[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP2917558B1 - Heat engine starter provided with a device for shock absorption by shearing - Google Patents

Heat engine starter provided with a device for shock absorption by shearing Download PDF

Info

Publication number
EP2917558B1
EP2917558B1 EP13801642.3A EP13801642A EP2917558B1 EP 2917558 B1 EP2917558 B1 EP 2917558B1 EP 13801642 A EP13801642 A EP 13801642A EP 2917558 B1 EP2917558 B1 EP 2917558B1
Authority
EP
European Patent Office
Prior art keywords
ring gear
starter according
starter
face
shock absorber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP13801642.3A
Other languages
German (de)
French (fr)
Other versions
EP2917558A2 (en
Inventor
Guillaume Seillier
BenoƮt BALEYDIER
Christian Mornieux
Enguerrand PRIOUX
Matthias Soddemann
Simon Furrer
Norbert Haberland
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Daetwyler Schweiz AG
Original Assignee
Daetwyler Schweiz AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Daetwyler Schweiz AG filed Critical Daetwyler Schweiz AG
Publication of EP2917558A2 publication Critical patent/EP2917558A2/en
Application granted granted Critical
Publication of EP2917558B1 publication Critical patent/EP2917558B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N15/00Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00Ā -Ā F02N13/00
    • F02N15/02Gearing between starting-engines and started engines; Engagement or disengagement thereof
    • F02N15/04Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears
    • F02N15/06Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears the toothed gears being moved by axial displacement
    • F02N15/062Starter drives
    • F02N15/063Starter drives with resilient shock absorbers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N15/00Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00Ā -Ā F02N13/00
    • F02N15/02Gearing between starting-engines and started engines; Engagement or disengagement thereof
    • F02N15/04Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears
    • F02N15/043Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears the gearing including a speed reducer
    • F02N15/046Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears the gearing including a speed reducer of the planetary type

Definitions

  • the invention relates to a motor starter with a shear absorption device.
  • the invention finds a particularly advantageous application, but not exclusive, with vehicles equipped with the function of stopping and restarting the engine (function called "stop and startā€ in English) depending on traffic conditions.
  • a combustion engine also called an internal combustion engine, in particular a motor vehicle
  • a rotating electrical machine in the form of a starter provided with a launcher capable of transmitting rotational energy. from the starter to a crankshaft of the engine through a drive gear.
  • This launcher is mounted on an output shaft of the electric machine.
  • a speed reducer is interposed between this output shaft, constituting the launcher shaft, and the shaft of the electric motor that comprises the rotating electrical machine.
  • the interposition of the reducer has the advantage of using a faster electric machine and thus obtain a higher starting torque while reducing the size and weight of the machine for a given power.
  • this speed reducer can be formed by a toothed wheel in the form of a pinion fixed at one end of the shaft of the electric motor of the electric machine and a ring gear rotationally fixed by friction means of the thrower shaft; this ring having inner teeth meshing with the pinion.
  • the electric motor shaft and the launcher shaft are offset relative to each other.
  • the speed reducer is formed by an epicyclic gear comprising planet wheels mounted rotatably about axes carried by a planet carrier comprising a transverse plate secured to the rear end of the starter shaft.
  • These planet gears mesh with the pinion integral with the shaft of the electric motor and with the inner teeth of the ring gear stationary in rotation relative to the housing that comprises the starter.
  • the electric motor shaft and the launcher shaft are coaxial.
  • the launcher comprises a pinion provided with teeth configured to mesh with teeth of the drive ring, also called start ring, rigidly or resiliently fixed to the crankshaft of the engine to start.
  • This launcher can undergo significant mechanical shocks during operation of the starter, especially during the launch of the engine.
  • the teeth of the pinion can slide against the teeth of the drive ring before engaging between them.
  • the axial overlap of the respective teeth of the pinion and the drive ring can then be very low and the kinetic energy of rotation of the starter is abruptly transmitted to the ring gear.
  • the contact stresses are very high, which can, with wear, cause the destruction of teeth of the crown. This phenomenon is known as milling.
  • a conventional assembly consists of a ring of plastic material on which are molded dampers elastomeric thermoplastic material capable of being compressed during the application of an over-torque. See for example EP 1 450 038 A1 .
  • the compression is effected by a relative angular displacement of the dampers integral in rotation with the ring gear with respect to compressor elements integral in rotation with the starter housing intended to bear against the dampers to compress them.
  • the invention aims to effectively remedy these disadvantages.
  • the invention thus makes it possible to damp the shocks in a more progressive manner than a damper working in compression, insofar as the absorbed torque evolves in a linear manner as a function of the rotation angle of the ring during the shearing of an element. elastic.
  • the invention therefore makes it possible to increase the life of the traction chain.
  • Shear absorbing device means an absorption device which is mounted to deform predominantly by shear to dampen the impact.
  • the elastic element has two of these faces integral in rotation with the crown on the one hand and the housing on the other hand allows the elastic element to work significantly in shear.
  • the first face of the elastic element comprises a radial surface integral in rotation with the support plate and in that the second face comprises a radial surface integral in rotation with the ring.
  • Radial surface means a surface whose projection is perpendicular to the axis of the ring.
  • the first face of the elastic element comprises an axial surface integral in rotation with the support plate and in that the second face comprises an axial surface integral in rotation with the ring.
  • Axial surface means a surface whose projection is parallel to the axis of the crown.
  • At least one of the first or second faces of the elastic element is of conical shape.
  • the second face of the absorption device and mounted against a transverse wall of the ring.
  • This embodiment makes it possible to arrange the damping device axially to reduce the radial space requirement.
  • the shock absorbing device is mounted radially between the crown and the housing.
  • This embodiment reduces the axial size of the starter.
  • the shear absorbing device further comprises an insert plate secured to the second face of the elastic element, this plate being mounted integral in rotation with the transverse wall of the ring.
  • the insert plate is attached to the second face of the elastic member.
  • the wafer is attached to the elastic element by overmolding or gluing.
  • the support plate is attached to the first face of the elastic member.
  • the support plate is fixed to the elastic element by overmolding or gluing.
  • the insert plate substantially covers the entire surface of the second face of the elastic element.
  • the transverse wall of the crown is fixed by gluing to the second face of the elastic element.
  • the transverse wall of the ring has openings for receiving pads from the insert plate. This allows for a means of fixing in easy rotation.
  • the first and second faces of the elastic element are inclined with respect to each other.
  • the starter further comprises a compression shock absorption device adapted to be biased when the ring exceeds an angular displacement threshold so as to limit the stress experienced by the shear absorption device.
  • the shear absorbing device and the compression shock absorber are mounted in the starter so that, during an impact, the shearing device initially deforms to the angular displacement threshold and then the two shock absorbers deform to absorb the shock.
  • the shear absorbing device and the compressive shock absorption device are mounted in the starter so that, during an impact, the device for absorbing shear impact is deformed in a first step up to the angular displacement threshold and then only the compression shock absorber deforms to absorb the shock.
  • the angular displacement threshold is between 15 and 25 degrees. This allows the shear absorption device to absorb non-abruptly part of the shock.
  • the device for absorbing shocks by compression comprises at least one damper integral in rotation with one of the transverse wall of the crown and the support plate and at least one corresponding compressor element integral in rotation with the other element intended to bear against the damper during the angular displacement of the ring beyond the angular displacement threshold.
  • the compression damper is integral in rotation with the support plate while the compressor element belongs to the transverse wall of the ring.
  • a portion of the damper is inserted into a rigid receiving cage located on the opposite side with respect to the compressor element forming a stop.
  • the damper has beveled corners on the side of the compressor element.
  • the shear absorbing device comprises two diametrically opposed elastic elements having a ring portion shape.
  • the compression shock absorption device comprises two dampers each located between two ends of the elastic elements facing one another and two compressor elements each located between an elastic member and a damper.
  • the rotating electrical machine is a starter motor 10 similar to the starter described in the document WO2005 / 054664 , so that the elements identical or similar to those of the figure 1 of this document WO2005 / 054664 , to which reference will be made for more details, will be assigned the same reference signs.
  • the starter comprises in this embodiment an output shaft 43, a launcher 30 mounted on the shaft 43 and an electric motor 11 composed of an inductor stator 12 and a rotor 13 induced coaxially mounted, the stator 12 surrounding the rotor 13, which is rotatably mounted about an axis 14 inside a cylinder head 15.
  • the latter is secured to a metal support of the starter for attachment to a fixed part of the motor vehicle.
  • the support 16 is here moldable material, for example based on aluminum and belongs to the housing of the machine.
  • the stator 12 comprises in one embodiment a plurality of permanent inductor magnets carried by the inner periphery of the cylinder head 15.
  • the stator 12 comprises an inductor winding 17 comprising two pairs of windings 18, which are each wound around a polar mass 19 integral with the cylinder head 15.
  • the polar masses 19 are fixed with screws 20 to the cylinder head 15, here metallic, as described in the document FR2611096 .
  • Each winding 18 is composed of a continuous conductor wound around the polar mass 19 in the direction of its thickness so as to form concentric contiguous turns of increasing diameter as better visible in the Figures 2 to 5 of the document EP749194 .
  • the axis of each winding 18 is radial relative to the axis 14 of the rotor 13, which constitutes the axis of rotation of the electric motor 11.
  • the rotor 13 comprises a bundle of plates provided with grooves for mounting electrical conductors 21 in the form of pins. These conductors 21 are interconnected to form a rotor winding in connection with the conductive blades 22 belonging to a collector 23 with an electrically insulating body integral with the shaft 24 of the electric motor 11. In a variant, the winding is in continuous wire.
  • Brushes 25 rub on the collector slats 22 of the manifold 23 to supply the rotor winding.
  • Brushes 25 belong to a brush holder 26 equipped with guiding cages and receiving brushes, which are biased towards the slats 22 by means of springs 27.
  • the brush holder 26 is integral with a metal rear bearing 29 having in the central part a housing for mounting a needle bearing 28.
  • the bearing 29 serves for rotatably mounting the rear end of the shaft 24 of the electric motor 11.
  • the axis of this shaft 24 coincides with the axis 14 of the rotor 13, and with the axis of the output shaft 43 of the starter constituting the starter shaft 30.
  • the rear bearing 29 serves as a centering device at the rear end of the yoke 15, and is connected by tie rods 31 to the support 16 of the starter 10.
  • Two threaded holes (not referenced) are formed in the support 16 for screwing the tie rods.
  • the tie rods 31 are located outside the cylinder head 15. Here a small clearance exists between the tie rods and the outer periphery of the cylinder-shaped cylinder head 15.
  • the metal cylinder head is interposed between the metal support 16 and the metal rear bearing 28.
  • the starter housing thus comprises the bearing 28, the cylinder head 15 and the support 16. This casing is intended to be connected to the mass of the vehicle. automobile via its support 16.
  • the starter 10 also comprises an electromagnetic contactor 32 extending parallel to the electric motor 11 by being radially implanted above it.
  • the contactor 32 has a metal tank 33 carried by the support 16, and equipped with an excitation coil B provided with at least one winding.
  • the tank 33 is closed at the rear by a cover 34 made of electrically insulating material.
  • the fixing of the cover 34 is made by folding the material of the free end of the tank 33.
  • a shoulder of the tank 33 ensures the axial setting of a fixed core 35, which is wedged axially in the other direction by the cover 34 carrying terminals 36, 37 of power supply.
  • the terminals 36, 37 are shaped to each form a fixed contact 38 inside the cover 34.
  • One of the terminals 36 is intended to be connected to the positive terminal of the battery, the other 37 is connected by the intermediate of a cable 39 at the input of the inductor winding 17 of the stator and brushes 25 of positive polarity.
  • a mobile core 40 is attracted by magnetic attraction towards the fixed core 35 to, firstly, act after catching a game on a rod (not referenced) carrying a movable contact (not referenced) to cause the closure of the contacts of the contactor 32 and supply the electric motor of the starter, and, on the other hand, operate a lever 41 for controlling the launcher.
  • the output shaft 43 is rotatably mounted in a bearing 42 before the support 16.
  • This bearing 42 is constituted by way of example by a needle bearing alternatively by a plain bearing.
  • This shaft 43 carries at the front a stop 53 adjacent to the bearing 42 to limit the movement of the launcher 30.
  • the rear end of the shaft 43 is configured to be secured to a plate of a planet carrier 47, for example by crimping, this planet carrier 47 belonging to an epicyclic gear train constituting the speed reducer 45 gear.
  • This planet carrier 47 carries satellites 47.1 meshing on the one hand with a ring 46 (described in more detail below) and with a sun gear 51 integral with the front end of the shaft 24 of the electric motor.
  • the gearbox 45 is of the type described in the document FR2787833 which will be referred to, the latter showing the mounting of the front end of the shaft 24 of the electric motor 11 in the rear end of the shaft 43 having a blind hole in which is housed the front end of the shaft 24 with the interposition of a plain bearing and a ball.
  • the satellites 47.1 are therefore rotatably mounted each about an axis. These axes extend between two plates of transverse orientation relative to the axis of the shaft 43 being carried by these plates, one of which is thicker than the other and is here fixed by crimping to the rear end of the shaft 43.
  • the planet carrier 47 comprises a single plate fixed to the rear end of the shaft 43 and carrying the axes.
  • the launcher 30 is slidably mounted on the output shaft 43, and comprises a drive gear 50, a driver 51 configured to be actuated by the control lever 41 pivoting, and a free wheel 52 with rollers interposed axially between the 51 and the pinion 50.
  • the teeth of the pinion 50 belong to a sleeve extended at the rear to form the cylindrical inner track of the free wheel 52 roller.
  • the driver 51 is axially extended at the front by a bushing configured internally to form the profiled external track of the freewheel 52 with wheels and to house the springs acting in known manner on the rollers. More specifically, the driver 51 comprises a sleeve integral with the front of a flange of transverse orientation relative to the axis of the shaft 43.
  • This flange is integral at its outer periphery with the sleeve of axial orientation by relative to the axis of the shaft 43 for forming a roller receiving cage closed at the front by washers.
  • the driver 51 carries a washer (not referenced) defining with the flange of the driver 51 a groove for receiving the fingers of the lower end of the lever 41 fork-shaped.
  • the upper end of the lever 41 is mounted in known manner to articulation on a rod (not referenced to the figure 2 ) elastically connected to the movable core 40 via a spring housed in the movable core 40.
  • the lever 41 is hingedly mounted on the movable core 40 and the spring surrounds the sleeve of the driver by bearing on the flange of the coach as described for example in the document DE2822165 .
  • the sleeve of the driver 51 is internally provided with helical splines (not referenced) in complementary engagement with external helical teeth carried by the output shaft 43 in the vicinity of its rear end here cylindrical and moreover large diameter.
  • the launcher 30 is thus animated by a helical movement when it is moved by the lever 41 in the direction of the stop 53 to come, via its pinion 50, in engagement with the drive ring, called the crown of starting (not shown), a heat engine also called internal combustion engine.
  • the freewheel device 52 can be replaced by a conical clutch coupling device, of the type described in the document FR2772433 or a clutch with multiple disks.
  • the launcher 30 variant is implanted in part outside the support 16 at the front thereof. More precisely, the pinion 50 of the launcher 30, instead of being implanted in the support (cf. figure 2 ), can be implanted outside the support as visible for example in the document FR2745855 which will be referred to for more details.
  • the control lever 41 is coupled, here elastically in a variant rigidly in the aforementioned manner, by its upper end to the movable core 40 of the contactor 32, and comprises in its middle part a pivot axis 54, which according to a characteristic is distinct, the toothed gear gear reducer gear ring 46 due to the structure of the assembly described below.
  • the lever 41 is in a molded part, preferably made of rigid thermoplastic material to reduce noise, preferably reinforced by fibers.
  • the mounting of the pivot axis 54 is for example made using a support piece as in the documents DE2822165 and FR2787833 or in the support 16 provided with projections for this purpose, the axis 54 being separate or integrated in the lever 41.
  • a sealing pad 158 of elastomer to absorb dimensional variations In the embodiment of the figure 2 as in the document DE2822165 , there is provided a sealing pad 158 of elastomer to absorb dimensional variations.
  • This stud 158 is in contact with the contact surface of the contactor and is integral with a plastic part 155 configured to replace the tongue or tabs 55 of the figure 1 of the document WO2005 / 054664 ; the housing of the support 16 being retained.
  • the pad 158 is removed and it is the plastic part 155 which is then in contact with the contact surface of the contactor.
  • the solution described in the document can also be used WO01 / 31195 . It all depends on the applications.
  • the ring 46 of the X-axis speed reducer 45 coincides with the axis 14 is of hollow form and has a wall 58 transverse to the outer periphery of which extends an annular skirt 46.1 of axial orientation provided with inner teeth meshing with satellites 47.1.
  • This transverse wall 58 is pierced centrally and mounted on a hub 68 reported to ensure its centering.
  • the hub 68 has at its center a through opening allowing the passage of the shaft 43.
  • the skirt 46.1 is axially oriented relative to the axis X and therefore has a cylindrical shape.
  • the teeth 46.4 of the skirt 46.1 have an axial orientation.
  • the ring 46 is closed at the rear by a cover 200 (cf. figure 2 ). The inside of the ring 46 can thus be filled with lubricating grease of the satellites 47.1 and the sun gear 49.
  • the starter 10 comprises a shock absorbing device 61 installed between the ring gear 46 and the starter housing, in this case the carrier 16, adapted to absorb shear shocks suffered by the ring 46 during overtemperature generated by the start of the engine.
  • the device 61 comprises a support plate 62 of annular shape also of X axis having on one of its faces of radial orientation of the pins 64 intended to be inserted inside unrepresented openings made in the support 16
  • the support plate 62 is thus integral in rotation with the support 16 and thus with the starter housing.
  • the pins 64 are angularly distributed regularly at the outer periphery of the support plate 62. In this case, these six pins 64 have a parallelepiped shape.
  • a central opening 67 of the support plate 62 allows the passage of the shaft 43.
  • the support plate 62 is for example made of metal and the pins 64 are made of material with the support plate 62.
  • the support plate 62 further comprises an indexing means 65 formed by a recess shown in FIG. figure 3a made at its outer periphery intended to cooperate with a projection of the support 16. This facilitates the angular positioning of the plate 62 relative to the support 16.
  • the support plate 62 is devoid of pins 64 and has an annular shoulder 66 at its outer periphery of axial orientation and a lug 78 of generally rectangular shape for its indexing and its connection in rotation with the support 16.
  • the lug 78 is intended to cooperate with a housing, not shown, of complementary shape formed in the support 16.
  • the support plate 62 also comprises an annular sleeve 79 of X axis delimiting the opening 67 on which is positioned the crown 46.
  • the shock absorbing device 61 also comprises two elastic elements 69 fixed on a radial face of the support plate 62 opposite the face comprising the pins 64 or the shoulder 66.
  • the fixing of the elastic elements 69 on the support plate 62 is effected for example by bonding a face 70 of the elastic elements 69 to the support plate 62.
  • Each elastic element 69 has, for example, a portion shape. annular extending for example on an angle A of the order of 112 degrees.
  • Each elastic element 69 has an inner radius R1 greater than an outer radius R2 of the sleeve 79 and an outer radius R3 slightly smaller than an outer radius R4 delimiting the plate 62.
  • the elastic elements 69 are for example made of rubber.
  • the elastic elements 69 have for example a Shore hardness of between 72 and 73 ShA at 80 degrees Celsius.
  • an insert plate 71 is integral with a face 72 of each elastic element 69 opposite the face 70 fixed to the support plate 62.
  • This plate 71 follows an outer contour of the face 72 (cf. figure 4a or 7a ) so that the wafer 71 has substantially the same surface as the face 72. In other words, the wafer 71 covers substantially the entire surface of the face 72.
  • the face 72 of the elastic element 69 carrying the wafer 71 is inclined relative to the face 70 fixed to the support plate 62. The stresses experienced by the material during shearing of the elastic elements 69 are thus homogenized. More specifically, the face 70 extends in a radial plane with respect to the axis. X.
  • the face 72 is inclined with respect to the face 70 towards the inside of the plate 62 so that the cross-section of each element 69 tends to decrease when moving from the outside to the inside of the plate. plate 62.
  • the angle of inclination B 'of the two faces relative to each other is for example of the order of 5 degrees.
  • the face of the wafer 71 attached to the element 69 has a corresponding inclination.
  • the plates 71 take for example each in the form of a thin plate made of metal.
  • the transverse wall 58 of the ring 46 is made integral in rotation with the wafer 71.
  • the wall 58 has openings 74 intended to receive studs 75 coming from the plates 71.
  • each plate 71 comprises three studs 75 positioned on the same circumference between the inner periphery and the outer periphery of the elastic element. These studs 75 are intended to cooperate with two sets of three diametrically opposed openings 75 formed in the transverse wall 58 of the ring 46 (cf. figure 5 ).
  • the transverse wall 58 is fixed by gluing to the wafer 71.
  • the starter 10 further comprises a compression damping device 80 biased when the ring 46 exceeds a threshold K1 angular displacement.
  • the threshold K1 of angular displacement is between 15 and 25 degrees and is preferably of the order of 23 degrees.
  • the device 80 comprises two dampers 81 integral in rotation with the support plate 62 used in combination with two compressor elements 82 integral in rotation with the ring 46.
  • each compressor element 82 is spaced angularly by relative to the damper 81 of an angle C equal to the threshold K1 of angular displacement (cf. figure 7a ).
  • Each compressor element 82 is thus intended to bear against the damper 82 when the angular displacement of the ring 46 exceeds the threshold K1.
  • a portion of each damper 82 is inserted inside a rigid receiving cage 84 located on the opposite side to the compressor element 82 associated therewith. The cage 84 thus forms a stop, so that when a compressor element 82 acts on a damper 81, the latter is compressed between the cage 84 and the compressor element 82.
  • the dampers 81 are diametrically opposite one another and have a ring portion shape. As shown on the figure 4a , the ring portions extend over an angle D at least two times smaller than the angle A on which the elastic elements 69 extend.
  • the inner and outer radii delimiting respectively the inner and outer periphery of the dampers 81 are substantially identical to those R1, R3 of the elastic elements 69.
  • Each damper 81 has bevelled angles on the side of the compressor element 82. The bevel is made on an angle E shown on the figure 7a worth, for example, 10 degrees.
  • Each damper 81 is positioned between two ends of the elastic elements 69 facing one another.
  • the dampers 81 are fixed to the support plate 62 by means of tabs shown from the support plate 62 penetrating the dampers 81.
  • the dampers 81 are for example made of elastomeric thermoplastic material.
  • the compressor elements 82 take for example the form of ribs coming from material with the support plate 62. These ribs of substantially parallelepiped shape have a trapezoidal section.
  • the elastic elements 69, the dampers 81 and the compressor elements 82 have a substantially identical height L, as clearly Figures 3a, 3b , and 4a .
  • the compressor element 82 which has moved freely to the damper 81 begins to compress the damper 81 which is sandwiched, that is to say stuck between the receiving cage 84 forming a stop and the compressor element 82.
  • the elastic element 69 continues to deform by shearing.
  • the absorbed torque then evolves exponentially as shown on the figure 8 by the part of the curve referenced P2.
  • the device 80 for compressive shock absorption thus makes it possible to limit the stress imposed on the elastic elements 69 during their shearing.
  • the dampers 81 may be made integral in rotation with the transverse wall 58 of the ring 46, while the compressor elements 82 are made integral in rotation with the support plate 62.
  • the number of elastic elements 69 may be greater than or less than two and in all cases at least one. It depends on the application. It is the same for the number of dampers 81 of the device 80 which may vary depending on the application.
  • the starter could also comprise only a shear absorbing device 80 and be devoid of device 61 for compressive shock absorption.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Gear Transmission (AREA)

Description

DOMAINE TECHNIQUE DE L'INVENTIONTECHNICAL FIELD OF THE INVENTION

L'invention concerne un dƩmarreur pour moteur thermique muni d'un dispositif d'absorption des chocs par cisaillement.The invention relates to a motor starter with a shear absorption device.

L'invention trouve une application particuliĆØrement avantageuse, mais non exclusive, avec les vĆ©hicules Ć©quipĆ©s de la fonction d'arrĆŖt et de redĆ©marrage du moteur thermique (fonction dite Ā« stop and start Ā» en anglais) en fonction des conditions de circulation.The invention finds a particularly advantageous application, but not exclusive, with vehicles equipped with the function of stopping and restarting the engine (function called "stop and start" in English) depending on traffic conditions.

ETAT DE LA TECHNIQUESTATE OF THE ART

Afin de dƩmarrer un moteur thermique, appelƩ Ʃgalement moteur Ơ combustion interne, notamment d'un vƩhicule automobile, il est connu d'utiliser une machine Ʃlectrique tournante sous la forme d'un dƩmarreur pourvu d'un lanceur capable de transmettre une Ʃnergie de rotation du dƩmarreur Ơ un vilebrequin du moteur thermique par l'intermƩdiaire d'une couronne d'entraƮnement.In order to start a combustion engine, also called an internal combustion engine, in particular a motor vehicle, it is known to use a rotating electrical machine in the form of a starter provided with a launcher capable of transmitting rotational energy. from the starter to a crankshaft of the engine through a drive gear.

Ce lanceur est montĆ© sur un arbre de sortie de la machine Ć©lectrique. Dans une forme de rĆ©alisation un rĆ©ducteur de vitesse est intercalĆ© entre cet arbre de sortie, constituant l'arbre du lanceur, et l'arbre du moteur Ć©lectrique que comporte la machine Ć©lectrique tournante. L'interposition du rĆ©ducteur prĆ©sente l'intĆ©rĆŖt d'utiliser une machine Ć©lectrique plus rapide et d'obtenir ainsi un couple de dĆ©marrage plus Ć©levĆ© tout en rĆ©duisant l'encombrement et le poids de la machine pour une puissance donnĆ©e. Comme dĆ©crit dans le document FR2632094 , ce rĆ©ducteur de vitesse peut ĆŖtre formĆ© par une roue dentĆ©e sous la forme d'un pignon fixĆ© Ć  une extrĆ©mitĆ© de l'arbre du moteur Ć©lectrique de la machine Ć©lectrique et d'une couronne dentĆ©e solidaire en rotation par des moyens de friction de l'arbre du lanceur; cette couronne ayant des dents intĆ©rieures engrenant avec le pignon. Dans ce cas, l'arbre du moteur Ć©lectrique et l'arbre du lanceur sont dĆ©calĆ©s l'un par rapport Ć  l'autre.This launcher is mounted on an output shaft of the electric machine. In one embodiment, a speed reducer is interposed between this output shaft, constituting the launcher shaft, and the shaft of the electric motor that comprises the rotating electrical machine. The interposition of the reducer has the advantage of using a faster electric machine and thus obtain a higher starting torque while reducing the size and weight of the machine for a given power. As described in the document FR2632094 , this speed reducer can be formed by a toothed wheel in the form of a pinion fixed at one end of the shaft of the electric motor of the electric machine and a ring gear rotationally fixed by friction means of the thrower shaft; this ring having inner teeth meshing with the pinion. In this case, the electric motor shaft and the launcher shaft are offset relative to each other.

En variante, comme dĆ©crit dans le document WO2005/054664 , le rĆ©ducteur de vitesse est formĆ© par un train Ć©picycloĆÆdal comportant des pignons satellites montĆ©s Ć  rotation autour d'axes portĆ©s par un porte-satellites comprenant un plateau transversal solidaire de l'extrĆ©mitĆ© arriĆØre de l'arbre du lanceur. Ces pignons satellites engrĆØnent avec le pignon solidaire de l'arbre du moteur Ć©lectrique et avec les dents intĆ©rieures de la couronne dentĆ©e immobile en rotation par rapport au carter que comporte le dĆ©marreur. Dans ce cas, l'arbre du moteur Ć©lectrique et l'arbre du lanceur sont coaxiaux.Alternatively, as described in the document WO2005 / 054664 , the speed reducer is formed by an epicyclic gear comprising planet wheels mounted rotatably about axes carried by a planet carrier comprising a transverse plate secured to the rear end of the starter shaft. These planet gears mesh with the pinion integral with the shaft of the electric motor and with the inner teeth of the ring gear stationary in rotation relative to the housing that comprises the starter. In this case, the electric motor shaft and the launcher shaft are coaxial.

Par ailleurs, le lanceur comporte un pignon pourvu de dents configurĆ©es pour engrener avec des dents de la couronne d'entraĆ®nement, dite aussi couronne de dĆ©marrage, solidaire de maniĆØre rigide ou Ć©lastique du vilebrequin du moteur thermique Ć  dĆ©marrer. Ce lanceur peut subir des chocs mĆ©caniques importants lors du fonctionnement du dĆ©marreur, notamment lors du lancement du moteur thermique. Par exemple, en dĆ©but de dĆ©marrage, lorsque la rotation du dĆ©marreur commence, les dents du pignon peuvent glisser contre les dents de la couronne d'entraĆ®nement avant de s'engager entre celles-ci. Le recouvrement axial des dents respectives du pignon et de la couronne d'entraĆ®nement peut alors ĆŖtre trĆØs faible et l'Ć©nergie cinĆ©tique de rotation du dĆ©marreur est brutalement transmise Ć  la couronne. A cet instant, les contraintes de contact sont trĆØs Ć©levĆ©es, ce qui peut, avec l'usure, entraĆ®ner la destruction de dents de la couronne. Ce phĆ©nomĆØne est connu sous le terme de fraisage.Furthermore, the launcher comprises a pinion provided with teeth configured to mesh with teeth of the drive ring, also called start ring, rigidly or resiliently fixed to the crankshaft of the engine to start. This launcher can undergo significant mechanical shocks during operation of the starter, especially during the launch of the engine. For example, at the start of start, when the rotation of the starter begins, the teeth of the pinion can slide against the teeth of the drive ring before engaging between them. The axial overlap of the respective teeth of the pinion and the drive ring can then be very low and the kinetic energy of rotation of the starter is abruptly transmitted to the ring gear. At this time, the contact stresses are very high, which can, with wear, cause the destruction of teeth of the crown. This phenomenon is known as milling.

En outre, en cours de dĆ©marrage du moteur thermique, si le systĆØme d'injection du vĆ©hicule prĆ©sente des dysfonctionnements alĆ©atoires, il peut se produire des explosions prĆ©maturĆ©es dans le cycle de combustion, gĆ©nĆ©ralement appelĆ©es en anglais 'back fire', qui sont susceptibles de gĆ©nĆ©rer des chocs importants lors de l'engrĆØnement du pignon avec la couronne d'entraĆ®nement. Des chocs peuvent se produire Ć©galement lors de l'arrĆŖt du moteur thermique. Ces chocs prĆ©sentent le risque de provoquer la cassure de dents du pignon ou de la couronne d'entraĆ®nement, rĆ©sultant en un incident majeur.In addition, during the start of the engine, if the injection system of the vehicle has random malfunctions, it can occur premature explosions in the combustion cycle, usually called back fire, which are likely to generate significant shocks when meshing the pinion with the driving ring. Shocks can also occur when stopping the engine. These shocks present the risk of causing the breakage of teeth of the pinion or the driving ring, resulting in a major incident.

Afin de ne pas endommager le dĆ©marreur lors de ces dĆ©marrages, il est connu d'Ć©quiper la couronne du rĆ©ducteur de vitesse de plots amortisseurs. Un assemblage classique consiste en une couronne en matĆ©riau plastique sur laquelle sont surmoulĆ©s des amortisseurs en matĆ©riau thermoplastique Ć©lastomĆØre aptes Ć  se comprimer lors de l'application d'un sur-couple. Voir par exemple EP 1 450 038 A1 . La compression est effectuĆ©e par un dĆ©placement angulaire relatif des amortisseurs solidaires en rotation avec la couronne par rapport Ć  des Ć©lĆ©ments compresseurs solidaires en rotation du carter du dĆ©marreur destinĆ©s Ć  venir en appui contre les amortisseurs pour les comprimer.In order not to damage the starter during these starts, it is known to equip the gearbox of damping sprockets. A conventional assembly consists of a ring of plastic material on which are molded dampers elastomeric thermoplastic material capable of being compressed during the application of an over-torque. See for example EP 1 450 038 A1 . The compression is effected by a relative angular displacement of the dampers integral in rotation with the ring gear with respect to compressor elements integral in rotation with the starter housing intended to bear against the dampers to compress them.

Cependant, on constate qu'une absorption des chocs par compression implique une absorption assez brusque des chocs dans la mesure oĆ¹ le couple absorbĆ© en fonction de l'angle de dĆ©placement de la couronne Ć©volue de maniĆØre exponentielle, comme cela est reprĆ©sentĆ© sur la figure 1. Une telle Ć©volution du couple absorbĆ© entraĆ®ne une usure rapide des amortisseurs au cours des utilisations successives du dĆ©marreur ainsi qu'une transmission d'efforts importants Ć  la chaĆ®ne de traction du dĆ©marreur, ce qui rĆ©duit sa durĆ©e de vie.However, it is found that absorption of shocks by compression implies a fairly sudden absorption of shocks to the extent that the torque absorbed as a function of the displacement angle of the ring changes exponentially, as shown in FIG. figure 1 . Such a change in the absorbed torque results in rapid wear of the dampers during successive uses of the starter and a transmission of significant forces to the starter traction chain, which reduces its life.

OBJET DE L'INVENTIONOBJECT OF THE INVENTION

L'invention vise Ơ remƩdier efficacement Ơ ces inconvƩnients.The invention aims to effectively remedy these disadvantages.

A cet effet, l'invention a pour objet un dƩmarreur pour moteur thermique de vƩhicule automobile, comportant :

  • un moteur Ć©lectrique comportant un arbre,
  • un arbre de sortie sur lequel est montĆ© un pignon d'entraĆ®nement destinĆ© Ć  engrener avec une couronne de dĆ©marrage du moteur thermique,
  • un ensemble rĆ©ducteur ayant une couronne dentĆ©e, l'ensemble rĆ©ducteur Ć©tant installĆ© entre l'arbre du moteur Ć©lectrique et l'arbre de sortie et reliant en rotation l'arbre du moteur Ć©lectrique Ć  l'arbre de sortie,
  • un carter,
  • au moins un dispositif d'absorption des chocs installĆ© entre la couronne dentĆ©e et le carter liant en rotation la couronne au carter, caractĆ©risĆ© en ce que le dispositif d'absorption de choc est montĆ© pour absorber par cisaillement des chocs subis par la couronne lors d'un dĆ©marrage du moteur thermique engendrant un dĆ©placement angulaire relatif de la couronne par rapport au carter du dĆ©marreur.
For this purpose, the subject of the invention is a starter for a motor vehicle engine, comprising:
  • an electric motor having a shaft,
  • an output shaft on which is mounted a drive pinion for meshing with a starting ring of the heat engine,
  • a gear unit having a ring gear, the gear unit being installed between the shaft of the electric motor and the output shaft and rotatingly connecting the shaft of the electric motor to the output shaft,
  • a housing,
  • at least one shock absorbing device installed between the ring gear and the casing which rotates the ring gear to the casing, characterized in that the shock absorbing device is mounted to shear absorb shocks to the ring gear during 'an engine start thermal generating relative angular displacement of the ring relative to the starter housing.

L'invention permet ainsi d'amortir les chocs de maniĆØre plus progressive qu'un amortisseur travaillant en compression dans la mesure oĆ¹ le couple absorbĆ© Ć©volue de maniĆØre linĆ©aire en fonction de l'angle de rotation de la couronne lors du cisaillement d'un Ć©lĆ©ment Ć©lastique. L'invention permet donc d'augmenter la durĆ©e de vie de la chaĆ®ne de traction.The invention thus makes it possible to damp the shocks in a more progressive manner than a damper working in compression, insofar as the absorbed torque evolves in a linear manner as a function of the rotation angle of the ring during the shearing of an element. elastic. The invention therefore makes it possible to increase the life of the traction chain.

Par dispositif d'absorption de choc par cisaillement on entend un dispositif d'absorption qui est montƩ pour se dƩformer majoritairement par cisaillement pour amortir le choc.Shear absorbing device means an absorption device which is mounted to deform predominantly by shear to dampen the impact.

Selon une rƩalisation, le dispositif d'absorption des chocs par cisaillement comporte:

  • une plaque de support solidaire en rotation avec le carter, et
  • au moins un Ć©lĆ©ment Ć©lastique ayant une premiĆØre face solidaire en rotation de la plaque de support et une deuxiĆØme face opposĆ©e Ć  la premiĆØre face solidaire en rotation avec la couronne apte Ć  tourner par rapport au carter en cas de chocs subis par la couronne.
According to one embodiment, the shear absorption device comprises:
  • a support plate secured to rotate with the housing, and
  • at least one elastic element having a first face rotationally fixed to the support plate and a second face opposite to the first face integral in rotation with the crown rotatable relative to the housing in case of shocks to the crown.

Le fait d'utiliser une plaque de support permet de faciliter le montage du dispositif d'absorption dans le carter d'un dƩmarreur. En effet sans cette plaque, une des mƩthodes de montage serait le collage d'une surface de l'ƩlƩment Ʃlastique au carter.The fact of using a support plate makes it easier to mount the absorption device in the casing of a starter. Indeed without this plate, one of the mounting methods would be the bonding of a surface of the elastic element to the housing.

De plus, le fait que l'ƩlƩment Ʃlastique a deux de ces faces solidaire en rotation avec d'une part la couronne et d'autre part le carter permet Ơ l'ƩlƩment Ʃlastique de travailler de faƧon importante en cisaillement.In addition, the fact that the elastic element has two of these faces integral in rotation with the crown on the one hand and the housing on the other hand allows the elastic element to work significantly in shear.

Selon une premiĆØre rĆ©alisation, la premiĆØre face de l'Ć©lĆ©ment Ć©lastique comprend une surface radiale solidaire en rotation avec la plaque de support et en ce que la deuxiĆØme face comprend une surface radiale solidaire en rotation avec la couronne. Par surface radiale, on entend une surface dont la projection est perpendiculaire Ć  l'axe de la couronne.According to a first embodiment, the first face of the elastic element comprises a radial surface integral in rotation with the support plate and in that the second face comprises a radial surface integral in rotation with the ring. Radial surface means a surface whose projection is perpendicular to the axis of the ring.

Selon une seconde rĆ©alisation, la premiĆØre face de l'Ć©lĆ©ment Ć©lastique comprend une surface axiale solidaire en rotation avec la plaque de support et en ce que la deuxiĆØme face comprend une surface axiale solidaire en rotation avec la couronne. Par surface axiale on entend une surface dont la projection est parallĆØle avec l'axe de la couronne.According to a second embodiment, the first face of the elastic element comprises an axial surface integral in rotation with the support plate and in that the second face comprises an axial surface integral in rotation with the ring. Axial surface means a surface whose projection is parallel to the axis of the crown.

Selon un autre mode de rĆ©alisation, au moins une des premiĆØres ou seconde faces de l'Ć©lĆ©ment Ć©lastique est de forme conique.According to another embodiment, at least one of the first or second faces of the elastic element is of conical shape.

Selon un mode de rĆ©alisation, la deuxiĆØme face du dispositif d'absorption et montĆ© contre une paroi transversale de la couronne.According to one embodiment, the second face of the absorption device and mounted against a transverse wall of the ring.

Ce mode de rƩalisation permet de disposer le dispositif d'amortissement axialement permettant de rƩduire l'encombrement radial.This embodiment makes it possible to arrange the damping device axially to reduce the radial space requirement.

Selon un autre mode de rƩalisation, le dispositif d'amortissement de choc est montƩ radialement entre la couronne et le carter.According to another embodiment, the shock absorbing device is mounted radially between the crown and the housing.

Ce mode de rƩalisation permet de rƩduire l'encombrement axial du dƩmarreur.This embodiment reduces the axial size of the starter.

Selon une rĆ©alisation, le dispositif d'absorption des chocs par cisaillement comporte en outre une plaquette rapportĆ©e solidaire de la deuxiĆØme face de l'Ć©lĆ©ment Ć©lastique, cette plaque Ć©tant montĆ©e solidaire en rotation avec la paroi transversale de la couronne.According to one embodiment, the shear absorbing device further comprises an insert plate secured to the second face of the elastic element, this plate being mounted integral in rotation with the transverse wall of the ring.

Selon une rĆ©alisation, la plaquette rapportĆ©e est fixĆ©e Ć  la deuxiĆØme face de l'Ć©lĆ©ment Ć©lastique.In one embodiment, the insert plate is attached to the second face of the elastic member.

Selon une rƩalisation, la plaquette est fixƩe Ơ l'ƩlƩment Ʃlastique par surmoulage ou collage.In one embodiment, the wafer is attached to the elastic element by overmolding or gluing.

Selon une rĆ©alisation, la plaque de support est fixĆ©e Ć  la premiĆØre face de l'Ć©lĆ©ment Ć©lastique.In one embodiment, the support plate is attached to the first face of the elastic member.

Selon une rƩalisation, la plaque de support est fixƩe Ơ l'ƩlƩment Ʃlastique par surmoulage ou collage.According to one embodiment, the support plate is fixed to the elastic element by overmolding or gluing.

Selon une rĆ©alisation, la plaquette rapportĆ©e couvre sensiblement la totalitĆ© de la surface de la deuxiĆØme face de l'Ć©lĆ©ment Ć©lastique.According to one embodiment, the insert plate substantially covers the entire surface of the second face of the elastic element.

Selon une rĆ©alisation, la paroi transversale de la couronne est fixĆ©e par collageĆ  la deuxiĆØme face de l'Ć©lĆ©ment Ć©lastique.According to one embodiment, the transverse wall of the crown is fixed by gluing to the second face of the elastic element.

Cela permet de rƩduire l'encombrement.This reduces clutter.

Selon une rĆ©alisation, la paroi transversale de la couronne prĆ©sente des ouvertures destinĆ©es Ć  recevoir des plots issus de la plaquette rapportĆ©e. Cela permet d'avoir un moyen de fixation en rotation facile. Selon une rĆ©alisation, pour homogĆ©nĆ©iser les contraintes subies par le matĆ©riau lors du cisaillement, la premiĆØre et la deuxiĆØme face de l'Ć©lĆ©ment Ć©lastique sont inclinĆ©es l'une par rapport Ć  l'autre.According to one embodiment, the transverse wall of the ring has openings for receiving pads from the insert plate. This allows for a means of fixing in easy rotation. According to one embodiment, to homogenize the stresses experienced by the material during shearing, the first and second faces of the elastic element are inclined with respect to each other.

Selon une rĆ©alisation, le dĆ©marreur comporte en outre un dispositif d'absorption des chocs par compression apte Ć  ĆŖtre sollicitĆ© lorsque la couronne dĆ©passe un seuil de dĆ©placement angulaire de maniĆØre Ć  limiter la contrainte subie par le dispositif d'absorption des chocs par cisaillement.According to one embodiment, the starter further comprises a compression shock absorption device adapted to be biased when the ring exceeds an angular displacement threshold so as to limit the stress experienced by the shear absorption device.

Le dispositif d'absorption des chocs par cisaillement et le dispositif d'absorption des chocs par compression sont montƩs dans le dƩmarreur pour que lors d'un choc, le dispositif par cisaillement se dƩforme dans un premier temps jusqu'au seuil de dƩplacement angulaire et ensuite les deux dispositifs d'absorptions de choc se dƩforment pour absorber le choc.The shear absorbing device and the compression shock absorber are mounted in the starter so that, during an impact, the shearing device initially deforms to the angular displacement threshold and then the two shock absorbers deform to absorb the shock.

Selon un autre mode de rƩalisation, le dispositif d'absorption des chocs par cisaillement et le dispositif d'absorption des chocs par compression sont montƩs dans le dƩmarreur pour que lors d'un choc, le dispositif pour absorber le choc par cisaillement se dƩforme dans un premier temps jusqu'au seuil de dƩplacement angulaire et ensuite uniquement l'ƩlƩment d'absorption de choc par compression se dƩforme pour absorber le choc.According to another embodiment, the shear absorbing device and the compressive shock absorption device are mounted in the starter so that, during an impact, the device for absorbing shear impact is deformed in a first step up to the angular displacement threshold and then only the compression shock absorber deforms to absorb the shock.

Dans ces deux modes de rƩalisation, dans le premier temps (jusqu'au seuil de dƩclenchement), uniquement le dispositif d'absorption des chocs par cisaillement se dƩforme.In these two embodiments, in the first stage (up to the tripping threshold), only the shear absorbing device deforms.

Selon une rƩalisation, le seuil de dƩplacement angulaire est compris entre 15 et 25 degrƩs. Cela permet dispositif d'absorption des chocs par cisaillement d'absorber de faƧon non brutale une partie du choc.In one embodiment, the angular displacement threshold is between 15 and 25 degrees. This allows the shear absorption device to absorb non-abruptly part of the shock.

Selon une rƩalisation, le dispositif d'absorption des chocs par compression comporte au moins un amortisseur solidaire en rotation avec un des ƩlƩments parmi la paroi transversale de la couronne et la plaque de support ainsi qu'au moins un ƩlƩment compresseur correspondant solidaire en rotation avec l'autre ƩlƩment destinƩ Ơ venir en appui contre l'amortisseur lors du dƩplacement angulaire de la couronne au-delƠ du seuil de dƩplacement angulaire.According to one embodiment, the device for absorbing shocks by compression comprises at least one damper integral in rotation with one of the transverse wall of the crown and the support plate and at least one corresponding compressor element integral in rotation with the other element intended to bear against the damper during the angular displacement of the ring beyond the angular displacement threshold.

Selon une rƩalisation, l'amortisseur par compression est solidaire en rotation avec la plaque de support tandis que l'ƩlƩment compresseur appartient Ơ la paroi transversale de la couronne.According to one embodiment, the compression damper is integral in rotation with the support plate while the compressor element belongs to the transverse wall of the ring.

Selon une rƩalisation, une partie de l'amortisseur est insƩrƩe dans une cage de rƩception rigide situƩe du cƓtƩ opposƩ par rapport Ơ l'ƩlƩment compresseur formant une butƩe.According to one embodiment, a portion of the damper is inserted into a rigid receiving cage located on the opposite side with respect to the compressor element forming a stop.

Selon une rƩalisation, l'amortisseur prƩsente des angles biseautƩs du cƓtƩ de l'ƩlƩment compresseur.In one embodiment, the damper has beveled corners on the side of the compressor element.

Selon une rƩalisation, le dispositif d'absorption des chocs par cisaillement comporte deux ƩlƩments Ʃlastiques diamƩtralement opposƩs ayant une forme de portion d'anneau.In one embodiment, the shear absorbing device comprises two diametrically opposed elastic elements having a ring portion shape.

Selon une rƩalisation, le dispositif d'absorption des chocs par compression comporte deux amortisseurs situƩs chacun entre deux extrƩmitƩs des ƩlƩments Ʃlastiques en regard l'une de l'autre et deux ƩlƩments compresseur situƩs chacun entre un ƩlƩment Ʃlastique et un amortisseur.According to one embodiment, the compression shock absorption device comprises two dampers each located between two ends of the elastic elements facing one another and two compressor elements each located between an elastic member and a damper.

BREVE DESCRIPTION DES FIGURESBRIEF DESCRIPTION OF THE FIGURES

L'invention sera mieux comprise Ơ la lecture de la description qui suit et Ơ l'examen des figures qui l'accompagnent. Ces figures ne sont donnƩes qu'Ơ titre illustratif mais nullement limitatif de l'invention.

  • La figure 1, dĆ©jĆ  dĆ©crite, montre une reprĆ©sentation graphique de l'Ć©volution du couple absorbĆ© en fonction d'un angle de rotation de la couronne d'un ensemble rĆ©ducteur lors d'un choc subi par le dĆ©marreur selon l'Ć©tat de la technique;
  • La figure 2 montre une vue en coupe longitudinale d'un dĆ©marreur selon l'invention ;
  • Les figures 3a et 3b reprĆ©sentent des vues en perspective sous deux angles diffĆ©rents d'une couronne d'un ensemble rĆ©ducteur et des dispositifs d'absorption des chocs selon l'invention qui lui sont associĆ©s ;
  • Les figures 4a et 4b montrent des vues Ć©clatĆ©es de l'avant et de l'arriĆØre de la couronne et des dispositifs d'absorption des chocs selon l'invention qui lui sont associĆ©s;
  • La figure 5 est une vue de dessus de la couronne et des dispositifs d'absorption des chocs selon l'invention;
  • La figure 6 montre une vue en coupe transversale suivant l'axe A-A de l'ensemble de la figure 5;
  • Les figures 7a-7c reprĆ©sentent les diffĆ©rents Ć©tats des dispositifs d'absorption des chocs selon l'invention lors de l'absorption d'un choc subi par le dĆ©marreur selon l'invention;
  • La figure 8 montre une reprĆ©sentation graphique de l'Ć©volution du couple absorbĆ© en fonction d'un angle de rotation de la couronne d'un ensemble rĆ©ducteur lors d'un choc subi par le dĆ©marreur selon l'invention.
The invention will be better understood on reading the description which follows and on examining the figures which accompany it. These figures are given for illustrative but not limiting of the invention.
  • The figure 1 , already described, shows a graphical representation of the evolution of the absorbed torque as a function of an angle of rotation of the crown of a reduction unit during a shock to the starter according to the state of the art;
  • The figure 2 shows a longitudinal sectional view of a starter according to the invention;
  • The Figures 3a and 3b represent perspective views from two different angles of a ring gear of a gear unit and shock absorption devices according to the invention associated with it;
  • The Figures 4a and 4b show exploded views of the front and rear of the crown and the shock absorbing devices according to the invention associated with it;
  • The figure 5 is a top view of the crown and shock absorbing devices according to the invention;
  • The figure 6 shows a cross-sectional view along the axis AA of the whole of the figure 5 ;
  • The Figures 7a-7c represent the different states of the shock absorption devices according to the invention during the absorption of an impact suffered by the starter according to the invention;
  • The figure 8 shows a graphical representation of the evolution of the absorbed torque as a function of an angle of rotation of the crown of a reduction unit during an impact on the starter according to the invention.

Les Ć©lĆ©ments identiques, similaires ou analogues conservent la mĆŖme rĆ©fĆ©rence d'une figure Ć  l'autre.Identical, similar or similar elements retain the same reference from one figure to another.

DESCRIPTION D'EXEMPLES DE REALISATION DE L'INVENTIONDESCRIPTION OF EXAMPLES OF EMBODIMENT OF THE INVENTION

Dans la description qui va suivre, on utilisera une orientation axiale d'arriĆØre en avant correspondant Ć  l'orientation de droite Ć  gauche conformĆ©ment Ć  la figure 2.In the following description, use will be made of an axial orientation from back to front corresponding to the right-to-left orientation in accordance with the figure 2 .

En rĆ©fĆ©rence Ć  la figure 2, la machine Ć©lectrique tournante est un dĆ©marreur 10 de moteur thermique similaire au dĆ©marreur dĆ©crit dans le document WO2005/054664 , en sorte que les Ć©lĆ©ments identiques ou similaires Ć  ceux de la figure 1 de ce document WO2005/054664 , auquel on se reportera pour plus de prĆ©cisions, seront affectĆ©s des mĆŖmes signes de rĆ©fĆ©rence. Le dĆ©marreur comporte dans ce mode de rĆ©alisation un arbre de sortie 43, un lanceur 30 montĆ© sur l'arbre 43 et un moteur Ć©lectrique 11 composĆ© d'un stator 12 inducteur et d'un rotor 13 induit montĆ©s de maniĆØre coaxiale, le stator 12 entourant le rotor 13, lequel est montĆ© tournant autour d'un axe 14 Ć  l'intĆ©rieur d'une culasse 15. Cette derniĆØre est solidaire d'un support 16 mĆ©tallique du dĆ©marreur destinĆ© Ć  ĆŖtre fixĆ© sur une partie fixe du vĆ©hicule automobile. Le support 16 est ici en matiĆØre moulable, par exemple Ć  base d'aluminium et appartient au carter de la machine.With reference to the figure 2 , the rotating electrical machine is a starter motor 10 similar to the starter described in the document WO2005 / 054664 , so that the elements identical or similar to those of the figure 1 of this document WO2005 / 054664 , to which reference will be made for more details, will be assigned the same reference signs. The starter comprises in this embodiment an output shaft 43, a launcher 30 mounted on the shaft 43 and an electric motor 11 composed of an inductor stator 12 and a rotor 13 induced coaxially mounted, the stator 12 surrounding the rotor 13, which is rotatably mounted about an axis 14 inside a cylinder head 15. The latter is secured to a metal support of the starter for attachment to a fixed part of the motor vehicle. The support 16 is here moldable material, for example based on aluminum and belongs to the housing of the machine.

De maniĆØre connue, le stator 12 comporte dans un mode de rĆ©alisation une pluralitĆ© d'aimants permanents inducteurs portĆ©s par la pĆ©riphĆ©rie interne de la culasse 15. En variante, comme montrĆ© dans le mode de rĆ©alisation de la figure 2, le stator 12 comporte un bobinage inducteur 17 comportant deux paires d'enroulements 18, qui sont enroulĆ©s chacun autour d'une masse polaire 19 solidaire de la culasse 15. Les masses polaires 19 sont fixĆ©es Ć  l'aide de vis 20 Ć  la culasse 15, ici mĆ©tallique, comme dĆ©crit dans le document FR2611096 . Chaque enroulement 18 est composĆ© d'un conducteur continu enroulĆ© autour de la masse polaire 19 dans le sens de son Ć©paisseur de maniĆØre Ć  former des spires jointives concentriques de diamĆØtre croissant comme mieux visible dans les Figures 2 Ć  5 du document EP749194 . L'axe de chaque enroulement 18 est radial par rapport Ć  l'axe 14 du rotor 13, lequel constitue l'axe de rotation du moteur Ć©lectrique 11.In known manner, the stator 12 comprises in one embodiment a plurality of permanent inductor magnets carried by the inner periphery of the cylinder head 15. Alternatively, as shown in the embodiment of FIG. figure 2 , the stator 12 comprises an inductor winding 17 comprising two pairs of windings 18, which are each wound around a polar mass 19 integral with the cylinder head 15. The polar masses 19 are fixed with screws 20 to the cylinder head 15, here metallic, as described in the document FR2611096 . Each winding 18 is composed of a continuous conductor wound around the polar mass 19 in the direction of its thickness so as to form concentric contiguous turns of increasing diameter as better visible in the Figures 2 to 5 of the document EP749194 . The axis of each winding 18 is radial relative to the axis 14 of the rotor 13, which constitutes the axis of rotation of the electric motor 11.

Le rotor 13 comporte un paquet de tƓles dotƩes de rainures pour le montage de conducteurs 21 Ʃlectriques en forme d'Ʃpingles. Ces conducteurs 21 sont reliƩs entre eux pour former un bobinage rotorique en liaison avec des lames 22 conductrices appartenant Ơ un collecteur 23 Ơ corps Ʃlectriquement isolant solidaire de l'arbre 24 du moteur Ʃlectrique 11. En variante, le bobinage est Ơ fil continu.The rotor 13 comprises a bundle of plates provided with grooves for mounting electrical conductors 21 in the form of pins. These conductors 21 are interconnected to form a rotor winding in connection with the conductive blades 22 belonging to a collector 23 with an electrically insulating body integral with the shaft 24 of the electric motor 11. In a variant, the winding is in continuous wire.

Des balais 25 frottent sur les lames 22 collectrices du collecteur 23 pour alimenter le bobinage rotorique. Les balais 25 appartiennent Ć  un porte-balais 26 Ć©quipĆ© de cages de guidage et de rĆ©ception des balais, lesquels sont sollicitĆ©s en direction des lames 22 collectrices par des ressorts 27. Le porte-balais 26 est solidaire d'un palier arriĆØre 29 mĆ©tallique prĆ©sentant dans la partie centrale un logement pour le montage d'un roulement Ć  aiguilles 28. Le palier 29 sert au montage Ć  rotation de l'extrĆ©mitĆ© arriĆØre de l'arbre 24 du moteur Ć©lectrique 11. L'axe de cet arbre 24 est confondu avec l'axe 14 du rotor 13, et avec l'axe de l'arbre de sortie 43 du dĆ©marreur, constituant l'arbre du lanceur 30. Le palier 29 arriĆØre sert de centreur Ć  l'extrĆ©mitĆ© arriĆØre de la culasse 15, et est reliĆ© par des tirants 31 au support 16 du dĆ©marreur 10. Deux trous taraudĆ©s (non rĆ©fĆ©rencĆ©s) sont mĆ©nagĆ©s dans le support 16 pour le vissage des tirants. Les tirants 31 sont implantĆ©s Ć  l'extĆ©rieur de la culasse 15. Ici un faible jeu existe entre les tirants et la pĆ©riphĆ©rie externe de la culasse 15 de forme tubulaire. La culasse 15 mĆ©tallique est intercalĆ©e Ć  serrage entre le support mĆ©tallique 16 et le palier arriĆØre mĆ©tallique 28. Le carter du dĆ©marreur comporte ainsi le palier 28, la culasse 15 et le support 16. Ce carter est destinĆ© Ć  ĆŖtre reliĆ© Ć  la masse du vĆ©hicule automobile via son support 16.Brushes 25 rub on the collector slats 22 of the manifold 23 to supply the rotor winding. Brushes 25 belong to a brush holder 26 equipped with guiding cages and receiving brushes, which are biased towards the slats 22 by means of springs 27. The brush holder 26 is integral with a metal rear bearing 29 having in the central part a housing for mounting a needle bearing 28. The bearing 29 serves for rotatably mounting the rear end of the shaft 24 of the electric motor 11. The axis of this shaft 24 coincides with the axis 14 of the rotor 13, and with the axis of the output shaft 43 of the starter constituting the starter shaft 30. The rear bearing 29 serves as a centering device at the rear end of the yoke 15, and is connected by tie rods 31 to the support 16 of the starter 10. Two threaded holes (not referenced) are formed in the support 16 for screwing the tie rods. The tie rods 31 are located outside the cylinder head 15. Here a small clearance exists between the tie rods and the outer periphery of the cylinder-shaped cylinder head 15. The metal cylinder head is interposed between the metal support 16 and the metal rear bearing 28. The starter housing thus comprises the bearing 28, the cylinder head 15 and the support 16. This casing is intended to be connected to the mass of the vehicle. automobile via its support 16.

Le dĆ©marreur 10 comporte Ć©galement un contacteur 32 Ć©lectromagnĆ©tique s'Ć©tendant parallĆØlement au moteur Ć©lectrique 11 en Ć©tant implantĆ© radialement au-dessus de celui-ci. Le contacteur 32 prĆ©sente une cuve 33 mĆ©tallique portĆ©e par le support 16, et Ć©quipĆ©e d'une bobine B d'excitation dotĆ©e d'au moins un enroulement. La cuve 33 est fermĆ©e Ć  l'arriĆØre par un capot 34 en matiĆØre Ć©lectriquement isolante. La fixation du capot 34 est rĆ©alisĆ©e par rabattement de matiĆØre de l'extrĆ©mitĆ© libre de la cuve 33. Un Ć©paulement de la cuve 33 permet d'assurer le calage axial d'un noyau fixe 35, lequel est calĆ© axialement dans l'autre sens par le capot 34 portant des bornes 36, 37 d'alimentation Ć©lectrique.The starter 10 also comprises an electromagnetic contactor 32 extending parallel to the electric motor 11 by being radially implanted above it. The contactor 32 has a metal tank 33 carried by the support 16, and equipped with an excitation coil B provided with at least one winding. The tank 33 is closed at the rear by a cover 34 made of electrically insulating material. The fixing of the cover 34 is made by folding the material of the free end of the tank 33. A shoulder of the tank 33 ensures the axial setting of a fixed core 35, which is wedged axially in the other direction by the cover 34 carrying terminals 36, 37 of power supply.

Les bornes 36, 37 sont conformĆ©es pour former chacune un contact fixe 38 Ć  l'intĆ©rieur du capot 34. L'une des bornes 36 est destinĆ©e Ć  ĆŖtre reliĆ©e Ć  la borne positive de la batterie, l'autre 37 est connectĆ©e par l'intermĆ©diaire d'un cĆ¢ble 39 Ć  l'entrĆ©e du bobinage inducteur 17 du stator et aux balais 25 de polaritĆ©s positives. De maniĆØre connue lors de l'excitation de la bobine B, un noyau mobile 40 est attirĆ© par attraction magnĆ©tique en direction du noyau fixe 35 pour, d'une part, agir aprĆØs rattrapage d'un jeu sur une tige (non rĆ©fĆ©rencĆ©e) portant un contact mobile (non rĆ©fĆ©rencĆ©) pour provoquer la fermeture des contacts du contacteur 32 et alimenter le moteur Ć©lectrique du dĆ©marreur, et, d'autre part, actionner un levier 41 de commande du lanceur.The terminals 36, 37 are shaped to each form a fixed contact 38 inside the cover 34. One of the terminals 36 is intended to be connected to the positive terminal of the battery, the other 37 is connected by the intermediate of a cable 39 at the input of the inductor winding 17 of the stator and brushes 25 of positive polarity. In known manner during the excitation of the coil B, a mobile core 40 is attracted by magnetic attraction towards the fixed core 35 to, firstly, act after catching a game on a rod (not referenced) carrying a movable contact (not referenced) to cause the closure of the contacts of the contactor 32 and supply the electric motor of the starter, and, on the other hand, operate a lever 41 for controlling the launcher.

L'arbre de sortie 43 est montĆ© rotatif dans un palier 42 avant du support 16. Ce palier 42 est constituĆ© Ć  titre d'exemple par un roulement Ć  aiguille en variante par un palier lisse. Cet arbre 43 porte Ć  l'avant une butĆ©e 53 adjacente au palier 42 pour limiter le dĆ©placement du lanceur 30. L'extrĆ©mitĆ© arriĆØre de l'arbre 43 est configurĆ©e pour ĆŖtre solidaire d'un plateau d'un porte-satellites 47 par exemple par sertissage, ce porte-satellites 47 appartenant Ć  un train Ć©picycloĆÆdal constituant le rĆ©ducteur 45 de vitesse Ć  engrenages. Ce porte-satellites 47 porte des satellites 47.1 engrenant d'une part avec une couronne 46 (dĆ©crite plus en dĆ©tail ci-dessous) et avec un pignon planĆ©taire 49 solidaire de l'extrĆ©mitĆ© avant de l'arbre 24 du moteur Ć©lectrique. Le rĆ©ducteur 45 est du type de celui dĆ©crit dans le document FR2787833 auquel on se reportera, celui-ci montrant le montage de l'extrĆ©mitĆ© avant de l'arbre 24 du moteur Ć©lectrique 11 dans l'extrĆ©mitĆ© arriĆØre de l'arbre 43 dotĆ© d'un trou borgne dans lequel est logĆ© l'extrĆ©mitĆ© avant de l'arbre 24 avec interposition d'un palier lisse et d'une bille. Les satellites 47.1 sont donc montĆ©s Ć  rotation chacun autour d'un axe. Ces axes s'Ć©tendent entre deux plateaux d'orientation transversale par rapport Ć  l'axe de l'arbre 43 en Ć©tant portĆ©s par ces plateaux, dont l'un est plus Ć©pais que l'autre et est ici fixĆ© par sertissage Ć  l'extrĆ©mitĆ© arriĆØre de l'arbre 43. En variante le porte-satellites 47 comporte un seul plateau fixĆ© Ć  l'extrĆ©mitĆ© arriĆØre de l'arbre 43 et portant les axes.The output shaft 43 is rotatably mounted in a bearing 42 before the support 16. This bearing 42 is constituted by way of example by a needle bearing alternatively by a plain bearing. This shaft 43 carries at the front a stop 53 adjacent to the bearing 42 to limit the movement of the launcher 30. The rear end of the shaft 43 is configured to be secured to a plate of a planet carrier 47, for example by crimping, this planet carrier 47 belonging to an epicyclic gear train constituting the speed reducer 45 gear. This planet carrier 47 carries satellites 47.1 meshing on the one hand with a ring 46 (described in more detail below) and with a sun gear 51 integral with the front end of the shaft 24 of the electric motor. The gearbox 45 is of the type described in the document FR2787833 which will be referred to, the latter showing the mounting of the front end of the shaft 24 of the electric motor 11 in the rear end of the shaft 43 having a blind hole in which is housed the front end of the shaft 24 with the interposition of a plain bearing and a ball. The satellites 47.1 are therefore rotatably mounted each about an axis. These axes extend between two plates of transverse orientation relative to the axis of the shaft 43 being carried by these plates, one of which is thicker than the other and is here fixed by crimping to the rear end of the shaft 43. In a variant, the planet carrier 47 comprises a single plate fixed to the rear end of the shaft 43 and carrying the axes.

Le lanceur 30 est montĆ© coulissant sur l'arbre de sortie 43, et comporte un pignon d'entraĆ®nement 50, un entraĆ®neur 51 configurĆ© pour ĆŖtre actionnĆ© par le levier de commande 41 pivotant, et une roue libre 52 Ć  galets intercalĆ©e axialement entre l'entraĆ®neur 51 et le pignon 50. De maniĆØre connue les dents du pignon 50 appartiennent Ć  un manchon prolongĆ© Ć  l'arriĆØre pour former la piste interne cylindrique de la roue libre 52 Ć  galets. L'entraĆ®neur 51 est prolongĆ© axialement Ć  l'avant par une douille configurĆ©e intĆ©rieurement pour former la piste externe profilĆ©e de la roue libre 52 Ć  galets et loger les ressorts agissant de maniĆØre connue sur les galets. Plus prĆ©cisĆ©ment l'entraĆ®neur 51 comporte un manchon solidaire Ć  l'avant d'un flasque d'orientation transversale par rapport Ć  l'axe de l'arbre 43. Ce flasque est solidaire Ć  sa pĆ©riphĆ©rie externe de la douille d'orientation axiale par rapport Ć  l'axe de l'arbre 43 pour formation d'une cage de rĆ©ception de galets fermĆ©e Ć  l'avant par des rondelles. L'entraĆ®neur 51 porte une rondelle (non rĆ©fĆ©rencĆ©e) dĆ©finissant avec le flasque de l'entraĆ®neur 51 une gorge pour la rĆ©ception des doigts de l'extrĆ©mitĆ© infĆ©rieure du levier 41 en forme de fourchette. L'extrĆ©mitĆ© supĆ©rieure du levier 41 est montĆ©e de maniĆØre connue Ć  articulation sur une tige (non rĆ©fĆ©rencĆ©e Ć  la figure 2) reliĆ©e Ć©lastiquement au noyau mobile 40 via un ressort logĆ© dans le noyau mobile 40. Bien entendu en variante, le levier 41 est montĆ© Ć  articulation sur le noyau mobile 40 et le ressort entoure le manchon de l'entraĆ®neur en prenant appui sur le flasque de l'entraĆ®neur comme dĆ©crit par exemple dans le document DE2822165 .The launcher 30 is slidably mounted on the output shaft 43, and comprises a drive gear 50, a driver 51 configured to be actuated by the control lever 41 pivoting, and a free wheel 52 with rollers interposed axially between the 51 and the pinion 50. In known manner the teeth of the pinion 50 belong to a sleeve extended at the rear to form the cylindrical inner track of the free wheel 52 roller. The driver 51 is axially extended at the front by a bushing configured internally to form the profiled external track of the freewheel 52 with wheels and to house the springs acting in known manner on the rollers. More specifically, the driver 51 comprises a sleeve integral with the front of a flange of transverse orientation relative to the axis of the shaft 43. This flange is integral at its outer periphery with the sleeve of axial orientation by relative to the axis of the shaft 43 for forming a roller receiving cage closed at the front by washers. The driver 51 carries a washer (not referenced) defining with the flange of the driver 51 a groove for receiving the fingers of the lower end of the lever 41 fork-shaped. The upper end of the lever 41 is mounted in known manner to articulation on a rod (not referenced to the figure 2 ) elastically connected to the movable core 40 via a spring housed in the movable core 40. Of course alternatively, the lever 41 is hingedly mounted on the movable core 40 and the spring surrounds the sleeve of the driver by bearing on the flange of the coach as described for example in the document DE2822165 .

De maniĆØre connue, le manchon de l'entraĆ®neur 51 est dotĆ© intĆ©rieurement de cannelures hĆ©licoĆÆdales (non rĆ©fĆ©rencĆ©es) en prise de maniĆØre complĆ©mentaire avec des dentures hĆ©licoĆÆdales externes portĆ©es par l'arbre de sortie 43 au voisinage de son extrĆ©mitĆ© arriĆØre ici cylindrique et de plus grand diamĆØtre. Le lanceur 30 est ainsi animĆ© d'un mouvement hĆ©licoĆÆdal lorsqu'il est dĆ©placĆ© par le levier 41 en direction de la butĆ©e 53 pour venir, par l'intermĆ©diaire de son pignon 50, en prise avec la couronne d'entraĆ®nement, dite couronne de dĆ©marrage (non reprĆ©sentĆ©e), d'un moteur thermique appelĆ© Ć©galement moteur Ć  combustion interne.In known manner, the sleeve of the driver 51 is internally provided with helical splines (not referenced) in complementary engagement with external helical teeth carried by the output shaft 43 in the vicinity of its rear end here cylindrical and moreover large diameter. The launcher 30 is thus animated by a helical movement when it is moved by the lever 41 in the direction of the stop 53 to come, via its pinion 50, in engagement with the drive ring, called the crown of starting (not shown), a heat engine also called internal combustion engine.

Il est clair que le dispositif Ć  roue libre 52 peut ĆŖtre remplacĆ© par un dispositif d'attelage Ć  embrayage conique, du type dĆ©crit dans le document FR2772433 ou un embrayage Ć  plusieurs disques. De mĆŖme il est clair que le lanceur 30 en variante est implantĆ© en partie Ć  l'extĆ©rieur du support 16 Ć  l'avant de celui-ci. Plus prĆ©cisĆ©ment, le pignon 50 du lanceur 30, au lieu d'ĆŖtre implantĆ© dans le support (cf. figure 2), peut ĆŖtre implantĆ© Ć  l'extĆ©rieur du support comme visible par exemple dans le document FR2745855 auquel on se reportera pour plus de prĆ©cisions.It is clear that the freewheel device 52 can be replaced by a conical clutch coupling device, of the type described in the document FR2772433 or a clutch with multiple disks. Similarly, it is clear that the launcher 30 variant is implanted in part outside the support 16 at the front thereof. More precisely, the pinion 50 of the launcher 30, instead of being implanted in the support (cf. figure 2 ), can be implanted outside the support as visible for example in the document FR2745855 which will be referred to for more details.

Le levier de commande 41 est accouplĆ©, ici Ć©lastiquement en variante rigidement de maniĆØre prĆ©citĆ©e, par son extrĆ©mitĆ© supĆ©rieure au noyau mobile 40 du contacteur 32, et comporte dans sa partie mĆ©diane un axe de pivotement 54, qui selon une caractĆ©ristique est distinct, de la couronne 46 dentĆ©e du rĆ©ducteur 45 de vitesse Ć  engrenages du fait de la structure de l'ensemble dĆ©crit ci-dessous. Le levier 41 est en une piĆØce moulĆ©e, de prĆ©fĆ©rence en matiĆØre thermoplastique rigide pour rĆ©duire les bruits, de prĆ©fĆ©rence renforcĆ©e par des fibres. Le montage de l'axe de pivotement 54 est par exemple rĆ©alisĆ© Ć  l'aide d'une piĆØce d'appui comme dans les documents DE2822165 et FR2787833 ou dans le support 16 dotĆ© de saillies Ć  cet effet, l'axe 54 Ć©tant distinct ou intĆ©grĆ© au levier 41. Dans le mode de rĆ©alisation de la figure 2, comme dans le document DE2822165 , il est prĆ©vu un plot d'Ć©tanchĆ©itĆ© 158 en Ć©lastomĆØre pour absorber les variations dimensionnelles. Ce plot 158 est en contact avec la face d'appui du contacteur et est solidaire d'une piĆØce en matiĆØre plastique 155 configurĆ©e pour remplacer la ou les languettes 55 de la figure 1 du document WO2005/054664 ; le logement du support 16 Ć©tant conservĆ©. En variante, le plot 158 est supprimĆ© et c'est la piĆØce en matiĆØre plastique 155 qui est alors en contact avec la face d'appui du contacteur. On peut Ć©galement faire appel Ć  la solution dĆ©crite dans le document WO01/31195 . Tout dĆ©pend des applications.The control lever 41 is coupled, here elastically in a variant rigidly in the aforementioned manner, by its upper end to the movable core 40 of the contactor 32, and comprises in its middle part a pivot axis 54, which according to a characteristic is distinct, the toothed gear gear reducer gear ring 46 due to the structure of the assembly described below. The lever 41 is in a molded part, preferably made of rigid thermoplastic material to reduce noise, preferably reinforced by fibers. The mounting of the pivot axis 54 is for example made using a support piece as in the documents DE2822165 and FR2787833 or in the support 16 provided with projections for this purpose, the axis 54 being separate or integrated in the lever 41. In the embodiment of the figure 2 as in the document DE2822165 , there is provided a sealing pad 158 of elastomer to absorb dimensional variations. This stud 158 is in contact with the contact surface of the contactor and is integral with a plastic part 155 configured to replace the tongue or tabs 55 of the figure 1 of the document WO2005 / 054664 ; the housing of the support 16 being retained. Alternatively, the pad 158 is removed and it is the plastic part 155 which is then in contact with the contact surface of the contactor. The solution described in the document can also be used WO01 / 31195 . It all depends on the applications.

La couronne 46 du rĆ©ducteur 45 de vitesse d'axe X confondu avec l'axe 14 est de forme creuse et comporte une paroi 58 transversale Ć  la pĆ©riphĆ©rie extĆ©rieure de laquelle s'Ć©tend une jupe 46.1 annulaire d'orientation axiale munie de dents intĆ©rieures engrenant avec les satellites 47.1. Cette paroi transversale 58 est trouĆ©e centralement et montĆ©e sur un moyeu 68 rapportĆ© assurant son centrage. Le moyeu 68 prĆ©sente en son centre une ouverture traversante autorisant le passage de l'arbre 43. Comme visible sur la figure 3a, la jupe 46.1 est d'orientation axiale par rapport Ć  l'axe X et a donc une forme cylindrique. Les dents 46.4 de la jupe 46.1 ont une orientation axiale. La couronne 46 est fermĆ©e Ć  l'arriĆØre par un capot 200 (cf. figure 2). L'intĆ©rieur de la couronne 46 peut ĆŖtre ainsi rempli de graisse de lubrification des satellites 47.1 et du pignon planĆ©taire 49.The ring 46 of the X-axis speed reducer 45 coincides with the axis 14 is of hollow form and has a wall 58 transverse to the outer periphery of which extends an annular skirt 46.1 of axial orientation provided with inner teeth meshing with satellites 47.1. This transverse wall 58 is pierced centrally and mounted on a hub 68 reported to ensure its centering. The hub 68 has at its center a through opening allowing the passage of the shaft 43. As visible on the figure 3a , the skirt 46.1 is axially oriented relative to the axis X and therefore has a cylindrical shape. The teeth 46.4 of the skirt 46.1 have an axial orientation. The ring 46 is closed at the rear by a cover 200 (cf. figure 2 ). The inside of the ring 46 can thus be filled with lubricating grease of the satellites 47.1 and the sun gear 49.

Afin d'absorber les chocs que subit la couronne 46 au cours des utilisations successives du dƩmarreur 10, le dƩmarreur 10 comporte un dispositif 61 d'absorption des chocs installƩ entre la couronne 46 dentƩe et le carter du dƩmarreur, en l'occurrence le support 16, apte Ơ absorber par cisaillement des chocs subis par la couronne 46 lors de sur-couples gƩnƩrƩs par le dƩmarrage du moteur thermique.In order to absorb the shock experienced by the ring 46 during successive uses of the starter 10, the starter 10 comprises a shock absorbing device 61 installed between the ring gear 46 and the starter housing, in this case the carrier 16, adapted to absorb shear shocks suffered by the ring 46 during overtemperature generated by the start of the engine.

Plus prĆ©cisĆ©ment, comme cela est bien visible sur les figures 3a et 3b, le dispositif 61 comporte une plaque de support 62 de forme annulaire Ć©galement d'axe X comportant sur une de ses face d'orientation radiale des pions 64 destinĆ©s Ć  s'insĆ©rer Ć  l'intĆ©rieur d'ouvertures non reprĆ©sentĆ©es rĆ©alisĆ©es dans le support 16. La plaque de support 62 est ainsi solidaire en rotation avec le support 16 et donc avec le carter du dĆ©marreur. Les pions 64 sont rĆ©partis angulairement de maniĆØre rĆ©guliĆØre Ć  la pĆ©riphĆ©rie externe de la plaque de support 62. En l'occurrence, ces pions 64 au nombre de six prĆ©sentent une forme parallĆ©lĆ©pipĆ©dique. Une ouverture centrale 67 de la plaque de support 62 autorise le passage de l'arbre 43. La plaque de support 62 est par exemple rĆ©alisĆ©e en mĆ©tal et les pions 64 viennent de matiĆØre avec la plaque de support 62.More precisely, as is clearly visible on the Figures 3a and 3b , the device 61 comprises a support plate 62 of annular shape also of X axis having on one of its faces of radial orientation of the pins 64 intended to be inserted inside unrepresented openings made in the support 16 The support plate 62 is thus integral in rotation with the support 16 and thus with the starter housing. The pins 64 are angularly distributed regularly at the outer periphery of the support plate 62. In this case, these six pins 64 have a parallelepiped shape. A central opening 67 of the support plate 62 allows the passage of the shaft 43. The support plate 62 is for example made of metal and the pins 64 are made of material with the support plate 62.

La plaque de support 62 comporte en outre un moyen d'indexage 65 formƩ par un Ʃvidement montrƩ Ơ la figure 3a rƩalisƩ Ơ sa pƩriphƩrie externe destinƩ Ơ coopƩrer avec une saillie du support 16. Cela permet de faciliter le positionnement angulaire de la plaque 62 par rapport au support 16.The support plate 62 further comprises an indexing means 65 formed by a recess shown in FIG. figure 3a made at its outer periphery intended to cooperate with a projection of the support 16. This facilitates the angular positioning of the plate 62 relative to the support 16.

En variante, comme cela est reprƩsentƩ sur les figures 4a et 4b, la plaque de support 62 est dƩpourvue de pions 64 et comporte un Ʃpaulement annulaire 66 Ơ sa pƩriphƩrie externe d'orientation axiale ainsi qu'un ergot 78 de forme globalement rectangulaire pour son indexage et sa liaison en rotation avec le support 16. A cet effet, l'ergot 78 est destinƩ Ơ coopƩrer avec un logement, non reprƩsentƩ, de forme complƩmentaire rƩalisƩ dans le support 16. La plaque de support 62 comporte Ʃgalement un manchon annulaire 79 d'axe X dƩlimitant l'ouverture 67 sur lequel est positionnƩ la couronne 46.Alternatively, as shown on the Figures 4a and 4b , the support plate 62 is devoid of pins 64 and has an annular shoulder 66 at its outer periphery of axial orientation and a lug 78 of generally rectangular shape for its indexing and its connection in rotation with the support 16. At this Indeed, the lug 78 is intended to cooperate with a housing, not shown, of complementary shape formed in the support 16. The support plate 62 also comprises an annular sleeve 79 of X axis delimiting the opening 67 on which is positioned the crown 46.

Comme bien visible sur la figure 4a, le dispositif 61 d'absorption des chocs comporte Ć©galement deux Ć©lĆ©ments Ć©lastiques 69 fixĆ©s sur une face radiale de la plaque de support 62 opposĆ©e Ć  la face comportant les pions 64 ou l'Ć©paulement 66. La fixation des Ć©lĆ©ments Ć©lastiques 69 sur la plaque de support 62 est effectuĆ©e par exemple par collage d'une face 70 des Ć©lĆ©ments Ć©lastiques 69 sur la plaque de support 62. Chaque Ć©lĆ©ment Ć©lastique 69 prĆ©sente par exemple une forme de portion annulaire s'Ć©tendant par exemple sur un angle A de l'ordre de 112 degrĆ©s. Chaque Ć©lĆ©ment Ć©lastique 69 prĆ©sente un rayon interne R1 supĆ©rieur Ć  un rayon externe R2 du manchon 79 et un rayon externe R3 lĆ©gĆØrement infĆ©rieur Ć  un rayon externe R4 dĆ©limitant la plaque 62. Les Ć©lĆ©ments Ć©lastiques 69 sont par exemple rĆ©alisĆ©s en caoutchouc. Les Ć©lĆ©ments Ć©lastiques 69 ont par exemple une duretĆ© Shore comprise entre 72 et 73 ShA Ć  80 degrĆ©s Celsius.As clearly visible on the figure 4a the shock absorbing device 61 also comprises two elastic elements 69 fixed on a radial face of the support plate 62 opposite the face comprising the pins 64 or the shoulder 66. The fixing of the elastic elements 69 on the support plate 62 is effected for example by bonding a face 70 of the elastic elements 69 to the support plate 62. Each elastic element 69 has, for example, a portion shape. annular extending for example on an angle A of the order of 112 degrees. Each elastic element 69 has an inner radius R1 greater than an outer radius R2 of the sleeve 79 and an outer radius R3 slightly smaller than an outer radius R4 delimiting the plate 62. The elastic elements 69 are for example made of rubber. The elastic elements 69 have for example a Shore hardness of between 72 and 73 ShA at 80 degrees Celsius.

En outre, comme montrĆ© sur la figure 6, une plaquette 71 rapportĆ©e est solidaire d'une face 72 de chaque Ć©lĆ©ment Ć©lastique 69 opposĆ©e Ć  la face 70 fixĆ©e Ć  la plaque de support 62. Cette plaquette 71 suit un contour extĆ©rieur de la face 72 (cf. figure 4a ou 7a) de sorte que la plaquette 71 prĆ©sente sensiblement la mĆŖme surface que la face 72. Autrement dit, la plaquette 71 couvre sensiblement la totalitĆ© de la surface de la face 72. La face 72 de l'Ć©lĆ©ment Ć©lastique 69 portant la plaquette 71 est inclinĆ©e par rapport Ć  la face 70 fixĆ©e Ć  la plaque de support 62. On homogĆ©nĆ©ise ainsi les contraintes subies par le matĆ©riau lors du cisaillement des Ć©lĆ©ments Ć©lastiques 69. Plus prĆ©cisĆ©ment, la face 70 s'Ć©tend dans un plan radial par rapport Ć  l'axe X. La face 72 est inclinĆ©e par rapport Ć  la face 70 vers l'intĆ©rieur de la plaque 62 de sorte que la section transversale de chaque Ć©lĆ©ment 69 a tendance Ć  diminuer lorsqu'on se dĆ©place de l'extĆ©rieur vers l'intĆ©rieur de la plaque 62. L'angle d'inclinaison B' des deux faces l'une par rapport Ć  l'autre est par exemple de l'ordre de 5 degrĆ©s. La face de la plaquette 71 fixĆ©e Ć  la l'Ć©lĆ©ment 69 prĆ©sente une inclinaison correspondante. Les plaquettes 71 prennent par exemple chacune la forme d'une plaque de faible Ć©paisseur rĆ©alisĆ©e en mĆ©tal.In addition, as shown on the figure 6 , an insert plate 71 is integral with a face 72 of each elastic element 69 opposite the face 70 fixed to the support plate 62. This plate 71 follows an outer contour of the face 72 (cf. figure 4a or 7a ) so that the wafer 71 has substantially the same surface as the face 72. In other words, the wafer 71 covers substantially the entire surface of the face 72. The face 72 of the elastic element 69 carrying the wafer 71 is inclined relative to the face 70 fixed to the support plate 62. The stresses experienced by the material during shearing of the elastic elements 69 are thus homogenized. More specifically, the face 70 extends in a radial plane with respect to the axis. X. The face 72 is inclined with respect to the face 70 towards the inside of the plate 62 so that the cross-section of each element 69 tends to decrease when moving from the outside to the inside of the plate. plate 62. The angle of inclination B 'of the two faces relative to each other is for example of the order of 5 degrees. The face of the wafer 71 attached to the element 69 has a corresponding inclination. The plates 71 take for example each in the form of a thin plate made of metal.

La paroi transversale 58 de la couronne 46 est rendue solidaire en rotation avec la plaquette 71. A cet effet, comme montrĆ© sur les figures 4a, 6, 7a-7c, la paroi 58 prĆ©sente des ouvertures 74 destinĆ©es Ć  recevoir des plots 75 issus des plaquettes 71. En l'occurrence, chaque plaquette 71 comporte trois plots 75 positionnĆ©s sur une mĆŖme circonfĆ©rence entre la pĆ©riphĆ©rie interne et la pĆ©riphĆ©rie externe de l'Ć©lĆ©ment Ć©lastique 69. Ces plots 75 sont destinĆ©s Ć  coopĆ©rer avec deux ensembles de trois d'ouvertures 75 diamĆ©tralement opposĆ©s mĆ©nagĆ©s dans la paroi transversale 58 de la couronne 46 (cf. figure 5). En complĆ©ment ou en substitution de ce systĆØme de liaison, la paroi transversale 58 est fixĆ©e par collage Ć  la plaquette 71.The transverse wall 58 of the ring 46 is made integral in rotation with the wafer 71. For this purpose, as shown in FIGS. Figures 4a , 6 , 7a-7c the wall 58 has openings 74 intended to receive studs 75 coming from the plates 71. In this case, each plate 71 comprises three studs 75 positioned on the same circumference between the inner periphery and the outer periphery of the elastic element. These studs 75 are intended to cooperate with two sets of three diametrically opposed openings 75 formed in the transverse wall 58 of the ring 46 (cf. figure 5 ). In addition to or in substitution for this connection system, the transverse wall 58 is fixed by gluing to the wafer 71.

Le dƩmarreur 10 comporte en outre un dispositif 80 d'absorption des chocs par compression sollicitƩ lorsque la couronne 46 dƩpasse un seuil K1 de dƩplacement angulaire. Le seuil K1 de dƩplacement angulaire est compris entre 15 et 25 degrƩs et est de prƩfƩrence de l'ordre de 23 degrƩs.The starter 10 further comprises a compression damping device 80 biased when the ring 46 exceeds a threshold K1 angular displacement. The threshold K1 of angular displacement is between 15 and 25 degrees and is preferably of the order of 23 degrees.

A cet effet, le dispositif 80 comporte deux amortisseurs 81 solidaires en rotation de la plaque de support 62 utilisƩs en combinaison avec deux ƩlƩments compresseur 82 solidaires en rotation avec la couronne 46. A l'Ʃtat repos, chaque ƩlƩment compresseur 82 est espacƩ angulairement par rapport Ơ l'amortisseur 81 d'un angle C Ʃgal au seuil K1 de dƩplacement angulaire (cf figure 7a). Chaque ƩlƩment compresseur 82 est ainsi destinƩ Ơ venir en appui contre l'amortisseur 82 lorsque le dƩplacement angulaire de la couronne 46 dƩpasse le seuil K1. De prƩfƩrence, une partie de chaque amortisseur 82 est insƩrƩe Ơ l'intƩrieur d'une cage de rƩception 84 rigide situƩe du cƓtƩ opposƩ Ơ l'ƩlƩment compresseur 82 qui lui est associƩ. La cage 84 forme ainsi une butƩe, de sorte que lorsqu'un ƩlƩment compresseur 82 agit sur un amortisseur 81, ce dernier est compressƩ entre la cage 84 et l'ƩlƩment compresseur 82.For this purpose, the device 80 comprises two dampers 81 integral in rotation with the support plate 62 used in combination with two compressor elements 82 integral in rotation with the ring 46. In the idle state, each compressor element 82 is spaced angularly by relative to the damper 81 of an angle C equal to the threshold K1 of angular displacement (cf. figure 7a ). Each compressor element 82 is thus intended to bear against the damper 82 when the angular displacement of the ring 46 exceeds the threshold K1. Preferably, a portion of each damper 82 is inserted inside a rigid receiving cage 84 located on the opposite side to the compressor element 82 associated therewith. The cage 84 thus forms a stop, so that when a compressor element 82 acts on a damper 81, the latter is compressed between the cage 84 and the compressor element 82.

En l'occurrence, les amortisseurs 81 sont diamĆ©tralement opposĆ©s l'un par rapport Ć  l'autre et prĆ©sentent une forme de portion d'anneau. Comme montrĆ© sur la figure 4a, les portions d'anneau s'Ć©tendent sur un angle D au moins deux fois infĆ©rieur Ć  l'angle A sur lequel s'Ć©tendent les Ć©lĆ©ments Ć©lastiques 69. Les rayons interne et externe dĆ©limitant respectivement la pĆ©riphĆ©rie interne et externe des amortisseur 81 sont sensiblement identiques Ć  ceux R1, R3 des Ć©lĆ©ments Ć©lastiques 69. Chaque amortisseur 81 comporte des angles biseautĆ©s du cĆ“tĆ© de l'Ć©lĆ©ment compresseur 82. Le biseau est effectuĆ© sur un angle E reprĆ©sentĆ© sur la figure 7a valant par exemple 10 degrĆ©s. Chaque amortisseur 81 est positionnĆ© entre deux extrĆ©mitĆ©s des Ć©lĆ©ments Ć©lastiques 69 en regard l'une de l'autre. Les amortisseurs 81 sont fixĆ©s Ć  la plaque de support 62 au moyen de pattes non reprĆ©sentĆ©es issues de la plaque de support 62 pĆ©nĆ©trant dans les amortisseurs 81. Les amortisseurs 81 sont par exemple rĆ©alisĆ©s en matĆ©riau thermoplastique Ć©lastomĆØre.In this case, the dampers 81 are diametrically opposite one another and have a ring portion shape. As shown on the figure 4a , the ring portions extend over an angle D at least two times smaller than the angle A on which the elastic elements 69 extend. The inner and outer radii delimiting respectively the inner and outer periphery of the dampers 81 are substantially identical to those R1, R3 of the elastic elements 69. Each damper 81 has bevelled angles on the side of the compressor element 82. The bevel is made on an angle E shown on the figure 7a worth, for example, 10 degrees. Each damper 81 is positioned between two ends of the elastic elements 69 facing one another. The dampers 81 are fixed to the support plate 62 by means of tabs shown from the support plate 62 penetrating the dampers 81. The dampers 81 are for example made of elastomeric thermoplastic material.

Les Ć©lĆ©ments compresseur 82 prennent par exemple la forme de nervures venant de matiĆØre avec la plaque de support 62. Ces nervures de forme sensiblement parallĆ©lĆ©pipĆ©dique prĆ©sentent une section trapĆ©zoĆÆdale.The compressor elements 82 take for example the form of ribs coming from material with the support plate 62. These ribs of substantially parallelepiped shape have a trapezoidal section.

Les ƩlƩments Ʃlastiques 69, les amortisseurs 81 ainsi que les ƩlƩments compresseurs 82 ont une hauteur L sensiblement identique, comme cela ressort clairement des figures 3a, 3b, et 4a.The elastic elements 69, the dampers 81 and the compressor elements 82 have a substantially identical height L, as clearly Figures 3a, 3b , and 4a .

On dĆ©crit ci-aprĆØs, en rĆ©fĆ©rence avec les figures 7a Ć  7c, le fonctionnement du systĆØme d'absorption des chocs selon l'invention. Ces figures montrent les Ć©tats d'un seul des Ć©lĆ©ments Ć©lastiques 69 et d'un seul des amortisseurs 81 mais il est clair que l'autre Ć©lĆ©ment Ć©lastique 69 et l'autre amortisseur 81 non reprĆ©sentĆ©s prĆ©sentent des Ć©tats correspondants. Il est Ć  noter Ć©galement que sur ces figures l'Ć©lĆ©ment compresseur 82 est liĆ© en rotation avec la paroi transversale 58 de la couronne 46 qui n'a pas Ć©tĆ© reprĆ©sentĆ©e par souci de clartĆ©. La reprĆ©sentation de la plaque de support 62 est Ć©galement simplifiĆ©e.Hereinafter described with reference to the Figures 7a to 7c , the operation of the shock absorption system according to the invention. These figures show the states of only one of the elastic elements 69 and only one of the dampers 81 but it is clear that the other elastic element 69 and the other damping 81 not shown have corresponding states. It should also be noted that in these figures the compressor element 82 is connected in rotation with the transverse wall 58 of the ring 46 which has not been shown for the sake of clarity. The representation of the support plate 62 is also simplified.

Comme montrƩ sur la figure 7a, lorsque la couronne 46 ne subit pas de choc lors du dƩmarrage du moteur thermique et demeure donc immobile, ce qui correspond Ơ un Ʃtat repos, les ƩlƩments Ʃlastiques 69 ne sont pas cisaillƩs par un dƩplacement de la couronne 46 tandis que l'amortisseur 81 n'est pas contraint par l'ƩlƩment compresseur 82.As shown on the figure 7a when the ring 46 does not undergo a shock when starting the engine and therefore remains stationary, which corresponds to a state of rest, the elastic elements 69 are not sheared by a displacement of the ring 46 while the damper 81 is not constrained by the compressor element 82.

Comme montrĆ© sur la figure 7b, en cas de chocs subis par la couronne 46, cette derniĆØre tourne suivant la flĆØche F autour de l'axe X par rapport au carter du dĆ©marreur, ce qui a pour effet de dĆ©placer suivant une direction tangentielle Dt la plaquette 71, et donc la face 72 de l'Ć©lĆ©ment Ć©lastique 69, tandis que la face 70 de l'Ć©lĆ©ment Ć©lastique 69 reliĆ©e Ć  la plaque de support 62 demeure immobile. On note que la direction tangentielle Dt de dĆ©placement de chaque point de la plaquette 71 (et de la face 72) correspond Ć  une direction perpendiculaire Ć  un rayon Ri passant par l'axe X de la plaque 62 et chaque point de la plaquette 71, cette direction Dt se trouvant dans un plan parallĆØle Ć  la face 70 fixĆ©e Ć  la plaque de support 62. Un tel dĆ©placement des deux faces 70, 72 de l'Ć©lĆ©ment Ć©lastique 69 l'une par rapport Ć  l'autre crĆ©e un effet de cisaillement permettant d'absorber les chocs de maniĆØre linĆ©aire comme cela est reprĆ©sentĆ© sur la figure 8 par la partie de la courbe rĆ©fĆ©rencĆ©e P1. Tant que le dĆ©placement angulaire de la couronne 46 reste infĆ©rieur au seuil de dĆ©placement angulaire K1, le dispositif 80 n'est pas sollicitĆ© et ne participe donc pas Ć  l'absorption des chocs dans la mesure oĆ¹ l'Ć©lĆ©ment compresseur 82 n'entre pas en appui contre l'amortisseur 81.As shown on the figure 7b , in the event of shocks to the ring 46, the latter rotates along the arrow F about the X axis relative to the starter housing, which has the effect of moving in a tangential direction Dt the wafer 71, and therefore the face 72 of the elastic member 69, while the face 70 of the elastic member 69 connected to the support plate 62 remains stationary. Note that the tangential direction Dt of displacement of each point of the wafer 71 (and of the face 72) corresponds to a direction perpendicular to a radius R1 passing through the axis X of the plate 62 and each point of the wafer 71, this direction Dt itself located in a plane parallel to the face 70 fixed to the support plate 62. Such a displacement of the two faces 70, 72 of the elastic element 69 relative to each other creates a shearing effect to absorb shocks in a linear fashion as shown on the figure 8 by the part of the curve referenced P1. As long as the angular displacement of the ring 46 remains below the angular displacement threshold K1, the device 80 is not stressed and therefore does not participate in the absorption of the shocks to the extent that the compressor element 82 does not enter. in support against the shock absorber 81.

Comme cela est reprƩsentƩ sur la figure 7c, lorsque le dƩplacement angulaire de la couronne 46 dƩpasse le seuil K1, l'ƩlƩment compresseur 82 qui s'est dƩplacƩ librement jusqu'Ơ l'amortisseur 81 commence Ơ comprimer l'amortisseur 81 qui est pris en sandwich, c'est-Ơ-dire coincƩ, entre la cage de rƩception 84 formant butƩe et l'ƩlƩment compresseur 82. Pendant ce temps, l'ƩlƩment Ʃlastique 69 continue de se dƩformer par cisaillement. Le couple absorbƩ Ʃvolue alors de faƧon exponentielle comme cela est reprƩsentƩ sur la figure 8 par la partie de la courbe rƩfƩrencƩe P2. Le dispositif 80 d'absorption des chocs par compression permet ainsi de limiter la contrainte imposƩe aux ƩlƩments Ʃlastiques 69 lors de leur cisaillement.As shown on the Figure 7c when the angular displacement of the ring 46 exceeds the threshold K1, the compressor element 82 which has moved freely to the damper 81 begins to compress the damper 81 which is sandwiched, that is to say stuck between the receiving cage 84 forming a stop and the compressor element 82. During this time, the elastic element 69 continues to deform by shearing. The absorbed torque then evolves exponentially as shown on the figure 8 by the part of the curve referenced P2. The device 80 for compressive shock absorption thus makes it possible to limit the stress imposed on the elastic elements 69 during their shearing.

Bien entendu, l'homme du mĆ©tier pourra modifier la structure des dispositifs d'absorption des chocs 61 et 80 prĆ©cĆ©demment dĆ©crits sans sortir du cadre de l'invention. Ainsi, de maniĆØre Ć©quivalente, les amortisseurs 81 pourront ĆŖtre rendus solidaires en rotation de la paroi transversale 58 de la couronne 46, tandis que les Ć©lĆ©ments compresseur 82 sont rendus solidaires en rotation de la plaque de support 62. Bien entendu, le nombre d'Ć©lĆ©ments Ć©lastiques 69 pourra ĆŖtre supĆ©rieur ou infĆ©rieur Ć  deux et dans tous les cas au moins Ć©gal Ć  un. Cela dĆ©pend de l'application. Il en est de mĆŖme pour le nombre d'amortisseurs 81 du dispositif 80 qui pourra varier en fonction de l'application. En variante, le dĆ©marreur pourrait Ć©galement comporter uniquement un dispositif 80 d'absorption des chocs par cisaillement et ĆŖtre dĆ©pourvu de dispositif 61 d'absorption des chocs par compression.Of course, those skilled in the art can modify the structure of the shock absorbing devices 61 and 80 previously described without departing from the scope of the invention. Thus, in an equivalent manner, the dampers 81 may be made integral in rotation with the transverse wall 58 of the ring 46, while the compressor elements 82 are made integral in rotation with the support plate 62. Of course, the number of elastic elements 69 may be greater than or less than two and in all cases at least one. It depends on the application. It is the same for the number of dampers 81 of the device 80 which may vary depending on the application. Alternatively, the starter could also comprise only a shear absorbing device 80 and be devoid of device 61 for compressive shock absorption.

Claims (15)

  1. A starter (10) for a combustion engine of an automotive vehicle comprising:
    - an electric motor (11) comprising a shaft (24),
    - an output shaft (43), on which a drive pinion (50) is mounted which is intended to engage with a starting ring gear of the combustion engine,
    - a reduction gear unit (45) having a ring gear (46), the reduction gear unit being installed between the shaft (24) of the electric motor and the output shaft (43) in order to connect the shaft of the electric motor to the output shaft in a rotational manner,
    - a casing (16),
    - at least one shock absorber (61) installed between the ring gear (46) and the casing (16) connecting the ring gear to the casing in a rotational manner, characterised in that the shock absorber is capable of absorbing by shear shocks experienced by the ring gear (46) during a start-up of the combustion engine giving rise to a relative angular displacement of the ring gear (46) with respect to the casing (16) of the starter.
  2. The starter according to claim 1, characterised in that the shear shock absorber (61) comprises:
    - a support plate (62) connected in a rotationally fixed manner to the casing, and
    - at least one elastic element (69) having a first face (70) connected in a rotationally fixed manner to the support plate (62) and a second face (72) opposite the first face (70) connected in a rotationally fixed manner to the ring gear (46) capable of rotating with respect to the casing in the event of shocks experienced by the ring gear (46).
  3. The starter according to claim 2, characterised in that the shear shock absorber (61) further comprises an attached plate (71) connected fixedly to the second face (72) of the elastic element (69), this plate being mounted in a rotationally fixed manner with the side wall (58) of the ring gear.
  4. The starter according to claim 3, characterised in that the attached plate (71) essentially covers the whole of the surface of the second face (72) of the elastic element (69).
  5. The starter according to claim 3 or 4, characterised in that the side wall (58) of the ring gear (46) is fixed by gluing to the attached plate (71).
  6. The starter according to any one of claims 3 to 5, characterised in that the side wall (58) of the ring gear (46) comprises openings intended to receive studs (75) emerging from the attached plate (71).
  7. The starter according to any one of claims 2 to 6, characterised in that the first (70) and the second face (72) of the elastic element (69) are inclined with respect to one another.
  8. The starter according to any one of claims 1 to 7, characterised in that it also comprises a compression shock absorber (80) mounted between the ring gear and the support plate in a manner such as to be stressed only when the ring gear (46) exceeds an angular displacement threshold (K1) in such a way as to limit the stress experienced by the shear shock absorber (61).
  9. The starter according to claim 8, characterised in that the angular displacement threshold (K1) is between 15 and 25 degrees.
  10. The starter according to claims 2 and 8 or 9, characterised in that the compression shock absorber (80) comprises at least one damper (81) connected in a rotationally fixed manner to one of the elements among the side wall (58) of the ring gear (46) and the support plate (62) as well as at least one corresponding compressor element (82) connected in a rotationally fixed manner to the other element intended to come to rest against the damper (81) during the angular displacement of the ring gear (46) beyond the angular displacement threshold (K1).
  11. The starter according to claim 10, characterised in that the damper (81) is connected in a rotationally fixed manner to the support plate (62) whilst the compressor element (82) belongs to the side wall (58) of the ring gear (46).
  12. The starter according to claim 10 or 11, characterised in that a part of the damper (81) is inserted into a rigid receiving cage (84) located at the opposite side with respect to the compressor element (82) forming a stop.
  13. The starter according to any one of claims 10 to 12, characterised in that the damper (81) has bevelled angles on the side facing the compressor element (82).
  14. The starter according to any one of claims 1 to 13, characterised in that the shear shock absorber (61) comprises two diametrically opposed elastic elements (69) having a shape of a ring portion.
  15. The starter according to claims 10 and 14, characterised in that the compression shock absorber (80) comprises two dampers (81) each located between two ends of the elastic elements (69) opposite one another and two compressor elements (82) each located between an elastic element (69) and a damper (81).
EP13801642.3A 2012-11-08 2013-11-08 Heat engine starter provided with a device for shock absorption by shearing Not-in-force EP2917558B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1260590A FR2997732A1 (en) 2012-11-08 2012-11-08 THERMAL MOTOR STARTER PROVIDED WITH SHEAR ABSORPTION DEVICE
PCT/FR2013/052675 WO2014072651A2 (en) 2012-11-08 2013-11-08 Heat engine starter provided with a device for shock absorption by shearing

Publications (2)

Publication Number Publication Date
EP2917558A2 EP2917558A2 (en) 2015-09-16
EP2917558B1 true EP2917558B1 (en) 2019-03-27

Family

ID=47598959

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13801642.3A Not-in-force EP2917558B1 (en) 2012-11-08 2013-11-08 Heat engine starter provided with a device for shock absorption by shearing

Country Status (3)

Country Link
EP (1) EP2917558B1 (en)
FR (1) FR2997732A1 (en)
WO (1) WO2014072651A2 (en)

Family Cites Families (12)

* Cited by examiner, ā€  Cited by third party
Publication number Priority date Publication date Assignee Title
DE2822165A1 (en) 1978-05-20 1979-11-22 Bosch Gmbh Robert Starter motor drive actuator for IC engine - has plastics engagement lever pinned to solenoid armature for engaging motor pinion
FR2611096B1 (en) 1987-02-17 1989-05-12 Equip Electr Moteur CARCASS OF ROTATING ELECTRIC MACHINE
AU611275B2 (en) 1988-05-26 1991-06-06 International Business Machines Corporation Apparatus and method for accessing data stored in a page mode memory
FR2735294B1 (en) 1995-06-12 1997-07-18 Valeo Equip Electr Moteur STARTER OF A MOTOR VEHICLE PROVIDED WITH A REDUCED THICKNESS INDUCING COIL.
FR2745855B1 (en) 1996-03-08 1998-04-10 Valeo Equip Electr Moteur STARTER OF A MOTOR VEHICLE COMPRISING IMPROVED THRUST MEANS FOR ITS TRAINER
FR2772433B1 (en) 1997-12-17 2000-02-04 Valeo Equip Electr Moteur MOTOR VEHICLE STARTER COMPRISING AN IMPROVED LAUNCHER
FR2787833B1 (en) 1998-12-23 2001-03-02 Valeo Equip Electr Moteur STARTER OF A MOTOR VEHICLE WITH GEAR REDUCER COMPRISING TORSION SHOCK ABSORBER MEANS
FR2800422B1 (en) 1999-10-29 2001-11-30 Valeo Equip Electr Moteur STARTER EQUIPPED WITH AN IMPROVED LEVER SUPPORT PART
US6993989B2 (en) * 2002-04-26 2006-02-07 Denso Corporation Starting apparatus
JP4135524B2 (en) * 2003-02-19 2008-08-20 ę Ŗ式会ē¤¾ćƒ‡ćƒ³ć‚½ćƒ¼ Starter
JP4111017B2 (en) * 2003-03-13 2008-07-02 ę Ŗ式会ē¤¾ćƒ‡ćƒ³ć‚½ćƒ¼ Starter
DE602004013827D1 (en) 2003-11-28 2008-06-26 Valeo Equip Electr Moteur A CYLINDER HEAD AND SUBSTITUTING CENTER ON THE BODY COMPRISING A COMBUSTION ENGINE STARTER

Non-Patent Citations (1)

* Cited by examiner, ā€  Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP2917558A2 (en) 2015-09-16
WO2014072651A2 (en) 2014-05-15
FR2997732A1 (en) 2014-05-09
WO2014072651A3 (en) 2014-07-17

Similar Documents

Publication Publication Date Title
EP2655863B1 (en) Electric motor and internal combustion engine starter speed reducer
WO2013171432A1 (en) Starter motor provided with a translatably fixed free wheel
EP1769154B1 (en) Starter motor, particularly for a motor vehicle, provided with a friction free-wheel starter
WO2011114052A2 (en) Combustion engine starter with output pinion
WO2014068255A1 (en) Friction starter drive unit for meshing with a starter ring gear of a heat engine, and corresponding heat engine starter
WO2017178759A1 (en) Motor vehicle heat engine starter with a self-centring reduction gear ring
EP2917558B1 (en) Heat engine starter provided with a device for shock absorption by shearing
EP2984330A1 (en) Improved pignon cage assembly, corresponding starter drive assembly and starter for a motor vehicle
FR2993320A1 (en) Starter for thermal engine of car, has elastic ring installed between toothed crown and support, and intended to be axially compressed and deformed to absorb shocks, where cover exerts axial pressure on elastic ring
EP3443217B1 (en) Starter for combustion engine of motor vehicle provided with shape-optimized shock absorbing elements
EP2890889B1 (en) Starter provided with a ring gear axially connected to an elastic shock-absorbing element
WO2014170598A1 (en) Ring gear provided with an insert for a speed reducer of a heat engine starter and corresponding speed reducer assembly
FR2827341A1 (en) Automobile starter motor, spigot once meshed with engine crown wheel is stopped from rotating, by a friction, cooperating shape or toothed blocking system
FR3004497A1 (en) LAUNCHER STARTER WITH AN INTERMEDIATE FRICTION REDUCTION ELEMENT BETWEEN A CONTROL LEVER AND A TRAINER
EP1778970A1 (en) Starter, in particular for motor vehicle, equipped with a friction-driven free-wheel drive assembly
WO2006000667A1 (en) Starter provided with a friction freewheel drive
FR2878908A1 (en) IC engine starting device for e.g. motor vehicle, has epicycloidal speed reducing gear train that comprises rotation axles connected to pulley, and planet gears mounted in freely rotating manner on pulley constituting planet carriers
FR3003307A1 (en) STARTER STARTER HAVING A FRICTION CLUTCH WITH DOUBLE CONTROL LEVERS
EP2865882A1 (en) Starter drive assembly with improved friction clutch and corresponding starter for the heat engine of a motor vehicle
FR2881798A1 (en) Internal combustion engine e.g. heat engine, starting device for e.g. private vehicle, has overrunning clutch integrated in central hole of pulley and axially fixed, where clutch has driver engaged with pulley in continuous manner
FR2894089A1 (en) Electrical rotating machine e.g. internal combustion engine starter, for motor vehicle, has cylinder head comprising external part with length shorter than that of internal part for increasing external thickness of cylinder head
FR3078552A1 (en) MOTOR VEHICLE THERMAL MOTOR STARTER WITH CONFIGURED REDUCER CROWN FOR SHOCK ABSORBING
EP1669592A1 (en) Starter apparatus for an internal combustion engine

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20150520

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
RIN1 Information on inventor provided before grant (corrected)

Inventor name: SEILLIER, GUILLAUME

Inventor name: SODDEMANN, MATTHIAS

Inventor name: FURRER, SIMON

Inventor name: MORNIEUX, CHRISTIAN

Inventor name: BALEYDIER, BENOIT

Inventor name: HABERLAND, NORBERT

Inventor name: PRIOUX, ENGUERRAND

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20180717

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1113390

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190415

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602013053023

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190627

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190628

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190627

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1113390

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190727

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190727

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602013053023

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

26N No opposition filed

Effective date: 20200103

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191130

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191108

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191130

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20191130

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20191108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191108

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20131108

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20211122

Year of fee payment: 9

Ref country code: FR

Payment date: 20211119

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190327

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602013053023

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230601

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130