FLUID COUPLING
20170307028 · 2017-10-26
Inventors
Cpc classification
F16D3/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0278
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D25/0635
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D33/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H45/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0294
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0247
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16D25/0635
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A torque converter includes a front cover, an impeller, an output shaft member, a turbine and a clutch. The turbine includes a turbine shell, a turbine blade, a coupling portion and a piston portion. The turbine shell is supported by the output shaft member. Additionally, the turbine shell slides on the output shaft member in an axial direction. The turbine blade is attached to the turbine shell. The coupling portion extends from the turbine shell toward the front cover. The piston portion extends from the coupling portion in a radial direction. The clutch is disposed between the piston portion and the front cover.
Claims
1. A fluid coupling rotatable about a rotational axis, the fluid coupling comprising: a front cover into which a torque is inputted; an impeller including an impeller shell and an impeller blade, the impeller shell being fixed to the front cover, the impeller blade being attached to the impeller shell; an output shaft member rotatable about the rotational axis, the output shaft member outputting the torque; a turbine including a turbine shell, a turbine blade, a coupling portion and a piston portion, the turbine shell being supported by the output shaft member, the turbine shell being capable of sliding on the output shaft member in an axial direction, the turbine blade being attached to the turbine shell, the coupling portion extending from the turbine shell toward the front cover, the piston portion extending from the coupling portion in a radial direction; and a clutch disposed between the piston portion and the front cover.
2. The torque converter according to claim 1, further comprising: a damper mechanism coupling the turbine and the output shaft member so as to make the turbine and the output shaft member rotatable relatively to each other.
3. The fluid coupling according to claim 2, wherein the damper mechanism includes a holder member and an elastic member, the holder member unitarily rotated with the output shaft member, the elastic member held by the holder member.
4. The fluid coupling according to claim 3, wherein the turbine further includes a first engaging part extending from the turbine shell to the elastic member.
5. The fluid coupling according to claim 3, wherein the turbine further includes a second engaging part extending from the piston portion to the elastic member.
6. The fluid coupling according to claim 1, wherein the clutch is a friction member attached to the piston portion.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0018]
[0019]
DETAILED DESCRIPTION OF EMBODIMENTS
[0020] A torque converter 100, which is an exemplary embodiment of a fluid coupling according to the present disclosure, will be hereinafter explained with reference to drawings.
[0021] As shown in
[0022] The front cover 1 is a member into which a torque from the engine is inputted. When described in detail, the front cover 1 includes a disc part 11 and a tubular part 12. The tubular part 12 extends from an outer peripheral end of the disc part 11 toward the transmission.
[0023] The impeller 2 includes an impeller shell 21 and a plurality of impeller blades 22. The impeller shell 21 is fixed to the front cover 1. When described in detail, the impeller shell 21 is welded to the front cover 1.
[0024] The impeller blades 22 are attached to the impeller shell 21. When described in detail, the impeller blades 22 are fixed to the inner peripheral surface of the impeller shell 21.
[0025] The turbine 4 includes a turbine shell 41, a plurality of turbine blades 42, a coupling portion 43 and a piston portion 44. The turbine 4 is disposed in opposition to the impeller 2. The turbine shell 41, the coupling portion 43 and the piston portion 44 are integrally provided.
[0026] The turbine shell 41 is supported by the output shaft member 3. When described in detail, the turbine shell 41 makes contact at its inner peripheral surface 411 with the output shaft member 3. The turbine shell 41 is capable of axially sliding on the output shaft member 3. Additionally, the turbine shell 41 is rotatable relatively to the output shaft member 3. When described in detail, the turbine shell 41 radially extends from the output shaft member 3.
[0027] The turbine blades 42 are attached to the turbine shell 41. When described in detail, the turbine blades 42 are fixed to the inner peripheral surface of the turbine shell 41.
[0028] The coupling portion 43 extends from the turbine shell 41 toward the front cover 1. When described in detail, the coupling portion 43 extends from the outer peripheral end of the turbine shell 41. Additionally, the coupling portion 43 extends along the axial direction. The coupling portion 43 has a cylindrical shape.
[0029] The coupling portion 43 is fixed to the turbine shell 41. For example, the coupling portion 43 is welded to the turbine shell 41. It should be noted that the coupling portion 43 maybe integrated with the turbine shell 41 as a single member.
[0030] The piston portion 44 radially extends from the coupling portion 43. When described in detail, the piston portion 44 extends radially inside from the coupling portion 43. The piston portion 44 extends from the front cover 1—side end of the coupling portion 43 toward the output shaft member 3. The piston portion 44 may be integrated with the coupling portion 43 as a single member.
[0031] The piston portion 44 is an annular plate. The outer peripheral end of the piston portion 44 and that of the turbine shell 41 are coupled through the coupling portion 43. The piston portion 44 is disposed in the radial vicinity of the outer peripheral end of the front cover 1.
[0032] The piston portion 44 includes an opening in its middle part. An inner peripheral surface 411 of the piston portion 44 is located radially away from the output shaft member 3. In other words, the inner peripheral surface 441 of the piston portion 44 does not make contact with the output shaft member 3. Therefore, a space is produced between the output shaft member 3 and the inner peripheral surface 441 of the piston portion 44.
[0033] For example, the distance between the outer peripheral surface of the output shaft member 3 and the inner peripheral surface 441 of the piston portion 44 is about 30 mm or greater. Additionally, the inner diameter of the piston portion 44 is, for instance, greater than or equal to about twice the outer diameter of the output shaft member 3. It should be noted that torque converters have various sizes, and hence, the upper limit of the distance between the outer peripheral surface of the output shaft member 3 and the inner peripheral surface 441 of the piston portion 44 is not limited to a specific value.
[0034] The turbine 4 further includes a plurality of first engaging parts 45. The first engaging parts 45 extend from the turbine shell 41 to elastic members 72 of the damper mechanism 7 to be described, respectively. Each first engaging part 45 is engaged with each elastic member 72. When described in detail, each first engaging part 45 makes contact with one end surface of each elastic member 72 in the circumferential direction. The first engaging parts 45 are disposed at intervals in the circumferential direction. The first engaging parts 45 are welded to the turbine shell 41.
[0035] The stator 6 is configured to regulate the flow of hydraulic oil returning from the turbine 4 to the impeller 2. The stator 6 is disposed between the impeller 2 and the turbine 4. The stator 6 includes a stator carrier 61 having a disc shape and a plurality of blades 62 mounted to the outer peripheral surface of the stator carrier 61.
[0036] The stator 6 is rotatable about the rotational axis O. When described in detail, the stator 6 is supported by a stationary shaft (not shown in the drawing) through a bearing (not shown in the drawing).
[0037] The clutch 5 is disposed between the piston portion 44 and the front cover 1. The clutch 5 is configured to transmit or block the torque from the front cover 1 to the piston portion 44.
[0038] The clutch 5 is a friction member 51 attached to the piston portion 44. It should be noted that the friction member 51 may be attached to the front cover 1. In this construction, the friction member 51 is opposed to the piston portion 44.
[0039] The output shaft member 3 is rotatable about the rotational axis O. The output shaft member 3 outputs the torque. When described in detail, the output shaft member 3 outputs the torque from the engine to the transmission. It should be noted that when a lock-up state is not being made, the output shaft member 3 outputs to the transmission the torque sequentially transmitted thereto in the order of the front cover 1, the impeller 2, the turbine 4 and the damper mechanism 7. When the lock-up state is being made, the output shaft member 3 outputs to the transmission the torque sequentially transmitted thereto in the order of the front cover 1, the turbine 4 and the damper mechanism 7.
[0040] For example, the output shaft member 3 is made in the shape of a cylinder extending in the axial direction. A transmission-side member (e.g., an input shaft member) is fitted to the interior of the output shaft member 3. With this construction, the output shaft member 3 and the transmission-side member are unitarily rotated.
[0041] The damper mechanism 7 couples the turbine 4 and the output shaft member 3 so as to make the turbine 4 and the output shaft member 3 rotatable relatively to each other. When described in detail, the damper mechanism 7 elastically connects the turbine 4 and the output shaft member 3 in the circumferential direction. The damper mechanism 7 includes a holder member 71 and the plurality of elastic members 72.
[0042] The holder member 71 extends in the radial direction. The holder member 71 is unitarily rotated with the output shaft member 3. In other words, the holder member 71 is fixed to the output shaft member 3. For example, the holder member 71 is fixed thereto by fastening members such as swaging rivets. It should be noted that the holder member 71 may be integrated with the output shaft member 3 as a single member.
[0043] The holder member 71 may be composed of a plurality of plates. The holder member 71 includes a plurality of third engaging parts 73. When described in detail, each third engaging part 73 makes contact with the other end of each elastic member 72 in the circumferential direction. The number of the third engaging parts 73 is the same as that of the first engaging parts 45. Each third engaging part 73 and each first engaging part 45 interpose each elastic member 72 therebetween in the circumferential direction.
[0044] The elastic members 72 are held by the holder member 71. The respective elastic members 72 are, for instance, coil springs. It should be noted that the elastic members 72 are disposed at intervals in the circumferential direction.
[0045] Next, explanation will be provided for an action to be performed by the torque converter 100 when the lock-up state is made. When the lock-up state is made in the torque converter 100, the hydraulic oil is supplied to the space between the turbine shell 41 and the impeller shell 21. When described in detail, the space between the turbine shell 41 and the impeller shell 21 has been already filled with the hydraulic oil. Hence, the hydraulic oil, residing in the space between the turbine shell 41 and the impeller shell 21, is raised in hydraulic pressure by further supplying the hydraulic oil to the space.
[0046] When the hydraulic oil, residing in the space between the turbine shell 41 and the impeller shell 21, is raised in hydraulic pressure, the turbine 4 is moved in a direction separating from the impeller 2, i.e., toward the front cover 1. As a result, the friction member 51 attached to the piston portion 44 is engaged by friction with the front cover 1. The front cover 1 and the turbine 4 are unitarily rotated. In other words, the torque from the front cover 1 is transmitted to the turbine 4 without through the impeller 2.
[0047] When the lock-up state is released in the torque converter 100, the hydraulic oil is supplied to the space between the turbine shell 41 and the front cover 1. The turbine 4 is thereby moved in a direction separating from the front cover 1. As a result, frictional engagement between the friction member 51 attached to the piston portion 44 and the front cover 1 is released. In other words, the torque from the front cover 1 is transmitted to the turbine 4 through the impeller 2.
[0048] In the torque converter 100 according to the aforementioned exemplary embodiment, the directions of the hydraulic oil to be supplied when the lock-up state is made and when the lock-up state is released are the same as those in a well-known torque converter.
[0049] Additionally, in the torque converter 100, the piston portion 44 is supported by the output shaft member 3 through the coupling portion 43 and the turbine shell 41. With this construction, only an outer peripheral side space is required for disposing the piston portion 44. Hence, it is possible to form a space between the inner peripheral surface 441 of the piston portion 44 and the output shaft member 3. Therefore, by utilizing this space for the purposes of, e.g., installation of a component of the torque converter, the torque converter can be made compact by that much.
[0050] [Modifications]
[0051] The exemplary embodiment of the present disclosure has been described above. However, the present disclosure is not limited to the aforementioned exemplary embodiment, and a variety of changes can be made without departing from the scope of the present disclosure.
[0052] Modification 1
[0053] As shown in
[0054] Modification 2
[0055] The clutch 5 may be a multi-plate clutch. In other words, the clutch 5 maybe constructed to include a plurality of friction plates.
[0056] Modification 3
[0057] The damper mechanism 7 may include another type of elastic members on the radially inner side of the elastic members 72. In other words, the torque from the turbine 4 may be transmitted to the output shaft member 3 through two types of elastic members composed of elastic members disposed on the outer peripheral side and elastic members disposed on the inner peripheral side.
REFERENCE SIGNS LIST
[0058] 1 Front cover [0059] 2 Impeller [0060] 21 Impeller shell [0061] 22 Impeller blade [0062] 3 Output shaft member [0063] 4 Turbine [0064] 41 Turbine shell [0065] 42 Turbine blade [0066] 43Coupling portion [0067] 44 Piston portion [0068] 45 First engaging part [0069] 46 Second engaging part [0070] 5 Clutch [0071] 51 Friction member [0072] 7 Damper mechanism [0073] 100 Torque converter