WO2020012905A1 - Rotational variation reducing device - Google Patents

Rotational variation reducing device Download PDF

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Publication number
WO2020012905A1
WO2020012905A1 PCT/JP2019/024399 JP2019024399W WO2020012905A1 WO 2020012905 A1 WO2020012905 A1 WO 2020012905A1 JP 2019024399 W JP2019024399 W JP 2019024399W WO 2020012905 A1 WO2020012905 A1 WO 2020012905A1
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WO
WIPO (PCT)
Prior art keywords
output shaft
output
planetary gear
input
gear mechanism
Prior art date
Application number
PCT/JP2019/024399
Other languages
French (fr)
Japanese (ja)
Inventor
小林 篤
村田 豊
Original Assignee
ユニプレス株式会社
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
Application filed by ユニプレス株式会社 filed Critical ユニプレス株式会社
Priority to JP2019553579A priority Critical patent/JP6656491B1/en
Publication of WO2020012905A1 publication Critical patent/WO2020012905A1/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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/133Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses using springs as elastic members, e.g. metallic springs
    • F16F15/134Wound springs
    • 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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/30Flywheels
    • 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
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion

Definitions

  • the present invention relates to a rotation fluctuation reduction device that reduces rotation fluctuation of a prime mover and transmits the rotation fluctuation to an output shaft of a transmission, and more particularly to a rotation fluctuation reduction device provided with a planetary gear mechanism.
  • a rotation fluctuation reduction device that reduces the rotation fluctuation of the prime mover and transmits it to the output shaft of the transmission
  • a torque converter that is configured by combining an elastic damper mechanism using a coil spring as an elastic body with a planetary gear mechanism.
  • the elastic body is arranged in the rotation direction between the input member and the output member, and one of the rotating elements of the planetary gear mechanism including the carrier, the ring gear, and the sun gear is provided on the input member.
  • the other one is connected to the output member, and the other one of the rotating elements is arranged so as to be free to participate in power transmission.
  • the free rotating element increases the damper mass in the rotating inertial system and can contribute to the reduction of rotation fluctuation.
  • the connection between the elastic damper mechanism and the rotating element and the planetary gear mechanism is the same in that a straight-type pinion is used, but various things that are slightly different in the connection between the elements have been proposed. (Patent Documents 1 to 3). Further, as a device related to the same person as the present applicant, a device using a so-called Ravigneaux gear as a pinion has been proposed (Patent Document 4).
  • the above-described rotation fluctuation reducing device configured by combining an elastic damper mechanism with a planetary gear mechanism is generally intended for use in combination with a lock-up clutch of a torque converter.
  • engagement of the lock-up clutch is performed from a low rotation speed region.
  • This is an effective means as a countermeasure for suppressing specific noise such as muffled noise which becomes a problem.
  • the torque converter oil used as a torque transmission medium in the torque converter can be used for lubrication of the gear meshing portion of the planetary gear mechanism as it is, and the elastic damper mechanism is housed in the torque converter housing together with the planetary gear mechanism. Therefore, there is an advantage that a lubrication device dedicated to lubrication is not required.
  • a rotation fluctuation reducing device configured by combining an elastic damper mechanism with a planetary gear mechanism has been generally intended for use in a torque converter housing as described above.
  • the planetary gear mechanism is installed coaxially with the drive shaft and a coil spring is arranged on the outer peripheral side.
  • smooth elastic deformation of the coil spring may be hindered due to friction with the support portion that receives the deformation of the coil spring under a force, and a problem such as a limitation on the degree of freedom of the elastic characteristic of the coil spring may occur. There was also concern.
  • a rotation fluctuation reduction device is a rotation fluctuation reduction device that reduces the rotation fluctuation of a prime mover and transmits the reduced rotation fluctuation to an output shaft.
  • the rotation fluctuation reduction device includes at least an input member on the prime mover side and an output member on the output shaft side.
  • An elastic damper mechanism configured by arranging an elastic body having torsional rigidity in the rotational direction between the output shafts; a carrier configured by rotatably supporting a plurality of pinions;
  • a planetary gear mechanism having at least three rotating gear elements, and at least two gears meshing with each other, and a resilient damper mechanism provides an elasticity in addition to the output shaft (hereinafter referred to as a first output shaft).
  • a second output shaft for taking a rotary motion on the input member side of the body is branched, one of the rotating elements of the planetary gear mechanism is provided by the first output shaft, and the other is provided by a second output shaft.
  • Drive each by And at least one of the remaining rotating elements not involved in power transmission functions as a damper mass, and the elastic damper mechanism houses a planetary gear mechanism and lubricating oil for lubricating the planetary gear mechanism.
  • a connection of the first output shaft and the second output shaft to corresponding rotating elements of the planetary gear mechanism is made through a wall portion of the housing. It has become.
  • the housing for accommodating the planetary gear mechanism is also a housing for accommodating a speed change mechanism for shifting the rotation of the prime mover and transmitting the speed to an output shaft, and the first output shaft forms an input shaft of the speed change mechanism. Can be.
  • the elastic body damper mechanism includes an input member on the prime mover side, an output member on the output shaft side, and an elastic body for connecting the input member and the output member in a rotational direction, and the second output shaft is connected to the input member. It is possible to adopt a configuration of branching more.
  • the elastic damper mechanism connects the input member on the prime mover side, the output member on the first output shaft side, the intermediate member between the input member and the output member, and the rotational direction connection between the input member and the intermediate member.
  • a second elastic body that connects the intermediate member and the output member in a rotational direction, and the second output shaft can be branched from the input member.
  • the elastic damper mechanism includes an input member on the prime mover side, an output member on the first output shaft side, an intermediate member installed between the input member and the output member, and an intermediate member provided between the input member and the intermediate member. And a second elastic body that connects between the intermediate member and the output member in the rotational direction, wherein the second output shaft is branched from the intermediate member. can do.
  • the elastic body damper mechanism includes an input member on the prime mover side, an output member on the first output shaft side, a first elastic body that connects the input member and the output member in a rotational direction, a damper mass, A second elastic body that couples the damper mass to the output member without participating in power transmission, wherein the second output shaft is branched from the input member.
  • a clutch that is engaged and disengaged between the second output shaft extending in the housing and the planetary gear mechanism.
  • bearings with seals on the inner peripheral side and the outer peripheral side can be provided for sealing the first output shaft and the second output shaft with the wall of the housing.
  • the elastic damper mechanism and the planetary gear mechanism are separated from each other, and the planetary gear mechanism is installed in a housing that can supply lubricating oil, so that the planetary gear mechanism can operate stably even in a dry environment. It is possible to add a vibration damping effect by the gear mechanism.
  • the degree of freedom in designing each structure and layout is increased, and the optimal design of the rotation fluctuation reducing device using the planetary gear mechanism becomes possible. That is, in the conventional planetary gear type rotation fluctuation reduction device built in the torque converter, a large centrifugal force applied to the elastic body is imposed due to a structural constraint that the elastic body must be arranged on the outer peripheral side of the planetary gear mechanism. There is a problem that the degree of freedom in designing the elastic body for obtaining the desired vibration damping characteristics is limited due to measures against the above (for example, a low-rigidity coil spring cannot be used).
  • the planetary gear mechanism which needs to be installed inside the housing, and the elastic damper mechanism, which does not require lubrication, can be arranged outside, so the degree of freedom in the design of the elastic body is increased.
  • the restriction on the setting of vibration damping characteristics (particularly, low rigidity) is reduced, and a design closer to the optimal design can be performed.
  • the present invention relates to an elastic body using a planetary gear mechanism, which attenuates a rotation fluctuation component included in the driving force from a prime mover and transmits the transmission to a transmission mechanism, with respect to an elastic damper mechanism not using a planetary gear mechanism. It is possible to maximize the advantage of the damper mechanism.
  • FIG. 1 is a diagram showing a configuration of a rotation fluctuation reducing device according to a first embodiment of the present invention.
  • FIG. 2 is a diagram showing a configuration of a rotation fluctuation reducing device according to a second embodiment of the present invention.
  • FIG. 3 is a cross-sectional view (along the line VII-VII in FIG. 5) of a detailed configuration of a main part of a rotation fluctuation reducing device according to a second embodiment of the present invention shown in a diagram in FIG.
  • FIG. 4 is a perspective view showing each part of the rotation fluctuation reducing device in an exploded state.
  • FIG. 5 is a front view of the elastic fluctuation damper mechanism in the rotation fluctuation reducing device of FIG. 3 in an assembled state.
  • FIG. 6 is a sectional view taken along section line VI-VI in FIG.
  • FIG. 7 is a sectional view taken along section line VII-VII in FIG.
  • FIG. 8 is a sectional view taken along section line VIII-VIII in FIG.
  • FIG. 9 is a perspective view illustrating a preferred assembly procedure of the intermediate member shown in FIG.
  • FIG. 10 is a diagram showing a configuration of a rotation fluctuation reducing device according to a third embodiment of the present invention.
  • FIG. 11 shows a detailed configuration of a main part of a rotation fluctuation reducing device according to a third embodiment of the present invention shown in a diagrammatic view in FIG. 10 as a sectional view on one side of a rotation center.
  • FIG. 11 shows a detailed configuration of a main part of a rotation fluctuation reducing device according to a third embodiment of the present invention shown in a diagrammatic view in FIG. 10 as a sectional view on one side of a rotation center.
  • FIG. 12 is a diagram showing a configuration of a rotation fluctuation reducing device according to a fourth embodiment of the present invention.
  • FIG. 13 is a diagram showing a configuration of a rotation fluctuation reducing device according to a fifth embodiment of the present invention.
  • FIG. 14 is a graph showing the frequency characteristics of the rotation fluctuation of the transmission input shaft in the embodiment (first and second embodiments) of the present invention in comparison with the prior art.
  • FIG. 15 is a graph showing the frequency characteristics of the rotation fluctuation of the transmission input shaft in the embodiment of the present invention (the first embodiment and the fifth embodiment including the clutch) in comparison with the conventional technology.
  • FIG. 1 is a schematic diagram of a first embodiment of the present invention.
  • a generator is driven by a prime mover 2 (internal combustion engine), and a driving motor for driving driving wheels is driven by the generator.
  • the present invention is directed to a device for reducing rotation fluctuation in a drive train of a hybrid vehicle. Describing this drive train, the prime mover 2 drives a generator (not shown) of the hybrid vehicle.
  • a transmission 4 is provided for optimally controlling the speed of rotation from the prime mover 2 via the flywheel 3 and transmitting the rotation to the generator.
  • the transmission 4 includes a casing 5 (a housing of the present invention), a transmission mechanism 6 disposed in the casing 5, an input shaft 7, and an output shaft 8.
  • a second input shaft 10 is provided in addition to the input shaft 7 (hereinafter referred to as a first input shaft 7) for connection between an elastic damper mechanism and a planetary gear mechanism, which will be described later, and the first input shaft 7 and the second input shaft are provided.
  • the shaft 10 is concentrically arranged and is supported by the casing 5 while sealing the lubricating oil.
  • the speed change mechanism 6 includes an input gear 11 on a first input shaft 7 that meshes in series, an output gear 12 on an output shaft 8, and an intermediate gear 14 between the input gear 11 and the output gear 12.
  • the casing 5 is sealed with lubricating oil for lubricating the meshing portion between the gears 11, ⁇ 12, ⁇ 14 ⁇ , and if necessary, well-known means for circulating the lubricating oil are provided.
  • the flywheel 3 provided on the output shaft side of the prime mover 2 is for dealing with the rotational fluctuation inevitably appearing on the output shaft side of the prime mover 2, but it alone cannot sufficiently reduce the rotational fluctuation. Therefore, the rotation fluctuation reducing device 16 is provided.
  • the rotation fluctuation reducing device 16 includes an elastic damper mechanism 18 and a planetary gear mechanism 20.
  • the planetary gear mechanism 20 is installed in the casing 5 of the transmission 4 and needs to be shared with the lubrication of the meshing part of the transmission mechanism 6 because it is necessary to lubricate the meshing portions of the gears constituting the planetary gear mechanism 20. ing.
  • the elastic damper mechanism 18 is installed outside the casing 5 because lubrication with lubricating oil is not required for the intended operation.
  • the elastic damper mechanism 18 installed outside the casing 5 and constituting the rotation fluctuation reducing device 16 of the present invention is an elastic member that connects the input member 26, the output member 28, and the input member 26 and the output member 28 in the rotational direction. And a body 30.
  • the input member 26 is connected to the prime mover 2 via the flywheel 3.
  • the elastic damper mechanism 18 has a first output shaft 34 from the output member 28 and a second output shaft 36 branched from the input member 26.
  • the planetary gear mechanism 20 according to the embodiment of the present invention installed in the casing 5 is a so-called Ravigneaux type planetary gear mechanism, and has a stepped pinion 38 (a plurality of which are arranged at intervals in the circumferential direction as is well known).
  • a Ravigneaux type planetary gear mechanism can include up to five rotating elements.
  • a carrier 46 that supports a stepped pinion 38, a small diameter sun gear 40, and a large diameter sun gear 42 And three rotating elements.
  • the connection between the elastic damper mechanism 18 and the planetary gear mechanism 20 will be described.
  • the first output shaft 34 connected to the output member 28 is directly connected to the first input shaft 7 in the casing 5 of the transmission 4.
  • the large-diameter sun gear 42 of the planetary gear mechanism 20 is installed on the first input shaft 7, and the large-diameter sun gear 42 is configured to rotate integrally with the first input shaft 7.
  • the second output shaft 36 branched from the input member 26 of the elastic damper mechanism 18 extends as it is to the second input shaft 10 of the transmission 4, and in the casing 5, the small diameter sun gear 40 of the planetary gear mechanism 20. Are rotated integrally with the second input shaft 10.
  • the elastic body 30 is arranged in series with the drive train extending from the prime mover 2 to the first input shaft 7 of the transmission 4 to change the output torque of the prime mover 2.
  • the elastic body 30 functions so as to suppress the rotation fluctuation.
  • the large-diameter sun gear 42 on the first input shaft 7 connected thereto by the first output shaft 34 is driven, and the small-diameter sun gear 40 on the second input shaft 10 connected thereto by the second output shaft 36. Driving force is transmitted.
  • the large-diameter sun gear 42 meshes with the small-diameter portion 38-2 of the stepped pinion 38, and the small-diameter sun gear 40 meshes with the large-diameter portion 38-1 (integral with the small-diameter portion 38-2) of the stepped pinion 38. If the output shaft of the prime mover 2 has no rotational fluctuation, the stepped pinion 38 rotates integrally with the carrier 46 (not shown), and the stepped pinion 38 does not rotate relative to the small-diameter sun gear 40 and the large-diameter sun gear 42.
  • the difference in the number of teeth between the small-diameter portion 38-2 and the large-diameter portion 38-1 causes a difference in rotation speed between the large-diameter sun gear 42 and the small-diameter sun gear 40.
  • the stepped pinion 38 rotates in accordance with the difference in number, and the stepped pinion 38 revolves with a carrier 46 (not shown in FIG. 1) that rotatably supports the stepped pinion 38.
  • the operation of the rotation fluctuation reduction device 16 of the present embodiment is performed by a rotation fluctuation reduction device including an elastic damper mechanism and a planetary gear mechanism housed in a housing of a conventionally proposed various types of torque converters (Patent Document 1). Operation equivalent to 1 to 4) is achieved.
  • the output from the elastic damper mechanism 18 that operates the elastic body 30 having the torsional rigidity in the rotation direction is output from the first output shaft 34 from the output member 28 and the first output shaft 34 from the input member 26. Because the two output shafts 36 are divided into two systems, the planetary gear mechanism 20 that requires lubrication of the gear meshing portion is installed in the casing 5, and the elastic damper mechanism 18 that does not require lubrication is disposed outside the casing 5.
  • FIG. 2 is a schematic view of a rotation fluctuation reducing device 116 according to a second embodiment of the present invention.
  • the difference from the rotation fluctuation reducing device 16 of FIG. 1 is only an elastic damper mechanism 118 installed outside the casing 5.
  • the elastic body of the elastic body damper mechanism 118 is composed of a first elastic body 30A and a second elastic body 30B, and an intermediate member is provided between the first elastic body 30A and the second elastic body 30B.
  • the feature is that 44 is arranged, and there is no difference in other configurations from FIG. Therefore, the same reference numbers are used for other parts.
  • the intermediate member 44 disposed between the first elastic body 30A and the second elastic body 30B in the elastic body damper mechanism 118 serves as an additional mass for torsional vibration in the drive train of the transmission 4 from the prime mover 2, It is possible to more effectively suppress the torque fluctuation component in the drive train.
  • FIGS. 3 to 8 show a structural example of the rotation fluctuation reducing device 116 of the second embodiment shown as a diagram in FIG.
  • the casing 5 is partially illustrated, and a partition wall between the casing 5 and an elastic damper mechanism 118 installed outside the casing 5 is formed by 5-1 (see also FIG. 4).
  • a partition wall for supporting the planetary gear mechanism 20 and the first input shaft 7 of the transmission 4 arranged in S is indicated by 5-2 (see also FIG. 4).
  • the transmission 4 in FIG. 1 is also disposed in the space S, but only the input gear 11 is shown.
  • the input gear 11 has an inner spline 11-1 meshed with a spline 7-1 of the first input shaft 7, and the input gear 11 rotates integrally with the first input shaft 7.
  • FIG. 2 shows a carrier 46 (formed by welding a carrier plate 46-2 to a carrier base 46-1), and a stepped pinion 38 is rotatably mounted on the carrier 46 by a pin 47. (See also FIG. 4 for the configuration of the carrier 46).
  • the structure of the elastic damper mechanism 118 installed outside the casing 5 will be described.
  • the input member 26, the output member 28, the elastic members 30A and 30B, and the intermediate member 44 in FIGS. This is shown in the schematic diagram of FIG.
  • the positional relationship between the input member 26 and the output member 28 on the rotation axis is opposite to that in FIG.
  • the elastic bodies 30A and 30B are realized as coil springs arranged alternately in the circumferential direction on the same diameter surface.
  • the coil springs 30A and 30B instead of the elastic bodies 30A and 30B, the coil springs 30A and 30B will be described.
  • 30B The three coil springs 30A and 30B are alternately arranged in the rotation direction.
  • the input member 26 is formed with three spring receiving portions 26-1 protruding radially outward and spaced apart in the circumferential direction.
  • Each spring receiving portion 26-1 includes a pair of spring receiving seats 26-1a and 26-1b separated in the rotation direction.
  • spring inner peripheral holding parts 26-2a, # 26-2b and spring outer peripheral holding parts 26-9a, # 26-9b project outward and bend.
  • the outer peripheral portion of the spring receiving portion 26-1 of the input member 26 is bent to form an extended portion 26-3 extending in the axial direction toward the prime mover and a flywheel mounting portion 26-4 at the tip thereof.
  • a flyhole mounting bolt hole 26-4 ' is formed in the flywheel mounting portion 26-4'.
  • the input member 26 forms a cylindrical portion 26-6 corresponding to the second output shaft 36 in the schematic diagram of FIG. 2 and a cylindrical portion 26-7 serving as the second input shaft 10 (FIG. 3 also). reference).
  • the output member 28 includes three spring receiving portions 28-1 protruding outward in the radius at equal intervals in the circumferential direction.
  • each spring receiving portion 28-1 forms a pair of spring receiving seats 28-1a and 28-1b that are separated in the rotation direction.
  • Each spring receiving portion 28-1 includes spring inner peripheral holding portions 28-2a and # 28-2b and outer peripheral holding portions 28-4a and # 28-4b that are bent outward on both sides.
  • the spring receiving portion 28-1 of the output member 28 has substantially the same shape as the spring receiving portion 26-1 of the input member 26, and in the assembled state (neutral state described later) of FIG.
  • the spring receiving portion 26-1 of the input member 26 is not visible because the spring receiving portion 26-1 of the input member 26 is just hidden behind (the outer flywheel mounting portion 26-4 is visible).
  • the pair of spring receiving portions 26-1a and 26-1b of each spring receiving portion 26-1 of the input member 26 is connected to the pair of spring receiving portions 28-1 of the corresponding spring receiving portion 28-1 of the output member 28.
  • Each of the seats 28-1a and # 28-1b also overlaps in the rotational direction, and the spring seats 26-1a and # 26-1b are shown in parentheses in FIG.
  • a plurality of rivet holes 28-3 are formed in the inner peripheral portion of the output member 28, and in the assembling process, the rivet holes 28-3 integrate the separate mounting member 50 with the output member 28 by the rivets 52. (See FIG. 3).
  • the intermediate member 44 is joined by rivets 45 so as to be sandwiched between the front auxiliary plate 44 'and the rear auxiliary plate 44 "at three peripheral portions in the circumferential direction (see also FIG. 8).
  • the intermediate member 44 cooperates with the front and rear auxiliary plates 44 ', # 44 "to move the window frame-shaped opening 44-1 for accommodating the coil springs 30A, 30B in the circumferential direction.
  • Each window frame-shaped opening 44-1 is provided with a pair of spring seats 44-1a,... 44-1b (spring seats 44-1a,...
  • the planes which are flush with the spring seats 44-1a and 44-1b of the auxiliary plates 44 'and # 44 also play a role, but are not denoted for the sake of simplicity).
  • the intermediate member 44 has a cylindrical portion 44-4 (rotatably fitted to the boss portion 50-2 of the mounting member 50 for the input member 28) for maintaining a centered state with respect to the center of rotation at the center.
  • the input member 26 and the output member 28 are connected by coil springs 30A and 30B as described later.
  • FIG. 4 also shows the configuration of the planetary gear mechanism 20, and it can be seen that the planetary gear mechanism 20 is isolated from the elastic damper mechanism 118 by the partition wall portion 5-1 of the casing 5.
  • the carrier 46 of the planetary gear mechanism 20 is configured by fixing a carrier plate 46-2 to a carrier base 46-1.
  • Four stepped pinions 38 are attached to the carrier 46 by pins 47 therebetween.
  • the small-diameter sun gear 40 is hidden by the carrier 46 and is not visible, but is engaged with the large-diameter portion 38-1 of the stepped pinion 38, and the large-diameter sun gear 42 is engaged with the small-diameter portion 38-2 of the stepped pinion 38. Attached to engage.
  • FIG. 4 also shows the first input shaft 7 (including the above-described splines 7-1 and # 7-2) and the partition wall 5-2 supporting the first input shaft 7.
  • the assembly of the input member 26, the output member 28, the coil springs 30A and 30B, and the intermediate member 44 will be described.
  • the extension 26-3 of the input member 26 is connected to the intermediate member. 44 so as to fit into the window frame-shaped opening 44-1.
  • the first coil spring 30A is disposed between the spring seat 26-1a of the spring seat 26-1 of the input member 26 and the spring seat 44-1a of the intermediate member 44 which is circumferentially close to and opposed to the spring seat 26-1a.
  • the second coil spring 30B is disposed and accommodated between the spring seat 44-1b of the intermediate member 44 and the spring seat 26-1b of the input member 26 which is circumferentially close to and opposed to the spring seat 44-1b.
  • the positional relationship is such that the spring receiving portion 26-1 is split between the first coil spring 30A and the second coil spring 30B at the middle in the circumferential direction in one window frame-shaped opening 44-1. .
  • the first coil spring 30A and the second coil spring 30B are balanced in the amount of contraction so as to generate a set load, and each spring receiving portion 26-1 has a window frame-shaped opening 44-1 for accommodating the same. Is located in the middle in the circumferential direction.
  • the output member 28 is mounted. That is, the spring receiving portion 28-1 of the output member 28 is positioned so as to overlap the spring receiving portion 26-1 of the input member 26 from above, and between the overlapping spring receiving portion 28-1 and the spring receiving portion 26-1.
  • each of the spring receiving portions 28-1 of the output member 28 is axially extended from the corresponding spring receiving portion 26-1 of the input member 26 by the inner surfaces 28-1 'and 2626-3' of the extending portions 26-3.
  • the elastic member damper mechanism 118 shown in the sectional view of FIG. 3 in which the intermediate member 44 is positioned between the output member 28 and the input member 26 can be inserted while sliding. (Neutral state of the elastic damper mechanism 118).
  • the intermediate member 44 constituting the elastic damper mechanism 118 is formed by integrating the front auxiliary plate 44 ′ and the rear auxiliary plate 44 ′′ by rivets 45 from the beginning of assembly.
  • the preferred assembly procedure is somewhat different and will be useful for an understanding of the construction and function of the intermediate member 44, which will now be described with reference to FIG.
  • the member 44 is separated from the front auxiliary plate 44 ′ and the rear auxiliary plate 44 ′′, and the input member 26 is disposed between the rear auxiliary plate 44 ′′ and the intermediate member 44.
  • An auxiliary plate 44 ' is located.
  • the inter-member 44, the front auxiliary plate 44 ', and the rear auxiliary plate 44 "include a plurality of pairs of aligned rivet holes 44a," 44'a., "44” a.
  • the outer peripheral surface of the extension 26-3 is the inner peripheral concave surface 44" -2 of the rear auxiliary plate 44 "(the inner peripheral surface of the window frame-shaped opening 44-1 when the intermediate member 44 is assembled. ).
  • the intermediate member 44 and the front auxiliary plate 44 ' are aligned, and each rivet 45 is inserted into each pair of aligned rivet holes 44a, # 44'a, # 44 "a, and the tip is caulked.
  • the intermediate member 44 integrates the front auxiliary plate 44 'and the rear auxiliary plate 44 "with the input member 26 positioned between the rear auxiliary plate 44" and the first and second coil springs 30A. , # 30B and subsequent steps are the same as those already described with reference to FIGS.
  • the flyhole 3 has a ring shape, and is attached to the flywheel mounting portion 26-4 of the input member 26. It is fastened together with the connecting plate 54 by the bolt 58 and the nut 60.
  • the connecting plate 54 is fastened to the end face of the output shaft side member 64 of the motor by a bolt 62.
  • the input member 26 forms a cylindrical portion 26-6 just before the partition 5-1 of the casing 5, and this corresponds to the second output shaft 36 in the schematic diagram of FIG.
  • the second output shaft 36) forms a cylindrical portion 26-7 which is introduced into the casing 5 as it is, and the cylindrical portion 26-7 forms the second input shaft 10 of the transmission in FIG.
  • the outer peripheral spline teeth 26-7 'of the cylindrical portion 26-7 are spline-fitted with the spline teeth 40-1 of the small-diameter sun gear 40 of the planetary gear mechanism 20, and transmit rotational driving force.
  • a mounting member 50 integrally connected to the output member 28 by a rivet 52 is formed on an inner peripheral spline 50-1 (formed on the inner circumference of the central boss 50-2 of the mounting member 50) as shown in FIG.
  • the spline 7-2 at the tip of the first input shaft 7, which is also the first output shaft 34 in the schematic diagram, is spline-fitted.
  • reference numeral 65 denotes a fastener such as a snap ring for fixing the assembly of the elastic damper mechanism 118 on the shaft. Thrust bearings 74, ⁇ 75, ⁇ 76 ⁇ of each part inside the transmission 4 are shown.
  • the shaft sealing structure between the two output shafts of the elastic damper mechanism 118 and the two input shafts of the transmission including the planetary gear mechanism 20 in this embodiment will be described.
  • the inner peripheral side bearing 66 and the outer peripheral side bearing 68 are arranged concentrically on the partition wall portion 5-1. Both the inner peripheral side bearing 66 and the outer peripheral side bearing 68 can be configured as a well-known sealed bearing (such as a ball bearing). That is, on the partition wall portion 5-1 side, the inner peripheral bearing 66 is disposed between the transmission rotating shaft 7 and the cylindrical portion 26-6 of the input member 26, and the outer peripheral bearing 68 is connected to the cylindrical portion 26-6. It is arranged between the inner peripheral parts 5-1 'of the partition wall part 5-1.
  • a bearing 70 is provided for supporting the first input shaft 7 on the partition 5-2 side (see also FIG. 4).
  • FIG. 5 shows a case where there is no rotation fluctuation as described above.
  • each spring receiving portion 26-1 of the input member 26 compresses the second coil spring 30B via the spring receiving seat 26-1b, and the compressed The second coil spring 30B twists the intermediate member 44 via the spring seat 44-1b of the window frame-shaped opening 44-1.
  • the twist of the intermediate member 44 is caused by the first spring via the spring receiver 44-1a.
  • the compressed first coil spring 30A twists the output member 28 counterclockwise via the spring seat 28-1a of the spring receiving portion 28-1 of the output member 28 by compressing the coil spring 30A.
  • Rotational fluctuations can be suppressed by the torsional elasticity of the coil springs 30A and 30B in such torsional vibration and the revolution of the carrier 46 and the rotation of the stepped pinion 38, which are free rotating elements in the planetary gear mechanism 20, and Further, the addition of the mass element of the intermediate member 44 between the coil springs 30A and 30B can further increase the rotation fluctuation suppressing effect.
  • FIG. 10 shows a schematic diagram of a rotation fluctuation reducing device 216 according to a third embodiment of the present invention, which is similar to the embodiment of FIG. 2 except that the branch of the second output shaft 36 is shown in FIG. From the input member 26 to the elastic member damper mechanism 218 as the intermediate member 44.
  • the manner in which the output shafts 34 and 36 are connected to the rotating elements of the planetary gear mechanism 20 is the same, and the output shafts 34 and 36 are stepped on the large-diameter and small-diameter sun gears 42 and 40 on the input shafts 7 and 10 respectively connected to the output shafts 34 and 36.
  • the rotation fluctuation in the output of the prime mover 2 appears as a rotation speed difference between the intermediate member 44 and the output member 28, and the large and small sun gears 42 and # 40 have different rotations due to the rotation of the intermediate member 44 and the output member 28 at different rotation speeds.
  • This is driven by a number, and the rotation of the carrier 46, which is a free rotating element not involved in power transmission, and the rotation of the stepped pinion 38 cooperate with the coil springs 30A and 30B to suppress rotation fluctuation.
  • FIG. 11 illustrates the schematic structure of FIG. 10 as a specific cross-sectional view of an actual machine similar to that of FIG. 3 of the second embodiment.
  • a cylindrical portion 44-5 is formed as the second output shaft 36, and is introduced into the partition 5-1 of the casing 5 to form an integral cylindrical portion 44-6 as the second input shaft 10 of the transmission 4.
  • the cylindrical portion 44-6 is spline-fitted with the small diameter sun gear 40 of the planetary gear mechanism 20.
  • the inner peripheral bearing 66 and the outer peripheral bearing 68 with seals are arranged concentrically.
  • the inner peripheral bearing 66 is disposed between the first input shaft 7 of the transmission 4 and the cylindrical portion 44-5 of the intermediate member 44, and the outer peripheral bearing 68 is disposed between the cylindrical portion 44-5 of the intermediate member 44 and the partition wall.
  • 5-1 is disposed between the inner peripheral portions 5-1 ′.
  • FIG. 12 shows a rotation fluctuation reducing device 316 according to a fourth embodiment of the present invention.
  • the rotation fluctuation reduction device 316 of this embodiment has the same basic configuration as that of the first embodiment, but is free (independent of power transmission) of the output member 28 via the second elastic body 80 through the damper mass. 82 is different from the first embodiment.
  • the second elastic body 80 and the damper mass 82 do not contribute to the transmission of the driving force, and constitute a so-called dynamic vibration absorber.
  • By adding a dynamic vibration absorber to the planetary gear mechanism 20 it is possible to change and expand the vibration damping characteristics of the prime mover 2 against rotation fluctuations.
  • FIG. 13 shows a rotation fluctuation reducing device 416 according to a fifth embodiment of the present invention.
  • This embodiment has the same basic configuration as that of the first embodiment, except that an adjustment clutch 88 is provided in the transmission 4.
  • the adjustment clutch 88 is provided between the small-diameter sun gear 40 which is an input portion of the planetary gear mechanism 20 and the second output shaft 36 of the elastic damper mechanism 18.
  • the adjustment clutch 88 can be configured as a known friction clutch.
  • the adjustment clutch 88 can have functions of fastening, breaking, and incompletely fastening (arbitrarily sliding) the input from the output shaft 36 to the planetary gear mechanism 20.
  • the vibration damping function of the planetary gear mechanism 20, that is, the planetary damper is enabled, and when the adjusting clutch 88 is engaged, the planetary gear mechanism 20 is shut off to disable the function of the planetary damper.
  • the adjustment clutch 88 may be slid into an incompletely engaged state, thereby protecting the planetary gear mechanism against excessive input and improving the vibration damping effect due to the occurrence of hysteresis required by the vibration system. Can be.
  • FIGS. 14 and 15 show the frequency characteristics of the rotational fluctuations of the transmission input shaft after numerical analysis (this analysis method is well known and results are shown only) by modeling the vehicle drive system from the prime mover 2 to the output shaft.
  • A is a conventional damper having only a coil spring
  • b is a planetary damper having no intermediate mass such as the first embodiment (FIG. 1)
  • c is a planetary mass having an intermediate mass such as the second embodiment (FIG. 2).
  • the results of the damper are shown in FIG. 14, and the characteristic b of the planetary damper has a temporary peak frequency on the lower frequency side as compared with the conventional damper characteristic a in FIG.
  • the damper characteristic a is superior to the conventional damper characteristic a in that the rotation fluctuation at a low rotation around 20 Hz, which is a problem in noise control, can be suppressed well.
  • the planetary damper has an advantage here.
  • the characteristic a of the conventional damper is superior to the characteristics b and c of the planetary damper, which can be said to be a weak point of the planetary damper.
  • first elastic body (coil spring) 30B second elastic body (coil spring) 34, a first output shaft of the elastic damper mechanism 36, a second output shaft 38 of the elastic damper mechanism 38, a stepped pinion 40 of the planetary gear mechanism, a small sun gear 44 of the planetary gear mechanism, an intermediate member 44-1... Window frame opening 44-1a, 44-1b ... spring seat 44 '... front auxiliary plate 44 "... rear auxiliary plate 46 ... carrier of planetary gear mechanism 46-1 ... carrier plate 46-2... 46-2 54 ... Connecting plate 64 ... Motor output shaft side member 66 ... Inner peripheral side bearing 68 ... Outer peripheral side bearing 80 ... Second elastic body 82 ... Damper mass 88 ... Adjustment clutch

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Abstract

An elastic body damper mechanism 18 constituting a rotational variation reducing device provided with a planetary gear mechanism is disposed outside the casing 5 of a transmission 4 and is provided with a prime mover-side input member 26 and a first output member 28. An elastic body 30 having torsional rigidity in a rotational direction is disposed between the input member 26 and the output member 28. In addition to a first output shaft 34, a second output shaft 36 branches from the elastic body damper mechanism 18 at a position closer to the input member 26 than the elastic body 30. First and second output shafts 34, 36 are introduced into the casing through a wall surface section of the casing 5. The planetary gear mechanism 16 is mounted in the casing 5 of the transmission 4. One of the three rotating elements of the planetary gear mechanism 16 is rotationally driven by the first output shaft 34, and another one is rotationally driven by the second output shaft 36. The remaining rotational element which is not involved in the transmission of power functions as a damper mass.

Description

回転変動低減装置Rotation fluctuation reduction device
 この発明は、原動機の回転変動を低減して変速機の出力軸に伝達する回転変動低減装置に関し、特に、遊星歯車機構を備えた回転変動低減装置に関するものである。 The present invention relates to a rotation fluctuation reduction device that reduces rotation fluctuation of a prime mover and transmits the rotation fluctuation to an output shaft of a transmission, and more particularly to a rotation fluctuation reduction device provided with a planetary gear mechanism.
 原動機の回転変動を低減して変速機の出力軸に伝達する回転変動低減装置として、コイルスプリングを弾性体とする弾性体ダンパ機構を遊星歯車機構に組み合わせることにより構成されたものがあり、トルクコンバータを備えた変速機におけるロックアップクラッチとの組合せにおいて、ロックアップクラッチ係合による直接駆動時の回転変動低減の目的で広く採用されている。この種の回転変動低減装置においては、大抵は、弾性体は入力部材と出力部材との間において回転方向に配置され、キャリア、リングギヤ及びサンギヤからなる遊星歯車機構の回転要素の一つが入力部材に、別の一つが出力部材に連結され、残りの一つの回転要素は動力伝達に関与しないように言わばフリーに配置される。フリーな回転要素は回転慣性系におけるダンパマスを増大させ、回転変動低減に寄与させることができる。弾性体ダンパ機構との回転要素の遊星歯車機構との連結態様としては、ストレート型のピニオンを使用した点で同一であるが、要素間の連結態様において微妙に相違した様々のものが提案されている(特許文献1~3)。また、本出願人と同一人に係るものとしては、ピニオンとして所謂ラビニヨギヤを使用したものが提案されている(特許文献4)。そして、弾性体ダンパ機構を遊星歯車機構と組み合わせることにより構成された上記の回転変動低減装置は、大抵は、トルクコンバータのロックアップクラッチとの組合せにおいての使用を意図するものであった。トルクコンバータを備えた車両においては燃料消費効率の向上の観点ではロックアップクラッチの係合を低回転域から行うようになってきており、ダンパマスの増大は低回転域からのロックアップクラッチ係合動作により問題となるこもり音等の特定騒音の抑制への対策として有効な手段である。また、トルクコンバータにおいてトルク伝達媒体として使用されるトルクコンバータ油は、そのまま遊星歯車機構の歯車噛合部の潤滑に役立てることができ、弾性体ダンパ機構を遊星歯車機構と共にトルクコンバータのハウジングに収容することで潤滑専用の潤滑装置が不必要となるという好都合があった。 As a rotation fluctuation reduction device that reduces the rotation fluctuation of the prime mover and transmits it to the output shaft of the transmission, there is a torque converter that is configured by combining an elastic damper mechanism using a coil spring as an elastic body with a planetary gear mechanism. In a combination with a lock-up clutch in a transmission equipped with a lock-up clutch, it is widely used for the purpose of reducing rotation fluctuation at the time of direct drive by engagement of the lock-up clutch. In this type of rotation fluctuation reduction device, in most cases, the elastic body is arranged in the rotation direction between the input member and the output member, and one of the rotating elements of the planetary gear mechanism including the carrier, the ring gear, and the sun gear is provided on the input member. The other one is connected to the output member, and the other one of the rotating elements is arranged so as to be free to participate in power transmission. The free rotating element increases the damper mass in the rotating inertial system and can contribute to the reduction of rotation fluctuation. The connection between the elastic damper mechanism and the rotating element and the planetary gear mechanism is the same in that a straight-type pinion is used, but various things that are slightly different in the connection between the elements have been proposed. (Patent Documents 1 to 3). Further, as a device related to the same person as the present applicant, a device using a so-called Ravigneaux gear as a pinion has been proposed (Patent Document 4). The above-described rotation fluctuation reducing device configured by combining an elastic damper mechanism with a planetary gear mechanism is generally intended for use in combination with a lock-up clutch of a torque converter. In vehicles equipped with a torque converter, from the viewpoint of improving fuel consumption efficiency, engagement of the lock-up clutch is performed from a low rotation speed region. This is an effective means as a countermeasure for suppressing specific noise such as muffled noise which becomes a problem. Further, the torque converter oil used as a torque transmission medium in the torque converter can be used for lubrication of the gear meshing portion of the planetary gear mechanism as it is, and the elastic damper mechanism is housed in the torque converter housing together with the planetary gear mechanism. Therefore, there is an advantage that a lubrication device dedicated to lubrication is not required.
特開2011-58557JP 2011-558557 特開平11-159595JP-A-11-159595 特開平10-184799JP-A-10-184799 WO2016/47660WO2016 / 47660
 弾性体ダンパ機構を遊星歯車機構と組み合わせることにより構成された回転変動低減装置は、従来は、大抵は、上述のようにトルクコンバータのハウジング内での使用を意図したものであった。しかしながら、トルクコンバータ内への設置の場合、遊星歯車機構を駆動軸と同軸に設置し、外周側にコイルスプリングを配置する構成をとらざるを得ないという空間的な制約から、動作中の大きな遠心力下でのコイルスプリングの変形を受ける支持部との摩擦発生によりコイルスプリングの円滑な弾性変形に支障をきたす懸念があり、また、コイルスプリングの弾性特性の自由度の制限等の問題が生じ得るという懸念もあった。更に、トルクコンバータ内の空間的な制約はクラッチ設置等によるコイルスプリングと回転要素間の連結態様を変更といったより高度な制振特性制御への対応を困難としていた。また、市場性の観点では、弾性体ダンパ機構を遊星歯車機構と組み合わせた回転変動低減装置の優秀な制振特性の、より近年のトレンドであるハイブリッド車への適用可能性についても希求されていた。 (4) Conventionally, a rotation fluctuation reducing device configured by combining an elastic damper mechanism with a planetary gear mechanism has been generally intended for use in a torque converter housing as described above. However, in the case of installation in a torque converter, the planetary gear mechanism is installed coaxially with the drive shaft and a coil spring is arranged on the outer peripheral side. There is a concern that smooth elastic deformation of the coil spring may be hindered due to friction with the support portion that receives the deformation of the coil spring under a force, and a problem such as a limitation on the degree of freedom of the elastic characteristic of the coil spring may occur. There was also concern. Furthermore, spatial restrictions in the torque converter make it difficult to respond to more sophisticated control of vibration damping characteristics, such as changing the manner of connection between the coil spring and the rotating element by installing a clutch or the like. Also, from the viewpoint of marketability, there has been a demand for the applicability of the excellent vibration damping characteristics of the rotation fluctuation reduction device combining the elastic damper mechanism with the planetary gear mechanism to a hybrid vehicle, which is a more recent trend. .
 この発明に係る回転変動低減装置は、原動機の回転変動を低減して出力軸に伝達する回転変動低減装置であって、原動機側の入力部材及び出力軸側の出力部材を少なくとも備え、入力部材及び出力軸間に回転方向にねじり剛性を有した弾性体を配置して構成される弾性体ダンパ機構と、複数のピニオンを回転可能に軸支して構成されるキャリアと、前記ピニオンに個別的に噛合する少なくとも2個の歯車との、都合、少なくとも3個の回転歯車要素を備えた遊星歯車機構とを備え、弾性体ダンパ機構からは前記出力軸(以下第1の出力軸)に加えて弾性体より入力部材側において回転運動を取出す第2の出力軸が分岐され、遊星歯車機構の回転要素のうち一つは前記第1の出力軸により、また、別の一つは第2の出力軸により夫々回転駆動されるようにされ、残りの少なくとも一つの動力伝達に関与しない回転要素がダンパマスとして機能するようにされ、かつ前記弾性体ダンパ機構は、遊星歯車機構を収容し、遊星歯車機構の潤滑用の潤滑油のための油浴を形成する筺体の外部に設置され、かつ前記第1の出力軸及び第2の出力軸の遊星歯車機構の対応の回転要素への連結は筺体の壁面部を介して行われるようになっている。 A rotation fluctuation reduction device according to the present invention is a rotation fluctuation reduction device that reduces the rotation fluctuation of a prime mover and transmits the reduced rotation fluctuation to an output shaft. The rotation fluctuation reduction device includes at least an input member on the prime mover side and an output member on the output shaft side. An elastic damper mechanism configured by arranging an elastic body having torsional rigidity in the rotational direction between the output shafts; a carrier configured by rotatably supporting a plurality of pinions; A planetary gear mechanism having at least three rotating gear elements, and at least two gears meshing with each other, and a resilient damper mechanism provides an elasticity in addition to the output shaft (hereinafter referred to as a first output shaft). A second output shaft for taking a rotary motion on the input member side of the body is branched, one of the rotating elements of the planetary gear mechanism is provided by the first output shaft, and the other is provided by a second output shaft. Drive each by And at least one of the remaining rotating elements not involved in power transmission functions as a damper mass, and the elastic damper mechanism houses a planetary gear mechanism and lubricating oil for lubricating the planetary gear mechanism. And a connection of the first output shaft and the second output shaft to corresponding rotating elements of the planetary gear mechanism is made through a wall portion of the housing. It has become.
 遊星歯車機構を収容する前記筺体は原動機の回転を変速して出力軸に伝達する変速機構を収容するための筺体でもあり、前記第1の出力軸は変速機構の入力軸をなすようにすることができる。 The housing for accommodating the planetary gear mechanism is also a housing for accommodating a speed change mechanism for shifting the rotation of the prime mover and transmitting the speed to an output shaft, and the first output shaft forms an input shaft of the speed change mechanism. Can be.
 弾性体ダンパ機構は、原動機側の入力部材と,出力軸側の出力部材と、入力部材と出力部材との間を回転方向に連結する弾性体とを備え、前記第2の出力軸は入力部材より分岐させる構成とすることができる。 The elastic body damper mechanism includes an input member on the prime mover side, an output member on the output shaft side, and an elastic body for connecting the input member and the output member in a rotational direction, and the second output shaft is connected to the input member. It is possible to adopt a configuration of branching more.
 弾性体ダンパ機構は、原動機側の入力部材と,第1の出力軸側の出力部材と、入力部材と出力部材との間の中間部材と、入力部材と中間部材との間を回転方向に連結する第1の弾性体と、中間部材と出力部材の間を回転方向に連結する第2の弾性体とを備え、前記第2の出力軸は入力部材より分岐される構成とすることができる。 The elastic damper mechanism connects the input member on the prime mover side, the output member on the first output shaft side, the intermediate member between the input member and the output member, and the rotational direction connection between the input member and the intermediate member. And a second elastic body that connects the intermediate member and the output member in a rotational direction, and the second output shaft can be branched from the input member.
 また、弾性体ダンパ機構は、原動機側の入力部材と,第1の出力軸側の出力部材と、入力部材と出力部材との間に設置された中間部材と、入力部材と中間部材との間を回転方向に連結する第1の弾性体と、中間部材と出力部材の間を回転方向に連結する第2の弾性体とを備え、前記第2の出力軸は中間部材より分岐させるように構成することができる。 Further, the elastic damper mechanism includes an input member on the prime mover side, an output member on the first output shaft side, an intermediate member installed between the input member and the output member, and an intermediate member provided between the input member and the intermediate member. And a second elastic body that connects between the intermediate member and the output member in the rotational direction, wherein the second output shaft is branched from the intermediate member. can do.
 更に、弾性体ダンパ機構は、原動機側の入力部材と,第1の出力軸側の出力部材と、入力部材と出力部材との間を回転方向に連結する第1の弾性体と、ダンパマスと、出力部材に対しダンパマスを動力伝達に関与することなく連結する第2の弾性体とを備え、前記第2の出力軸は入力部材より分岐される。また、筺体内に延設されて来た第2の出力軸と遊星歯車機構の間に係脱するクラッチを設置することができる。
 また、第1の出力軸及び第2の出力軸と筐体の壁面部との軸封のため内周側と外周側とのシール付ベアリングを設けることができる。
Further, the elastic body damper mechanism includes an input member on the prime mover side, an output member on the first output shaft side, a first elastic body that connects the input member and the output member in a rotational direction, a damper mass, A second elastic body that couples the damper mass to the output member without participating in power transmission, wherein the second output shaft is branched from the input member. Further, it is possible to install a clutch that is engaged and disengaged between the second output shaft extending in the housing and the planetary gear mechanism.
In addition, bearings with seals on the inner peripheral side and the outer peripheral side can be provided for sealing the first output shaft and the second output shaft with the wall of the housing.
 弾性体ダンパ機構と遊星歯車機構とを分離して、遊星歯車機構を潤滑油の供給を得ることができる筐体内に設置することで、ドライ環境下でも安定して作動する弾性体ダンパ機構に遊星歯車機構による制振効果を付加することが可能となる。 The elastic damper mechanism and the planetary gear mechanism are separated from each other, and the planetary gear mechanism is installed in a housing that can supply lubricating oil, so that the planetary gear mechanism can operate stably even in a dry environment. It is possible to add a vibration damping effect by the gear mechanism.
 弾性体ダンパ機構と遊星歯車機構とを分離することで、それぞれの構造、レイアウトの設計自由度が高まり、遊星歯車機構を用いた回転変動低減装置の最適設計が可能となる。即ち、従来のトルクコンバータ内に内蔵された遊星歯車式の回転変動低減装置では、弾性体を遊星歯車機構の外周側に配置せざるを得ない構造上の制約から、弾性体に加わる大きな遠心力に対する対策から所期の制振特性を得るための弾性体の設計の自由度に制限が課されてしまう問題点(低剛性のコイルスプリングが使用できない等)があったが、本発明においては潤滑の必要な遊星歯車機構は筐体内部に配置し、潤滑の必要がない弾性体ダンパ機構を外部に配置することができるため、弾性体の設計の自由度が高くなり、弾性体ダンパ機構に求められる制振特性の設定(特に低剛性化)の制約が少なくなり、最適設計により近い設計が可能となる。 By separating the elastic damper mechanism and the planetary gear mechanism, the degree of freedom in designing each structure and layout is increased, and the optimal design of the rotation fluctuation reducing device using the planetary gear mechanism becomes possible. That is, in the conventional planetary gear type rotation fluctuation reduction device built in the torque converter, a large centrifugal force applied to the elastic body is imposed due to a structural constraint that the elastic body must be arranged on the outer peripheral side of the planetary gear mechanism. There is a problem that the degree of freedom in designing the elastic body for obtaining the desired vibration damping characteristics is limited due to measures against the above (for example, a low-rigidity coil spring cannot be used). The planetary gear mechanism, which needs to be installed inside the housing, and the elastic damper mechanism, which does not require lubrication, can be arranged outside, so the degree of freedom in the design of the elastic body is increased. The restriction on the setting of vibration damping characteristics (particularly, low rigidity) is reduced, and a design closer to the optimal design can be performed.
 また、弾性体ダンパ機構の構造設計の自由度を高くできることから、弾性体を介した質量要素(中間部材等)の付加が容易となり、遊星歯車機構との組合わせで、更なる制振効果の向上を期待することができきる。これを要するに、本発明は、遊星歯車機構を用いない弾性体ダンパ機構に対する、原動機からの駆動力に含まれる回転変動成分を十分減衰させて変速機構へ伝達するという遊星歯車機構を用いた弾性体ダンパ機構の優位性を最大限発揮させることを可能とする。 In addition, since the degree of freedom in the structural design of the elastic damper mechanism can be increased, it is easy to add a mass element (intermediate member, etc.) via the elastic body, and by combining with the planetary gear mechanism, a further vibration suppression effect can be obtained. We can expect improvement. In short, the present invention relates to an elastic body using a planetary gear mechanism, which attenuates a rotation fluctuation component included in the driving force from a prime mover and transmits the transmission to a transmission mechanism, with respect to an elastic damper mechanism not using a planetary gear mechanism. It is possible to maximize the advantage of the damper mechanism.
図1はこの発明の第1の実施形態の回転変動低減装置の構成を示す線図である。FIG. 1 is a diagram showing a configuration of a rotation fluctuation reducing device according to a first embodiment of the present invention. 図2はこの発明の第2の実施形態の回転変動低減装置の構成を示す線図である。FIG. 2 is a diagram showing a configuration of a rotation fluctuation reducing device according to a second embodiment of the present invention. 図3は図2に線図にて示したこの発明の第2の実施形態の回転変動低減装置の要部の詳細構成を、回転中心の片側における断面図(図5のVII-VII線に沿った矢視断面図)として示したものである。FIG. 3 is a cross-sectional view (along the line VII-VII in FIG. 5) of a detailed configuration of a main part of a rotation fluctuation reducing device according to a second embodiment of the present invention shown in a diagram in FIG. FIG. 図4は回転変動低減装置の各部を分解状態で表す斜視図である。FIG. 4 is a perspective view showing each part of the rotation fluctuation reducing device in an exploded state. 図5は図3の回転変動低減装置における弾性体ダンパ機構の組立状態における正面図である。FIG. 5 is a front view of the elastic fluctuation damper mechanism in the rotation fluctuation reducing device of FIG. 3 in an assembled state. 図6は図5の切断線VI-VIに沿った断面図である。FIG. 6 is a sectional view taken along section line VI-VI in FIG. 図7は図5の切断線VII-VIIに沿った断面図である。FIG. 7 is a sectional view taken along section line VII-VII in FIG. 図8は図5の切断線VIII-VIIIに沿った断面図である。FIG. 8 is a sectional view taken along section line VIII-VIII in FIG. 図9は図3に示す中間部材の好適な組み立て手順を説明する斜視図である。FIG. 9 is a perspective view illustrating a preferred assembly procedure of the intermediate member shown in FIG. 図10はこの発明の第3の実施形態の回転変動低減装置の構成を示す線図である。FIG. 10 is a diagram showing a configuration of a rotation fluctuation reducing device according to a third embodiment of the present invention. 図11は図10に線図にて示したこの発明の第3の実施形態の回転変動低減装置の要部の詳細構成を回転中心の片側における断面図として示したものである。FIG. 11 shows a detailed configuration of a main part of a rotation fluctuation reducing device according to a third embodiment of the present invention shown in a diagrammatic view in FIG. 10 as a sectional view on one side of a rotation center. 図12はこの発明の第4の実施形態の回転変動低減装置の構成を示す線図である。FIG. 12 is a diagram showing a configuration of a rotation fluctuation reducing device according to a fourth embodiment of the present invention. 図13はこの発明の第5の実施形態の回転変動低減装置の構成を示す線図である。FIG. 13 is a diagram showing a configuration of a rotation fluctuation reducing device according to a fifth embodiment of the present invention. 図14はこの発明の実施形態(第1及び第2の実施形態)における変速機入力軸の回転変動の周波数特性を従来技術との比較で示すグラフである。FIG. 14 is a graph showing the frequency characteristics of the rotation fluctuation of the transmission input shaft in the embodiment (first and second embodiments) of the present invention in comparison with the prior art. 図15はこの発明の実施形態(第1の実施形態及びクラッチを備えた第5の実施形態)における変速機入力軸の回転変動の周波数特性を従来技術との比較で示すグラフである。FIG. 15 is a graph showing the frequency characteristics of the rotation fluctuation of the transmission input shaft in the embodiment of the present invention (the first embodiment and the fifth embodiment including the clutch) in comparison with the conventional technology.
 図1はこの発明の第1の実施形態の模式的線図であり、この実施形態は、原動機2(内燃機関)により発電機を駆動し、発電機により駆動輪の駆動用電動機を駆動するタイプのハイブリッド車の駆動トレーンにおける回転変動低減装置に向けられたものである。この駆動トレーンについて説明すると、原動機2はハイブリッド車の図示しない発電機を駆動するためのものである。発電機は図示されていないが、原動機2からのフライホイール3を介した回転を最適に調速して発電機に伝達するために変速機4が設けられる。変速機4は、ケーシング5(本発明の筐体)と、ケーシング5内に配置された変速機構6と、入力軸7と、出力軸8とを備える。後述の弾性体ダンパ機構と遊星歯車機構との接続のため前記入力軸7(以下第1の入力軸7)に加え第2の入力軸10を備え、第1の入力軸7と第2の入力軸10とは同芯配置され、かつ潤滑油の封止を行いつつケーシング5に軸支される。変速機構6は、一連に噛合する第1の入力軸7上の入力歯車11と、出力軸8上の出力歯車12と、入力歯車11と出力歯車12間の中間歯車14とから構成される。歯車11, 12, 14 間の噛合部の潤滑のためケーシング5には潤滑油が封止され、かつ必要あれば、潤滑油の循環のための周知の手段が設けられる。また、原動機2の出力軸側に設けたフライホイール3は原動機2の出力軸側に不可避的に出現する回転変動の対処のためのものであるが、それだけでは十分な回転変動低減がなしえないため、回転変動低減装置16が設置される。回転変動低減装置16は弾性体ダンパ機構18と遊星歯車機構20とから構成される。この発明によれば、遊星歯車機構20は、それを構成する歯車の噛合部の潤滑の必要上、変速機4のケーシング5内に設置され、変速機構6の噛合部の潤滑と共用するようにしている。他方、弾性体ダンパ機構18は、所期の動作のために潤滑油による潤滑は必要ないため、ケーシング5外に設置されている。 FIG. 1 is a schematic diagram of a first embodiment of the present invention. In this embodiment, a generator is driven by a prime mover 2 (internal combustion engine), and a driving motor for driving driving wheels is driven by the generator. The present invention is directed to a device for reducing rotation fluctuation in a drive train of a hybrid vehicle. Describing this drive train, the prime mover 2 drives a generator (not shown) of the hybrid vehicle. Although a generator is not shown, a transmission 4 is provided for optimally controlling the speed of rotation from the prime mover 2 via the flywheel 3 and transmitting the rotation to the generator. The transmission 4 includes a casing 5 (a housing of the present invention), a transmission mechanism 6 disposed in the casing 5, an input shaft 7, and an output shaft 8. A second input shaft 10 is provided in addition to the input shaft 7 (hereinafter referred to as a first input shaft 7) for connection between an elastic damper mechanism and a planetary gear mechanism, which will be described later, and the first input shaft 7 and the second input shaft are provided. The shaft 10 is concentrically arranged and is supported by the casing 5 while sealing the lubricating oil. The speed change mechanism 6 includes an input gear 11 on a first input shaft 7 that meshes in series, an output gear 12 on an output shaft 8, and an intermediate gear 14 between the input gear 11 and the output gear 12. The casing 5 is sealed with lubricating oil for lubricating the meshing portion between the gears 11, {12, {14}, and if necessary, well-known means for circulating the lubricating oil are provided. Further, the flywheel 3 provided on the output shaft side of the prime mover 2 is for dealing with the rotational fluctuation inevitably appearing on the output shaft side of the prime mover 2, but it alone cannot sufficiently reduce the rotational fluctuation. Therefore, the rotation fluctuation reducing device 16 is provided. The rotation fluctuation reducing device 16 includes an elastic damper mechanism 18 and a planetary gear mechanism 20. According to the present invention, the planetary gear mechanism 20 is installed in the casing 5 of the transmission 4 and needs to be shared with the lubrication of the meshing part of the transmission mechanism 6 because it is necessary to lubricate the meshing portions of the gears constituting the planetary gear mechanism 20. ing. On the other hand, the elastic damper mechanism 18 is installed outside the casing 5 because lubrication with lubricating oil is not required for the intended operation.
 この発明の回転変動低減装置16を構成する、ケーシング5外に設置される弾性体ダンパ機構18は入力部材26と、出力部材28と、入力部材26と出力部材28とを回転方向に連結する弾性体30とを具備している。入力部材26はフライホイール3を介して原動機2に連結される。弾性体ダンパ機構18は出力部材28からの第1の出力軸34と、入力部材26から分岐する第2の出力軸36を具備している。ケーシング5に設置されるこの発明の実施形態の遊星歯車機構20は、所謂ラビニヨ型の遊星歯車機構であり、段付ピニオン38(周知のように円周方向に複数が間隔をおいて配置される)を回転自在に軸支したキャリア46(図1には図示を省略(図3及び図4参照))と、段付ピニオン38の大径部38-1に内周側で噛合する小径サンギヤ40と、段付ピニオン38の小径部38-2(歯のピッチは大径部38-1と同一)に内周側で噛合する大径サンギヤ42とを具備して構成される。周知のようにラビニヨ型の遊星歯車機構は、最大5個の回転要素を備えることができるが、この実施形態では段付ピニオン38を軸支したキャリア46と、小径サンギヤ40と、大径サンギヤ42との3個の回転要素から構成される。 The elastic damper mechanism 18 installed outside the casing 5 and constituting the rotation fluctuation reducing device 16 of the present invention is an elastic member that connects the input member 26, the output member 28, and the input member 26 and the output member 28 in the rotational direction. And a body 30. The input member 26 is connected to the prime mover 2 via the flywheel 3. The elastic damper mechanism 18 has a first output shaft 34 from the output member 28 and a second output shaft 36 branched from the input member 26. The planetary gear mechanism 20 according to the embodiment of the present invention installed in the casing 5 is a so-called Ravigneaux type planetary gear mechanism, and has a stepped pinion 38 (a plurality of which are arranged at intervals in the circumferential direction as is well known). ) Is rotatably supported (not shown in FIG. 1 (see FIGS. 3 and 4)), and a small-diameter sun gear 40 meshed with the large-diameter portion 38-1 of the stepped pinion 38 on the inner peripheral side. And a large-diameter sun gear 42 meshing on the inner peripheral side with the small-diameter portion 38-2 (the pitch of the teeth is the same as the large-diameter portion 38-1) of the stepped pinion 38. As is well known, a Ravigneaux type planetary gear mechanism can include up to five rotating elements. In this embodiment, a carrier 46 that supports a stepped pinion 38, a small diameter sun gear 40, and a large diameter sun gear 42 And three rotating elements.
 そして、弾性体ダンパ機構18と遊星歯車機構20との連結関係を説明すると、出力部材28に連結される第1の出力軸34はそのまま変速機4のケーシング5内の第1の入力軸7まで延びており、この第1の入力軸7上に遊星歯車機構20の大径サンギヤ42が設置され、大径サンギヤ42は第1の入力軸7と一体回転するようにされる。そして、弾性体ダンパ機構18の入力部材26から分岐する第2の出力軸36はそのまま変速機4の第2の入力軸10まで延びており、ケーシング5内において、遊星歯車機構20の小径サンギヤ40は第2の入力軸10と一体回転するようにされる。 The connection between the elastic damper mechanism 18 and the planetary gear mechanism 20 will be described. The first output shaft 34 connected to the output member 28 is directly connected to the first input shaft 7 in the casing 5 of the transmission 4. The large-diameter sun gear 42 of the planetary gear mechanism 20 is installed on the first input shaft 7, and the large-diameter sun gear 42 is configured to rotate integrally with the first input shaft 7. The second output shaft 36 branched from the input member 26 of the elastic damper mechanism 18 extends as it is to the second input shaft 10 of the transmission 4, and in the casing 5, the small diameter sun gear 40 of the planetary gear mechanism 20. Are rotated integrally with the second input shaft 10.
 以上説明の実施形態の回転変動低減装置16の動作を説明すると、弾性体30は原動機2から変速機4の第1の入力軸7に至る駆動トレーンに直列配置され、原動機2の出力トルクを変速機4に伝達し、回転変動に対しては弾性体30がそれを抑制するように機能する。他方、第1の出力軸34によりこれに連なる第1の入力軸7上の大径サンギヤ42が駆動され、第2の出力軸36によりこれに連なる第2の入力軸10上の小径サンギヤ40に駆動力が伝達される。大径サンギヤ42は段付ピニオン38の小径部38-2と噛合し、小径サンギヤ40は段付ピニオン38の大径部38-1(小径部38-2と一体)と噛合する。原動機2の出力軸に回転変動が無いとすれば段付ピニオン38は図示しないキャリア46と一体回転し、また、段付ピニオン38の小径サンギヤ40及び大径サンギヤ42に対する相対回転は生じない。他方、原動機2の出力軸の回転変動に対しては、小径部38-2と大径部38-1の歯数差により大径サンギヤ42と小径サンギヤ40とに回転数差が生じ、この回転数差に応じて段付ピニオン38は自転すると共に、段付ピニオン38はそれを回転自在に軸支する図1には図示しないキャリア46と共に公転運動を行う。このような、段付ピニオン38の自転及び公転に伴う慣性力は、弾性体ダンパ機構18の弾性体30の弾性力と相俟って原動機2からの回転変動を効果的に抑制することができる。このような本実施形態の回転変動低減装置16の動作は、従来から各種提案されているトルクコンバータのハウジング内に収納された弾性体ダンパ機構と遊星歯車機構とよりなる回転変動低減装置(特許文献1~4)と同等の動作を達成する。そして、本実施形態においては、回転方向にねじり剛性をもたせた弾性体30を作動させる弾性体ダンパ機構18からの出力が、出力部材28からの第1の出力軸34と入力部材26からの第2の出力軸36の2系統に分けられていることにより、歯車噛合部の潤滑の必要な遊星歯車機構20をケーシング5内に設置し、潤滑の必要がない弾性体ダンパ機構18をケーシング5外に設置が可能となる。そのため、空間の大きさの制約のあるケーシング5の空間を有効利用しつつ、弾性体ダンパ機構18を、トルクコンバータのハウジングのような制約の大きい空間に配置する必要がなくなり、弾性体ダンパ機構18の設計上の大きな自由度を得ることができる。 The operation of the rotation fluctuation reducing device 16 according to the above-described embodiment will be described. The elastic body 30 is arranged in series with the drive train extending from the prime mover 2 to the first input shaft 7 of the transmission 4 to change the output torque of the prime mover 2. The elastic body 30 functions so as to suppress the rotation fluctuation. On the other hand, the large-diameter sun gear 42 on the first input shaft 7 connected thereto by the first output shaft 34 is driven, and the small-diameter sun gear 40 on the second input shaft 10 connected thereto by the second output shaft 36. Driving force is transmitted. The large-diameter sun gear 42 meshes with the small-diameter portion 38-2 of the stepped pinion 38, and the small-diameter sun gear 40 meshes with the large-diameter portion 38-1 (integral with the small-diameter portion 38-2) of the stepped pinion 38. If the output shaft of the prime mover 2 has no rotational fluctuation, the stepped pinion 38 rotates integrally with the carrier 46 (not shown), and the stepped pinion 38 does not rotate relative to the small-diameter sun gear 40 and the large-diameter sun gear 42. On the other hand, with respect to the rotation fluctuation of the output shaft of the prime mover 2, the difference in the number of teeth between the small-diameter portion 38-2 and the large-diameter portion 38-1 causes a difference in rotation speed between the large-diameter sun gear 42 and the small-diameter sun gear 40. The stepped pinion 38 rotates in accordance with the difference in number, and the stepped pinion 38 revolves with a carrier 46 (not shown in FIG. 1) that rotatably supports the stepped pinion 38. Such an inertial force caused by the rotation and revolution of the stepped pinion 38, together with the elastic force of the elastic body 30 of the elastic body damper mechanism 18, can effectively suppress the rotation fluctuation from the prime mover 2. . The operation of the rotation fluctuation reduction device 16 of the present embodiment is performed by a rotation fluctuation reduction device including an elastic damper mechanism and a planetary gear mechanism housed in a housing of a conventionally proposed various types of torque converters (Patent Document 1). Operation equivalent to 1 to 4) is achieved. In the present embodiment, the output from the elastic damper mechanism 18 that operates the elastic body 30 having the torsional rigidity in the rotation direction is output from the first output shaft 34 from the output member 28 and the first output shaft 34 from the input member 26. Because the two output shafts 36 are divided into two systems, the planetary gear mechanism 20 that requires lubrication of the gear meshing portion is installed in the casing 5, and the elastic damper mechanism 18 that does not require lubrication is disposed outside the casing 5. It becomes possible to install it. Therefore, it is not necessary to dispose the elastic damper mechanism 18 in a space having a large restriction such as a housing of the torque converter while effectively utilizing the space of the casing 5 in which the size of the space is restricted. A great degree of freedom in design can be obtained.
 図2はこの発明の第2の実施形態の回転変動低減装置116の模式図であり、図1の回転変動低減装置16との相違点は、ケーシング5外に設置される弾性体ダンパ機構118のみであり、弾性体ダンパ機構118の弾性体を第1の弾性体30Aと第2の弾性体30Bとから構成し、かつ第1の弾性体30Aと第2の弾性体30Bとの間に中間部材44を配置した点が特徴であり、その他の構成については図1と相違するところがない。従って、他の部分については同一参照番号を使用するものとする。 FIG. 2 is a schematic view of a rotation fluctuation reducing device 116 according to a second embodiment of the present invention. The difference from the rotation fluctuation reducing device 16 of FIG. 1 is only an elastic damper mechanism 118 installed outside the casing 5. The elastic body of the elastic body damper mechanism 118 is composed of a first elastic body 30A and a second elastic body 30B, and an intermediate member is provided between the first elastic body 30A and the second elastic body 30B. The feature is that 44 is arranged, and there is no difference in other configurations from FIG. Therefore, the same reference numbers are used for other parts.
 弾性体ダンパ機構118における第1の弾性体30Aと第2の弾性体30B間に配置される中間部材44は、原動機2から変速機4の駆動トレーンにおける捩じり振動に対する付加的なマスとなり、駆動トレーンにおけるより効果的なトルク変動成分の抑制を行うことができる。 The intermediate member 44 disposed between the first elastic body 30A and the second elastic body 30B in the elastic body damper mechanism 118 serves as an additional mass for torsional vibration in the drive train of the transmission 4 from the prime mover 2, It is possible to more effectively suppress the torque fluctuation component in the drive train.
 図3-図8は図2に線図として示した第2の実施形態の回転変動低減装置116を具体化した構造例を示す。図3において、ケーシング5が部分的に図示され、ケーシング5外に設置される弾性体ダンパ機構118との間の隔壁部分を5-1(図4も参照)により、また、ケーシング5の内部空間S内に配置される遊星歯車機構20及び変速機4の第1の入力軸7の支持のための隔壁を5-2(図4も参照)により示す。また、図1の変速機4もこの空間部分Sに配置されるが、そのうちの入力歯車11のみ図示される。入力歯車11は内周のスプライン11-1が第1の入力軸7のスプライン7-1に噛合され、入力歯車11は第1の入力軸7と一体回転される。遊星歯車機構20の構成として、図2にも示される段付ピニオン38と、段付ピニオン38の大径部38-1に内周側で噛合する小径サンギヤ40と、段付ピニオン38の小径部38-2に内周側で噛合する大径サンギヤ42とが示される。大径サンギヤ42は内周のスプライン42-1が第1の入力軸7のスプライン7-1に噛合され、大径サンギヤ42は第1の入力軸7と一体回転される。また、図2には省略されたキャリア46(キャリアベース46-1にキャリアプレート46-2 を溶接して構成される)が示され、キャリア46に段付ピニオン38がピン47により回転自在に軸支される(キャリア46の構成については図4も参照)。 FIGS. 3 to 8 show a structural example of the rotation fluctuation reducing device 116 of the second embodiment shown as a diagram in FIG. In FIG. 3, the casing 5 is partially illustrated, and a partition wall between the casing 5 and an elastic damper mechanism 118 installed outside the casing 5 is formed by 5-1 (see also FIG. 4). A partition wall for supporting the planetary gear mechanism 20 and the first input shaft 7 of the transmission 4 arranged in S is indicated by 5-2 (see also FIG. 4). The transmission 4 in FIG. 1 is also disposed in the space S, but only the input gear 11 is shown. The input gear 11 has an inner spline 11-1 meshed with a spline 7-1 of the first input shaft 7, and the input gear 11 rotates integrally with the first input shaft 7. As the configuration of the planetary gear mechanism 20, a stepped pinion 38 also shown in FIG. 2, a small-diameter sun gear 40 meshed with the large-diameter portion 38-1 of the stepped pinion 38 on the inner peripheral side, and a small-diameter portion of the stepped pinion 38 The large-diameter sun gear 42 meshing on the inner peripheral side is shown at 38-2. The large-diameter sun gear 42 has an inner peripheral spline 42-1 meshed with the spline 7-1 of the first input shaft 7, and the large-diameter sun gear 42 rotates integrally with the first input shaft 7. FIG. 2 shows a carrier 46 (formed by welding a carrier plate 46-2 to a carrier base 46-1), and a stepped pinion 38 is rotatably mounted on the carrier 46 by a pin 47. (See also FIG. 4 for the configuration of the carrier 46).
 ケーシング5外に設置される弾性体ダンパ機構118の構成を説明すると、図3及び図4における入力部材26、出力部材28、弾性体30A, 30B及び中間部材44に関しては、基本的な構成部材として図2の概略図には示されている。また、回転軸上での入力部材26と出力部材28の位置関係は図2とは逆となっている。弾性体30A, 30Bは図4の分解図に示すように同一直径面において円周方向に交互に配置されたコイルスプリングとして実現されており、以下、弾性体30A, 30Bの代わりにコイルスプリング30A, 30Bと称するものとする。コイルスプリング30A, 30Bは回転方向に交互に3個ずつ配置されている。図4において、入力部材26は半径外方に突出したスプリング受部26-1を円周方向に離間して3個形成する。各スプリング受部26-1は回転方向に離間した一対のスプリング受座26-1a, 26-1bを備える。各スプリング受部26-1の両側にスプリング内周保持部26-2a, 26-2b、スプリング外周保持部26-9a, 26-9bが外向きに突出し曲折形成される。そして、入力部材26のスプリング受部26-1の外周部は曲折されて原動機側に軸方向へ延びた延出部26-3及びその先端のフライホイール取付部26-4を形成する。フライホイール取付部26-4 にフライホール取付け用のボルト孔26-4’が穿設される。また、入力部材26は、図2の略図における第2の出力軸36に相当する筒状部26-6と、第2の入力軸10となる筒状部26-7を形成する(図3も参照)。 The structure of the elastic damper mechanism 118 installed outside the casing 5 will be described. The input member 26, the output member 28, the elastic members 30A and 30B, and the intermediate member 44 in FIGS. This is shown in the schematic diagram of FIG. The positional relationship between the input member 26 and the output member 28 on the rotation axis is opposite to that in FIG. As shown in the exploded view of FIG. 4, the elastic bodies 30A and 30B are realized as coil springs arranged alternately in the circumferential direction on the same diameter surface. Hereinafter, instead of the elastic bodies 30A and 30B, the coil springs 30A and 30B will be described. 30B. The three coil springs 30A and 30B are alternately arranged in the rotation direction. In FIG. 4, the input member 26 is formed with three spring receiving portions 26-1 protruding radially outward and spaced apart in the circumferential direction. Each spring receiving portion 26-1 includes a pair of spring receiving seats 26-1a and 26-1b separated in the rotation direction. On both sides of each spring receiving part 26-1, spring inner peripheral holding parts 26-2a, # 26-2b and spring outer peripheral holding parts 26-9a, # 26-9b project outward and bend. The outer peripheral portion of the spring receiving portion 26-1 of the input member 26 is bent to form an extended portion 26-3 extending in the axial direction toward the prime mover and a flywheel mounting portion 26-4 at the tip thereof. A flyhole mounting bolt hole 26-4 'is formed in the flywheel mounting portion 26-4'. Further, the input member 26 forms a cylindrical portion 26-6 corresponding to the second output shaft 36 in the schematic diagram of FIG. 2 and a cylindrical portion 26-7 serving as the second input shaft 10 (FIG. 3 also). reference).
 出力部材28は半径外方に突出するスプリング受部28-1を円周方向に等間隔に離間して3個備える。図4において、各スプリング受部28-1は、回転方向に離間した一対のスプリング受座28-1a, 28-1bを形成する。各スプリング受部28-1は両側において外向きに曲折されたスプリング内周保持部28-2a, 28-2b及び外周保持部28-4a, 28-4bを備える。出力部材28のスプリング受部28-1は、正面から見ると、入力部材26のスプリング受部26-1と実質的に同一形状をなし、図5の組立状態(後述中立状態)では、出力部材28のスプリング受部28-1の背後に入力部材26のスプリング受部26-1は丁度隠されてしまうため見えていない(外側のフライホイール取付部26-4は見えている)。そして、中立状態においては、入力部材26の各スプリング受部26-1の一対のスプリング受座26-1a, 26-1bは、出力部材28の対応するスプリング受部28-1の一対のスプリング受座28-1a, 28-1bと、夫々、回転方向の位置も重なっており、図5ではスプリング受座26-1a, 26-1bは括弧を付して示す。また、出力部材28の内周部にリベット孔28-3が複数形成され、組立工程においては、このリベット孔28-3は、別体の取付部材50をリベット52により出力部材28と一体化するのに使用される(図3参照)。 The output member 28 includes three spring receiving portions 28-1 protruding outward in the radius at equal intervals in the circumferential direction. In FIG. 4, each spring receiving portion 28-1 forms a pair of spring receiving seats 28-1a and 28-1b that are separated in the rotation direction. Each spring receiving portion 28-1 includes spring inner peripheral holding portions 28-2a and # 28-2b and outer peripheral holding portions 28-4a and # 28-4b that are bent outward on both sides. When viewed from the front, the spring receiving portion 28-1 of the output member 28 has substantially the same shape as the spring receiving portion 26-1 of the input member 26, and in the assembled state (neutral state described later) of FIG. The spring receiving portion 26-1 of the input member 26 is not visible because the spring receiving portion 26-1 of the input member 26 is just hidden behind (the outer flywheel mounting portion 26-4 is visible). In the neutral state, the pair of spring receiving portions 26-1a and 26-1b of each spring receiving portion 26-1 of the input member 26 is connected to the pair of spring receiving portions 28-1 of the corresponding spring receiving portion 28-1 of the output member 28. Each of the seats 28-1a and # 28-1b also overlaps in the rotational direction, and the spring seats 26-1a and # 26-1b are shown in parentheses in FIG. Also, a plurality of rivet holes 28-3 are formed in the inner peripheral portion of the output member 28, and in the assembling process, the rivet holes 28-3 integrate the separate mounting member 50 with the output member 28 by the rivets 52. (See FIG. 3).
 図4において、中間部材44は円周方向の3箇所における外周部位において、前面補助板44´と後面補助板44″とで挟まれるようにリベット45で合体させた3ピース構造(図8も参照)をなすことが分かる。中間部材44は、前面及び後面の補助板44’, 44”と協働し、コイルスプリング30A, 30Bの収容のための窓枠状開口部44-1を円周方向に離間して等間隔に3個形成している。各窓枠状開口部44-1は、回転方向に離間した一対のスプリング受座44-1a, 44-1b(スプリング受座44-1a, 44-1bの形成には図4に示す通り前後の補助板44’, 44”のスプリング受座44-1a, 44-1bと面一をなす面も関与するが簡明のため符号は付してない)を形成し、また、スプリング受座44-1a, 44-1bに近接して、前面補助板44´と後面補助板44″は相互に離間方向に曲折部をなし、これにより、夫々、一対のスプリング外周保持部44’-1a, 44”-1a及び44’-1b, 44”-1bを形成する。中間部材44は中心部に回転中心に対する芯合状態を維持するための筒状部44-4(入力部材28用の取付部材50のボス部50-2に回転可能に嵌合される)を有しており、入力部材26及び出力部材28に、後述のように、コイルスプリング30A, 30Bにより連結される。 In FIG. 4, the intermediate member 44 is joined by rivets 45 so as to be sandwiched between the front auxiliary plate 44 'and the rear auxiliary plate 44 "at three peripheral portions in the circumferential direction (see also FIG. 8). The intermediate member 44 cooperates with the front and rear auxiliary plates 44 ', # 44 "to move the window frame-shaped opening 44-1 for accommodating the coil springs 30A, 30B in the circumferential direction. Are formed at equal intervals. Each window frame-shaped opening 44-1 is provided with a pair of spring seats 44-1a,... 44-1b (spring seats 44-1a,... The planes which are flush with the spring seats 44-1a and 44-1b of the auxiliary plates 44 'and # 44 "also play a role, but are not denoted for the sake of simplicity). , # 44-1b, the front auxiliary plate 44 'and the rear auxiliary plate 44 "form a bent portion in a direction away from each other, whereby a pair of spring outer peripheral holding portions 44'-1a," 44 "-are respectively provided. 1a and 44'-1b, forming "44" -1b. The intermediate member 44 has a cylindrical portion 44-4 (rotatably fitted to the boss portion 50-2 of the mounting member 50 for the input member 28) for maintaining a centered state with respect to the center of rotation at the center. The input member 26 and the output member 28 are connected by coil springs 30A and 30B as described later.
 図4には遊星歯車機構20の構成も描かれており、ケーシング5の隔壁部分5-1により弾性体ダンパ機構118と隔離されることが分かる。遊星歯車機構20のキャリア46はキャリアベース46-1にキャリアプレート46-2を固定して構成され、その間に4個の段付ピニオン38がピン47によって取り付けられている。小径サンギヤ40は図4においては、キャリア46により隠れて見えていないが、段付ピニオン38の大径部38-1に噛合され、大径サンギヤ42は段付ピニオン38の小径部38-2に噛合するように取り付けられる。図4には第1の入力軸7(上述のスプライン7-1, 7-2を備える)及び第1の入力軸7を支持する隔壁5-2も見えている。 FIG. 4 also shows the configuration of the planetary gear mechanism 20, and it can be seen that the planetary gear mechanism 20 is isolated from the elastic damper mechanism 118 by the partition wall portion 5-1 of the casing 5. The carrier 46 of the planetary gear mechanism 20 is configured by fixing a carrier plate 46-2 to a carrier base 46-1. Four stepped pinions 38 are attached to the carrier 46 by pins 47 therebetween. In FIG. 4, the small-diameter sun gear 40 is hidden by the carrier 46 and is not visible, but is engaged with the large-diameter portion 38-1 of the stepped pinion 38, and the large-diameter sun gear 42 is engaged with the small-diameter portion 38-2 of the stepped pinion 38. Attached to engage. FIG. 4 also shows the first input shaft 7 (including the above-described splines 7-1 and # 7-2) and the partition wall 5-2 supporting the first input shaft 7.
 入力部材26、出力部材28、コイルスプリング30A, 30B及び中間部材44の組立について説明すると、入力部材26を中間部材44の手前においた状態で、入力部材26の延出部26-3を中間部材44の窓枠状開口部44-1に嵌まり込むように位置させる。第1のコイルスプリング30Aは、入力部材26のスプリング受部26-1のスプリング受座26-1aとこれに円周方向に近接対向する中間部材44のスプリング受座44-1aとの間に配置収容し、他方、第2のコイルスプリング30Bは中間部材44のスプリング受座44-1bとこれに円周方向に近接対向する入力部材26のスプリング受座26-1bとの間に配置収容する。即ち、一つの窓枠状開口部44-1において円周方向の中間においてスプリング受部26-1が第1のコイルスプリング30Aと第2のコイルスプリング30B間に割って入るような位置関係となる。この状態においては第1のコイルスプリング30Aと第2のコイルスプリング30Bとは設定荷重を生ずるべく収縮量が均衡し、各スプリング受部26-1はそれを収容する窓枠状開口部44-1の円周方向の中間に位置することになる。この状態において出力部材28の装着が行なわれる。即ち、出力部材28のスプリング受部28-1は入力部材26のスプリング受部26-1に上から重なるように位置され、この重なり合ったスプリング受部28-1とスプリング受部26-1間で、スプリング受座28-1aがスプリング受座26-1aと、スプリング受座28-1bがスプリング受座26-1bと、回転方向に整列位置する。そのため、出力部材28の各スプリング受部28-1を入力部材26の対応のスプリング受部26-1から軸方向に延出部26-3の内面同士28-1’, 26-3’同士で摺接させつつ挿入することができ、その結果、出力部材28と入力部材26との間に中間部材44を位置させた図3の断面図にて示す弾性体ダンパ機構118の組立て状態(作動中の弾性体ダンパ機構118の中立状態)を得ることができる。 The assembly of the input member 26, the output member 28, the coil springs 30A and 30B, and the intermediate member 44 will be described. With the input member 26 in front of the intermediate member 44, the extension 26-3 of the input member 26 is connected to the intermediate member. 44 so as to fit into the window frame-shaped opening 44-1. The first coil spring 30A is disposed between the spring seat 26-1a of the spring seat 26-1 of the input member 26 and the spring seat 44-1a of the intermediate member 44 which is circumferentially close to and opposed to the spring seat 26-1a. On the other hand, the second coil spring 30B is disposed and accommodated between the spring seat 44-1b of the intermediate member 44 and the spring seat 26-1b of the input member 26 which is circumferentially close to and opposed to the spring seat 44-1b. In other words, the positional relationship is such that the spring receiving portion 26-1 is split between the first coil spring 30A and the second coil spring 30B at the middle in the circumferential direction in one window frame-shaped opening 44-1. . In this state, the first coil spring 30A and the second coil spring 30B are balanced in the amount of contraction so as to generate a set load, and each spring receiving portion 26-1 has a window frame-shaped opening 44-1 for accommodating the same. Is located in the middle in the circumferential direction. In this state, the output member 28 is mounted. That is, the spring receiving portion 28-1 of the output member 28 is positioned so as to overlap the spring receiving portion 26-1 of the input member 26 from above, and between the overlapping spring receiving portion 28-1 and the spring receiving portion 26-1. The spring seat 28-1a and the spring seat 26-1b are aligned with the spring seat 26-1b in the rotation direction. Therefore, each of the spring receiving portions 28-1 of the output member 28 is axially extended from the corresponding spring receiving portion 26-1 of the input member 26 by the inner surfaces 28-1 'and 2626-3' of the extending portions 26-3. The elastic member damper mechanism 118 shown in the sectional view of FIG. 3 in which the intermediate member 44 is positioned between the output member 28 and the input member 26 can be inserted while sliding. (Neutral state of the elastic damper mechanism 118).
 以上の図4-図8の説明においては、弾性体ダンパ機構118を構成する中間部材44は、組立ての最初から、前面補助板44´と後面補助板44″とをリベット45により一体化した3ピース構造をなしているように説明しているが、これは、中間部材44の各部の構成をその機能との関連で説明するために好都合であることからそのようにしたものであるが、実際の好適な組立手順は、幾分様相が相違しており、また、中間部材44の構成及び機能の理解のため有益と思われるので、これを図9により説明する。図9に示すように中間部材44は前面補助板44´と後面補助板44″とは、分離された状態でかつ入力部材26が後面補助板44″と中間部材44との間に配置され、中間部材44の手前に前面補助板44´が位置される。中間部材44、前面補助板44´、後面補助板44″は、整列したリベット孔44a, 44’a. 44"aの複数の対を備える。入力部材26の延出部26-3を後面補助板44″に、延出部26-3の外周面が後面補助板44″の内周凹面44”-2(中間部材44の組立て状態で窓枠状開口部44-1の内周面となる)に沿接するように挿入する。この状態で中間部材44及び前面補助板44´を合わせ、整列したリベット孔44a, 44’a. 44"aの各対に夫々のリベット45が挿入され、先端をかしめる。その結果、中間部材44は後面補助板44″との間に入力部材26を位置させた状態で前面補助板44´及び後面補助板44″を一体化する。これに継続する、第1、第2のコイルスプリング30A, 30Bの組み付け以降の工程は図4-図8により既に説明したものと同一である。 In the above description of FIGS. 4 to 8, the intermediate member 44 constituting the elastic damper mechanism 118 is formed by integrating the front auxiliary plate 44 ′ and the rear auxiliary plate 44 ″ by rivets 45 from the beginning of assembly. Although it is described as having a piece structure, this is because it is convenient to explain the configuration of each part of the intermediate member 44 in relation to its function, but this is not the case. The preferred assembly procedure is somewhat different and will be useful for an understanding of the construction and function of the intermediate member 44, which will now be described with reference to FIG. The member 44 is separated from the front auxiliary plate 44 ′ and the rear auxiliary plate 44 ″, and the input member 26 is disposed between the rear auxiliary plate 44 ″ and the intermediate member 44. An auxiliary plate 44 'is located. The inter-member 44, the front auxiliary plate 44 ', and the rear auxiliary plate 44 "include a plurality of pairs of aligned rivet holes 44a," 44'a., "44" a. On the plate 44 ", the outer peripheral surface of the extension 26-3 is the inner peripheral concave surface 44" -2 of the rear auxiliary plate 44 "(the inner peripheral surface of the window frame-shaped opening 44-1 when the intermediate member 44 is assembled. ). In this state, the intermediate member 44 and the front auxiliary plate 44 'are aligned, and each rivet 45 is inserted into each pair of aligned rivet holes 44a, # 44'a, # 44 "a, and the tip is caulked. As a result, the intermediate member 44 integrates the front auxiliary plate 44 'and the rear auxiliary plate 44 "with the input member 26 positioned between the rear auxiliary plate 44" and the first and second coil springs 30A. , # 30B and subsequent steps are the same as those already described with reference to FIGS.
 このように組み立てられた弾性体ダンパ機構118の原動機側及び変速機側への連結を説明すると、図3において、フライホール3はリング形状をなし、入力部材26のフライホイール取付部26-4に連結板54と共にボルト58及びナット60により締結される。連結板54はボルト62によって原動機の出力軸側部材64の端面に締結される。また、入力部材26はケーシング5の隔壁部分5-1の手前で筒状部26-6を形成し、これが図2の略図における第2の出力軸36に相当し、筒状部26-6(第2の出力軸36)はそのままケーシング5内に導入される筒状部26-7を形成し、筒状部26-7は図2における変速機の第2の入力軸10を形成する。筒状部26-7は外周のスプライン歯26-7’が遊星歯車機構20の小径サンギヤ40のスプライン歯40-1とスプライン嵌合し、回転駆動力の伝達を行なう。また、出力部材28については出力部材28とリベット52にて一体連結された取付部材50が内周スプライン50-1(取付部材50の中心ボス部50-2の内周に形成)において図2の略図において第1の出力軸34でもある第1の入力軸7の先端のスプライン7-2とスプライン嵌合する。このスプライン嵌合部の外周面(中心ボス部50-2の外周面)に中間部材44の筒状支持部44-4が嵌合することにより、中間部材44は回転中心との芯合状態をいつも維持しつつ回転することができる。尚、図3において、65は弾性体ダンパ機構118の組立体を軸上に固定するためのスナップリング等の締結具を示す。また、変速機4内部の各部のスラスト軸受74, 75, 76 で示す。 The connection of the elastic damper mechanism 118 assembled in this way to the prime mover side and the transmission side will be described. In FIG. 3, the flyhole 3 has a ring shape, and is attached to the flywheel mounting portion 26-4 of the input member 26. It is fastened together with the connecting plate 54 by the bolt 58 and the nut 60. The connecting plate 54 is fastened to the end face of the output shaft side member 64 of the motor by a bolt 62. The input member 26 forms a cylindrical portion 26-6 just before the partition 5-1 of the casing 5, and this corresponds to the second output shaft 36 in the schematic diagram of FIG. The second output shaft 36) forms a cylindrical portion 26-7 which is introduced into the casing 5 as it is, and the cylindrical portion 26-7 forms the second input shaft 10 of the transmission in FIG. The outer peripheral spline teeth 26-7 'of the cylindrical portion 26-7 are spline-fitted with the spline teeth 40-1 of the small-diameter sun gear 40 of the planetary gear mechanism 20, and transmit rotational driving force. As for the output member 28, a mounting member 50 integrally connected to the output member 28 by a rivet 52 is formed on an inner peripheral spline 50-1 (formed on the inner circumference of the central boss 50-2 of the mounting member 50) as shown in FIG. The spline 7-2 at the tip of the first input shaft 7, which is also the first output shaft 34 in the schematic diagram, is spline-fitted. By fitting the cylindrical support portion 44-4 of the intermediate member 44 to the outer peripheral surface of the spline fitting portion (the outer peripheral surface of the center boss portion 50-2), the intermediate member 44 is aligned with the center of rotation. You can rotate while always maintaining. In FIG. 3, reference numeral 65 denotes a fastener such as a snap ring for fixing the assembly of the elastic damper mechanism 118 on the shaft. Thrust bearings 74, {75, {76} of each part inside the transmission 4 are shown.
 この実施形態における弾性体ダンパ機構118の二本の出力軸と遊星歯車機構20を内臓した変速機の二本の入力軸との軸封構造について説明すると、変速機4の弾性体ダンパ機構118側の隔壁部分5-1に内周側軸受66と外周側軸受68とが同芯に配置される。内周側軸受66も外周側軸受68もいずれもそれ自体は周知のシール付ベアリング(ボールベアリング等)として構成することができる。即ち、隔壁部分5-1側においては、内周側軸受66は変速機回転軸7と入力部材26の筒状部26-6間に配置され、外周側軸受68は筒状部26-6と隔壁部分5-1の内周部5-1´間に配置される。これにより、弾性体ダンパ機構118とケーシング5間の同軸の二本の入・出力軸のケーシング5の隔壁部による支持及び軸封を達成することができる。また、第1の入力軸7の隔壁5-2側の支持のため軸受70が設けられる(図4も参照)。 The shaft sealing structure between the two output shafts of the elastic damper mechanism 118 and the two input shafts of the transmission including the planetary gear mechanism 20 in this embodiment will be described. The inner peripheral side bearing 66 and the outer peripheral side bearing 68 are arranged concentrically on the partition wall portion 5-1. Both the inner peripheral side bearing 66 and the outer peripheral side bearing 68 can be configured as a well-known sealed bearing (such as a ball bearing). That is, on the partition wall portion 5-1 side, the inner peripheral bearing 66 is disposed between the transmission rotating shaft 7 and the cylindrical portion 26-6 of the input member 26, and the outer peripheral bearing 68 is connected to the cylindrical portion 26-6. It is arranged between the inner peripheral parts 5-1 'of the partition wall part 5-1. Thereby, the support and shaft sealing of the two coaxial input / output shafts between the elastic damper mechanism 118 and the casing 5 by the partition wall of the casing 5 can be achieved. Further, a bearing 70 is provided for supporting the first input shaft 7 on the partition 5-2 side (see also FIG. 4).
 図3-図8の回転変動低減装置116の動作を、弾性体ダンパ機構118を中心に説明すると、図5は上述の通り回転変動が無い場合を示す。この状態から入力部材26が時計方向に捻られると、入力部材26の各スプリング受部26-1がスプリング受座26-1aを介して第1のコイルスプリング30Aを圧縮し、圧縮された第1のコイルスプリング30Aは、窓枠状開口部44-1のスプリング受座44-1aを介して中間部材44を捻り、中間部材44の捻りはスプリング受座44-1bを介して第2のコイルスプリング30Bを圧縮し、圧縮された第2のコイルスプリング30Bは、スプリング受部28-1のスプリング受座28-1bを介して出力部材28を時計方向に捻る。逆に、入力部材26が反時計方向に捻られると、入力部材26の各スプリング受部26-1がスプリング受座26-1bを介して第2のコイルスプリング30Bを圧縮し、圧縮された第2のコイルスプリング30Bは、窓枠状開口部44-1のスプリング受座44-1bを介して中間部材44を捻り、中間部材44の捻りはスプリング受部44-1aを介して、第1のコイルスプリング30Aを圧縮し、圧縮された第1のコイルスプリング30Aは、出力部材28のスプリング受部28-1のスプリング受座28-1aを介し出力部材28を反時計方向に捻る。このような捻り振動におけるコイルスプリング30A, 30Bの捻り弾性と遊星歯車機構20におけるフリーな回転要素であるキャリア46の公転及び段付ピニオン38の自転とにより回転変動の抑制を行なうことができ、また、コイルスプリング30A, 30B間の中間部材44の質量要素の付加による一層の回転変動抑制効果の増大を得ることができる。 動作 The operation of the rotation fluctuation reduction device 116 shown in FIGS. 3 to 8 will be described focusing on the elastic damper mechanism 118. FIG. 5 shows a case where there is no rotation fluctuation as described above. When the input member 26 is twisted clockwise from this state, each spring receiving portion 26-1 of the input member 26 compresses the first coil spring 30A via the spring receiving seat 26-1a, and the compressed first coil spring 30A is pressed. The coil spring 30A twists the intermediate member 44 through the spring seat 44-1a of the window frame-shaped opening 44-1. The torsion of the intermediate member 44 is adjusted by the second coil spring through the spring seat 44-1b. The compressed second coil spring 30B twists the output member 28 clockwise through the spring seat 28-1b of the spring receiving portion 28-1. Conversely, when the input member 26 is twisted counterclockwise, each spring receiving portion 26-1 of the input member 26 compresses the second coil spring 30B via the spring receiving seat 26-1b, and the compressed The second coil spring 30B twists the intermediate member 44 via the spring seat 44-1b of the window frame-shaped opening 44-1. The twist of the intermediate member 44 is caused by the first spring via the spring receiver 44-1a. The compressed first coil spring 30A twists the output member 28 counterclockwise via the spring seat 28-1a of the spring receiving portion 28-1 of the output member 28 by compressing the coil spring 30A. Rotational fluctuations can be suppressed by the torsional elasticity of the coil springs 30A and 30B in such torsional vibration and the revolution of the carrier 46 and the rotation of the stepped pinion 38, which are free rotating elements in the planetary gear mechanism 20, and Further, the addition of the mass element of the intermediate member 44 between the coil springs 30A and 30B can further increase the rotation fluctuation suppressing effect.
 図10は本発明の第3の実施形態の回転変動低減装置216の模式的線図を示し、図2の実施形態と類似するが、相違点は、第2の出力軸36の分岐を図2の入力部材26から中間部材44として弾性体ダンパ機構218に構成したものである。出力軸34, 36の遊星歯車機構20の回転要素に対する連結態様は同様であり、出力軸34, 36に夫々連結される入力軸7, 10上の大径、小径のサンギヤ42, 40に段付ピニオン38の小、大経部38-2, 38-1を噛合させる構成は相違がない。原動機2の出力における回転変動は中間部材44と出力部材28との回転数差として現れ、中間部材44と出力部材28との異なる回転数の回転により大、小径のサンギヤ42, 40は異なった回転数により駆動され、これは、動力伝達に関与しないフリーな回転要素であるキャリア46の公転及び段付ピニオン38の自転とによりコイルスプリング30A, 30Bと相俟って回転変動の抑制を行なう。 FIG. 10 shows a schematic diagram of a rotation fluctuation reducing device 216 according to a third embodiment of the present invention, which is similar to the embodiment of FIG. 2 except that the branch of the second output shaft 36 is shown in FIG. From the input member 26 to the elastic member damper mechanism 218 as the intermediate member 44. The manner in which the output shafts 34 and 36 are connected to the rotating elements of the planetary gear mechanism 20 is the same, and the output shafts 34 and 36 are stepped on the large-diameter and small-diameter sun gears 42 and 40 on the input shafts 7 and 10 respectively connected to the output shafts 34 and 36. There is no difference in the configuration in which the small and large suture portions 38-2 and 38-1 of the pinion 38 are engaged. The rotation fluctuation in the output of the prime mover 2 appears as a rotation speed difference between the intermediate member 44 and the output member 28, and the large and small sun gears 42 and # 40 have different rotations due to the rotation of the intermediate member 44 and the output member 28 at different rotation speeds. This is driven by a number, and the rotation of the carrier 46, which is a free rotating element not involved in power transmission, and the rotation of the stepped pinion 38 cooperate with the coil springs 30A and 30B to suppress rotation fluctuation.
 図11は図10の概略構造を第2の実施形態の図3と同様な実機での具体的断面図として画いたものであり、図3との相違点を中心に説明すると、中間部材44が第2の出力軸36として筒状部44-5を形成し、ケーシング5の隔壁5-1に導入され、変速機4の第2の入力軸10として一体の筒状部44-6を形成し、筒状部44-6は遊星歯車機構20の小径サンギヤ40とスプライン嵌合される。図3と同様にシール付の内周側軸受66と外周側軸受68とが同芯に配置される。内周側軸受66は変速機4の第1の入力軸7と中間部材44の筒状部44-5間に配置され、外周側軸受68は中間部材44の筒状部44-5と隔壁部分5-1の内周部5-1’間に配置される。これにより、弾性体ダンパ機構218とケーシング5間の同軸の二本の入・出力軸のケーシング5の隔壁部による支持及び軸封を達成することができる。この実施形態では入力部材26は出力軸側にはフリーであり、中間開口部26-5が中間部材44の筒状部44-5と同芯を維持しつつスムーズに回転可能に嵌合される。 FIG. 11 illustrates the schematic structure of FIG. 10 as a specific cross-sectional view of an actual machine similar to that of FIG. 3 of the second embodiment. A cylindrical portion 44-5 is formed as the second output shaft 36, and is introduced into the partition 5-1 of the casing 5 to form an integral cylindrical portion 44-6 as the second input shaft 10 of the transmission 4. The cylindrical portion 44-6 is spline-fitted with the small diameter sun gear 40 of the planetary gear mechanism 20. As in FIG. 3, the inner peripheral bearing 66 and the outer peripheral bearing 68 with seals are arranged concentrically. The inner peripheral bearing 66 is disposed between the first input shaft 7 of the transmission 4 and the cylindrical portion 44-5 of the intermediate member 44, and the outer peripheral bearing 68 is disposed between the cylindrical portion 44-5 of the intermediate member 44 and the partition wall. 5-1 is disposed between the inner peripheral portions 5-1 ′. Thereby, the support and shaft sealing of the two coaxial input / output shafts between the elastic damper mechanism 218 and the casing 5 by the partition of the casing 5 can be achieved. In this embodiment, the input member 26 is free on the output shaft side, and the intermediate opening 26-5 is smoothly rotatably fitted while maintaining the same concentricity with the cylindrical portion 44-5 of the intermediate member 44. .
 図12は本発明の第4の実施形態の回転変動低減装置316を示す。この実施形態の回転変動低減装置316は第1の実施形態と基本構成は同様であるが、出力部材28に対してフリーに(動力伝達とは無関係に)第2の弾性体80を介してダンパマス82を取付けた点が相違する。この実施形態においては、第2の弾性体80及びダンパマス82は駆動力の伝達には関与せず、所謂動吸振器を構成している。遊星歯車機構20に動吸振器を付加することで、原動機2からの回転変動への制振特性の変更、拡張を可能とする。 FIG. 12 shows a rotation fluctuation reducing device 316 according to a fourth embodiment of the present invention. The rotation fluctuation reduction device 316 of this embodiment has the same basic configuration as that of the first embodiment, but is free (independent of power transmission) of the output member 28 via the second elastic body 80 through the damper mass. 82 is different from the first embodiment. In this embodiment, the second elastic body 80 and the damper mass 82 do not contribute to the transmission of the driving force, and constitute a so-called dynamic vibration absorber. By adding a dynamic vibration absorber to the planetary gear mechanism 20, it is possible to change and expand the vibration damping characteristics of the prime mover 2 against rotation fluctuations.
 図13は本発明の第5の実施形態の回転変動低減装置416を示す。この実施形態も第1の実施形態と基本構成は同様であるが、調整クラッチ88が変速機4内に前置される点が相違する。調整クラッチ88は遊星歯車機構20の入力部である小径サンギヤ40と弾性体ダンパ機構18の第2の出力軸36間に設置されている。調整クラッチ88は、周知の摩擦クラッチとして構成することができる。調整クラッチ88は、出力軸36から遊星歯車機構20への入力を締結、遮断、及び不完全締結(任意に滑らせる)の機能を持たせることができる。調整クラッチ88の締結状態では遊星歯車機構20、即ち、遊星ダンパの制振機能を有効とさせ、調整クラッチ88の締結状態では遊星歯車機構20を遮断することで遊星ダンパの機能を無効とすることができる。また、使用状況によっては調整クラッチ88を滑らせ不完全締結状態とすることで、過大な入力に対する遊星歯車機構の保護や、振動系が必要とするヒステリシスの発生による制振効果の向上を図ることができる。 FIG. 13 shows a rotation fluctuation reducing device 416 according to a fifth embodiment of the present invention. This embodiment has the same basic configuration as that of the first embodiment, except that an adjustment clutch 88 is provided in the transmission 4. The adjustment clutch 88 is provided between the small-diameter sun gear 40 which is an input portion of the planetary gear mechanism 20 and the second output shaft 36 of the elastic damper mechanism 18. The adjustment clutch 88 can be configured as a known friction clutch. The adjustment clutch 88 can have functions of fastening, breaking, and incompletely fastening (arbitrarily sliding) the input from the output shaft 36 to the planetary gear mechanism 20. When the adjusting clutch 88 is engaged, the vibration damping function of the planetary gear mechanism 20, that is, the planetary damper is enabled, and when the adjusting clutch 88 is engaged, the planetary gear mechanism 20 is shut off to disable the function of the planetary damper. Can be. In addition, depending on the situation of use, the adjustment clutch 88 may be slid into an incompletely engaged state, thereby protecting the planetary gear mechanism against excessive input and improving the vibration damping effect due to the occurrence of hysteresis required by the vibration system. Can be.
 図14及び図15は原動機2から出力軸までの車両駆動系をモデル化し、数値解析(この解析法は周知のため結果のみ示す)後の変速機入力軸の回転変動の周波数特性を示しており、aはコイルスプリングのみの従来のダンパ、bは第1の実施形態(図1)等の中間マスの無い遊星ダンパ、cは第2の実施形態(図2)等の中間マスを備えた遊星ダンパの結果を示し、図14にて従来のダンパ特性aと比較して遊星ダンパの特性bは一時ピークの周波数が低周波数側に出る(中間マスを付けるとcのように一層低周波数側となる)ため、騒音対策上問題となる20ヘルツ付近の低回転での回転変動を良く抑えられる点で従来のダンパ特性aより優れていることが分かる。騒音対策としては20ヘルツ付近の回転変動を抑えることが特に有利なためここに遊星ダンパの優位性がある。しかしながら、60ヘルツ付近を越えた当たりの周波数(高回転)側では従来のダンパの特性aが遊星ダンパの特性b、cより優れており、これが遊星ダンパの弱点ともなっていると言い得る。 FIGS. 14 and 15 show the frequency characteristics of the rotational fluctuations of the transmission input shaft after numerical analysis (this analysis method is well known and results are shown only) by modeling the vehicle drive system from the prime mover 2 to the output shaft. , A is a conventional damper having only a coil spring, b is a planetary damper having no intermediate mass such as the first embodiment (FIG. 1), and c is a planetary mass having an intermediate mass such as the second embodiment (FIG. 2). The results of the damper are shown in FIG. 14, and the characteristic b of the planetary damper has a temporary peak frequency on the lower frequency side as compared with the conventional damper characteristic a in FIG. Therefore, it can be seen that the damper characteristic a is superior to the conventional damper characteristic a in that the rotation fluctuation at a low rotation around 20 Hz, which is a problem in noise control, can be suppressed well. As a countermeasure against noise, it is particularly advantageous to suppress the rotation fluctuation around 20 Hz, so that the planetary damper has an advantage here. However, on the side of the frequency (high rotation) exceeding about 60 Hz, the characteristic a of the conventional damper is superior to the characteristics b and c of the planetary damper, which can be said to be a weak point of the planetary damper.
 図15は、図13の実施形態により調整クラッチ88を付けた場合をd, d´により示し、f1の周波数は50ヘルツ付近のクラッチを遮断するポイントを示しており、f1までは調整クラッチ88の締結により遊星ダンパの特性bと略一致する周波数特性dとなり、調整クラッチ88を遮断するf1以降の周波数ではd´のように従来ダンパの特性aに近い特性が得られ、スプリングのみの従来ダンパと遊星ダンパとの都合の良いところを継ぎ合わせたより理想的な特性を得ることができる。
符号の説明
15 shows a case where with a modulating clutch 88 by the embodiment of FIG. 13 d, by d', frequency of f 1 indicates the point of blocking clutch of around 50 Hz, to f 1 is adjusted clutch 88 substantially matches the frequency characteristic becomes d and properties of planetary damper b by engagement of, characteristics similar to the conventional damper characteristic a as d'at f 1 after a frequency to block the modulating clutch 88 is obtained, the spring only It is possible to obtain more ideal characteristics obtained by splicing convenient portions of the conventional damper and the planetary damper.
Explanation of reference numerals
2…原動機(内燃機関)
3…フライホイール
4…変速機
5…ケーシング(本発明の筐体)
 5-1, 5-2…ケーシングの隔壁部分
6…変速機構
7…変速機構の第1の入力軸
8…変速機構の出力軸
10…変速機構の第2の入力軸
11…変速機構の入力歯車
16, 116, 216, 316, 416…回転変動低減装置
18, 118, 218…弾性体ダンパ機構
20…弾性体ダンパ機構の遊星歯車機構
 26…弾性体ダンパ機構の入力部材
 26-1…スプリング受部
26-1a, 26-1b…スプリング受座
28…弾性体ダンパ機構の出力部材
 28-1…スプリング受部
28-1a, 28-1b…スプリング受座
30……弾性体ダンパ機構の弾性体
30A…第1の弾性体(コイルスプリング)
30B…第2の弾性体(コイルスプリング)
34…弾性体ダンパ機構の第1の出力軸
36…弾性体ダンパ機構の第2の出力軸
38…遊星歯車機構の段付ピニオン
40…遊星歯車機構の小径サンギヤ
44…中間部材
44-1…窓枠状開口部
44-1a, 44-1b …スプリング受座
44´…前面補助板
44″…後面補助板
46…遊星歯車機構のキャリア
 46-1…キャリアプレート
46-2…46-2
 54…連結板
64…原動機の出力軸側部材
 66…内周側軸受
68…外周側軸受
80…第2の弾性体
82…ダンパマス
88…調整クラッチ
2. Motor (internal combustion engine)
3: Flywheel 4: Transmission 5: Casing (housing of the present invention)
5-1 5-2 Partition wall part of casing 6 Transmission mechanism 7 First input shaft 8 of transmission mechanism Output shaft 10 of transmission mechanism Second input shaft 11 of transmission mechanism Input gear of transmission mechanism
16, 116, 216, 316, 416… Rotation fluctuation reduction device
18, 118, 218 elastic body damper mechanism 20 planetary gear mechanism of elastic body damper mechanism 26 input member of elastic body damper mechanism 26-1 spring receiving part
26-1a, 26-1b ... Spring seat 28 ... Output member of elastic damper mechanism 28-1 ... Spring receiver
28-1a, 28-1b ... spring seat 30 ... elastic body 30A of elastic body damper mechanism ... first elastic body (coil spring)
30B: second elastic body (coil spring)
34, a first output shaft of the elastic damper mechanism 36, a second output shaft 38 of the elastic damper mechanism 38, a stepped pinion 40 of the planetary gear mechanism, a small sun gear 44 of the planetary gear mechanism, an intermediate member
44-1… Window frame opening
44-1a, 44-1b ... spring seat 44 '... front auxiliary plate 44 "... rear auxiliary plate 46 ... carrier of planetary gear mechanism 46-1 ... carrier plate
46-2… 46-2
54 ... Connecting plate 64 ... Motor output shaft side member 66 ... Inner peripheral side bearing 68 ... Outer peripheral side bearing 80 ... Second elastic body 82 ... Damper mass 88 ... Adjustment clutch

Claims (8)

  1. 原動機の回転変動を低減して出力軸に伝達する回転変動低減装置であって、原動機側の入力部材及び出力軸側の出力部材を少なくとも備え、入力部材及び出力軸間に回転方向にねじり剛性を有した弾性体を配置して構成される弾性体ダンパ機構と、複数のピニオンを回転可能に軸支して構成されるキャリアと、前記ピニオンに個別的に噛合する少なくとも2個の歯車との、都合、少なくとも3個の回転歯車要素を備えた遊星歯車機構とを備え、弾性体ダンパ機構からは前記出力軸(以下第1の出力軸)に加えて弾性体より入力部材側において回転運動を取出す第2の出力軸が分岐され、遊星歯車機構の回転要素のうち一つは前記第1の出力軸により、また、別の一つは第2の出力軸により夫々回転駆動されるようにされ、残りの少なくとも一つの動力伝達に関与しない回転要素がダンパマスとして機能するようにされ、かつ前記弾性体ダンパ機構は、遊星歯車機構を収容し、遊星歯車機構の潤滑用の潤滑油のための油浴を形成する筺体の外部に設置され、かつ前記第1の出力軸及び第2の出力軸の遊星歯車機構の対応の回転要素への連結は筺体の壁面部を介して行われるようにされる回転変動低減装置。 A rotation fluctuation reducing device that reduces the rotation fluctuation of a motor and transmits the rotation to an output shaft, comprising at least an input member on the motor side and an output member on the output shaft side, and having a torsional rigidity in the rotational direction between the input member and the output shaft. An elastic damper mechanism configured by disposing an elastic body having the carrier, a carrier configured to rotatably support a plurality of pinions, and at least two gears individually meshed with the pinions, A planetary gear mechanism having at least three rotary gear elements, and in addition to the output shaft (hereinafter referred to as a first output shaft), a rotary motion is extracted from the elastic body on the input member side from the elastic body. A second output shaft is branched, one of the rotating elements of the planetary gear mechanism is driven to rotate by the first output shaft, and the other is driven to rotate by the second output shaft, respectively. At least one remaining A rotating element that does not contribute to the power transmission of the planetary gear mechanism functions as a damper mass, and the elastic damper mechanism houses a planetary gear mechanism and forms an oil bath for lubricating oil for lubricating the planetary gear mechanism. A rotation fluctuation reducing device installed outside the housing, and wherein the first output shaft and the second output shaft are connected to corresponding rotating elements of the planetary gear mechanism via a wall surface of the housing.
  2.  請求項1に記載の回転変動低減装置において、前記弾性体ダンパ機構は、入力部材と,出力部材と、入力部材と出力部材との間を回転方向に連結する弾性体とを備え、前記第2の出力軸は入力部材より分岐される回転変動低減装置。 2. The rotation fluctuation reducing device according to claim 1, wherein the elastic body damper mechanism includes an input member, an output member, and an elastic body that connects the input member and the output member in a rotational direction, and the second member includes: The output shaft of is a rotation fluctuation reduction device branched from the input member.
  3.  請求項1に記載の回転変動低減装置において、前記弾性体ダンパ機構は、入力部材と,出力部材と、入力部材と出力部材との間に設置された中間部材と、入力部材と中間部材との間を回転方向に連結する第1の弾性体と、中間部材と出力部材の間を回転方向に連結する第2の弾性体とを備え、前記第2の出力軸は入力部材より分岐される回転変動低減装置。 2. The rotation fluctuation reducing device according to claim 1, wherein the elastic body damper mechanism includes an input member, an output member, an intermediate member installed between the input member and the output member, and an input member and an intermediate member. A first elastic member connecting the intermediate member and the output member in a rotational direction, and a second elastic member connecting the intermediate member and the output member in a rotational direction, wherein the second output shaft is branched from the input member. Fluctuation reduction device.
  4.  請求項1に記載の回転変動低減装置において、前記弾性体ダンパ機構は、入力部材と,出力部材と、入力部材と出力部材との間に設置された中間部材と、入力部材と中間部材との間を回転方向に連結する第1の弾性体と、中間部材と出力部材の間を回転方向に連結する第2の弾性体とを備え、前記第2の出力軸は中間部材より分岐される回転変動低減装置。 2. The rotation fluctuation reducing device according to claim 1, wherein the elastic body damper mechanism includes an input member, an output member, an intermediate member installed between the input member and the output member, and an input member and an intermediate member. A first elastic member that connects the intermediate member and the output member in a rotational direction, and a second elastic member that connects the intermediate member and the output member in a rotational direction, wherein the second output shaft is branched from the intermediate member. Fluctuation reduction device.
  5.  請求項1に記載の回転変動低減装置において、前記弾性体ダンパ機構は、入力部材と,出力部材と、入力部材と出力部材との間を回転方向に連結する第1の弾性体と、ダンパマスと、出力部材に対しダンパマスを動力伝達に関与しないように接続する第2の弾性体とを備え、前記第2の出力軸は入力部材より分岐される回転変動低減装置。 2. The rotation fluctuation reducing device according to claim 1, wherein the elastic damper mechanism includes an input member, an output member, a first elastic member that connects the input member and the output member in a rotational direction, and a damper mass. 3. A second elastic body that connects the damper mass to the output member so as not to be involved in power transmission, wherein the second output shaft is branched from the input member.
  6.  請求項1から5のいずれか一項記載の回転変動低減装置において、筺体内における前記第2の出力軸を遊星歯車機構に対して係脱するクラッチを備えた回転変動低減装置。 The rotation fluctuation reducing device according to any one of claims 1 to 5, further comprising a clutch that engages and disengages the second output shaft in a housing with respect to a planetary gear mechanism.
  7.  請求項1から6のいずれか一項に記載の回転変動低減装置において、前記筐体の壁面部における前記第1の出力軸及び第2の出力軸の遊星歯車機構の対応の回転要素への連結部の軸封のための軸封装置を具備した回転変動低減装置。 The rotation fluctuation reducing device according to any one of claims 1 to 6, wherein the first output shaft and the second output shaft on a wall portion of the housing are connected to corresponding rotation elements of a planetary gear mechanism. A rotation fluctuation reducing device provided with a shaft sealing device for sealing a part.
  8. 請求項7に記載の回転変動低減装置において、遊星歯車機構を収容する前記筺体は、原動機からの回転を出力軸より受け取り伝達する動力伝達機構を収容し、前記第1の出力軸は動力伝達機構の入力軸に連結され、第2の出力軸の遊星歯車機構への連結部は変速機構の入力軸と同芯の円筒状軸をなし、前記軸封装置は変速機構の入力軸と円筒状軸との間の第1のシール付ベアリングと、円筒状軸と前記筺体との間の第2のシール付ベアリングとから構成される回転変動低減装置。 8. The rotation fluctuation reducing device according to claim 7, wherein the housing that houses the planetary gear mechanism houses a power transmission mechanism that receives and transmits rotation from a motor from an output shaft, and the first output shaft is a power transmission mechanism. And a connecting portion of the second output shaft to the planetary gear mechanism forms a cylindrical shaft concentric with the input shaft of the transmission mechanism, and the shaft sealing device comprises an input shaft and a cylindrical shaft of the transmission mechanism. And a second sealed bearing between the cylindrical shaft and the housing.
PCT/JP2019/024399 2018-07-11 2019-06-20 Rotational variation reducing device WO2020012905A1 (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58108656U (en) * 1982-10-06 1983-07-23 ヤンマーディーゼル株式会社 Planetary gear speed increaser
US4867290A (en) * 1988-09-02 1989-09-19 Ford Motor Company High excursion torsional vibration damper for controlled energy absorption
JPH07208547A (en) * 1993-12-22 1995-08-11 Fichtel & Sachs Ag Torsional vibration damper
JP2017180817A (en) * 2016-03-23 2017-10-05 トヨタ自動車株式会社 Torque converter having torsional vibration reduction device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58108656U (en) * 1982-10-06 1983-07-23 ヤンマーディーゼル株式会社 Planetary gear speed increaser
US4867290A (en) * 1988-09-02 1989-09-19 Ford Motor Company High excursion torsional vibration damper for controlled energy absorption
JPH07208547A (en) * 1993-12-22 1995-08-11 Fichtel & Sachs Ag Torsional vibration damper
JP2017180817A (en) * 2016-03-23 2017-10-05 トヨタ自動車株式会社 Torque converter having torsional vibration reduction device

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