the oil passage is supplied to the transmission mechanism and the torque converter 2. The oil supplied to the transmission mechanism side is used for driving and lubricating the transmission mechanism unit.
- an insertion hole 610 is provided in the central portion of the partition wall portion 61.
- the insertion hole 610 penetrates the partition wall portion 61 in the thickness direction (rotation axis X direction).
- a cylindrical support wall portion 62 surrounding the insertion hole 610 is provided on the forward / backward switching mechanism 3 side (left side in FIG. 1) of the partition wall portion 61.
- the output shaft 20 of the torque converter 2 inserts the insertion hole 610 of the cover member 6 from the torque converter 2 side to the transmission mechanism portion side (left side in the drawing).
- the output shaft 20 is a transmission shaft involved in torque transmission from the torque converter 2 to the transmission mechanism unit.
- the output shaft 20 is provided along the rotation axis X.
- a turbine hub 231 is spline-fitted to one end 20a of the output shaft 20.
- the turbine runner 23 of the torque converter 2 is fixed to the turbine hub 231.
- the turbine runner 23 is integrally rotatably connected to the output shaft 20 via the turbine hub 231.
- the pump impeller 21 and the turbine runner 23 are provided so as to be relatively rotatable on a common rotation shaft X.
- a stator 22 is located between the pump impeller 21 and the turbine runner 23.
- the stator 22 is supported by the stator shaft 8 via a one-way clutch 24.
- the stator shaft 8 is provided in a direction along the rotation axis X.
- the stator shaft 8 is extrapolated to the output shaft 20 of the torque converter 2, and the inner race 24a of the one-way clutch 24 is spline-fitted on the outer periphery of the stator shaft 8 on the tip 8a side.
- the stator shaft 8 penetrates the insertion hole 610 of the cover member 6 from the transmission mechanism side to the torque converter 2 side (right side in the drawing).
- the fitting portion 81 on the base end 8b side of the stator shaft 8 is press-fitted into the inner circumference of the support wall portion 62 of the cover member 6, and the stator shaft 8 is supported by the cover member 6 which is a fixed side member. ..
- the tip 8a side of the stator shaft 8 penetrates the opening 251 provided in the housing 25 of the torque converter 2 and is located inside the housing 25.
- a sleeve 211 integrally formed with the pump impeller 21 is extrapolated to the stator shaft 8.
- the sleeve 211 is a tubular member provided in a direction along the rotation axis X, and the inner circumference of the sleeve 211 is supported by the outer circumference of the stator shaft 8 via a bush BS.
- the sleeve 211 is provided across the opening 251 of the housing 25 on the transmission mechanism side.
- the tip 211a of the sleeve 211 faces the partition wall portion 61 of the cover member 6.
- a lip seal RS provided in the opening 251 of the housing 25 is elastically in contact with the outer periphery of the sleeve 211, and the internal space A of the housing 25 is oil-tightly sealed by the lip seal RS.
- the tip 211a of the sleeve 211 is press-fitted into the inner circumference of the drive sprocket 27, and the sleeve 211 and the drive sprocket 27 are connected so as not to rotate relative to each other.
- the inner circumference of the drive sprocket 27 is supported by the outer circumference of the stator shaft 8 via the bush BS.
- the output rotation of the drive source (not shown) is input to the pump impeller 21, and the pump impeller 21 rotates around the rotation axis X. Then, the sleeve 211 integrally formed with the pump impeller 21 and the drive sprocket 27 fixed to the sleeve 211 also rotate around the rotation axis X.
- a chain (not shown) is wound around the drive sprocket 27, and the rotation of the sleeve 211 is transmitted to an oil pump (not shown) via the chain to drive the oil pump. As a result, the original pressure is supplied to the hydraulic control circuit (not shown).
- stator shaft 8 in which the drive sprocket 27 was supported on the outer periphery via the bush BS was wound around the drive sprocket 27 in a region opposite to the oil pump (upper region in FIG. 1).
- a stress acts from the chain toward the rotation axis X side.
- the stress input to the stator shaft 8 acts on the cover member 6 (support wall portion 62) on which the stator shaft 8 is supported.
- the rotation of the pump impeller 21 is transmitted to the turbine runner 23 via the fluid in the housing 25. Then, the rotation of the turbine runner 23 is transmitted to the output shaft 20 via the turbine hub 231 and the output shaft 20 rotates around the rotation shaft X.
- the output shaft 20 penetrates the support wall portion 62 provided on the cover member 6 in the rotation axis X direction and extends to the inner diameter side of the forward / backward switching mechanism 3.
- a connecting portion 545 of the clutch drum 54 is spline-fitted on the outer periphery of the region of the output shaft 20 protruding from the support wall portion 62.
- the output shaft 20 is connected to the clutch drum 54 on the forward / backward switching mechanism 3 side so as not to rotate relative to each other. Therefore, in the automatic transmission 1, the output rotation of the torque converter 2 is input to the clutch drum 54 of the forward / backward switching mechanism 3 via the output shaft 20.
- the forward / backward switching mechanism 3 includes a planetary gear mechanism 4, a forward clutch 5, and a reverse brake (not shown). As shown in FIG. 3, the planetary gear mechanism 4 has a sun gear 41, a ring gear 42, a pinion gear 43, a pinion shaft 44, and a carrier 45.
- the planetary gear mechanism 4 is housed inside the clutch drum 54 (outer wall portion 542) of the forward clutch 5.
- the forward clutch 5 has an inner diameter side plate 51, an outer diameter side plate 52, and a piston 53 that strokes in the rotation axis X direction.
- the inner diameter side plate 51 is spline-fitted to the outer circumference of the cylinder wall portion 551 of the clutch hub 55.
- the inner diameter side of the clutch hub 55 is fixed to the side surface of the sun gear 41, and the clutch hub 55 rotates integrally with the sun gear 41 around the rotation axis X.
- the outer diameter side plate 52 is spline-fitted to the inner circumference of the outer wall portion 542 of the clutch drum 54.
- the inner diameter side plate 51 and the outer diameter side plate 52 are alternately arranged in the rotation axis X direction.
- the clutch drum 54 has a bottom wall portion 541 provided in a direction orthogonal to the rotation axis X.
- the bottom wall portion 541 is ring-shaped when viewed from the rotation axis X direction, and the outer circumference and the inner circumference of the bottom wall portion 541 are the tubular outer wall portion 542 and the inner wall portion 543 over the entire circumference, respectively. being surrounded.
- the inner wall portion 543 is extrapolated to the tubular member 7 (first annular member).
- the tubular member 7 is press-fitted onto the outer periphery of the support wall portion 62.
- the inner wall portion 543 is rotatably supported by the support wall portion 62 of the cover member 6 via the tubular member 7.
- a disk portion 544 extending toward the inner diameter side is provided.
- the disk portion 544 is arranged in the gap between the sun gear 41 and the support wall portion 62.
- a thrust needle bearing NB1 positioned on the side surface of the sun gear 41 is located between the disk portion 544 and the sun gear 41.
- the thrust needle bearing NB2 positioned by the disc portion 544 is located between the disc portion 544 and the support wall portion 62.
- the inner circumference of the disk portion 544 extends to the inner diameter side of the stator shaft 8.
- a tubular connecting portion 545 is provided at an end portion of the disk portion 544 on the inner diameter side.
- the connecting portion 545 is provided so as to be oriented along the rotation shaft X, and the connecting portion 545 is spline-fitted to the outer periphery of the output shaft 20 of the torque converter 2.
- a piston 53 is provided between the inner wall portion 543 and the outer wall portion 542.
- the piston 53 has a base portion 531 that forms a ring shape when viewed from the rotation axis X direction, and a peripheral wall portion 532 that surrounds the outer periphery of the base portion 531.
- the tip end side of the peripheral wall portion 532 is bent toward the outer diameter side to form a pressing portion 533 forming a ring shape when viewed from the rotation axis X direction.
- the pressing portion 533 faces the region where the inner diameter side plate 51 and the outer diameter side plate 52 overlap in the rotation axis X direction.
- a disc spring 523 is located between the pressing portion 533 and the outer diameter side plate 52.
- the piston 53 is inserted between the inner wall portion 543 and the outer wall portion 542 of the clutch drum 54 from the planetary gear mechanism 4 side (left side in the drawing).
- An oil chamber R to which the operating hydraulic pressure (oil OL) of the piston 53 is supplied is formed between the base portion 531 of the piston 53 and the bottom wall portion 541 of the clutch drum 54.
- One end of the spring Sp is in contact with the base 531 of the piston 53 from the rotation axis X direction.
- the other end of the spring Sp is supported by the spring retainer 56.
- the displacement of the spring retainer 56 in the direction away from the piston 53 (to the left in the drawing) is regulated by the snap ring 561 engaged with the outer circumference of the inner wall portion 543.
- the piston 53 is urged by a spring Sp in a direction away from the planetary gear mechanism 4.
- the piston 53 is displaced in the direction approaching the planetary gear mechanism 4 (leftward in the drawing) while compressing the spring Sp in the rotation axis X direction.
- the inner diameter side plate 51 and the outer diameter side plate 52 are fastened to each other between the retaining plate 522 positioned by the snap ring 521 and the pressing portion 353 of the piston 53 so as not to rotate relative to each other.
- FIG. 4 is a diagram illustrating a supply route of oil OL to the oil chamber R.
- 5A-5F are diagrams for explaining the operation of the seal ring 9 and the seal ring 9.
- FIG. 5A is a diagram showing a state before the gap between the inner circumference 543a of the inner wall portion 543 of the clutch drum 54 and the outer circumference 7c of the tubular member 7 is sealed by the seal ring 9.
- FIG. 5B is an enlarged view of the region A in FIG. 5A.
- FIG. 5C is an enlarged view of the region B in FIG. 5A.
- FIG. 5D is a diagram showing a state in which the gap between the inner circumference 543a of the inner wall portion 543 of the clutch drum 54 and the outer circumference 7c of the tubular member 7 is sealed by the seal ring 9.
- FIG. 5E is an enlarged view of the region C in FIG. 5D.
- FIG. 5F is a diagram illustrating a seal ring 9'related to a comparative example.
- the cover member 6 is provided with oil OL supply paths 68 and 69.
- the supply path 68 communicates with a hydraulic control circuit (not shown) and is open to the inner circumference of the support wall portion 62.
- the supply path 69 is provided at a position adjacent to the supply path 68.
- the supply path 69 communicates the inner circumference and the outer circumference of the support wall portion 62.
- the supply path 69 communicates with the supply path 68 via an oil groove 821 provided on the outer periphery of the stator shaft 8. Oil OL supplied to the supply path 68 from a hydraulic control circuit (not shown) is supplied to the supply path 69 through the oil groove 821.
- the supply path 69 opens to the outer periphery of the region where the tubular member 7 is press-fitted in the support wall portion 62.
- an oil hole 71 is opened in the inner circumference of the region facing the supply path 69.
- the oil hole 71 communicates with an oil groove 72 that opens on the outer periphery of the tubular member 7.
- the oil hole 71 opens substantially in the center of the oil groove 72 in the X direction of the rotation axis.
- an oil hole 546 is formed in a region facing the oil hole 71 and the oil groove 72.
- the oil hole 546 communicates with the oil chamber R described above.
- the oil chamber R communicates with the supply path 69 via the oil hole 546 of the inner wall portion 543 and the oil groove 72 and the oil hole 71 of the tubular member 7.
- ring grooves 73 and 73 are provided on both sides of the oil hole 71 in the rotation axis X direction. As shown in FIG. 7B, the ring grooves 73, 73 are provided over the entire circumference in the circumferential direction around the rotation axis X.
- low friction type seal rings 9 and 9 are externally fitted in the ring grooves 73 and 73.
- the seal ring 9 has a base portion 91 on the outer diameter side and a protruding portion 92 protruding from the inner circumference of the base portion 91.
- the protruding portion 92 protrudes at a predetermined height h (see FIG. 5C) over the entire circumference in the circumferential direction around the rotation axis X.
- the protruding portion 92 protrudes from the substantially central portion of the base portion 91 in the width direction (rotation axis X direction) toward the inner diameter side.
- the seal ring 9 has a substantially T-shape.
- the width W1 of the protrusion 92 in the rotation axis X direction is narrower than the width W2 of the base 91 in the rotation axis X direction (see FIG. 5B).
- One side surface 92b of the protrusion 92 in the rotation axis X direction is located at a position offset from the side surface 91b of the base 91 toward the other side surface 92c.
- the seal ring 9 is loosely fitted in the ring groove 73 and can be displaced in the rotation axis X direction (horizontal direction in FIG. 5A) and the radial direction (vertical direction in FIG. 5A).
- the ring groove 73 passes through a gap between the inner circumference 543a of the inner wall portion 543 of the clutch drum 54 and the outer circumference 7c of the tubular member 7, and the oil is passed through the ring groove 73.
- Oil OL is supplied from the groove 72 side.
- the oil OL supplied to the ring groove 73 acts on the inner circumference 91d and the side surface 91c of the base 91 of the seal ring 9 and the inner circumference 92d and the side surface 92c of the protrusion 92 to obtain the seal ring 9 in FIG. 5E. Move to the position shown in.
- the seal ring 9 presses the outer circumference 91a of the base portion 91 against the inner circumference 543a of the inner wall portion 543 and presses the side surface 91b against the side surface 73b of the ring groove 73 to form an inner circumference 543a of the inner wall portion 543.
- the gap between the tubular member 7 and the outer circumference 7c is sealed.
- a part of the oil OL supplied to the oil chamber R does not leak from the ring groove 73 through the gap between the inner circumference 543a of the inner wall portion 543 and the outer circumference 7c of the tubular member 7. Will be done.
- the outer circumference 91a and the side surface 91b of the seal ring 9 may be held in contact with the inner circumference 543a of the inner wall portion 543 and the side surface 73b of the ring groove 73, respectively.
- the clutch drum 54 and the support wall portion 62 (cylindrical member 7) rotate relative to each other, the side surface 91b of the seal ring 9 that presses against the side surface 73b of the ring groove 73 becomes a resistance to the relative rotation, and automatic transmission is performed. It may affect the fuel efficiency of the vehicle equipped with the machine 1.
- a seal ring 9 having a protruding portion 92 having a predetermined height h is adopted, and the area of pressure contact with the side surface 73b of the ring groove 73 (the area of the side surface 91b) does not have the protruding portion 92. It is made narrower than the example seal ring 9'(see FIG. 5F).
- the pressure of the oil OL acting on the side surface 92b of the protruding portion 92 acts in the direction of separating the side surface 91b of the seal ring 9 from the side surface 73b of the ring groove 73. Therefore, the pressure contact force of the side surface 91b of the seal ring 9 with respect to the side surface 73b of the ring groove 73 is reduced as compared with the seal ring 9'of the comparative example. As a result, after the inflow of oil OL into the ring groove 73 is stopped, it becomes difficult for the side surface 91b of the seal ring 9 to be held in contact with the side surface 73b of the ring groove 73. This also reduces the resistance (friction) when the clutch drum 54 and the support wall portion 62 (cylindrical member 7) rotate relative to each other.
- the seal ring 9 slides and displaces in the ring groove 73 in conjunction with switching between supply / non-supply of oil OL to the oil chamber R. Further, when the clutch drum 54 and the tubular member 7 rotate relative to each other, they slide in the ring groove 73.
- the tubular member 7 on which the ring groove 73 is formed is formed separately from the cover member 6 (support wall portion 62) formed of the aluminum-based material, and the seal ring 9 is formed. It is made of an iron-based material with high wear resistance. As a result, the ring groove 73 is less likely to be worn by the slidingly displaced seal ring 9.
- FIG. 6A-6B are views for explaining the superiority of the oil passage structure 10 according to the present embodiment.
- FIG. 6A is an enlarged view of a support wall portion 62 provided with an oil passage 63.
- FIG. 6B is a diagram showing a support wall portion 62'corresponding to a comparative example.
- 7A-7B are views for explaining the oil passage structure 10 according to the present embodiment.
- FIG. 7A is a cross-sectional view taken along the line VIIa-VIIa in FIG.
- FIG. 7B is a perspective view schematically showing a cross section of the cover member 6 cut along the center line CL in FIG. 7A. Note that FIG. 7B shows a cross section of the support wall portion 62 of the cover member 6 cut at the portion of the oil passage 63.
- an oil passage 63 is also formed inside the support wall portion 62 as in the partition wall portion 61.
- the oil passage 63 is provided to supply the oil OL for lubrication to the thrust needle bearing NB2 arranged to face the tip 62b of the support wall portion 62.
- the oil passage 63 is composed of an internal oil passage 64 and an oil groove 65 in which an opening on the outer peripheral side is closed by a tubular member 7.
- the internal oil passage 64 extends in the support wall portion 62 in a direction away from the partition wall portion 61 (to the left in the drawing).
- the internal oil passage 64 is provided along a straight line L inclined with respect to the rotation axis X.
- the internal oil passage 64 is formed so as to approach the outer periphery of the support wall portion 62 as the distance from the partition wall portion 61 increases.
- the end portion of the internal oil passage 64 on the inner diameter side communicates with the oil passage 611 provided in the partition wall portion 61 on the inner diameter side of the partition wall portion 61.
- the oil passage 611 opens on the inner circumference of the insertion hole 610, and the opening of the oil passage 611 is sealed by the outer circumference of the stator shaft 8 press-fitted into the inner circumference of the support wall portion 62. There is. Therefore, the oil OL supplied to the oil passage 611 from the hydraulic control circuit (not shown) flows into the internal oil passage 64 in the support wall portion 62.
- the outer diameter side end of the internal oil passage 64 communicates with an oil groove 65 that opens on the outer periphery of the support wall portion 62.
- the oil groove 65 in the support wall portion 62 is provided at one position in the circumferential direction around the rotation axis X.
- the oil groove 65 when viewed from the rotation axis X direction has a semicircular shape with the apex P facing the rotation axis X side.
- the oil groove 65 is provided on the outer periphery of the support wall portion 62 in a direction along the rotation axis X.
- the oil groove 65 extends linearly from the tip 62b of the partition wall portion 61 toward the partition wall portion 61 side (right side in the drawing).
- a step portion 622 is provided on the outer periphery of the support wall portion 62.
- the oil groove 65 is formed from the tip 62b to a position shifted from the step portion 622 to the tip 62b side by a predetermined distance Wx.
- a counterbore portion 651 is provided at the end of the oil groove 65 on the partition wall portion 61 side (right side in the drawing). The counterbore portion 651 is formed so as to extend along the inner diameter side (rotation axis X side) of the oil groove 65 in the direction along the straight line L passing through the center of the oil passage 63 described above.
- the bottom surface 641a of the counterbore portion 651 is a flat surface orthogonal to the straight line L, and the bottom surface 641a of the counterbore portion 651 is open with an internal oil passage 64 formed in a direction orthogonal to the bottom surface 641a. ..
- a recess 621 is formed at a position intersecting the oil groove 65. As shown in FIG. 7A, the recess 621 is formed by cutting out a region of the support wall portion 62 on the tip 62b side in the radial direction.
- the recess 621 has a predetermined width Wy when viewed from the rotation axis X direction, and an oil groove 65 is opened inside the recess 621.
- the recess 621 is recessed toward the partition wall portion 61 (right side in the drawing) by a predetermined depth D1 from the other end 7b of the tubular member 7 and the base end 8b of the stator shaft 8. There is.
- the thrust needle bearing NB2 supported by the clutch drum 54 (disk portion 544) is located on the extension of the support wall portion 62.
- the tip 62b of the support wall portion 62 projects by ⁇ L toward the thrust needle bearing NB2 side from the other end 7b of the tubular member 7 and the base end 8b of the stator shaft 8. Therefore, when the clutch drum 54 is displaced in the rotation axis X direction, only the support wall portion 62 comes into contact with the thrust needle bearing NB2 that is displaced together with the clutch drum 54.
- One end 7a of the tubular member 7 press-fitted into the outer periphery of the support wall portion 62 is abutted against the step portion 622 on the outer periphery of the support wall portion 62 from the rotation axis X direction.
- the opening on the outer peripheral side of the oil groove 65 is closed by the tubular member 7.
- an oil passage extending along the rotation axis X to the tip 62b of the support wall portion 62 is formed between the outer circumference 62c of the support wall portion 62 and the inner circumference 7d of the tubular member 7.
- the oil groove 65 is formed up to a position shifted to the tip 62b side from the partition wall portion 61 (a position offset to the tip 62b side with respect to the partition wall portion 61). Therefore, a seal region SL having a predetermined distance Wx that does not participate in the formation of the oil passage is formed between the outer circumference 62c of the support wall portion 62 and the inner circumference 7d of the tubular member 7.
- the oil OL supplied to the oil groove 65 through the internal oil passage 64 is press-fitted into the outer circumference 62c of the support wall portion 62, and the gap between the tubular member 7 and the step portion 622 on the partition wall portion 61 side. It is designed not to leak from.
- curved surface processing Rx is applied to the inner circumference of the tubular member 7 on the one end 7a side, and a pocket PK1 is formed on the inner circumference of the tubular member 7 on the one end 7a side.
- the pocket PK1 is provided to capture impurities generated when the tubular member 7 is press-fitted into the outer periphery of the support wall portion 62.
- the surface of the support wall portion 62 is scraped to generate impurities.
- the contaminants generated in the press-fitting process are pushed by the tubular member 7 and move to the step portion 622 side. If the pocket PK1 is not provided, the generated contaminants may be sandwiched between one end 7a of the tubular member 7 and the step portion 622 to form a gap. Further, the generated contaminants may cause a gap between the inner circumference 7d of the tubular member 7 and the outer circumference 62c of the support wall portion 62. In such a case, the oil OL supplied from the internal oil passage 64 to the oil groove 65 may leak from the partition wall portion 61 side through the generated gap.
- the pocket PK1 is formed on the inner circumference of one end 7a side of the tubular member 7 to prevent the occurrence of such a situation.
- the fitting portion 81 of the stator shaft 8 is press-fitted into the inner circumference of the support wall portion 62.
- the fitting portion 81 has a press-fitting portion 810 and a serration fitting portion 811.
- the serration fitting portion 811 is formed with an outer diameter larger than that of the press-fit portion 810.
- the serration fitting portion 811 is located on the base end 8b side (left side in the drawing) when viewed from the press-fitting portion 810.
- the outer circumference of the serration fitting portion 811 is serrated.
- the serrations 811a are formed in a straight line in a direction along the rotation axis X, and the serrations 811a are provided on the outer circumference of the serration fitting portion 811 over the entire circumference in the circumferential direction around the rotation axis X. In the serration fitting portion 811 the serration 811a is provided over the entire length in the rotation axis X direction.
- the inner diameter side of the region where the oil groove 65 is provided is the fitted portion 623 to which the serration fitting portion 811 fits.
- the region on the tip 62b side (left side in the drawing) of the counterbore portion 651 in the oil groove 65 is the fitted portion 623.
- a pocket PK2 is formed between the serration fitting portion 811 and the press-fitting portion 810. It has become so.
- the serration fitting portion 811 When the serration fitting portion 811 is serrated and fitted to the inner circumference of the support wall portion 62, the surface of the support wall portion 62 (the inner circumference of the fitted portion 623) is scraped to generate impurities. The impurities generated in the process of serration fitting are pushed by the serration fitting portion 811 and move. If the pocket PK2 is not provided, the generated contaminants may create a gap between the inner circumference of the support wall portion 62 (fitted portion 623) and the outer circumference of the fitting portion 81. is there. In the present embodiment, the pocket PK2 in the rotation axis X direction is formed between the serration fitting portion 811 and the support wall portion 62, so that the occurrence of such a situation can be prevented.
- the present inventor simply changed the constituent material of the cover member 6 from a conventional iron-based material to an aluminum alloy-based material in order to reduce the weight of the cover member 6, and found that the support wall portion 62. It was found that the ring grooves 67 and 67 (see FIG. 6B) provided on the outer periphery of the'was worn. This is due to the following reasons. -The seal ring 9 slides in the ring groove 67 in the process of repeatedly supplying / shutting off the hydraulic pressure (oil OL) to the oil chamber R and in the process of relative rotation between the clutch drum 54 and the support wall portion 62. Since the aluminum alloy-based material has a lower wear resistance to the seal ring 9 made of a fluorine-based material than the iron-based material, it is scraped by the seal ring 9 on which the ring groove 67 slides.
- the cover member 6 made of an aluminum alloy-based material if the radial thickness Wb of the support wall portion 62'is reduced for the purpose of further weight reduction, the radial thicknesses Wc and Wd are also reduced. The total amount of constituent materials in the area surrounding the road 63'is reduced. Then, as a result of the ratio of the constituent material to the support wall portion 62'decreasing, the support rigidity of the support wall portion 62'decreases. Further, the wear of the ring groove 67 may cause deterioration of the sealing property due to the seal ring 9'.
- the tubular member 7 made of an iron-based material having high wear resistance to the seal ring 9 is press-fitted into the outer periphery of the support wall portion 62 made of an aluminum alloy-based material, and the tubular member 7 is pressed.
- Ring grooves 67, 67 into which the seal ring 9 is loosely fitted are formed on the outer periphery of the ring groove 67.
- the support wall portion 62 made of an aluminum alloy-based material is prevented from being worn by the sliding seal ring 9.
- an oil passage structure 10 in which an oil passage 63 along the rotation axis X direction is formed between the outer circumference of the support wall portion 62 and the inner circumference of the tubular member 7 press-fitted into the outer circumference of the support wall portion 62 is adopted.
- the oil passage along the rotation axis X is prevented from being formed in a state of being completely embedded inside the support wall portion 62.
- the rigidity of the support wall portion 62 can be ensured only by securing the thickness We (see FIG. 6A) on the inner diameter side of the oil passage 63. Therefore, in a comparative example in which an oil passage is embedded inside the radial thickness Wa (see FIG. 6A) of the entire support wall portion 62 including the thickness of the tubular member 7 press-fitted into the outer periphery of the support wall portion 62.
- the thickness of the support wall portion 62'(see FIG. 6B) can be made thinner than the thickness Wb.
- the sleeve 211 that rotates integrally with the drive sprocket 27 is extrapolated to the stator shaft 8 supported by the support wall portion 62. Therefore, when the oil pump (not shown) is driven, stress acts on the stator shaft 8 from the chain wound around the drive sprocket 27 toward the rotation shaft X side. Then, the stress input to the stator shaft 8 acts on the cover member 6 (support wall portion 62) on which the stator shaft 8 is supported.
- the support wall portion 62 is provided with a support strength that can withstand the stress input from the stator shaft 8 side, more specifically, the stress input from the stator 22 of the torque converter 2 via the stator shaft 8. Becomes possible.
- the oil passage structure 10 has the following configuration.
- the oil passage structure 10 is A support wall portion 62 surrounding the insertion hole 610 of the output shaft 20 (shaft), and A tubular member 7 (first tubular member) that is externally fitted to the support wall portion 62, It has a stator shaft 8 (second tubular member) that fits inside the support wall portion 62 and supports the outer circumference of the output shaft 20.
- an oil passage 63 along the rotation axis X direction of the output shaft 20 is provided between the support wall portion 62 and the tubular member 7 (see FIG. 3).
- the constituent material of the support wall portion 62' is formed in order to secure the rigidity of the support wall portion 62'.
- the support rigidity of the support wall portion 62' is reduced.
- the oil passage 63 is formed by utilizing the mating surface of the support wall portion 62 and the tubular member 7.
- the rigidity of the support wall portion 62 can be ensured only by securing the thickness We (see FIG. 6A) on the inner diameter side of the oil passage 63. Therefore, in a comparative example in which an oil passage is embedded inside the radial thickness Wa (see FIG.
- the thickness of the support wall portion 62' (see FIG. 6B) can be made thinner than the thickness Wb.
- the oil passage structure 10 has the following configuration.
- the oil passage 63 has a region formed by closing the opening on the outer peripheral side of the oil groove 65 provided on the outer periphery of the support wall portion 62 with the inner circumference 7d of the tubular member 7.
- oil passage is formed by closing the opening on the outer peripheral side of the oil groove 65 provided on the outer periphery of the support wall portion 62 with the inner circumference 7d of the tubular member 7, oil is formed in the support wall portion 62 having a reduced radial thickness.
- the amount of constituent material around the path can be greater than if the oil path is formed inside the support wall portion 62. Thereby, the support rigidity of the output shaft 20 (shaft) in the support wall portion 62 can be secured.
- the oil passage can be formed only by providing the oil groove 65 on the outer periphery of the support wall portion 62, the work load is reduced as compared with the case where the oil passage is provided inside the support wall portion 62. This can be expected to reduce the work cost of forming the oil passage.
- the oil passage structure 10 has the following configuration. (3) In the stator shaft 8, the outer circumference of the serration fitting portion 811 on the base end 8b side is serrated. In the stator shaft 8, the serration-processed serration fitting portion 811 is serrated-fitted to the inner circumference of the support wall portion 62 and fixed to the inner circumference of the support wall portion 62.
- the stress caused by the serration fitting acts on the region where the stator shaft 8 is serrated-fitted in the support wall portion 62. Therefore, when the oil passage 63'(see FIG. 6B) is embedded inside the support wall portion 62', the radial thicknesses Wc and Wd (FIG. 6B) of the constituent material surrounding the oil passage 63' are formed. See) to be thicker, i.e., the support wall portion 62'needs to be thicker in the radial direction. This is to ensure the rigidity that can withstand serration fitting while ensuring the support rigidity of the output shaft 20. Then, it becomes difficult to reduce the radial thickness (outer diameter) of the support wall portion 62'for the purpose of weight reduction.
- the opening of the oil groove 65 provided on the outer periphery of the support wall portion 62 is closed by the inner circumference 7d of the tubular member 7 to form an oil passage, at least all of the oil passage 63 is embedded inside the support wall portion 62. Even if the outer diameter of the support wall portion 62 is smaller than that in the case of forming, the rigidity of the support wall portion 62 can be ensured. Therefore, it becomes easy to secure the support rigidity of the output shaft 20 and the rigidity that can withstand serration fitting while suppressing the outer diameter of the support wall portion 62. Therefore, the weight can be reduced while reducing the outer diameter of the support wall portion 62 as compared with the case where the oil passage 63'is formed in the support wall portion 62'.
- the oil passage 63 is provided on the outer peripheral side of the support wall portion 62, the cutting piece generated when the serration fitting portion 811 of the stator shaft 8 is press-fitted into the inner circumference of the support wall portion 62 is an oil passage. The possibility of mixing in 63 can be reduced.
- the oil passage structure 10 has the following configuration. (4) In the support wall portion 62, a partition wall portion 61 (large diameter portion) having an outer diameter larger than that of the support wall portion 62 is provided at one end in the rotation axis X direction. In the support wall portion 62, the tubular member 7 is press-fitted into the outer periphery of the support wall portion 62 from the tip 62b (the other end) side in the rotation axis X direction. The oil passage 63 is formed by closing the opening of the oil groove 65 provided on the outer periphery of the support wall portion 62 with the inner circumference 7d of the tubular member 7.
- the oil groove 65 extends from a position shifted toward the tip 62b side of the partition wall portion 61 to the tip 62b.
- the oil passage 63 communicates with the oil passage 611 in the partition wall portion 61 on the inner peripheral side of the support wall portion 62 via the internal oil passage 64 provided in the support wall portion 62.
- the region adjacent to the partition wall portion 61 where the oil groove 65 is not provided is the outer circumference 62c of the support wall portion 62. It functions as a seal region SL that seals the gap between the tubular member 7 and the inner circumference 7d.
- the oil groove 65 on the outer periphery of the support wall portion 62 is formed extending to the partition wall portion 61, the tubular member 7 is formed between one end 7a of the tubular member 7 and the partition wall portion 61 in the rotation axis X direction. There is a possibility that the ground product produced by the press-fitting of the material will be caught and a gap will be created.
- the oil passage structure 10 has the following configuration. (5)
- the partition wall portion 61 is a cover member 6 that closes the opening of the transmission case of the automatic transmission.
- the output shaft 20 is the output shaft of the torque converter 2
- the stator shaft 8 is the stator shaft of the torque converter 2.
- the oil passage structure 10 has the following configuration. (6) Ring grooves 73, 73 into which the seal rings 9 and 9 are loosely fitted are provided on the outer circumference 7c of the tubular member 7.
- the tubular member 7 is made of a material having higher wear resistance to the seal ring 9 than the material constituting the support wall portion 62.
- the radial thickness Wa (see FIG. 6A) including the tubular member 7 externally fitted to the support wall portion 62 is the radial thickness Wb when the ring groove 67 is directly provided on the support wall portion 62'. It can be smaller than (see FIG. 6B).
- the tubular member 7 is made of an iron-based material
- the support wall portion 62 is made of an aluminum alloy-based material, which is lighter than the iron-based material but has lower wear resistance to the seal ring 9 than the iron-based material.
- the weight can be reduced while ensuring the support rigidity of the output shaft 20.
- the aluminum alloy-based material is easier to process than the iron-based material, it is possible to easily process the groove on the outer periphery of the support wall portion.
- a clutch drum 54 (inner wall portion 543), which is a rotating body of the forward clutch 5, is extrapolated to the tubular member 7 (first tubular member) made of an iron-based material.
- the clutch drum 54 is rotatably supported by the outer circumference 7c of the tubular member 7.
- two ring grooves 73, 73 are provided at intervals in the rotation axis X direction.
- An oil OL supply path (oil hole 71, oil groove 72) for driving the forward clutch 5 (friction fastening device) is opened between the ring grooves 73 and 73 provided at intervals in the rotation axis X direction. ing.
- the seal ring 9 loosely fitted in the ring groove 73 seals a gap between the outer circumference 7c of the tubular member 7 and the inner circumference 543a of the inner wall portion 543 with oil supplied from the supply path.
- the seal ring 9 is integrally formed from an annular base portion 91 that presses and contacts the inner circumference 543a of the inner wall portion 543 of the clutch drum 54 in the radial direction, and a protruding portion 92 that protrudes from the inner circumference of the base portion 91 toward the inner diameter side. It is formed.
- the seal ring 9 has a ring groove 73 of the ring groove 73 by the height h of the protrusion 92 as compared with the seal ring 9'(see FIG. 5E) of the comparative example having the same radial height h'.
- the contact area with the side surface 73b becomes smaller. Therefore, the clutch drum 54 and the support wall portion 62 (cylindrical member 7) are kept in contact with the outer circumference 91a and the side surface 91b of the seal ring 9 in contact with the inner circumference 543a of the inner wall portion 543 and the side surface 73b of the ring groove 73, respectively. ) And relative rotation, the resistance (friction) becomes small.
- the seal ring 9 is provided with the projecting portion 92, the depth of the ring groove 73 in the radial direction becomes deeper, but the ring groove 73 is provided on the tubular member 7 that is externally fitted to the support wall portion 62. Therefore, at least, the rigidity of the support wall portion 62 can be ensured even if the outer diameter of the support wall portion 62 is smaller than that in the case where all of the oil passages 63 are embedded in the support wall portion 62.
- the tip 62b of the support wall portion 62 faces the thrust needle bearing NB2 supported by the disc portion 544 of the clutch drum 54.
- the tip 62b of the support wall portion 62 is a thrust needle rather than the other end 7b of the tubular member 7 press-fitted into the outer circumference of the support wall portion 62 and the base end 8b of the stator shaft 8 press-fitted into the inner circumference of the support wall portion 62. It is located on the bearing NB2 side.
- [Modification example] 8A-8B are views for explaining the oil passage structures 10A and 10B according to the modified example.
- the oil groove 65 provided on the outer circumference of the support wall portion 62 is closed by the inner circumference of the tubular member 7 press-fitted into the outer circumference of the support wall portion 62 to form an oil passage along the rotation axis X direction.
- the oil passage structure 10 was illustrated.
- the oil groove 75 provided on the inner circumference of the tubular member 7 is closed by the outer circumference 62c of the support wall portion 62 to form an oil passage 63A along the rotation axis X direction as an oil passage structure 10A. Is also good.
- the oil passage 63A of the oil passage structure 10A is composed of an internal oil passage 64A provided in the support wall portion 62 along a straight line L and an oil passage 65A.
- an oil passage 63B may be provided between the support wall portion 62 and the stator shaft 8B press-fitted into the inner circumference of the support wall portion 62.
- an internal oil passage 64B along the rotation axis X is provided inside the support wall portion 62, and an oil groove 624 that opens on the inner peripheral side is provided on the extension of the internal oil passage 64B. It is provided.
- the opening on the inner peripheral side of the oil groove 624 is closed by the large diameter portion 811B of the stator shaft 8B press-fitted into the inner circumference of the support wall portion 62 to form an oil passage 65B.
- the oil passage structure 10B has the following configuration. (10)
- the oil passage 63B has an oil passage 65B formed by closing the opening of the oil groove 624 provided on the inner circumference of the support wall portion 62 with the outer circumference of the stator shaft 8 (second tubular member).
- the support wall portion 63B when the oil passage 63B is formed by closing the opening of the oil groove 624 provided on the inner circumference of the support wall portion 62 with the outer circumference of the stator shaft 8, the support wall portion having a reduced outer diameter.
- the amount of the constituent material around the oil passage 65B can be increased as compared with the case where the oil passage is formed inside the support wall portion, so that the radial thickness of the support wall portion 62 can be increased, so that the support wall portion can be increased.
- the support rigidity of the output shaft 20 in 62 can be secured.
- the opening of the oil groove provided on the outer periphery of the stator shaft 8 (second tubular member) may be closed by the inner circumference of the support wall portion 62 to form an oil passage.
- the outer diameter of the support wall portion can be reduced to the minimum outer diameter capable of exhibiting the support rigidity required for supporting the output shaft 20 (shaft), so that the weight can be further reduced.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Architecture (AREA)
- Fluid Mechanics (AREA)
- General Details Of Gearings (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202080086893.XA CN114829804B (zh) | 2019-12-14 | 2020-12-02 | 油路结构 |
| US17/785,014 US11852226B2 (en) | 2019-12-14 | 2020-12-02 | Oil passage structure |
| JP2021563887A JP7429243B2 (ja) | 2019-12-14 | 2020-12-02 | 油路構造 |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2019226017 | 2019-12-14 | ||
| JP2019-226017 | 2019-12-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2021117573A1 true WO2021117573A1 (ja) | 2021-06-17 |
Family
ID=76330266
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2020/044848 Ceased WO2021117573A1 (ja) | 2019-12-14 | 2020-12-02 | 油路構造 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US11852226B2 (https=) |
| JP (1) | JP7429243B2 (https=) |
| CN (1) | CN114829804B (https=) |
| WO (1) | WO2021117573A1 (https=) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12276325B1 (en) * | 2023-11-10 | 2025-04-15 | Schaeffler Technologies AG & Co. KG | Hybrid module thrust bushing |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02217658A (ja) * | 1989-02-17 | 1990-08-30 | Jatco Corp | 自動変速機の潤滑装置 |
| JPH08285036A (ja) * | 1995-04-10 | 1996-11-01 | Nissan Motor Co Ltd | 自動変速機のトルクコンバータ |
| WO2013094044A1 (ja) * | 2011-12-21 | 2013-06-27 | トヨタ自動車株式会社 | 自動変速機の潤滑装置 |
| JP2018123857A (ja) * | 2017-01-30 | 2018-08-09 | アイシン・エィ・ダブリュ株式会社 | 油路構造およびそれを備えた動力伝達装置 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07217724A (ja) | 1994-02-04 | 1995-08-15 | Toyo A Tec Kk | トランスミッションのオイルポンプカバー |
| JP2004052813A (ja) * | 2002-07-16 | 2004-02-19 | Jatco Ltd | 自動変速機用歯車変速装置 |
| JP4776352B2 (ja) | 2005-11-17 | 2011-09-21 | アイシン・エィ・ダブリュ株式会社 | 自動変速機における潤滑装置 |
| US7585243B2 (en) | 2005-11-17 | 2009-09-08 | Aisin Aw Co., Ltd. | Automatic transmission |
| DE112009002360B4 (de) * | 2009-04-28 | 2015-11-26 | Toyota Jidosha Kabushiki Kaisha | Öldurchgangsstruktur einer Ölpumpe mit Kettenantrieb |
| JP5428820B2 (ja) * | 2009-12-11 | 2014-02-26 | アイシン精機株式会社 | クラッチ装置 |
| JP5900214B2 (ja) | 2012-07-19 | 2016-04-06 | アイシン・エィ・ダブリュ株式会社 | オイルポンプ装置 |
| WO2015005492A1 (ja) * | 2013-07-12 | 2015-01-15 | アイシン・エィ・ダブリュ株式会社 | 動力伝達装置 |
| JP6695624B2 (ja) * | 2016-02-16 | 2020-05-20 | ジヤトコ株式会社 | 油路構造 |
-
2020
- 2020-12-02 CN CN202080086893.XA patent/CN114829804B/zh active Active
- 2020-12-02 WO PCT/JP2020/044848 patent/WO2021117573A1/ja not_active Ceased
- 2020-12-02 US US17/785,014 patent/US11852226B2/en active Active
- 2020-12-02 JP JP2021563887A patent/JP7429243B2/ja active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02217658A (ja) * | 1989-02-17 | 1990-08-30 | Jatco Corp | 自動変速機の潤滑装置 |
| JPH08285036A (ja) * | 1995-04-10 | 1996-11-01 | Nissan Motor Co Ltd | 自動変速機のトルクコンバータ |
| WO2013094044A1 (ja) * | 2011-12-21 | 2013-06-27 | トヨタ自動車株式会社 | 自動変速機の潤滑装置 |
| JP2018123857A (ja) * | 2017-01-30 | 2018-08-09 | アイシン・エィ・ダブリュ株式会社 | 油路構造およびそれを備えた動力伝達装置 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114829804B (zh) | 2023-09-29 |
| US11852226B2 (en) | 2023-12-26 |
| US20230009118A1 (en) | 2023-01-12 |
| CN114829804A (zh) | 2022-07-29 |
| JPWO2021117573A1 (https=) | 2021-06-17 |
| JP7429243B2 (ja) | 2024-02-07 |
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