WO2016021668A1 - ダンパ装置 - Google Patents
ダンパ装置 Download PDFInfo
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- WO2016021668A1 WO2016021668A1 PCT/JP2015/072296 JP2015072296W WO2016021668A1 WO 2016021668 A1 WO2016021668 A1 WO 2016021668A1 JP 2015072296 W JP2015072296 W JP 2015072296W WO 2016021668 A1 WO2016021668 A1 WO 2016021668A1
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- WIPO (PCT)
- Prior art keywords
- damper device
- elastic body
- torque
- intermediate element
- input
- Prior art date
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/12—Suppression 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
- F16F15/131—Suppression 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
- F16F15/133—Suppression 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
- F16F15/134—Wound springs
- F16F15/13469—Combinations of dampers, e.g. with multiple plates, multiple spring sets, i.e. complex configurations
- F16F15/13476—Combinations of dampers, e.g. with multiple plates, multiple spring sets, i.e. complex configurations resulting in a staged spring characteristic, e.g. with multiple intermediate plates
- F16F15/13484—Combinations of dampers, e.g. with multiple plates, multiple spring sets, i.e. complex configurations resulting in a staged spring characteristic, e.g. with multiple intermediate plates acting on multiple sets of springs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
- F16H2045/0205—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type two chamber system, i.e. without a separated, closed chamber specially adapted for actuating a lock-up clutch
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
- F16H2045/0221—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means
- F16H2045/0226—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means comprising two or more vibration dampers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
- F16H2045/0221—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means
- F16H2045/0226—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means comprising two or more vibration dampers
- F16H2045/0231—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means comprising two or more vibration dampers arranged in series
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H45/00—Combinations of fluid gearings for conveying rotary motion with couplings or clutches
- F16H45/02—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
- F16H2045/0273—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type characterised by the type of the friction surface of the lock-up clutch
- F16H2045/0278—Combinations of fluid gearings for conveying rotary motion with couplings or clutches with mechanical clutches for bridging a fluid gearing of the hydrokinetic type characterised by the type of the friction surface of the lock-up clutch comprising only two co-acting friction surfaces
Definitions
- the present disclosure relates to a damper device including an input element to which power from an internal combustion engine is transmitted and an output element.
- a double-pass damper used in connection with a torque converter is known (for example, see Patent Document 1).
- the vibration path from the engine and the lockup clutch to the output hub is divided into two parallel vibration paths B and C, each of which includes a pair of springs, A separate intermediate flange is disposed between the pair of springs.
- the turbine of the torque converter is coupled to the intermediate flange of the vibration path B in order to make the resonance frequencies of the two vibration paths different, and the natural frequency of the intermediate flange of the vibration path B is determined by the intermediate flange of the vibration path C. Is less than the natural frequency of.
- vibration from the engine enters the two vibration paths B and C of the damper device.
- an engine vibration of a certain frequency reaches a vibration path B including an intermediate flange coupled to the turbine
- the vibration phase between the intermediate flange of the vibration path B and the output hub is 180 degrees with respect to the input vibration phase. It is shifted.
- the vibration that has entered the vibration path C is output without causing a phase shift (shift). Transmitted to the hub.
- the vibration at the output hub can be attenuated by shifting the phase of the vibration transmitted from the vibration path B to the output hub and the phase of the vibration transmitted from the vibration path C to the output hub by 180 degrees. it can.
- the two intermediate flanges (36, 38) are arranged so as to face each other in the axial direction of the double-pass damper (see FIGS. 5A and 5B of the same document). Accordingly, the pair of springs (35a, 35b) constituting the vibration path B are arranged so as to be aligned in the radial direction of the double pass damper, and the pair of springs (37a, 37b) constituting the vibration path C are also arranged in the diameter of the double pass damper. Arranged in a direction.
- a damper device is a damper device including an input element to which power from an internal combustion engine is transmitted and an output element, and transmits torque between the first intermediate element and the input element and the first intermediate element. And a first torque transmission path including a second elastic body that transmits torque between the first intermediate element and the output element, a second intermediate element, the input element, and the second intermediate A third elastic body that transmits torque to and from the element; and a fourth elastic body that transmits torque between the second intermediate element and the output element, and is provided in parallel with the first torque transmission path.
- a second torque transmission path wherein the first and second elastic bodies are arranged along the circumferential direction of the damper device, and the third and fourth elastic bodies are arranged along the circumferential direction. The first and second elastic bodies are lined up But also it is positioned outward in the radial direction of the damper device.
- the phase of vibration transmitted from the first torque transmission path to the output element, and the phase of vibration transmitted from the second torque transmission path to the output element Is set, for example, to an anti-resonance point at which the vibration amplitude of the output element is theoretically zero when it is shifted by 180 degrees due to the occurrence of resonance according to the natural frequency of the second torque transmission path (second intermediate element).
- the phase of vibration transmitted from the first torque transmission path to the output element Is set, for example, to an anti-resonance point at which the vibration amplitude of the output element is theoretically zero when it is shifted by 180 degrees due to the occurrence of resonance according to the natural frequency of the second torque transmission path (second intermediate element).
- the third and fourth elastic bodies of the second torque transmission path are arranged on the outer side in the radial direction of the damper device relative to the first and second elastic bodies of the first torque transmission path, so that the first to fourth elasticity
- the degree of freedom in setting the natural frequency of the first and second torque transmission paths (first and second intermediate elements) by adjusting the rigidity of the body can be improved.
- Another damper device of the present disclosure includes a first intermediate element, a torque between the input element and the first intermediate element in a damper device including an input element to which power from an internal combustion engine is transmitted and an output element.
- a first elastic body for transmitting torque, and a first torque transmission path including a second elastic body for transmitting torque between the first intermediate element and the output element, a second intermediate element, the input element, and the first
- a spring constant of the first, second, third, and fourth elastic bodies based on the frequency of the anti-resonance point at which the vibration amplitude of the output element is theoretically zero. And inertia moment of the first and second intermediate elements One in which capital and is determined.
- FIG. 5 is an explanatory diagram illustrating the relationship between the engine speed and torque fluctuations in the output element of the damper device shown in FIG. 4.
- FIG. 1 is a schematic configuration diagram illustrating a starting device 1 including a damper device 10 according to an embodiment of the present disclosure
- FIG. 2 is a cross-sectional view illustrating the starting device 1.
- a starting device 1 shown in these drawings is mounted on a vehicle including an engine (internal combustion engine) as a prime mover, and in addition to a damper device 10, a front as an input member connected to a crankshaft of the engine.
- the cover 3 is connected to a pump impeller (input side fluid transmission element) 4 fixed to the front cover 3, a turbine runner (output side fluid transmission element) 5 rotatable coaxially with the pump impeller 4, and a damper device 10.
- a damper hub 7 as a power output member fixed to an input shaft IS of a transmission which is an automatic transmission (AT) or a continuously variable transmission (CVT), a lock-up clutch 8 and the like are included.
- axial direction basically indicates the extending direction of the central axis (axial center) of the starting device 1 or the damper device 10, unless otherwise specified.
- the “radial direction” is basically the radial direction of the rotating element such as the starting device 1, the damper device 10, and the damper device 10, unless otherwise specified, that is, the center of the starting device 1 or the damper device 10.
- An extending direction of a straight line extending from the axis in a direction (radial direction) orthogonal to the central axis is shown.
- the “circumferential direction” basically corresponds to the circumferential direction of the rotating elements of the starting device 1, the damper device 10, the damper device 10, etc., ie, the rotational direction of the rotating element, unless otherwise specified. Indicates direction.
- the pump impeller 4 includes a pump shell 40 that is tightly fixed to the front cover 3 and a plurality of pump blades 41 that are disposed on the inner surface of the pump shell 40.
- the turbine runner 5 includes a turbine shell 50 and a plurality of turbine blades 51 disposed on the inner surface of the turbine shell 50.
- An inner peripheral portion of the turbine shell 50 is fixed to the turbine hub 52 via a plurality of rivets.
- the turbine hub 52 is rotatably supported by the damper hub 7, and movement of the turbine hub 52 (turbine runner 5) in the axial direction of the starting device 1 is restricted by the damper hub 7 and a snap ring attached to the damper hub 7.
- the pump impeller 4 and the turbine runner 5 face each other, and a stator 6 that rectifies the flow of hydraulic oil (working fluid) from the turbine runner 5 to the pump impeller 4 is coaxially disposed between the two.
- the stator 6 has a plurality of stator blades 60, and the rotation direction of the stator 6 is set in only one direction by the one-way clutch 61.
- the pump impeller 4, the turbine runner 5, and the stator 6 form a torus (annular flow path) for circulating hydraulic oil, and function as a torque converter (fluid transmission device) having a torque amplification function.
- the stator 6 and the one-way clutch 61 may be omitted, and the pump impeller 4 and the turbine runner 5 may function as a fluid coupling.
- the lockup clutch 8 executes a lockup for connecting the front cover 3 and the damper hub 7 via the damper device 10 and releases the lockup.
- the lock-up clutch 8 is configured as a single-plate hydraulic clutch, and is disposed in the front cover 3 and in the vicinity of the inner wall surface of the front cover 3 on the engine side, and with respect to the damper hub 7. It has a lock-up piston (power input member) 80 that is movably fitted in the direction. As shown in FIG. 2, a friction material 81 is attached to the outer peripheral side of the lockup piston 80 and the surface on the front cover 3 side.
- a lockup chamber 85 is defined between the lockup piston 80 and the front cover 3 and connected to a hydraulic control device (not shown) via an oil passage formed in the hydraulic oil supply passage and the input shaft IS.
- the pump impeller 4 and the pump impeller 4 and the turbine runner 5 from the axial center side (around the one-way clutch 61) through the oil passage formed in the input shaft IS and radially outward. Hydraulic oil from a hydraulic control device supplied to the turbine runner 5 (torus) can flow in. Therefore, if the inside of the fluid transmission chamber 9 and the lockup chamber 85 defined by the front cover 3 and the pump shell of the pump impeller 4 are kept at an equal pressure, the lockup piston 80 is moved to the front cover 3 side. The lockup piston 80 does not move and does not frictionally engage the front cover 3.
- a multi-plate hydraulic clutch including at least one friction engagement plate (a plurality of friction materials) may be employed.
- the damper device 10 includes a drive member (input element) 11, a first intermediate member (first intermediate element) 12, and a second intermediate member (second intermediate element) 14 as rotating elements. And a driven member (output element) 16. Furthermore, the damper device 10 includes a plurality of (for example, three in this embodiment) first springs that transmit torque between the drive member 11 and the first intermediate member 12 as torque transmission elements (torque transmission elastic bodies).
- First elastic body SP1 a plurality (for example, three in this embodiment) of second springs (second elastic bodies) SP2 for transmitting torque between the first intermediate member 12 and the driven member 16, a drive member
- a plurality of (for example, three in the present embodiment) fourth springs (fourth elastic bodies) SP4 that transmit torque between them are included.
- the damper device 10 has a first torque transmission path P1 and a second torque transmission path P2 provided in parallel with each other, as shown in FIG.
- the first torque transmission path P1 includes a first intermediate member 12, first and second springs SP1, SP2 as elements disposed between the drive member 11 and the driven member 16, and includes a plurality of first springs SP1, Torque is transmitted between the drive member 11 and the driven member 16 via the first intermediate member 12 and the plurality of second springs SP2.
- the second torque transmission path P2 includes a second intermediate member 14, third and fourth springs SP3, SP4 as elements disposed between the drive member 11 and the driven member 16, and includes a plurality of third springs. Torque is transmitted between the drive member 11 and the driven member 16 via SP3, the second intermediate member 14 and the plurality of fourth springs SP4.
- first to fourth springs SP1 to SP4 linear coil springs made of a metal material spirally wound so as to have an axial center extending straight when no load is applied are employed.
- the first to fourth springs SP1 to SP4 are more appropriately expanded and contracted along the axial center, and so-called hysteresis (the input torque to the drive member 11 is increased). It is possible to reduce the difference between the torque output from the driven member 16 when going and the torque output from the driven member 16 when the input torque decreases.
- the first and second springs SP1 and SP2 have an outer diameter (coil diameter) larger than the outer diameter (coil diameter) of the third and fourth springs SP3 and SP4, as shown in FIG.
- the wire diameters (outer diameters of the coil wires) of the first and second springs SP1 and SP2 are larger than the wire diameters (outer diameters of the coil wires) of the third and fourth springs SP3 and SP4 as shown in FIG. Is also big.
- the drive member 11 of the damper device 10 is rotatable by an annular first plate member (first input member) 111 fixed to the lockup piston 80 of the lockup clutch 8 and the damper hub 7.
- An annular second plate member (second input member) 112 that is supported (aligned) and connected to the first plate member 111 so as to rotate integrally with the first plate member 111, and disposed adjacent to the turbine runner 5
- an annular third plate member (third input member) 113 connected (fixed) to the second plate member 112 via a plurality of rivets.
- the first plate member 111 includes an annular fixed portion 111a that is fixed to the inner surface (the surface to which the friction material 81 is not attached) of the lockup piston 80 via a plurality of rivets, and an outer peripheral portion of the fixed portion 111a.
- a cylindrical portion 111b extending in the axial direction, and a plurality (for example, three in this embodiment) of spring abutments extending radially outward from the cylindrical portion 111b at regular intervals (equal intervals) Part (outer contact part) 111c.
- a plurality of engaging convex portions that are fitted into corresponding concave portions formed on the outer peripheral portion of the second plate member 112 are formed at the free end portion of the cylindrical portion 111 b of the first plate member 111.
- the second plate member 112 includes a plurality of (for example, three in this embodiment) spring support portions 112a arranged in the circumferential direction along the inner peripheral edge (equal intervals), and a plurality of spring support portions 112a.
- the third plate member 113 includes a plurality (for example, three in this embodiment) of spring support portions 113a arranged in the circumferential direction along the inner peripheral edge (equally spaced), and a plurality of spring supports.
- a plurality (for example, three in the present embodiment) that are arranged at equal intervals in the circumferential direction on the outer peripheral side of the portion 113a (equal intervals) and that respectively correspond to the corresponding spring support portions 113a in the radial direction of the third plate member 113 )
- the plurality of spring support portions 112a of the second plate member 112 support (guide) the side portions on the lockup piston 80 side of the corresponding first and second springs SP1, SP2 (one each) from the inner peripheral side.
- the plurality of spring support portions 112b support (guide) the side portions on the lockup piston 80 side of the corresponding first and second springs SP1, SP2 (one each) from the outer peripheral side.
- the plurality of spring support portions 113a of the third plate member 113 support (guide) the side portions on the turbine runner 5 side of the corresponding first and second springs SP1, SP2 (one each) from the inner peripheral side. To do.
- the plurality of spring support portions 113b support (guide) the side portions on the turbine runner 5 side of the corresponding first and second springs SP1, SP2 (one each) from the outer peripheral side.
- the first and second springs SP1 and SP2 are paired one by one (act in series) and the drive members 11 are arranged alternately along the circumferential direction of the first intermediate member 12 (damper device 10).
- the second plate member 112 is supported by the spring support portions 112 a and 112 b of the second plate member 112 and the spring support portions 113 a and 113 b of the third plate member 113.
- the plurality of spring contact portions 112c of the second plate member 112 are provided one by one between the spring support portions 112a and 112b adjacent to each other along the circumferential direction.
- Each spring contact portion 112c is supported by different spring support portions 112a, 112b, 113a, 113b and does not form a pair (does not work in series) in the mounted state of the damper device 10. It abuts against both ends between SP2.
- the plurality of spring contact portions 113c of the third plate member 113 are provided one by one between the spring support portions 113a and 113b adjacent to each other along the circumferential direction.
- Each spring contact portion 113c is supported between the first and second springs SP1 and SP2 that are supported (not paired) by different spring support portions 112a, 112b, 113a, and 113b in a state where the damper device 10 is attached. It abuts against both ends.
- the first intermediate member 12 is configured as a plate-shaped annular member, and is rotatably formed by a plurality of protrusions 16b that are formed on the inner periphery of the driven member 16 at intervals in the circumferential direction and project in the axial direction. It is supported (alignment).
- the first intermediate member 12 has a plurality of (for example, three in this embodiment) spring accommodating portions (openings) (not shown) in which the first and second springs SP1 and SP2 that are paired with each other (act in series) are arranged. Part) and a plurality of spring contact parts 12c.
- the plurality of spring contact portions 12c are provided one by one between the spring accommodating portions adjacent to each other along the circumferential direction.
- Each spring contact portion 12c is supported by the same spring support portions 112a, 112b, 113a, 113b and abuts against both end portions between the first and second springs SP1, SP2 paired with each other.
- one end of each first spring SP1 contacts the corresponding spring contact portion 112c, 113c of the drive member 11, and the other end of each first spring SP1 is the first intermediate It contacts the corresponding spring contact portion 12c of the member 12.
- one end of each second spring SP ⁇ b> 2 comes into contact with the corresponding spring contact portion 12 c of the first intermediate member 12, and the other end of each second spring SP ⁇ b> 2 is connected to the drive member 11. It contacts the corresponding spring contact portions 112c, 113c.
- the second intermediate member 14 is annular so as to support (guide) the outer peripheral portions of the plurality of third and fourth springs SP3, SP4, the side portion on the lock-up piston 80 side (the right side portion in FIG. 2), and the like. Is formed. As shown in FIG. 2, the second intermediate member 14 is rotatably supported (aligned) by the outer peripheral surface of the cylindrical portion (support portion) 111 b of the first plate member 111 constituting the drive member 11. As a result, the second intermediate member 14 is positioned outside the first intermediate member 12 in the radial direction of the damper device 10 so as to surround the first intermediate member 12 in the outer peripheral side region in the fluid transmission chamber 9. Be placed. By disposing the second intermediate member 14 in the outer peripheral region in the fluid transmission chamber 9 in this way, the inertia moment (inertia) of the second intermediate member 14 can be further increased.
- the second intermediate member 14 supports the third and fourth springs SP3 and SP4 so as to be alternately arranged along the circumferential direction of the second intermediate member 14 (damper device 10).
- the third and fourth springs SP3 and SP4 are more radial in the damper device 10 than the first and second springs SP1 and SP2 supported by the drive member 11 (second and third plate members 112 and 113). Is arranged outside.
- the third and fourth springs SP3 and SP4 are disposed in the outer peripheral side region in the fluid transmission chamber 9 so as to surround the first and second springs SP1 and SP2.
- the shaft length can be further shortened.
- the second intermediate member 14 includes a plurality (for example, three in this embodiment) of first spring contact portions (elastic body contact portions) 141c, and corresponding first spring contact portions 141c and axial directions. And a plurality (for example, three in this embodiment) of second spring contact portions (elastic body contact portions) 142c.
- the first and second spring contact portions 141c and 142c are in contact with the end portions of the third and fourth springs SP3 and SP4 that are paired (act in series) with each other.
- a spring contact portion 111c of the first plate member 111 constituting the drive member 11 is disposed between the third and fourth springs SP3 and SP4 that do not make a pair (do not act in series).
- each spring contact portion 111c of the drive member 11 is in contact with both ends between the third and fourth springs SP3 and SP4 that do not make a pair.
- one end of each third spring SP3 comes into contact with the corresponding spring contact portion 111c of the drive member 11, and the other end of each third spring SP3 is connected to the second intermediate member 14. It contacts with the corresponding spring contact portions 141c and 142c.
- one end of each of the fourth springs SP4 comes into contact with the corresponding first and second spring contact portions 141c and 142c of the second intermediate member 14, and other than each of the fourth springs SP4. The end contacts the corresponding spring contact portion 111c of the drive member 11.
- the driven member 16 is disposed between the second plate member 112 and the third plate member 113 of the drive member 11 in the axial direction and is fixed to the damper hub 7 by, for example, welding.
- the driven member 16 includes a plurality (for example, three in this embodiment) of inner spring contact portions (inner contact portions) 16ci formed at intervals in the circumferential direction so as to be close to the inner peripheral edge thereof, and a plurality of driven members 16 And a plurality (for example, three in this embodiment) of outer spring abutting portions (outer abutting portions) 16co that are formed on the radially outer side of the inner spring abutting portion 16ci at intervals in the circumferential direction. .
- each inner spring contact portion 16ci of the driven member 16 is supported by different spring support portions 112a, 112b, 113a, 113b, like the spring contact portions 112c, 113c of the drive member 11.
- the first and second springs SP1 and SP2 that are made (not paired) come into contact with both ends.
- the one end of each first spring SP1 also abuts the corresponding inner spring contact portion 16ci of the driven member 16, and the other end of each second spring SP2 is the driven member.
- 16 corresponding inner spring contact portions 16ci also contact.
- each outer spring contact portion 16co of the driven member 16 does not form a pair (does not act in series), like each spring contact portion 111c of the drive member 11.
- the fourth springs SP3 and SP4 are in contact with both ends.
- the one end of each third spring SP3 is also in contact with the corresponding outer spring contact portion 16co of the driven member 16, and the other end of each fourth spring SP4 is the driven member.
- the corresponding 16 outer spring contact portions 16co also contact.
- the driven member 16 is connected to the drive member 11 via the plurality of first springs SP1, the first intermediate member 12, and the plurality of second springs SP2, that is, the first torque transmission path P1, and the plurality of first springs SP1.
- the three springs SP3, the second intermediate member 14, and the plurality of fourth springs SP4, that is, the second torque transmission path P2, are coupled to the drive member 11.
- an annular turbine connecting member 55 is fixed to the turbine shell 50 of the turbine runner 5 by welding, for example.
- a plurality (for example, three in this embodiment) of spring contact portions 55c extending in the axial direction with an interval in the circumferential direction are formed on the outer peripheral portion of the turbine connecting member 55.
- Each spring contact portion 55c of the turbine connecting member 55 is in contact with the ends of the third and fourth springs SP3 and SP4 that make a pair (act in series) with each other.
- the second intermediate member 14 and the turbine runner 5 are connected so as to rotate integrally.
- the substantial moment of inertia of the second intermediate member 14 (the total value of the moments of inertia of the second intermediate member 14 and the turbine runner 5) can be further increased. Further, by connecting the turbine runner 5 and the second intermediate member 14 arranged on the radially outer side of the first and second springs SP1 and SP2, that is, on the outer peripheral side region in the fluid transmission chamber 9, the turbine connecting member 55 is connected. Can be prevented from passing between the third plate member 113 of the drive member 11 and the first and second springs SP1 and SP2 and the turbine runner 5 in the axial direction. Thereby, it becomes possible to suppress the increase in the axial length of the damper device 10 and thus the starting device 1 more favorably.
- the damper device 10 includes a first stopper 21 that restricts the bending of the first spring SP1, a second stopper 22 that restricts the bending of the second spring SP2, and a bending of the third spring SP3. And a fourth stopper 24 for restricting the bending of the fourth spring SP4.
- the first stopper 21 is configured to restrict relative rotation between the drive member 11 and the first intermediate member 12.
- the second stopper 22 is configured to restrict relative rotation between the first intermediate member 12 and the driven member 16.
- the third stopper 23 is configured to restrict relative rotation between the drive member 11 and the second intermediate member 14.
- the fourth stopper 24 is configured to restrict relative rotation between the second intermediate member 14 and the driven member 16.
- first to fourth stoppers 21 to 24 have a predetermined torque (first torque) in which the input torque to the drive member 11 is smaller than the torque T2 (second threshold) corresponding to the maximum torsion angle ⁇ max of the damper device 10. 1 is configured to regulate the bending of the corresponding spring after reaching T1.
- the damper device 10 can have a plurality of stages (two or more stages) of attenuation characteristics.
- three of the first to fourth stoppers 21 to 24 corresponding to the first to fourth springs SP1 to SP4 other than the one having the maximum spring constant are input to the drive member 11.
- the corresponding spring is restrained from bending.
- any of the first to fourth stoppers 21 to 24 corresponding to the first to fourth springs SP1 to SP4 having the maximum spring constant has the maximum torque input to the drive member 11. It is configured to operate when the torque T2 corresponding to the angle ⁇ max is reached.
- the damper device 10 has a two-stage (two-stage) attenuation characteristic.
- One of the first and second stoppers 21 and 22 may be configured to restrict relative rotation between the drive member 11 and the driven member 16, and one of the third and fourth stoppers 23 and 24 may be You may comprise so that the relative rotation of the drive member 11 and the driven member 16 may be controlled. That is, the configurations of the first to fourth stoppers 21 to 24 are not limited to those illustrated.
- Torque is transmitted to the driven member 16 and the damper hub 7 through P2.
- the first and second springs SP1 and SP2 and the third and fourth springs SP3 and SP4 act in parallel and are transmitted to the drive member 11 until the input torque to the drive member 11 reaches the torque T1. Attenuates (absorbs) torque fluctuations.
- the first and second springs SP1 and SP2 and the third and fourth springs SP3 and SP4 are arranged in parallel until the input torque transmitted to the drive member 11 reaches the torque T1. Act on.
- the first and second springs SP1 and SP2 and the third and fourth springs SP3 and SP4 act in parallel, the first and second springs are transmitted according to the frequency of vibration transmitted from the engine to the drive member 11. Resonance of the first and second intermediate members 12 and 14 or resonance mainly due to vibration of the entire damper device 10 and the drive shaft of the vehicle occurs in any of the torque transmission paths P1 and P2.
- Equation (1) “J 1 ” is the moment of inertia of the drive member 11, “J 21 ” is the moment of inertia of the first intermediate member 12, and J 22 ”is the second intermediate member 14. “J 3 ” is the moment of inertia of the driven member 16, “ ⁇ 1 ” is the twist angle of the drive member 11, and “ ⁇ 21 ” is the first intermediate member 12.
- ⁇ 22 is the torsion angle of the second intermediate member 14
- ⁇ 3 is the torsion angle of the driven member 16
- k 1 is the same as that of the drive member 11.
- 1 is a composite spring constant of a plurality of first springs SP1 acting in parallel with one intermediate member 12
- k 2 is a plurality of acting in parallel between the first intermediate member 12 and the driven member 16.
- k 3 is Dora
- k 4" is parallel with the second intermediate member 14 and the driven member 16
- k R is a rigidity, that is, a spring constant in a transmission, a drive shaft or the like disposed between the driven member 16 and the vehicle wheel
- T is an input torque transmitted from the engine to the drive member 11.
- the present inventors assume that the input torque T is periodically oscillating as shown in the following equation (2), the twist angle ⁇ 1 of the drive member 11, and the twist angle of the first intermediate member 12. It is assumed that ⁇ 21 , the twist angle ⁇ 22 of the second intermediate member 14, and the twist angle ⁇ 3 of the driven member 16 are periodically responsive (vibrated) as shown in the following equation (3).
- “ ⁇ ” in the equations (2) and (3) is an angular frequency in the periodic fluctuation (vibration) of the input torque T, and in the equation (3), “ ⁇ 1 ” is the torque from the engine.
- ⁇ 21 is the first generated as the torque from the engine is transmitted to the drive member 11.
- the amplitude (vibration amplitude) of the vibration of the intermediate member 12, and “ ⁇ 22 ” is the amplitude of vibration of the second intermediate member 14 (vibration amplitude) generated when torque from the engine is transmitted to the drive member 11.
- “ ⁇ 3 ” is an amplitude of vibration of the driven member 16 (vibration amplitude) that is generated when torque from the engine is transmitted to the drive member 11.
- the lockup rotation speed Nluup of the lockup clutch is further reduced, and torque from the engine is mechanically transmitted to the transmission at an early stage.
- the power transmission efficiency between the engine and the transmission can be improved, thereby improving the fuel efficiency of the engine.
- vibration transmitted from the engine to the drive member 11 via the lockup clutch becomes large, particularly in a 3-cylinder or 4-cylinder engine.
- the increase in the vibration level becomes remarkable in a vehicle equipped with such a cylinder-saving engine.
- a damper that transmits torque (vibration) from the engine to the transmission in a state where the lockup is executed. It is necessary to further reduce the vibration level in the rotation speed region near the lockup rotation speed Nlup of the entire apparatus 10 (driven member 16).
- the present inventors based on the lock-up speed Nluup determined for the lock-up clutch 8, the engine speed ranges from 500 rpm to 1500 rpm (assumed setting range of the lock-up speed Nlup).
- the damper device 10 is configured so that the anti-resonance point A described above is formed when it is within the bracket.
- the frequency fa of the antiresonance point A is expressed by the following equation (6):
- the combined spring constant k 1 of the plurality of first springs SP 1 , the combined spring constant k 2 of the plurality of second springs SP 2 , and the plurality of third springs SP 3 so as to satisfy the following expression (7):
- the combined spring constant k 3 , the combined spring constant k 4 of the plurality of fourth springs SP 4 , the inertia moment J 21 of the first intermediate member 12, and the inertia moment J 22 of the second intermediate member 14 (connected to rotate integrally) (Considering (summing up) the moment of inertia of the turbine runner, etc.) is selected and set.
- the spring constants k 1 , k 2 of the first, second, third and fourth springs SP1 to SP4 are based on the frequency fa (and the lockup rotation speed Nloop) at the antiresonance point A.
- K 3 , k 4 and the moments of inertia J 21 , J 22 of the first and second intermediate members 12, 14 are determined.
- the anti-resonance point A that can theoretically make the vibration amplitude ⁇ 3 of the driven member 16 zero (can be further reduced) is within a low rotational speed range from 500 rpm to 1500 rpm (assumed setting range of the lockup rotational speed Nloop).
- This allows lock-up at a lower rotational speed (connection between the engine and the drive member 11) and further improves the vibration damping performance of the damper device 10 in a low rotational speed range where vibration from the engine tends to increase. It becomes possible to make it.
- the resonance frequency causing the antiresonance point A is smaller than the frequency fa of the antiresonance point A and as small as possible.
- the frequency fa at the anti-resonance point can be made smaller, and lockup at a much lower rotational speed can be allowed.
- the frequency of the resonance (resonance point R1) (the second torque transmission path P2, that is, the second intermediate point).
- the frequency f R1 can be expressed by the following simple expression (8).
- Expression (8) indicates the natural frequency of the second torque transmission path P2 (second intermediate member 14) when it is assumed that the drive member 11 and the driven member 16 do not rotate relative to each other.
- the resonance of the second intermediate member 14 is a virtual one that does not occur in the rotation speed range where the damper device 10 is used, and the rotation speed corresponding to the natural frequency f R1 of the second intermediate member 14 is locked. It becomes lower than the lockup rotation speed Nlup of the up clutch 8.
- the next resonance (for example, the first intermediate member 12) is performed when the engine speed increases after the antiresonance point A occurs.
- Resonance see resonance point R2 in FIG. 3.
- the spring constants k 1 , k 2 , k 3 , k 4 , and moment of inertia J are set so that the frequency of resonance (resonance point R 2) generated on the high rotation side (high frequency side) is higher than the anti-resonance point A. preferably selected and set 21 and J 22.
- the resonance (resonance point R2) can be generated on the high rotation speed side where vibrations are hardly manifested, and the vibration damping performance of the damper device 10 in the low rotation speed range can be further improved. it can.
- the resonance frequency (the first torque transmission path P1, that is, the natural frequency of the first intermediate member 12) is set to “ Assuming that f R2 ′′, the frequency f R2 can be expressed by the following simple expression (9). Equation (9) represents the natural frequency of the first torque transmission path P1 (first intermediate member 12) when it is assumed that the drive member 11 and the driven member 16 do not rotate relative to each other. In this case, the rotation speed corresponding to the natural frequency f R2 of the first intermediate member 12 is higher than the lockup rotation speed Nlup.
- the moments of inertia J 21 and J 22 are selected and set. As a result, lockup by the lockup clutch 8 is executed while suppressing transmission of vibration to the input shaft IS of the transmission, and vibration from the engine is very good by the damper device 10 immediately after the lockup is executed. It becomes possible to attenuate to.
- the third and fourth springs SP3 and SP4 of the second torque transmission path P2 are more in the radial direction of the damper device 10 than the first and second springs SP1 and SP2 of the first torque transmission path P1. Arranged outside.
- the natural frequency of the first and second torque transmission paths P1, P2 (first and second intermediate members 12, 14) is set by adjusting the spring constant (rigidity) of the first to fourth springs SP1 to SP4. The degree of freedom can be improved.
- the second intermediate member 14 is arranged outside the first intermediate member 12 in the radial direction of the damper device 10.
- the natural frequency of the first and second intermediate moment of inertia J 21, first and second torque transfer path by adjusting the J 22 P1 of members 12, 14, P2 (the first and second intermediate members 12, 14) It is possible to improve the degree of freedom of setting and to further shorten the axial length of the damper device 10.
- the second intermediate member 14 is configured such that the inertia moment J 22 is larger than the inertia moment J 21 of the first intermediate member 12, and is connected to the turbine runner 5 so as to rotate integrally.
- the resonance frequency of the second intermediate member 14 and the frequency fa of the antiresonance point A can be further reduced to set the antiresonance point A to a lower rotation side (low frequency side).
- the first intermediate member 12 may be configured such that the moment of inertia J 21 is larger than the moment of inertia J 22 of the second intermediate member 14, and rotates integrally with the turbine runner 5. It may be connected.
- the damper device 10 By designing the damper device 10 based on the frequency fa at the antiresonance point A as described above, the first and second torque transmission paths P1 and P2 having the first or second intermediate members 12 and 14 are driven.
- the vibration damping performance of the damper device 10 included between the member 11 and the driven member 16 can be further improved.
- the damper device 10 when the lock-up rotation speed Nlup is set to a value around 1000 rpm, for example, the damper device 10 is set so as to satisfy 900 rpm ⁇ (120 / n) ⁇ fa ⁇ 1200 rpm, for example. It has been confirmed that a very good result can be obtained practically by configuring.
- the ratio of the spring constants k 1 , k 2 , k 3 , k 4 of the first to fourth springs SP1 to SP4 is 1.00 ⁇ k 1 / k total ⁇ 1.60 0.45 ⁇ k 2 / k total ⁇ 1.05 0.75 ⁇ k 3 / k total ⁇ 1.35 0.75 ⁇ k 4 / k total ⁇ 1.35 It has been found that the vibration damping performance of the damper device 10 can be ensured extremely well in practice by satisfying this condition.
- the spring constants of the first to fourth springs SP1 to SP4 are the combined spring constants (1 / k 3 + 1 / k 4 ) ⁇ 1 of the third and fourth springs SP3 and SP4 acting in series. Is smaller than the combined spring constant (1 / k 1 + 1 / k 2 ) ⁇ 1 of the first and second springs SP1 and SP2 acting in series. Accordingly, the natural frequency f R1 of the second torque transmission path P2, that is, the second intermediate member 14, can be made smaller than the natural frequency f R2 of the first torque transmission path P1, that is, the first intermediate member 12. It becomes.
- the outer diameters (coil diameters) of the first and second springs SP1, SP2 are larger than the outer diameters (coil diameters) of the third and fourth springs SP3, SP4.
- the torsion angles of the first and second springs SP1 and SP2 are set to the third and fourth springs SP3 and SP4 on the outer peripheral side. It is possible to increase the wire diameters of the first and second springs SP1 and SP2 while securing the torque sharing of the first torque transmission path P1 satisfactorily.
- the drive member 11 further includes spring contact portions 112c and 113c that contact the end portion of the first spring SP1 and a spring contact portion 111c that contacts the end portion of the third spring SP3.
- the third and fourth springs SP3 and SP4 of the second torque transmission path P2 are arranged on the outer side in the radial direction of the damper device 10 than the first and second springs SP1 and SP2 of the first torque transmission path P1. Is possible.
- the drive member 11 has a spring contact portion 111c that contacts the end portion of the third spring SP3 and a lock-up piston 80 to which power from the engine is transmitted.
- the first plate member 111 connected via the rivet, the spring contact portion 112c that contacts the end of the first spring SP1, and the first and second springs SP1 and SP2 and the third and fourth springs SP3 and SP3.
- a second plate member 112 coupled (fitted) to the first plate member 111 so as to rotate integrally with the SP4 in the radial direction and a spring contact portion 113c that contacts the end of the first spring SP1.
- a third plate portion connected to the second plate member 112 through a rivet so as to rotate integrally therewith. And a 113.
- the driven member 16 is disposed between the second plate member 112 and the third plate member 113 in the axial direction of the damper device (10). Accordingly, the third and fourth springs SP4 and SP4 can be disposed on the outer side in the radial direction of the damper device 10 with respect to the first and second springs SP1 and SP2 while suppressing an increase in the axial length of the damper device 10. It becomes possible.
- the connecting portion (the rivet that fastens both) of the lockup piston 80 and the first plate member 111 and the connecting portion (the rivet that fastens both) of the second plate member 112 and the third plate member 113 are: As shown in FIG. 2, it is provided between the first and springs SP1 and SP2 and the third and fourth springs SP3 and SP4 in the radial direction. Thereby, the axial length of the damper device 10 can be further shortened.
- the fixing portion between the turbine connecting member 55 and the turbine runner 5 is also formed between the first and second springs SP1 and SP2 and the third and fourth springs SP3 and SP4 as shown in FIG. Provided in the radial direction. Thereby, the 2nd intermediate member 14 and the turbine runner 5 can be connected, shortening the axial length of the damper apparatus 10 more.
- FIG. 4 is a cross-sectional view showing a starting device 1B including a damper device 10B according to another embodiment of the present disclosure. Note that, among the components of the starting device 1B and the damper device 10B, the same elements as those of the above-described starting device 1 and the damper device 10 are denoted by the same reference numerals, and redundant description is omitted.
- the damper device 10 ⁇ / b> B of the starting device 1 ⁇ / b> B includes a third intermediate member (first member) disposed between the second intermediate member 14 and the driven member 16 on the second torque transmission path P ⁇ b> 2 as a rotating element. 3 intermediate elements) 15.
- the damper device 10B includes a plurality of fifth springs (fifth elastic bodies) SP5 that transmit torque between the third intermediate member 15 and the driven member 16 as torque transmitting elements.
- the second torque transmission path P ⁇ b> 2 of the damper device 10 ⁇ / b> B is an element disposed between the drive member 11 and the driven member 16, and includes the second and third intermediate members 14 and 15, the third, fourth, and second
- the drive member 11 includes a plurality of third springs SP3, a second intermediate member 14, a plurality of fourth springs SP4, a third intermediate member 15, and a plurality of fifth springs SP5.
- torque is transmitted between the driven member 16 and the driven member 16.
- the damper device 10B includes a fifth stopper 25 that restricts the relative rotation between the third intermediate member 15 and the driven member 16 and restricts the bending of the fifth spring SP5.
- the phase of vibration transmitted from the first torque transmission path P1 to the driven member 16 and the second The phase of vibration transmitted from the torque transmission path P2 to the driven member 16 is reversed at least twice, and at least two anti-resonance points A1 and A2 can be set as shown in FIG. Accordingly, the first anti-resonance point A1 (frequency fa 1 ) on the low rotation side (low frequency side) is set in the same manner as the damper device 10 to thereby generate the first anti-resonance point A.
- the resonance point R1 of 1 is shifted to a lower rotation side (low frequency side) so as to be included in the non-lockup region, and lockup at a lower rotation number is allowed and the damper device 10B in the low rotation region is
- the vibration damping performance can be further improved.
- the second anti-resonance point A2 (frequency fa 2 ) on the higher rotation side (high frequency side) than the first anti-resonance point A1 and the second resonance point R2 is, for example, the resonance point of the input shaft IS of the transmission. Or the resonance point of the drive shaft, etc. (or closer), the occurrence of resonance or the like of the input shaft IS can be satisfactorily suppressed.
- the third intermediate member 15 is provided in the first torque transmission path P1 so that the first spring SP1 and the fifth spring SP5 act in series, thereby lowering the entire damper device 10B. Rigidity (long stroke) can be achieved.
- the spring constant of the fourth spring SP4 between the second and third intermediate members 14, 15 is set to the spring constant of the first, second, third, and fifth springs SP1, SP2, SP3, and SP5. It is better to make it larger.
- either one of the third and fifth stoppers 23 and 25 is configured to operate when the input torque to the drive member 11 reaches the torque T2 corresponding to the maximum torsion angle ⁇ max.
- the stopper may be configured to operate when the input torque reaches a torque smaller than the torque T2.
- the damper device 10B can have two or more stages (two stages) of attenuation characteristics.
- the rotation speed is lower than that of the first anti-resonance point A1.
- the second and third intermediate members 14 and 15 and the fourth spring SP4 can be resonated together on the side (low frequency side), and the first antiresonance point A1 can be set on the lower rotation side.
- the damper device of the present disclosure is the first intermediate element in the damper device (10, 10B) including the input element (11) to which power from the internal combustion engine is transmitted and the output element (16). (12), a first elastic body (SP1) for transmitting torque between the input element (11) and the first intermediate element (12), and the first intermediate element (12) and the output element (16) ), A second torque transmission path (P1) including a second elastic body (SP2) that transmits torque to the second intermediate element (14), the input element (11), and the second intermediate element (14). And a fourth elastic body (SP4) for transmitting torque between the second intermediate element (14) and the output element (16). , Provided in parallel with the first torque transmission path (P1).
- the fourth elastic bodies (SP3, SP4) are arranged on the outer side in the radial direction of the damper device (10, 10B) rather than the first and second elastic bodies (SP1, SP2) so as to be arranged along the circumferential direction. It is what is done.
- the phase of vibration transmitted from the first torque transmission path to the output element, and the phase of vibration transmitted from the second torque transmission path to the output element Is set, for example, to an anti-resonance point at which the vibration amplitude of the output element is theoretically zero when it is shifted by 180 degrees due to the occurrence of resonance according to the natural frequency of the second torque transmission path (second intermediate element).
- the phase of vibration transmitted from the first torque transmission path to the output element Is set, for example, to an anti-resonance point at which the vibration amplitude of the output element is theoretically zero when it is shifted by 180 degrees due to the occurrence of resonance according to the natural frequency of the second torque transmission path (second intermediate element).
- the third and fourth elastic bodies of the second torque transmission path are arranged on the outer side in the radial direction of the damper device relative to the first and second elastic bodies of the first torque transmission path, so that the first to fourth elasticity
- the degree of freedom in setting the natural frequency of the first and second torque transmission paths (first and second intermediate elements) by adjusting the rigidity of the body can be improved.
- the combined spring constant of the third and fourth elastic bodies (SP3, SP4) acting in series is smaller than the combined spring constant of the first and second elastic bodies (SP1, SP2) acting in series. Also good. Thereby, it is possible to make the natural frequency of the second torque transmission path (second intermediate element) smaller than the natural frequency of the first torque transmission path (first intermediate element).
- first to fourth elastic bodies may be coil springs
- the outer diameters of the first and second elastic bodies may be the third. And it may be larger than the outer diameter of the fourth elastic body (SP3, SP4).
- the wire diameters of the first and second elastic bodies can be increased to ensure good torque sharing of both, that is, the first torque transmission path.
- the second intermediate element (14) may be arranged on the outer side in the radial direction than the first intermediate element (12). This improves the degree of freedom in setting the natural frequency of the first and second torque transmission paths (first and second intermediate elements) by adjusting the moments of inertia of the first and second intermediate elements, and improves the damper device
- the shaft length can be further shortened.
- the moment of inertia of the second intermediate element (14) may be larger than the moment of inertia of the first intermediate element (12).
- the natural frequency of the second torque transmission path (second intermediate element) can be further reduced as compared with the natural frequency of the first torque transmission path (first intermediate element).
- the second intermediate element (12) may be coupled to rotate integrally with the turbine runner (5) of the fluid transmission device. Thereby, the substantial moment of inertia (total value of the moment of inertia) of the second intermediate element can be further increased.
- the input element (11) has an inner contact portion (112c, 113c) that contacts the end portion of the first elastic body (SP1) and an outer contact that contacts the end portion of the third elastic body (SP3).
- the output element (16) may include an inner contact portion (16ci) that contacts an end portion of the second elastic body (SP2) and the fourth elastic body (SP4). ) And an outer abutting portion (16co) that abuts on the end portion.
- the input element (11) includes the outer contact portion (111c) that contacts the end portion of the third elastic body (SP3), and a power input member (80) to which power from the internal combustion engine is transmitted. ) And the first abutting portion (112c) abutting against the end portion of the first elastic body (SP1) and the first and second elastic bodies (SP1, SP1).
- the output element may include 16) may be placed between the axial direction of the damper device (10) between the second said input member (112) the third input member (113).
- the connecting portion between the power input member (80) and the first input member (111) and the connecting portion between the second input member (112) and the third input member (113) may be provided between the first and second elastic bodies (SP1, SP2) and the third and fourth elastic bodies (SP3, SP4) in the radial direction. Thereby, the axial length of the damper device can be further shortened.
- the damper device (10) is a turbine connecting member fixed to a turbine runner (5) of a fluid transmission device and connecting the second intermediate element (14) and the turbine runner (5) so as to rotate integrally.
- (55) may be further provided, and the fixing portion between the turbine connecting member (55) and the turbine runner (5) may be the first and second elastic bodies (SP1, SP2) and the third and fourth. You may provide between the elastic bodies (SP3, SP4) in the said radial direction. As a result, it is possible to connect the second intermediate element and the turbine runner while further shortening the axial length of the damper device.
- first intermediate element (12) may be rotatably supported by a protrusion (16b) protruding in the axial direction of the damper device (110) from the output element (16).
- the second intermediate element (14) may be rotatably supported by a support part (111b) provided on the input element (11, 111).
- the damper device based on the frequency (fa) of the antiresonance point (A) at which the vibration amplitude of the output element (16) is theoretically zero, the first, second, third and fourth The spring constants of the elastic bodies (SP1, SP2, SP3, SP4) and the moments of inertia of the first and second intermediate elements (12, 14) are determined.
- the damper device based on the frequency of the anti-resonance point that can further reduce the vibration amplitude of the output element, two power transmissions each having an intermediate element disposed between a pair of elastic bodies It becomes possible to further improve the vibration damping performance of the damper device including the path between the input element and the output element.
- the spring constants of the first, second, third and fourth elastic bodies (SP1, SP2, SP3, SP4) and the moment of inertia of the first and second intermediate elements (12, 14) are It may be determined based on the frequency (fa) of the antiresonance point (A) and the number of cylinders (n) of the internal combustion engine.
- damper device (10) has the frequency of the antiresonance point (A) as “fa” and the number of cylinders of the internal combustion engine as “n”, 500rpm ⁇ (120 / n) ⁇ fa ⁇ 1500rpm It may be configured to satisfy.
- the anti-resonance point that can further reduce the vibration amplitude of the output element within a low speed range from 500 rpm to 1500 rpm, the connection between the internal combustion engine and the input element at a lower speed is allowed. At the same time, it is possible to further improve the vibration damping performance of the damper device in a low rotational speed range in which vibration from the internal combustion engine tends to be large.
- the frequency of the resonance that generates the antiresonance point is smaller than the frequency fa of the antiresonance point and as small as possible.
- the frequency fa of the anti-resonance point can be made smaller, and the connection between the internal combustion engine and the input element at a lower rotational speed can be allowed. Furthermore, by configuring the damper device so that the frequency of resonance generated on the high rotation side (high frequency side) is higher than the anti-resonance point, the resonance can be detected on the high rotation speed region side where vibration is difficult to be realized. Therefore, the vibration damping performance of the damper device in the low rotation speed region can be further improved.
- the damper device (10) may be configured to satisfy Nloop ⁇ (120 / n) ⁇ fa. As a result, when the internal combustion engine and the input element are connected by the lockup clutch, or immediately after the connection between the two, the vibration from the internal combustion engine can be damped very well by the damper device.
- the damper device (10) may be configured to satisfy 900 rpm ⁇ (120 / n) ⁇ fa ⁇ 1200 rpm.
- the frequency fa of the antiresonance point (A) may be expressed by the above formula (6).
- the second torque transmission path (P2) may further include a third intermediate element (15) and a fifth elastic body (SP5)
- the fourth elastic body (SP4) includes the second and second elastic bodies (SP4).
- Torque may be transmitted between the three intermediate elements (14, 15), and the fifth elastic body (SP5) may transmit torque between the third intermediate element (15) and the output element (16). May be communicated.
- the phase of vibration transmitted from the first torque transmission path to the output element and the phase of vibration transmitted from the second torque transmission path to the output element are reversed at least twice, and at least Two anti-resonance points can be set.
- the damper device (10) includes the first to fourth elasticity until the input torque (T) transmitted from the internal combustion engine to the input element (11) is equal to or greater than a predetermined threshold value (T1). You may be comprised so that the bending of a body (SP1, SP2, SP3, SP4) may not be controlled.
- the invention of the present disclosure can be used in the field of manufacturing damper devices.
Abstract
Description
1.00≦k1/ktotal≦1.60
0.45≦k2/ktotal≦1.05
0.75≦k3/ktotal≦1.35
0.75≦k4/ktotal≦1.35
を満たすようにすることで、ダンパ装置10の振動減衰性能を実用上極めて良好に確保し得ることが判明している。
500rpm≦(120/n)・fa≦1500rpm
を満たすように構成されてもよい。
Claims (21)
- 内燃機関からの動力が伝達される入力要素と、出力要素とを含むダンパ装置において、
第1中間要素、前記入力要素と前記第1中間要素との間でトルクを伝達する第1弾性体、および前記第1中間要素と前記出力要素との間でトルクを伝達する第2弾性体を含む第1トルク伝達経路と、
第2中間要素、前記入力要素と前記第2中間要素との間でトルクを伝達する第3弾性体、および前記第2中間要素と前記出力要素との間でトルクを伝達する第4弾性体を含み、前記第1トルク伝達経路と並列に設けられる第2トルク伝達経路とを備え、
前記第1および第2弾性体は、前記ダンパ装置の周方向に沿って並ぶように配置され、前記第3および第4弾性体は、前記周方向に沿って並ぶように前記第1および第2弾性体よりも前記ダンパ装置の径方向における外側に配置されるダンパ装置。 - 請求項1に記載のダンパ装置において、
直列に作用する前記第3および第4弾性体の合成ばね定数は、直列に作用する前記第1および第2弾性体の合成ばね定数よりも小さいダンパ装置。 - 請求項1または2に記載のダンパ装置において、
前記第1から第4弾性体は、コイルスプリングであり、
前記第1および第2弾性体の外径は、前記第3および第4弾性体の外径よりも大きいダンパ装置。 - 請求項1から3の何れか一項に記載のダンパ装置において、
前記第2中間要素は、前記第1中間要素よりも前記径方向における外側に配置されるダンパ装置。 - 請求項1から4の何れか一項に記載のダンパ装置において、
前記第2中間要素の慣性モーメントは、前記第1中間要素の慣性モーメントよりも大きいダンパ装置。 - 請求項1から5の何れか一項に記載のダンパ装置において、
前記第2中間要素は、流体伝動装置のタービンランナに一体回転するように連結されるダンパ装置。 - 請求項1から6の何れか一項に記載のダンパ装置において、
前記入力要素は、前記第1弾性体の端部と当接する内側当接部と、前記第3弾性体の端部と当接する外側当接部とを有し、
前記出力要素は、前記第2弾性体の端部と当接する内側当接部と、前記第4弾性体の端部と当接する外側当接部とを有するダンパ装置。 - 請求項7に記載のダンパ装置において、
前記入力要素は、前記第3弾性体の端部と当接する前記外側当接部を有すると共に前記内燃機関からの動力が伝達される動力入力部材に連結される第1入力部材と、前記第1弾性体の端部と当接する前記内側当接部を有すると共に前記第1および第2弾性体と前記第3および第4弾性体との前記径方向における間で前記第1入力部材に一体回転するように連結される第2入力部材と、前記第1弾性体の端部と当接する前記内側当接部を有すると共に前記第2入力部材に一体回転するように連結される第3入力部材とを含み、
前記出力要素は、前記第2入力部材と前記第3入力部材との前記ダンパ装置の軸方向における間に配置されるダンパ装置。 - 請求項8に記載のダンパ装置において、
前記動力入力部材と前記第1入力部材との連結部と、前記第2入力部材と前記第3入力部材との連結部とは、前記第1および第2弾性体と前記第3および第4弾性体との前記径方向における間に設けられるダンパ装置。 - 請求項9に記載のダンパ装置において、
流体伝動装置のタービンランナに固定されて前記第2中間要素と前記タービンランナとを一体回転するように連結するタービン連結部材を更に備え、
前記タービン連結部材と前記タービンランナとの固定部は、前記第1および第2弾性体と前記第3および第4弾性体との前記径方向における間に設けられるダンパ装置。 - 請求項1から10の何れか一項に記載のダンパ装置において、
前記第1中間要素は、前記出力要素から前記ダンパ装置の軸方向に突出する突起部により回転自在に支持されるダンパ装置。 - 請求項1から11の何れか一項に記載のダンパ装置において、
前記第2中間要素は、前記入力要素に設けられた支持部により回転自在に支持されるダンパ装置。 - 内燃機関からの動力が伝達される入力要素と、出力要素とを含むダンパ装置において、
第1中間要素、前記入力要素と前記第1中間要素との間でトルクを伝達する第1弾性体、および前記第1中間要素と前記出力要素との間でトルクを伝達する第2弾性体を含む第1トルク伝達経路と、
第2中間要素、前記入力要素と前記第2中間要素との間でトルクを伝達する第3弾性体、および前記第2中間要素と前記出力要素との間でトルクを伝達する第4弾性体を含み、前記第1トルク伝達経路と並列に設けられる第2トルク伝達経路とを備え、
前記出力要素の振動振幅が理論上ゼロになる反共振点の振動数に基づいて、前記第1、第2、第3および第4弾性体のばね定数と、前記第1および第2中間要素の慣性モーメントとが定められるダンパ装置。 - 請求項13に記載のダンパ装置において、
前記反共振点の振動数と前記内燃機関の気筒数とに基づいて、前記第1、第2、第3および第4弾性体のばね定数と、前記第1および第2中間要素の慣性モーメントとが定められるダンパ装置。 - 請求項13または14に記載のダンパ装置において、
前記反共振点の振動数を“fa”とし、前記内燃機関の気筒数を“n”としたときに、
500rpm≦(120/n)・fa≦1500rpm
を満たすように構成されるダンパ装置。 - 請求項13から15の何れか一項に記載のダンパ装置において、
前記反共振点の振動数を“fa”とし、前記内燃機関と前記入力要素とを連結するロックアップクラッチのロックアップ回転数を“Nlup”としたときに、
Nlup=(120/n)・fa
を満たすように構成されるダンパ装置。 - 請求項13から15の何れか一項に記載のダンパ装置において、
前記反共振点の振動数を“fa”とし、前記内燃機関と前記入力要素とを連結するロックアップクラッチのロックアップ回転数を“Nlup”としたときに、
Nlup<(120/n)・fa
を満たすように構成されるダンパ装置。 - 請求項15から17の何れか一項に記載のダンパ装置において、
900rpm≦(120/n)・fa≦1200rpm
を満たすように構成されるダンパ装置。 - 請求項1から14の何れか一項に記載のダンパ装置において、
前記第2トルク伝達経路は、第3中間要素と第5弾性体とを更に含み、
前記第4弾性体は、前記第2および第3中間要素の間でトルクを伝達し、前記第5弾性体は、前記第3中間要素と前記出力要素との間でトルクを伝達するダンパ装置。 - 請求項1から20の何れか一項に記載のダンパ装置において、
前記内燃機関から前記入力要素に伝達される入力トルクが予め定められた閾値以上になるまで、前記第1から第4弾性体の撓みが規制されないダンパ装置。
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JP2016540725A JP6311792B2 (ja) | 2014-08-05 | 2015-08-05 | ダンパ装置 |
CN201580038836.3A CN106536970B (zh) | 2014-08-05 | 2015-08-05 | 减振装置 |
US15/327,570 US20170159746A1 (en) | 2014-08-05 | 2015-08-05 | Damper device |
DE112015002955.9T DE112015002955T5 (de) | 2014-08-05 | 2015-08-05 | Dämpfervorrichtung |
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US (1) | US20170159746A1 (ja) |
JP (1) | JP6311792B2 (ja) |
CN (1) | CN106536970B (ja) |
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WO (1) | WO2016021668A1 (ja) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017159728A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
JP2017166585A (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159775A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159809A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159776A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2018061467A1 (ja) * | 2016-09-30 | 2018-04-05 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
US10883562B2 (en) | 2016-03-16 | 2021-01-05 | Aisin Aw Co., Ltd. | Damper apparatus and starting apparatus |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE112015002962B4 (de) * | 2014-08-05 | 2019-05-23 | Aisin Aw Co., Ltd. | Dämpfervorrichtung |
CN106536991B (zh) * | 2014-08-21 | 2019-01-11 | 爱信艾达株式会社 | 减振装置 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5694049A (en) * | 1979-12-26 | 1981-07-30 | Borg Warner | Two stage torsion and vibration damper |
DE102009013965A1 (de) * | 2009-03-19 | 2010-09-23 | Daimler Ag | Dämpfungseinrichtung |
JP2010230155A (ja) * | 2009-03-30 | 2010-10-14 | Aisin Aw Industries Co Ltd | ロックアップダンパ装置 |
JP2012506006A (ja) * | 2008-10-17 | 2012-03-08 | シェフラー テクノロジーズ ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | ダブルパストーショナルダンパ |
WO2012133816A1 (ja) * | 2011-03-30 | 2012-10-04 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4002043A (en) * | 1973-07-10 | 1977-01-11 | Toyota Jidosha Kogyo Kabushiki Kaisha | Apparatus for absorbing torque fluctuations produced by an internal combustion engine |
DE3529816A1 (de) * | 1984-08-21 | 1986-03-06 | Aisin Seiki K.K., Kariya, Aichi | Vorrichtung zur absorption einer drehmomentaenderung |
-
2015
- 2015-08-05 DE DE112015002955.9T patent/DE112015002955T5/de not_active Withdrawn
- 2015-08-05 US US15/327,570 patent/US20170159746A1/en not_active Abandoned
- 2015-08-05 WO PCT/JP2015/072296 patent/WO2016021668A1/ja active Application Filing
- 2015-08-05 CN CN201580038836.3A patent/CN106536970B/zh not_active Expired - Fee Related
- 2015-08-05 JP JP2016540725A patent/JP6311792B2/ja active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5694049A (en) * | 1979-12-26 | 1981-07-30 | Borg Warner | Two stage torsion and vibration damper |
JP2012506006A (ja) * | 2008-10-17 | 2012-03-08 | シェフラー テクノロジーズ ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | ダブルパストーショナルダンパ |
DE102009013965A1 (de) * | 2009-03-19 | 2010-09-23 | Daimler Ag | Dämpfungseinrichtung |
JP2010230155A (ja) * | 2009-03-30 | 2010-10-14 | Aisin Aw Industries Co Ltd | ロックアップダンパ装置 |
WO2012133816A1 (ja) * | 2011-03-30 | 2012-10-04 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108700172A (zh) * | 2016-03-16 | 2018-10-23 | 爱信艾达株式会社 | 减振装置 |
JPWO2017159775A1 (ja) * | 2016-03-16 | 2018-10-18 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159775A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159809A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159776A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
WO2017159777A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
JP2017166585A (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
CN108603563A (zh) * | 2016-03-16 | 2018-09-28 | 爱信艾达株式会社 | 减震器装置 |
US10883562B2 (en) | 2016-03-16 | 2021-01-05 | Aisin Aw Co., Ltd. | Damper apparatus and starting apparatus |
WO2017159728A1 (ja) * | 2016-03-16 | 2017-09-21 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
CN108700171A (zh) * | 2016-03-16 | 2018-10-23 | 爱信艾达株式会社 | 减振装置 |
CN108700169A (zh) * | 2016-03-16 | 2018-10-23 | 爱信艾达株式会社 | 减振装置 |
CN109790904A (zh) * | 2016-09-30 | 2019-05-21 | 爱信艾达株式会社 | 减振装置 |
EP3447330A4 (en) * | 2016-09-30 | 2019-08-28 | Aisin Aw Co., Ltd. | SHOCK ABSORBER DEVICE |
WO2018061467A1 (ja) * | 2016-09-30 | 2018-04-05 | アイシン・エィ・ダブリュ株式会社 | ダンパ装置 |
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DE112015002955T5 (de) | 2017-03-16 |
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CN106536970B (zh) | 2019-06-21 |
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