Motor vehicle starter pinion with improved acoustic performance
10900457 ยท 2021-01-26
Assignee
Inventors
Cpc classification
F16H55/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02N15/067
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02N15/062
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H55/088
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H1/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H55/17
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2055/176
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H55/0873
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02N15/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H1/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H55/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H55/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention relates mainly to an assembly comprising: a combustion engine ring gear having a plurality of teeth, the said ring gear being defined by a modulus and a pressure angle, a starter comprising a pinion (31) able to engage with the said ring gear of the said combustion engine, the said pinion (31) having a plurality of teeth (42) is defined by a modulus (Mp) and a pressure angle (alpha_p), characterized in that a pinion product which is the product of the modulus (Mp) of the said pinion (31) and the cosine of the pressure angle (alpha_p) of the said pinion (31) is greater than a ring-gear product equal to the product of the modulus of the said ring gear and the cosine of the pressure angle of the said ring gear.
Claims
1. An assembly comprising: a ring gear of a thermal engine with a plurality of teeth, the ring gear being defined by a modulus and a pressure angle; a starter comprising a pinion which can engage with the ring gear of the thermal engine, the pinion having a plurality of teeth being defined by a modulus and a pressure angle, wherein a pinion product which is the product of the modulus of the pinion and the cosine of the pressure angle of the pinion is greater than a ring gear product equal to the product of the modulus of the ring gear and the cosine of the pressure angle of the ring gear, and wherein, for a ring gear product of 2.070, the pinion product is between 2.079 and 2.084.
2. The assembly according to claim 1, wherein, for all teeth of the pinion, a thickness measured at a top of each tooth is greater by 35 to 45 micrometres than a thickness measured at a top of a tooth of a pinion which would have its pinion product equal to that of the ring gear product.
3. The assembly according to claim 1, wherein for each tooth the pinion has a thickness measured at a top of tooth of 2.012 mm plus or minus 0.036, and a thickness measured from one useful flank to another useful flank at a tooth root of 11.95 mm, plus or minus 0.11.
4. The assembly according to claim 1, wherein an input face in the ring gear, of each tooth of the pinion comprises beveling.
5. The assembly according to claim 1, wherein the pinion is of the sintered type.
6. The assembly according to claim 5, wherein the pinion has been subjected to treatment by cementation.
7. The assembly according to claim 1, wherein the pinion is obtained by cold heading.
8. An assembly comprising: a ring gear of a thermal engine with a plurality of teeth, the ring gear being defined by a modulus and a pressure angle; a starter comprising a pinion which can engage with the ring gear of the thermal engine, the pinion having a plurality of teeth being defined by a modulus and a pressure angle, wherein a pinion product which is the product of the modulus of the pinion and the cosine of the pressure angle of the pinion is greater than a ring gear product equal to the product of the modulus of the ring gear and the cosine of the pressure angle of the ring gear, and wherein, for a ring gear product of 2.387, the pinion product is between 2.401 and 2.41.
9. An assembly comprising: a ring gear of a thermal engine with a plurality of teeth, the ring gear being defined by a modulus and a pressure angle; a starter comprising a pinion which can engage with the ring gear of the thermal engine, the pinion having a plurality of teeth being defined by a modulus and a pressure angle, wherein a pinion product which is the product of the modulus of the pinion and the cosine of the pressure angle of the pinion is greater than a ring gear product equal to the product of the modulus of the ring gear and the cosine of the pressure angle of the ring gear, and wherein, for a ring gear product of 2.415, the pinion product is between 2.425 and 2.431.
Description
(1) The invention will be better understood by reading the following description and examining the figures which accompany it. These figures are provided purely by way of illustration and in no way limit the invention.
(2)
(3)
(4)
(5)
(6) Elements which are identical, similar or analogous retain the same references from one figure to another.
(7)
(8) This stator 13 comprises a yoke supporting a series of permanent magnets 15, which are designed to produce an inductor field. The permanent magnets 15 are formed according to cylindrical segments, whilst being angularly distributed at regular intervals inside the yoke.
(9) The rotor 12 comprises a rotor body 17 and a winding 18 wound in notches in the rotor body 17. The rotor body 17 consists of a set of metal plates with longitudinal notches 26. In order to form the winding 18, conductive wires in the form of a pin 21 are inserted in notches 26, generally on two distinct layers. The winding 18 forms chignons 19 on both sides of the rotor body 17.
(10) The rotor 12 is provided at the rear with a collector 22 comprising a plurality of contact parts connected electrically to the conductive elements of the winding 18, which elements are formed by the pins 21 in the example concerned.
(11) A group of brushes 23 and 24 is provided for the electrical supply to the winding 18, one of the brushes 23 being connected to the earth of the starter 10, and another one of the brushes 24 being connected to an electrical terminal 25 of a contactor 27.
(12) The brushes 23 and 24 rub on the collector 22 when the rotor 12 is rotating, thus permitting the supply to the rotor 12 by switching of the electric current in the sections of the rotor 12.
(13) In addition to the terminal 25 connected to the brush 24, the contactor 27 comprises a terminal 39, which is connected via an electrical connection element to an electrical supply of the vehicle, in particular a battery.
(14) The starter 10 also comprises a launcher assembly 29, which is fitted such as to be mobile in translation on a drive shaft 28, and can be rotated around the axis X by the rotor 12.
(15) A speed reducer 30 is interposed between a shaft of the rotor 12 and the drive shaft 28. The launcher assembly 29 comprises a drive element which is formed by a pinion 31, and is designed to be engaged on a drive unit of the thermal engine, such as a starter ring gear.
(16) The launcher assembly 29 also comprises a free wheel 32 and a washer 33, which define between one another a groove 34 for receipt of the end 35 of a control lever 37. The control lever 37 is activated by the contactor 27, in order to displace the launcher assembly 29 relative to the drive shaft 28, along the axis X, between a first position, in which the launcher assembly 29 drives the thermal engine by means of the drive pinion 31, and a second position, in which the drive pinion 31 is disengaged from the starter ring gear of the thermal engine. During the activation of the contactor 27, an inner contact plate (not represented) makes it possible to establish a connection between the terminals 25 and 39, in order to switch on the electric motor. This connection will be cut off when the contactor 27 is deactivated.
(17)
(18) As can be seen in
(19) The ring gear 45 is defined by a modulus Mc and a pressure angle alpha_c, whereas the pinion 31 is defined by a modulus Mp and a pressure angle alpha_p. The pinion product Mp*COS(alpha_p) equal to the product of the modulus of the pinion Mp and the cosine of the pressure angle of the pinion alpha_p is greater than the ring gear product Mc*COS(alpha_c) equal to the product of the modulus of the ring gear Mc and the cosine of the pressure angle of the ring gear alpha_c.
(20) For the different types of ring gear 45 possible corresponding to the standard designs, pinion products are defined which make it possible to obtain pinions 31 with positive fHalpha according to the following table.
(21) TABLE-US-00001 Ring gear design Positive fHalpha Pressure of the pinion Modulus angle Product Mp*COS(alpha_p) Mc(mm) Alpha_c() Mc*COS(alpha_c) Min Max 2.11667 12 2.070 2.079 2.084 2.54 20 2.387 2.401 2.41 2.5 15 2.415 2.425 2.431
(22) There is definition of the basic pitch of the ring gear 45 and of the corresponding pinion 31, which are equal to the product of the modulus and the pressure angle multiplied by according to the following table:
(23) TABLE-US-00002 Basic pitch - positive Ring gear design fHalpha of the pinion Pressure angle Basic pitch *Mp*COS(alfa_p).sup.2 Alpha_c() *Mc*COS(alfa_c) Min Max 12 6.504 6.531 6.547 20 7.498 7.543 7.571 15 7.586 7.618 7.637 .sup.2Translator's note: Starting from this point on the present page, the spelling alfa is used, rather than alpha as previously. The same spelling as in the original text has been used in the translation.
(24) As can be seen clearly in
(25) According to one embodiment, for each tooth, the pinion 31 has a thickness E1 of height of tooth of 2.012 mm plus or minus 0.036, and a thickness E2 measured at the junction between a tooth root and a useful flank of 11.95 mm plus or minus 0.11.
(26) As can be seen clearly in
(27) In order to obtain the form of the pinion 31 easily, the pinion 31 can be a sintered pinion obtained by compacting a powder based on iron and carbon in an appropriate mould.
(28) In addition, in order to improve its mechanical strength, the pinion 31 can be subjected to treatment by cementation. This operation consists of thermochemical treatment, i.e. it is a high-temperature heat treatment which is accompanied by modification of the chemical composition of the basic alloy by enrichment and diffusion of carbon provided by an atmosphere of the furnace which is rich in a carbon element. Since the pinion 31 to be treated is in contact with this atmosphere rich in carbon in the treatment furnace, the carbon will then enrich the surface and subsequently be diffused to a certain depth, thus creating a gradient of concentration of carbon which decreases from the surface and to a certain depth, until the initial carbon content of the alloy is obtained once more.
(29) Once this high-temperature step has been carried out, a quenching operation will then be carried out consisting of a stage of sudden cooling of the part. This will make it possible to obtain transformations of metallurgical structures and modifications of hardness in order to obtain a hardness profile which decreases in the entire cemented surface layer (from the surface and to a certain depth). Finally, the parts are not left in the untreated quenched state (otherwise they would be very fragile). The parts are subjected to a stress-relieving anneal which has a slight impact on the hardness on the surface and in its vicinity, i.e. to a depth of approximately 0.2 mm for example, but not on the remainder of the hardness profile.
(30) Alternatively, the pinion 31 is obtained by cold heading.
(31) It will be appreciated that the foregoing description has been provided purely by way of example, and does not limit the field of the invention, a departure from which would not be constituted by replacing the different elements by any other equivalents.