Torque converter for a motor vehicle
10054207 ยท 2018-08-21
Assignee
Inventors
Cpc classification
F16H2045/0278
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2041/246
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H45/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0205
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H41/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H41/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0247
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2045/0215
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16H41/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H41/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A torque converter comprising a torque input element (19), an impeller wheel (3) rotationally coupled to the torque input element (19) and able to hydrokinetically drive a turbine wheel (4), a torque output element (8), clutch means (10, 38) movable between an engaged position in which the torque input element (19) and the torque output element (8) are rotationally coupled through damping means (12, 43, 44, 45), and a disengaged position in which the torque input element (19) and the torque output element (8) are rotationally coupled through the impeller wheel (3) and the turbine wheel (4), with a first bearing (31) being axially mounted between the impeller wheel (3) and the reactor (5), with a second bearing (31) being axially mounted between the reactor (5) and the turbine wheel (4).
Claims
1. A torque converter for a motor vehicle, comprising: a torque input element (19) non-rotatably coupled to a crankshaft (1); an impeller wheel (3) non-rotatably coupled to the torque input element (19) and configured to hydrokinetically drive a turbine wheel (4) through a reactor (5), a torque output element (8), intended to be coupled to a transmission input shaft (2), clutch device (10, 38) movable between an engaged position in which the torque input element (19) and the torque output element (8) are rotationally coupled, and a disengaged position in which the torque input element (19) and the torque output element (8) are rotationally coupled through the impeller wheel (3) and the turbine wheel (4); a first bearing (31) axially mounted between the impeller wheel (3) and the reactor (5); and a second bearing (31) axially mounted between the reactor (5) and the turbine wheel (4), at least one of the first bearing and the second bearing comprising a friction ring (31, 31), the first bearing (31) and the second bearing (31) being axially separated from one another by the reactor (5); the reactor (5) comprising a hub (14) and blades 13 extending radially outwardly from the hub (14), the hub (14) having a first radial surface (15) and an axially opposite second radial surface (16); the friction ring (31, 31) comprising an axially extending coupling pad (32) disposed in a recess (33, 37) in one of the impeller wheel (3), the turbine wheel (4) and the hub (14) of the reactor (5); the coupling pad (32) being complementary to the recess (33, 37) so as to non-rotatably couple the friction ring (31, 31) to one of the impeller wheel (3), the turbine wheel (4) and the hub (14) of the reactor (5).
2. The torque converter according to claim 1, wherein the first bearing comprises a first friction ring (31) non-rotatably coupled to one of the reactor (5) and the impeller wheel (3), and wherein another one of the reactor (5) and the impeller wheel (3) is configured to rest and rub on the first bearing friction ring (31).
3. The torque converter according to claim 2, wherein the second bearing comprises a second friction ring (31) non-rotatably coupled to one of the turbine wheel (4) and the reactor (5), and wherein another one of the turbine wheel (4) and the reactor (5) is configured to rest and rub on the second friction ring (31).
4. The torque converter according to claim 3, wherein the first friction ring (31) and the second friction ring (31) have identical structures.
5. The torque converter according to claim 3, wherein one of the first friction ring (31) and the second friction ring (31) comprises the coupling pad (32) engaged in the recess (33, 37) in one of the impeller wheel (3), the turbine wheel (4) and the hub (14) of the reactor (5), and wherein the coupling pad (32) is complementary to the recess (33, 37) so as to non-rotatably couple the first friction ring (31) to one of the impeller wheel (3) and the hub (14) of the reactor (5) or to non-rotatably couple the second friction ring (31) to one of the turbine wheel (4) and the hub (14) of the reactor (5).
6. The torque converter according to claim 3, wherein at least one of the first friction ring (31) and the second friction ring (31) comprises at least one first oil circulation channel (34) which is radially spaced from and extends parallel to an axis (X) of the torque converter, and which opens into a lubricated space of the torque converter.
7. The torque converter according to claim 3, wherein the first friction ring (31) comprises a first axially extending coupling pad (32) engaged in the recess (33) in the hub (14) of the reactor (5), wherein the first coupling pad (32) is complementary to the recess (33) to non-rotatably couple the first friction ring (31) to the hub (14) of the reactor (5), wherein the second friction ring (31) comprises a second axially extending coupling pad (32) engaged in a recess (37) in the turbine wheel (4), and wherein the second coupling pad (32) is complementary to the recess (37) to non-rotatably couple the second friction ring (31) to the turbine wheel (4).
8. The torque converter according to claim 2, wherein the friction ring (31, 31) comprises at least one first oil circulation channel (34) which is radially spaced from and extends parallel to an axis (X) of the friction ring (31, 31), and which opens into a lubricated space of the torque converter.
9. The torque converter according to claim 1, wherein the friction ring (31, 31) comprises at least one first oil circulation channel (34) which is radially spaced from and extends parallel to an axis (X) of the torque converter, and which opens into a lubricated space of the torque converter.
10. The torque converter according to claim 9, wherein the at least one first oil circulation channel (34) extends axially through the coupling pad (32).
11. The torque converter according to claim 1, wherein the friction ring (31, 31) comprises at least one second oil circulation channel (35) which extends radially and opens at a radial friction surface (36) of the friction ring (31, 31), with the impeller wheel (3), the turbine wheel (4) or the reactor (5) being adapted to rest on and pivot relative to the radial friction surface (36).
12. The torque converter according to claim 11, wherein the reactor (5) comprises an annular backing plate (17) attached to a hub (14) of the reactor (5) and having a radial surface (18) resting on the friction surface (36) of the friction ring (31, 31).
13. The torque converter according to claim 1, wherein the friction ring (31, 31) is made of a synthetic material.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will be better understood, and other details, characteristics and advantages of the invention will appear upon reading the following description given by way of a non restrictive example while referring to the appended drawings wherein:
(2)
(3)
(4)
(5)
(6)
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S)
(8)
(9) In the following, the words axial and radial are defined relative to the X axis.
(10) The torque converter conventionally comprises an impeller bladed wheel 3, able to hydrokinetically drive a turbine bladed wheel 4 through a reactor 5.
(11) The turbine wheel 4 more particularly comprises vanes 11 mounted on an annular support 12.
(12) The reactor 5 comprises blades 13 which extend radially outwards from a hub 14 positioned radially inside of the blades 13. The hub 14 of the reactor 5 more particularly comprises a front radial surface 15 and a back radial surface 16.
(13) An annular backing plate 17 which extends in the radial plane is attached to the hub 14 of the reactor 5 and rests on the back radial face 16 of said hub 14. Said plate 17 forms a radial friction surface 18 turned backwards.
(14) The impeller wheel 3 is fastened to a cover consisting of two belt-shaped parts 19a, 19b assembled together by welding and defining an internal volume 20 accommodating the impeller wheel 3, the turbine wheel 4 and the reactor 5. Said cover 19a, 19b, also more generally referred to as the cover 19, comprises fastening means 21 making it possible to non-rotatably couple said cover 19 with the crankshaft 1.
(15) The part 19a of the cover is attached, for instance by welding, to an impeller hub 22. The impeller hub 22 comprises a radial annular back part 23, the radially internal periphery of which is extended forwards by a tubular cylindrical part 24.
(16) The radial part 23 of the impeller hub 22 comprises a back radial surface 25 turned towards, and located opposite, the front radial surface 15 of the hub 14 of the reactor 5.
(17) The turbine wheel 4 of the torque converter further comprises a turbine hub 8, also called the X axis turbine hub 8, a radially internal periphery of which is ribbed and accommodated in the internal volume 20 of the cover 19. The turbine hub 8 comprises an annular rim 27 radially extending outwards and positioned at the front end thereof.
(18) The turbine hub further comprises a cylindrical part 28 positioned at the back end thereof, with said cylindrical part 28 defining a radial shoulder, with the radial surface 29 of said shoulder facing backwards.
(19) The front end of the hub forms a radial surface 30 turned towards, and located opposite, the back radial surface 16 of the hub 14 of the reactor 5.
(20) A first friction ring 31 is axially inserted between the front radial face 15 of the hub 14 of the reactor 5 and the back radial face 25 of the impeller hub 22. The first friction ring 31 comprises cylindrical coupling pads 32 which extend axially backwards toward the hub 14 of the reactor 5 and are regularly distributed over the circumference of the first friction ring 31. The coupling pads 32 are for instance eight in number. The coupling pads 32 are engaged in complementary recesses 33 in the hub 14 of the reactor 5 so as to non-rotatably couple the first friction ring 31 and of the reactor 5. Each of the coupling pads 32 of the first friction ring 31 has a shape which matches (i.e., is complementary to) one of the recesses 33 in the hub 14 of the reactor 5. The friction ring 31 further comprises first oil circulation channels 34 which are radially spaced from and extend parallel to the X axis of the matching ring 31, and which open into a lubricated space of the torque converter. Each first channel 34 goes through the ring 31 at one of the coupling pads 32.
(21) The first friction ring 31 further comprises second channels 35 which extend radially. The second channels 35 extend from a radially internal rim to a radially external rim of the first friction ring 31 and are regularly distributed on the whole circumference of the first friction ring 31. Each second channel 35 is additionally formed by a groove provided on a friction surface 36 of the first friction ring 31, i.e. a front facing face. Each second channel 35 has a circular or rounded section.
(22) A second friction ring 31 is axially inserted between the back radial face 18 of the backing plate 17 and the front radial face 30 of the turbine hub 8.
(23) The second friction ring 31 has the same structure as the first friction ring 31. The coupling pads 32 of the second friction ring 31 are engaged in complementary recesses 37 in the turbine hub 8 so as to non-rotatably couple the second friction ring 31 and the turbine hub 8. Each of the coupling pads 32 of the second friction ring 31 has a shape which matches (i.e., is complementary to) one of the recesses 37 in the turbine hub 8. Thus, the the first bearing (31) and the second bearing (31) are axially spaced and separated from one another by the reactor (5). The recesses 37 more particularly go through the annular rim 27 of the turbine hub 8. The first friction ring 31 and the second friction ring 31 are rotatable relative to one another as the turbine wheel 4 and the reactor 5 are rotatable relative to one another.
(24) The first friction ring 31 and/or the second friction ring 31 are made of a synthetic material, for instance a thermoplastic.
(25) The torque converter further comprises clutch device 10 comprising an annular piston 38 which extends radially and is accommodated in the inner space 20 of the cover 19, the radially external periphery of which comprises a resting area equipped with clutch lining 39 and adapted to rest on the part 19b of the cover 19 in an engaged position, so as to provide a rotational coupling of the cover 19 and of the piston 38.
(26) The radially internal periphery of the piston 38 comprises a cylindrical rim 40 which is so mounted as to be free to rotate and to move in translation along the X axis about the cylindrical part 28 of the turbine hub 8.
(27) The piston 38 can thus move in translation between an engaged position in which the piston 38 and the cover 19 are rotationally coupled and a disengaged position in which the piston 38 is positioned away from the cover 19 so that the piston 38 is not directly rotationally coupled to the cover 19.
(28) The motion of the piston 38 is controlled by pressure chambers positioned on either side of the piston 38. Besides, the motion of the piston 38 in the disengaged position may be limited by the radially internal periphery of the piston 38 resting on the radial surface 29 of the shoulder of the turbine hub 8.
(29) A linking member 41 is fastened to the piston, for instance by welding or by rivets, in a zone positioned radially inside the clutch lining 39. The linking member 41 and the cover 38 may of course consist of one single part, without the operation of the torque converter being affected.
(30) It should be noted that, in one not shown embodiment, the piston 38 can be so mounted as to pivot directly about the transmission input shaft 2.
(31) The clutch device 10 is configured to transmit a torque from the crankshaft 1 to the transmission input shaft 2, in a determined operation phase, without any action by the hydrokinetic coupling means consisting of the impeller wheel 3, the turbine wheel 4 and the reactor 5.
(32) The torque converter further comprises damping device comprising an annular wheel disc 42 extending radially, the radially inner periphery of which is fixed to the annular rim 27 of the turbine hub 8, for instance by riveting or welding. The damping device comprises two guiding washers 43 extending radially, and positioned axially on either side of the annular wheel disc 42. First elastic members 44, such as, for instance coil compression springs, are mounted between the annular wheel disc 42 and the guiding washers 43.
(33) Second elastic members 45, such as, for instance coil compression springs, are mounted between the guiding washers 43 and the linking member 41 attached to the piston 38.
(34) The first and second elastic members 44, 45 are so designed as to act against the rotation of the piston 38 relative to the turbine hub 8.
(35) Such damping device is configured to damp and filter the engine rotation acyclism.
(36) The torque converter further comprises an annular inertia mass 46 connected to the radially internal periphery of the annular wheel disc 42 through an annular steel sheet 47 and elastic members 48 mounted between the inertia mass 46 and the annular steel sheet 47, so as to form an inertial vibration dampening mass. The elastic members 48 are for instance coil compression springs. Such an inertial vibration dampening mass is intended to filter vibrations at at least one determined frequency, more specifically an engine resonance frequency.
(37) The radially internal periphery of the steel sheet 47 of the inertial vibration dampening mass and of the support 12 of the turbine wheel 4 are axially mounted between the annular wheel disc 42 and the rim 27 of the turbine hub 8. The steel sheet 47, the support 12, the annular wheel disc 42 and the rim 27 of the turbine hub 8 can be attached together, for instance using rivets.
(38) Holes 49 are provided in the annular wheel disc 42, the steel sheet 47 and the support 12, opposite the holes 37 of the annular rim 27 of the turbine hub 8 and the first oil circulation channels 34 of the second friction ring 31.
(39) In operation, in the disengaged position of the piston 38, the torque from the crankshaft 1 is transmitted to the cover 19 through the fastening means 21. In the disengaged position of the piston 38, the torque goes through the hydrokinetic coupling means, i.e. the impeller wheel 3 and then the turbine wheel 4 fixed to the hub 8. The torque is then transmitted to the transmission input shaft 2 coupled to the turbine hub 8 through the internal ribs 26 of the hub 8.
(40) In the engaged position of the piston 38, the torque from the cover 19 is transmitted to the turbine hub 8 through, in sequence, the piston 38, the linking member 41, the elastic members 45, the guiding washers 43, the elastic members 44 and the annular wheel disc 42.
(41) In operation too, the turbine hub 8 and the impeller hub 22 pivot relative to the reactor 5 hub 14. The friction rings 31, 31 act as bearings, the friction surfaces 36 of which are lubricated, with lubrication being facilitated by the presence of the first and second oil circulation channels 34, 35.
(42) Using such friction rings 31, 31 makes it possible to reduce the production cost as well as the axial overall dimensions of the torque converter.