Damper device
10352396 ยท 2019-07-16
Assignee
Inventors
Cpc classification
F16F15/12373
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16F15/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A damper device includes a first rotary member, a second rotary member, a plurality of coil springs, an intermediate member and a slide spring. The first rotary member is a member into which a power of an engine is inputted. The second rotary member is disposed to be rotatable with respect to the first rotary member. The plurality of coil springs are configured to be compressed between the first rotary member and the second rotary member. The intermediate member is configured to engage the plurality of coil springs and couple the plurality of coil springs together. The slide spring is disposed axially between the first rotary member and the intermediate member. The slide spring is configured to slide against the first rotary member. The slide spring is configured not to slide with respect to the intermediate member.
Claims
1. A damper device, comprising: a first rotary member into which a power of an engine is inputted; a second rotary member disposed to be rotatable with respect to the first rotary member; a plurality of coil springs configured to be compressed between the first rotary member and the second rotary member; an intermediate member configured to engage the plurality of coil springs and couple the plurality of coil springs together; and a slide spring disposed axially between the first rotary member and the intermediate member, and configured to slide against the first rotary member and configured not to slide with respect to the intermediate member, the slide spring being formed independently of the intermediate member and being positioned on the intermediate member.
2. The damper device according to claim 1, wherein the second rotary member has a first body and a pressing part, the first body being disposed on an inner peripheral side of the plurality of coil springs, the pressing part extending radially outward from the first body and configured to press the plurality of coil springs, the intermediate member has a second body and an engaging part, the second body being disposed on the inner peripheral side of the plurality of coil springs, the engaging part extending radially outward from the second body and configured to engage respectively with the plurality of coil springs, the pressing part and the engaging part are disposed to be circumferentially aligned, and the slide spring is disposed radially inward of the pressing part and the engaging part with respect to an axial position between the first rotary member and both of the pressing part and the engaging part.
3. The damper device according to claim 2, wherein the intermediate member has a protruding part protruding toward the first rotary member, and the slide spring has a spring part and a restriction part, the spring part being configured to contact the first rotary member and the intermediate member, the restriction part being configured to engage the protruding part and restrict circumferential movement of the slide spring.
4. The damper device according to claim 3, wherein the slide spring is a wave spring, and the spring part has a first convex part and a second convex part, the first convex part contacting the first rotary member, the second convex part being disposed circumferentially adjacent to the first convex part and contacting the intermediate member.
5. The damper device according to claim 1, wherein the intermediate member has a protruding part protruding toward the first rotary member, and the slide spring has a spring part and a restriction part, the spring part being configured to contact the first rotary member and the intermediate member, the restriction part being configured to engage the protruding part and restrict circumferential movement of the slide spring.
6. The damper device according to claim 5, wherein the slide spring is a wave spring, and the spring part has a first convex part and a second convex part, the first convex part contacting the first rotary member, the second convex part being disposed circumferentially adjacent to the first convex part and contacting the intermediate member.
7. The damper device according to claim 6, wherein the protruding part is an embossed part formed by embossing the intermediate member.
8. The damper device according to claim 5, wherein the protruding part is an embossed part formed by embossing the intermediate member.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Referring now to the attached drawings which form a part of this original disclosure:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
(12)
(13)
(14)
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
(15) <Entire Construction>
(16) A flywheel assembly 1 (an exemplary damper device) according to a first exemplary embodiment will be hereinafter explained with reference to
(17) As shown in
(18) <Input Plate>
(19) Power of the engine is inputted into the input plate 2. Put differently, the input plate 2 is a member into which power generated by the engine is inputted. The input plate 2 is disposed on an engine side. The input plate 2 is fixed to a crankshaft (not shown in the drawings) of the engine.
(20) As shown in
(21) As shown in
(22) As shown in
(23) As shown in
(24) As shown in
(25) As shown in
(26) As shown in
(27) The first protruding parts 22c are disposed on the outer peripheral side of the outer peripheral part (e.g., engaging parts 43 to be described; in detail, second extension parts 45) of the support plate 4. Further, each first protruding part 22c is contactable to the outer peripheral part (relevant one of the rotation restriction parts 44 to be described; see
(28) As shown in
(29) <Output Plate>
(30) The output plate 3 outputs the power of the engine to the transmission. The output plate 3 is disposed to be rotatable with respect to the input plate 2. The output plate 3 is fixed to an output shaft (not shown in the drawings) coupled to the transmission.
(31) As shown in
(32) As shown in
(33) <Support Plate>
(34) As shown in
(35) As shown in
(36) As shown in
(37) Further, as shown in
(38) The rotation restriction parts 44 serve to restrict rotation of the support plate 4. As shown in
(39) As shown in
(40) <Coil Springs>
(41) As shown in
(42) As shown in
(43) As shown in
(44) <First Stopper Mechanism>
(45) The first stopper mechanism 81 is configured to deactivate the first coil springs 51 and the second coil springs 61 by causing the support plate 4 and the output plate 3 to contact each other.
(46) When described in detail, the first stopper mechanism 81 is configured to deactivate the first coil springs 51 and the second coil springs 61 by causing the inner peripheral part of the support plate 4 and that of the output plate 3 to contact each other.
(47) When described in more detail, as shown in
(48) It should be noted that when the first coil springs 51 and the second coil springs 61 are deactivated (become incompressible), the first stopper mechanism 81 and the second stopper mechanism 85 (to be described) are configured to be simultaneously activated.
(49) <Second Stopper Mechanism>
(50) The second stopper mechanism 85 is configured to deactivate the first coil springs 51 and the second coil springs 61 by causing the input plate 2 and the support plate 4 to make contact with each other. A torsion angle at which the second stopper mechanism 85 is activated is the same as a torsion angle at which the first stopper mechanism 81 is activated. In other words, the second stopper mechanism 85 is configured to be simultaneously activated with the first stopper mechanism 81.
(51) When described in detail, the second stopper mechanism 85 is configured to deactivate the first coil springs 51 and the second coil springs 61 by causing the outer peripheral part of the second plate 22 and that of the support plate 4 to contact each other.
(52) When described in detail, as shown in
(53) It should be noted that when the first coil springs 51 and the second coil springs 61 are deactivated (become incompressible), the first stopper mechanism 81 and the second stopper mechanism 85 are configured to be simultaneously activated.
(54) <Shock Absorber Member>
(55) As shown in
(56) In detail, the shock absorber members 70 become compressible inside the first coil springs 51 and the second coil springs 61 when a torsion angle (an exemplary rotary angle) of the output plate 3 relative to the input plate 2 becomes a predetermined first angle 1 (see
(57) In more detail, the shock absorber members 70 become compressible between the support plate 4 and the output plate 3 when the torsion angle of the output plate 3 relative to the input plate 2 is greater than or equal to the predetermined first angle 1 and less than the torsion angle 2 at which the first stopper mechanism 81 and the second stopper mechanism 85 are activated. For example, the shock absorber member 70, disposed inside each first coil spring 51, is compressible between the first pressing part 27 of the first and second plates 21 and 22 and the engaging part 43 of the support plate 4. On the other hand, the shock absorber member 70, disposed inside each second coil spring 61, is compressible between the engaging part 43 of the support plate 4 and the third pressing part 34 of the output plate 3.
(58) It should be noted that the predetermined first angle 1 is less than the torsion angle 2 at which the first stopper mechanism 81 and the second stopper mechanism 85 are activated.
(59) When large torque is abruptly inputted into the input plate 2 under the aforementioned condition, the shock absorber members 70 hinder the first stopper mechanism 81 and the second stopper mechanism 85 from being activated. Further, in activation of the first stopper mechanism 81 and the second stopper mechanism 85, the shock absorber members 70 also lessen activation sound of the first stopper mechanism 81 and the second stopper mechanism 85.
(60) <Wave Spring>
(61) The wave spring 40 is configured to generate slide resistance by sliding against a member disposed axially adjacent thereto. As shown in
(62) Further, as shown in
(63) As shown in
(64) In the spring part 40a, the second convex parts 44b are circumferentially aligned at predetermined intervals. Further, each second convex part 44b is located between adjacent two of the first convex parts 44a. The second convex parts 44b are arranged to contact the support plate 4.
(65) As shown in
(66) As described above, the restriction parts 40b are engaged with the support plate 4. Hence, slide resistance to be generated between the second convex parts 44b and the support plate 4 is small. Therefore, in the present flywheel assembly 1, slide resistance to be generated between the first convex parts 44a and the input plate 2 (the second plate 22) can be considered as substantive slide resistance.
(67) <Actions of Flywheel Assembly>
(68) Actions (torsional characteristics) of the flywheel assembly 1 will be explained with reference to
(69) <Positive-side Torsional Characteristic>
(70) First, power of the engine is inputted into the flywheel assembly 1, and in turn, the input plate 2 begins to be rotated with respect to the output plate 3 in the first direction (the R1 direction in
(71) Then, the second coil spring 61 and the first coil spring 51 are compressed between the input plate 2 and the output plate 3 through the support plate 4. When described in detail, the second coil spring 61 is compressed between the relevant second pressing part 28 of the input plate 2 and the relevant engaging part 43 of the support plate 4 through the spring sheets. On the other hand, the first coil spring 51 is compressed between the engaging part 43 of the support plate 4 and the relevant third pressing part 34 of the output plate 3 through the spring sheets. Accordingly, a first stage torsional stiffness K1 is formed as shown in
(72) Subsequently, when the torsion angle increases, the shock absorber members 70 disposed inside the first coil spring 51 and the second coil spring 61 become contactable to their relevant spring sheets. At this time, the torsion angle is 1. The shock absorber member 70 disposed inside the second coil spring 61 is herein compressed between the second pressing part 28 of the input plate 2 and the engaging part 43 of the support plate 4 through the spring sheets. On the other hand, the first coil spring 51 is compressed between the engaging part 43 of the support plate 4 and the third pressing part 34 of the output plate 3 through the spring sheets. Accordingly, a second stage torsional stiffness K2 is formed as shown in
(73) When the torsion angle further increases and reaches 2 under the condition, the first stopper mechanism 81 and the second stopper mechanism 85 are activated.
(74) When described in detail, on the inner peripheral side of the first coil spring 51, the relevant second contact part 42 of the support plate 4 contacts the relevant first contact part 33 of the output plate 3. Accordingly, the first coil spring 51 is deactivated. In more detail, the first coil spring 51 and the second coil spring 61 are deactivated when the second contact part 42 of the support plate 4 contacts the first contact part 33 of the output plate 3, and further, when the first protruding part 22c of the second plate 22, which is disposed on the outer peripheral side of the second coil spring 61, contacts the relevant rotation restriction part 44 of the support plate 4. This is a condition that the torsion angle has reached the maximum torsion angle 2.
(75) <Negative-side Torsional Characteristics>
(76) Negative-side torsional characteristics are substantially the same as the positive-side torsional characteristics, and therefore, will be explained with reference to
(77) First, power of the engine is inputted into the flywheel assembly 1, and in turn, the input plate 2 begins to be rotated with respect to the output plate 3 in the second direction (the R2 direction in
(78) Then, the second coil spring 61 and the first coil spring 51 are compressed between the input plate 2 and the output plate 3 through the support plate 4. When described in detail, the first coil spring 51 is compressed between the relevant first pressing part 27 of the input plate 2 and the relevant engaging part 43 of the support plate 4 through the spring sheets. On the other hand, the second coil spring 61 is compressed between the engaging part 43 of the support plate 4 and the relevant third pressing part 34 of the output plate 3 through the spring sheets. Accordingly, the first stage torsional stiffness K1 is formed as shown in
(79) Subsequently, when the torsion angle increases, the shock absorber members 70 disposed inside the first coil spring 51 and the second coil spring 61 become contactable to their relevant spring sheets. At this time, the torsion angle is 1. The second coil spring 61 is herein compressed between the engaging part 43 of the support plate 4 and the third pressing part 34 of the output plate 3 and through the spring sheets. On the other hand, the shock absorber member 70 disposed inside the first coil spring 51 is compressed between the first pressing part 27 of the input plate 2 and the engaging part 43 of the support plate 4 through the spring sheets. Accordingly, the second stage torsional stiffness K2 is formed as shown in
(80) When the torsion angle further increases and reaches 2 under the condition, the first stopper mechanism 81 and the second stopper mechanism 85 are activated.
(81) When described in detail, on the inner peripheral side of the second coil spring 61, the relevant second contact part 42 of the support plate 4 contacts the relevant first contact part 33 of the output plate 3. Accordingly, the second coil spring 61 is deactivated. In more detail, the first coil spring 51 and the second coil spring 61 are deactivated when the second contact part 42 of the support plate 4 contacts the first contact part 33 of the output plate 3, and further, when the first protruding part 22c of the second plate 22, which is disposed on the outer peripheral side of the first coil spring 51, contacts the relevant rotation restriction part 44 of the support plate 4. This is a condition that the torsion angle has reached the maximum torsion angle 2.
(82) <Features>
(83) The present flywheel assembly 1 includes the input plate 2, the output plate 3, the plurality of coil springs 50, the support plate 4 and the wave spring 40. The input plate 2 is a member in which power of the engine is inputted. The output plate 3 is disposed to be rotatable with respect to the input plate 2. The plurality of coil springs 50 are configured to be compressed between the input plate 2 and the output plate 3. The support plate 4 is engaged with the plurality of coil springs 50 and couples the coil springs 50. The wave spring 40 is disposed axially between the input plate 2 and the support plate 4. Further, the wave spring 40 is configured to slide against the input plate 2. Yet further, the wave spring 40 is positioned on the support plate 4.
(84) In the present flywheel assembly 1, when inputted into the input plate 2, the power of the engine is sequentially transmitted to the input plate 2, the support plate 4 and the output plate 3 in this order. In the power transmission path, the plurality of coil springs 50 are configured to be compressed between the input plate 2 and the output plate 3 through the support plate 4. Further, the wave spring 40 is configured to slide against the input plate 2 while being positioned on the support plate 4.
(85) According to the present flywheel assembly 1, the wave spring 40 is configured to slide against the input plate 2 while being positioned on the support plate 4. Put differently, the support plate 4 generates slide resistance between itself and the input plate 2, while being restricted from circumferentially moving. Thus, the present flywheel assembly 1 can stably generate slide resistance.
(86) In the present flywheel assembly 1, the output plate 3 has the annular part 32 and the third pressing parts 34. The annular part 32 is disposed on the inner peripheral side of the coil springs 50. The third pressing parts 34 extend radially outward from the annular part 32 and are capable of pressing the coil springs 50. Further, the support plate 4 has the annular body 41 and the engaging parts 43. The annular body 41 is disposed on the inner peripheral side of the coil springs 50. The engaging parts 43 extend radially outward from the annular body 41 and are capable of being engaged with the respective coil springs 50. Herein, the third pressing parts 34 of the output plate 3 and the engaging parts 43 of the support plate 4 are disposed to be circumferentially aligned. Yet further, the wave spring 40 is disposed axially between the input plate 2 and both of the third pressing parts 34 and the engaging parts 43.
(87) In the present flywheel assembly 1, the wave spring 40 is positioned on the support plate 4. Thus, slide resistance can be stably generated between the wave spring 40 and the input plate 2 even when the third pressing parts 34 of the output plate 3 and the engaging parts 43 of the support plate 4 are disposed to be circumferentially aligned, and further, the wave spring 40 is disposed between the input plate 2 and both of the third pressing parts 34 and the engaging parts 43.
(88) In the present flywheel assembly 1, the support plate 4 has the second protruding parts 48 protruding toward the input plate 2. Further, the wave spring 40 has the spring part 40a and the restriction parts 40b. The spring part 40a makes contact with the input plate 2 and the support plate 4. The restriction parts 40b are engaged with the second protruding parts 48 and restrict circumferential movement of the wave spring 40.
(89) In the present flywheel assembly 1, the spring part 40a contacts the input plate 2 and the support plate 4. Thus, the support plate 4 can be axially positioned with respect to the input plate 2. Further, the restriction parts 40b are engaged with the second protruding parts 48 and restrict circumferential movement of the wave spring 40. Thus, slide resistance can be stably generated between the spring part 40a and the input plate 2.
(90) In the present flywheel assembly 1, the spring part 40a has the first convex parts 44a and the second convex parts 44b. The first convex parts 44a contact the input plate 2. The second convex parts 44b are disposed circumferentially adjacent to the first convex parts 44a and contact the support plate 4.
(91) In the present flywheel assembly 1, the first convex parts 44a of the wave spring 40 contact the input plate 2, whereas the second convex parts 44b of the wave spring 40 contact the support plate 4. Thus, even when the support plate 4 is axially moved due to variation in torque or so forth, the support plate 4 can be axially positioned with respect to the input plate 2 by the wave spring 40.
(92) Further, the wave spring 40 can maintain a condition that the first convex parts 44a thereof always contact the input plate 2. Thus, slide resistance can be stably generated between the wave spring 40 and the input plate 2.
(93) In the present flywheel assembly 1, the second protruding parts 48 are embossed parts formed by embossing the support plate 4.
(94) In the present flywheel assembly 1, the second protruding parts 48 are formed by embossing. Thus, the second protruding parts 48 can be easily formed, and further, can reliably exert required stiffness.
Other Exemplary Embodiments
(95) The present invention is not limited to the aforementioned exemplary embodiment, and a variety of changes and modifications can be made without departing from the scope of the present invention as defined in the appended claims.
(96) The aforementioned exemplary embodiment has exemplified the construction that the restriction parts 40b are formed on the inner peripheral part of the spring part 40a. However, the restriction parts 40b may be formed in any position on the spring part 40a as long as they can be engaged with the support plate 4.
(97) The aforementioned exemplary embodiment has exemplified the construction that the second protruding parts 48 are formed by embossing the support plate 4. However, the second protruding parts 48 may be formed by any suitable method as long as they protrude toward the input plate 2. Alternatively, the second protruding parts 48 may be formed as discrete elements provided separately from the support plate 4.
(98) The present invention is widely applicable to damper devices.