Classifications

• • H—ELECTRICITY
  • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
  • H02K—DYNAMO-ELECTRIC MACHINES
  • H02K49/00—Dynamo-electric clutches; Dynamo-electric brakes
  • H02K49/02—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type
  • H02K49/04—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type
  • H02K49/043—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type with a radial airgap

Definitions

• the present invention relates to an eddy current retarder for a vehicle, intended to slow down the rotation of a driven shaft around its axis.
• the invention relates more particularly to those which are intended to slow down the rotation of a motor shaft driven around its axis, in particular of the crankshaft of a vehicle engine, this engine comprising a casing which itself comprises a front wall extending substantially in a plane perpendicular to the axis of the motor shaft, which motor shaft has one end which is oriented towards the front wall of the motor housing and at which the retarder is mounted door-to-door -false on the front wall of the motor housing by means of connection, the retarder comprising a rotor part integral in coaxial rotation with the motor shaft, a stator part coaxial with the motor shaft and integral with the front wall of the housing of the motor, an armature belonging to the rotor part, and an inductor belonging to the stator part, the inductor being arranged on a fixed annular part of the stator part, in r with regard to the armature.
• the document JP9201037 describes an eddy current retarder which is of the type mentioned above.
• Such a retarder has the advantage of having a simplified structure, as well as a reduced weight and dimensions, given its geometry with a ferromagnetic central disc integral in rotation with the crankshaft and rotatable between two discs which support constituted excitation means permanent magnets projecting axially towards the central disc, one of the two permanent magnet discs can also be rotated by a servomotor.
• this retarder does not completely cancel the magnetic flux, and in particular the magnetic flux tangent to the discs, which remains very important.
• This retarder lies in the fact that it is disposed between the engine and a pulley for driving the distribution and accessories, located at the outlet of the crankshaft.
• the pulley thus spaced from the engine, will generate a significant overhang of the drive belt of the annexed members of the engine, which usually surrounds this pulley, such an overhang imposing a displacement of all the accessories, and therefore a similar overhang of said auxiliary members to avoid causing, in the long run, the rupture of this belt surrounding the pulley.
• the present invention aims in particular to remedy these drawbacks.
• the rotor part of the retarder according to the invention has symmetry of revolution about the axis of the motor shaft so as to have a peripheral face opposite a peripheral face of the stator part, the inductor the retarder being provided with at least one electromagnet winding.
• the eddy current retarder retains a compact structure, while allowing simple and easy control of its magnetic flux thanks to the presence of electromagnets.
• one and / or the other of the following arrangements are used:
• the rotor part comprises an external part of substantially cylindrical shape which surrounds the stator part and which constitutes the armature of the retarder, said external part comprising a radial flange fixed to the motor shaft, said flange being pierced with a plurality of holes ;
• the retarder inductor is an inductor with poles each surrounded by an inductor winding and projecting radially outwards on the external face of said annular part of the stator part;
• the poles are integral with a first ring, while all of the inductor windings constitute a second ring of larger diameter than that of the first ring, said second ring being assembled coaxially to said first ring by fitting each pole into a respective inductor winding;
• the retarder inductor is a claw inductor and with a single inductor winding; a first set of claws constitutes a first ring and a second set of claws constitutes a second ring of the same diameter as that of the first ring, said inductor winding surrounding a cylindrical piece of smaller diameter than that of the first and second rings, these the latter being assembled coaxially to said cylindrical part so that each claw of the first set of claws is interposed between two adjacent claws of the second set of claws.
• the connecting means comprise a frame which comprises at least one substantially radial flange centered on the motor shaft and pierced with a plurality of holes, said flange itself comprising arms which extend from it in engine steering for fixing the frame to the front wall of the motor housing, the electromagnetic retarder being housed in a space delimited by the flange, the fixing arms and the front wall of the engine;
• a pulley located at the outlet of the motor shaft is arranged between the motor housing and the retarder; the flange of the external part advantageously integrating the pulley, to reduce the number of parts of the assembly;
• inductor winding (s) is or are energized from an electric source of the vehicle regulated in power.
• - Figure 1 is an exploded perspective view of the eddy current retarder according to a first embodiment of the invention, before its mounting on the motor housing;
• - Figure 2 is a cross-sectional view of the retarder of Figure 1, after assembly of its rotor and its stator;
• - Figure 3 is a perspective view of the retarder of Figure 1, representing the latter in the mounted position on the motor housing;
• a first embodiment of the eddy current retarder 1 comprises an induced rotor 2 which rotates with a shaft driven in rotation about a substantially horizontal axis X, this shaft being constituted in particular by the crankshaft (not shown) of a vehicle engine M.
• This engine comprises a casing 3 which itself comprises a front wall 3a extending substantially in a plane perpendicular to the axis X of the crankshaft.
• the eddy current retarder 1 further comprises an inductor stator 4 comprising electromagnetic windings 5 which are constituted respectively by coils.
• the aforementioned retarder 1 is intended to be disposed at the outlet of the crankshaft, on the side of the pulley 6, therefore on the side opposite to the outlet of the engine shaft connected to the gearbox, said retarder being mounted in overhang on the front wall 3a of the casing 3 of the motor M as shown in FIG. 3.
• the pulley 6, which is conventionally located in crankshaft outlet and which is intended to be surrounded by a belt 7 suitable for driving the annexed members of the engine, such as in particular the camshafts 8 and the alternator 9, as well as the water pump, is interposed between the retarder 1 and the front wall 3a of the casing 3 of the motor M so as to eliminate any problem of alignment of the belt 7 and of the members which it drives.
• This solution thus proves to be much more compact than that adopted in the prior art described above since it does not oblige to compensate the overhang of the pulley and of the belt by a cantilever. of the organs it drives.
• the rotor 2 comprises an outer part which is substantially cylindrical of revolution around the axis X, and which has a circular section. This part is hollow so as to surround the stator 4. It has an envelope 10, and a bottom 11 forming flange, the assembly being made of ferromagnetic material, generally steel, and provided, on the outside of the casing 10, with ribs 12, for example helical, made of material with the casing 10, which are intended to make function of radiator fins to cool the rotor 2 heated by eddy currents.
• These ribs 12 are also capable, by means of a suitable profile, of making the rotor 2 play a role of fan by sweeping with a stream of cooling air the hot surfaces to be cooled of the rotor 2, when the retarder is in service.
• the rotor 2 is arranged coaxially to the axis X of the crankshaft, the flange 11 being fixed to the crankshaft by means of an axial screw which passes through the flange 11 and is fixed in the opposite end of the crankshaft.
• the flange 11 has a peripheral edge which is pierced with a plurality of holes 13, for example circular, the usefulness of which will be seen later in the description.
• the flange 11 can integrate the pulley 6, these two elements then being produced in one piece with the rest of the induced rotor 2.
• the stator 4 has two rings 14 and 15 which each have a substantially annular shape.
• Polar cores 16 protrude from the outer peripheral surface of the ring 14, in a radial direction relative to the latter.
• Said polar cores which are twelve in number in the example shown, but the number of which may be any, are regularly distributed around the ring 14, each polar core extending parallel to the axis X of the crankshaft.
• the crown 15 is in turn constituted by a succession of twelve electromagnetic coils 5 close to each other so as to substantially define a circle centered on the axis X of the crankshaft.
• the crown 15 has a diameter slightly greater than that of the crown 14 so as to be assembled coaxially with the crown 14 by fitting each pole core 16 into a respective coil 5.
• the different electromagnetic coils 5 are connected to a source of direct electric current, such as, preferably, the battery (not shown) of the vehicle, through appropriate control and adjustment members (not shown).
• a source of direct electric current such as, preferably, the battery (not shown) of the vehicle
• the electromagnetic coils 5 are traversed by an electric current and generate eddy currents in the rotor 2 which then passes in front of the polar cores 16 alternately positive and negative. This results in a slowing torque of the crankshaft and a heating of the rotor 2 which is partially compensated for by the ventilation by the ribs 12.
• Such an assembly of the stator 4 therefore advantageously makes it possible to control the magnetic flux in a simpler and faster manner than in the retarder described in the prior art mentioned above. It is thus possible to completely cancel this flow by extinguishing the current delivered by the battery.
• the inductor stator assembly constituted by the assembly of the two crowns 14 and 15 has a diameter and an axial length slightly less than those of the rotor 2, so that during the mounting of the retarder 1, this assembly is introduced into the external part of the rotor 2, a thin air gap E (for example from 1 to 3 mm) being left free between the internal surface of the casing 10 of the rotor 2 and the corresponding polar cores 16 of the ring 14 of the stator 4.
• a thin air gap E for example from 1 to 3 mm
• the crown 14 of the stator 4 is provided, on its inner periphery, with bosses 17 which extend selorr ⁇ direction of the axis X of the crankshaft.
• bosses 17 which extend selorr ⁇ direction of the axis X of the crankshaft.
• these bosses are six in number and are arranged in the extension of a first, third, fifth, seventh, ninth and eleventh polar core 16 successive.
• the bosses 17 are each pierced with an axial threaded bore 18, which is intended to receive a screw (not shown) for fixing the crown 14 of the stator 4 to a frame 19.
• This frame is itself intended to be fixed to the front wall 3a of the casing 3 of the vehicle engine M, as shown in FIG. 3.
• the frame 19 is a rigid part which can be produced for example from an alloy of cast iron and aluminum.
• This part comprises a flange 20 which has a substantially annular shape and which is arranged in a substantially radial plane, coaxial with the axis X of the crankshaft.
• the flange 20 has a central opening 21 for its lightening. It further comprises a peripheral part 22 which is pierced with a plurality of holes 23, for example rectangular, the usefulness of which will be seen later in the description.
• the frame 19 also includes arms 24 which each extend substantially in the direction of the axis X of the crankshaft, from the outer edge of the peripheral part 22 of the flange 20.
• Each arm 24 has a base 25 pierced with a hole 26 which is adapted to receive a screw (not shown) so as to be able to fix the frame 19 on the front wall 3a of the casing 3 of the motor M, as shown in FIG. 3.
• the arms 24 are three in number and are distributed at regular intervals of 120 ° around the flange 20.
• the internal edge of the peripheral part 22 of the flange 20 is in turn provided with fixing parts 27 which each have a tapped hole. These fixing parts 27 are six in number and are distributed at regular intervals around said internal edge.
• the flange 20 has an external diameter slightly greater than that of the casing 10 of the rotor 2 and, on the other hand, the fixing arms 24 have a length slightly greater than the axial length of the rotor 2, so that in the position mounted on the front wall 3a of the casing 3 of the motor M, the retarder 1 is housed entirely between the flange 20 of the frame 19, the arms 24 of the latter and the front wall 3a of the casing 3 of the motor M, as can be seen in FIG. 3.
• the rotor 2 has the advantage, given its conformation and its arrangement , to be able to play the role of a flywheel complementing the flywheel 28 as shown in Figure 3, which is disposed against the rear wall 3b of the casing 3 of the motor M.
• This assembly also has the advantage of being particularly light, not only because of the hollow cylindrical geometry of the assembly constituted by the frame 19 and the retarder 1, but also because of the presence of the holes 13 and 23 respectively. made in the flange 11 of the rotor 2 and in the flange 20 of the frame 19. It should be noted that the holes 13 and 23 also have the function of allowing the circulation of cooling air in the direction of the stator 4 so as to reduce the heating of the electromagnetic coils 5. In addition, the set of holes 13 forms a thermal barrier which prevents the heat energy dissipated by the retarder 1 from propagating by conduction in the direction of the pulley 6.
• the retarder 1 comprises, like the first embodiment described above, a rotor 2 which is identical in all points to the rotor shown in FIGS. 1 and 2, and which, for this reason, n is neither described in detail nor shown.
• the retarder 1 of Figure 4 differs from that of Figures 1 and 2 only by the fact that it comprises a stator 4 'in three parts instead of two.
• this stator 4 ′ comprises a substantially cylindrical part 4 ′ a of revolution around the axis X and of circular section.
• the cylindrical part 4 'a has an envelope surrounded by a conductive wire 5' which is wound so as to form several successive turns 5 'a of circular section. In a manner known as such, all of these turns of wire 5'a constitutes the inductor winding of the retarder 1.
• the turns 5'a wound around the cylindrical part 4'a are connected to a source of direct electric current, such as, preferably, the vehicle battery (not shown).
• the stator 4 'further comprises two rings 14' and 15 'which each have a substantially annular shape. These rings are identical in all respects and consist respectively of a radial flange 14 'a, 15' pierced with a central coaxial hole 29 and a succession of claws 14'b, 15'b which have, in the 'example shown, a substantially triangular shape.
• the claws 14'b and 15'b are distributed at regular intervals around their respective crowns, each claw 14'b, 15'bs' extending along an axis parallel to the axis X of the crankshaft, from the peripheral edge of the flange 14'a, 15'a associated with it.
• the rings 14 'and 15' have a diameter slightly greater than that of the cylindrical part 4'a so as to be assembled on the latter, said crowns 14 'and 15' then being arranged coaxially with the cylindrical part 4'a.
• the axial length of the rings 14 ′ and 15 ′ is determined in such a way that they together substantially completely surround the cylindrical part 4 ′ a, each claw 14 ′ b of the crown 14 ′ being interposed between two adjacent claws 15 ′ b of the crown 15 '.
• the assembly constituted by the assembly of the two rings 14 ′ and 15 ′ on the cylindrical part 4 'a has a diameter and an axial length slightly smaller than that of the rotor 2, so that when mounting the retarder, this assembly is completely introduced into the external part of the rotor 2, a thin air gap (for example 1 3 mm) being left free between the internal surface of the casing 10 of the rotor 2 and the corresponding claws 14'b and 15'b of the stator 4 ', which thus allows the external part of the rotor 2 to pass in front of the claws 14'b and 15'b of the stator 4 '.
• a thin air gap for example 1 3 mm
• the operating principle of the retarder equipped with the stator 4 ' is similar to that of the retarder according to the first embodiment described above. That is to say that when the retarder according to the second embodiment is energized, all of the turns 5 ′ a is traversed by an electric current and generates eddy currents in the rotor 2 which then passes before the claws 14 'b and 15'b of stator 4', alternately positive and negative. This results in a slowing torque of the crankshaft.
• stator 4 In a similar manner to stator 4 as illustrated in FIG. 1, the crown 14 'of the stator 4' is pierced with peripheral holes 18 'which are intended to each receive a screw (not shown) in order to be able to fix said crown 14 'on frame 19.

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• Engineering & Computer Science (AREA)
• Power Engineering (AREA)
• Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)
• Lubricants (AREA)

Applications Claiming Priority (3)

Publications (1)

Family

ID=9553620

Family Applications (1)

Country Status (5)

Families Citing this family (12)

Family Cites Families (10)

• 1999
  • 1999-12-22 FR FR9916241A patent/FR2803134B1/fr not_active Expired - Fee Related
• 2000
  • 2000-12-20 WO PCT/FR2000/003612 patent/WO2001047093A1/fr not_active Application Discontinuation
  • 2000-12-20 JP JP2001547717A patent/JP2003518897A/ja not_active Withdrawn
  • 2000-12-20 EP EP00990080A patent/EP1155491A1/de not_active Withdrawn
  • 2000-12-20 US US09/913,694 patent/US6700265B1/en not_active Expired - Fee Related

Non-Patent Citations (1)

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