EP1023936A1 - Magnetic drive agitator and method for adjusting the torque for force transmission of a such agitator - Google Patents
Magnetic drive agitator and method for adjusting the torque for force transmission of a such agitator Download PDFInfo
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- EP1023936A1 EP1023936A1 EP99420233A EP99420233A EP1023936A1 EP 1023936 A1 EP1023936 A1 EP 1023936A1 EP 99420233 A EP99420233 A EP 99420233A EP 99420233 A EP99420233 A EP 99420233A EP 1023936 A1 EP1023936 A1 EP 1023936A1
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- European Patent Office
- Prior art keywords
- rotor
- axis
- shaft
- sleeve
- propeller
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- 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.)
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F33/00—Other mixers; Mixing plants; Combinations of mixers
- B01F33/45—Magnetic mixers; Mixers with magnetically driven stirrers
- B01F33/453—Magnetic mixers; Mixers with magnetically driven stirrers using supported or suspended stirring elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F33/00—Other mixers; Mixing plants; Combinations of mixers
- B01F33/45—Magnetic mixers; Mixers with magnetically driven stirrers
- B01F33/453—Magnetic mixers; Mixers with magnetically driven stirrers using supported or suspended stirring elements
- B01F33/4535—Magnetic mixers; Mixers with magnetically driven stirrers using supported or suspended stirring elements using a stud for supporting the stirring element
Definitions
- the invention relates to a stirrer with magnetic drive and a method for adjusting the transmission limit torque effort of such an agitator.
- Agitators are conventionally used for brewing a mixture located inside a container to avoid decantation or any other alteration of the mixture during time.
- the advantage of a stirrer with magnetic drive that the setting in motion of the propeller which it comprises is realized by a magnetic coupling which takes place without contact physics between two rotating parts, one of which is driven by the output shaft of an electric motor while the other consists of a propeller. This allows the part associated with the electric motor shaft outside the container while the propeller is installed inside the container. Any danger of leakage from the agitator can thus be dismissed. This is particularly useful when the mixture is toxic or when pollution of it by external agents should be avoided as, for example, in the case of a drug composition.
- the magnetic coupling used for an industrial stirrer must be intense in order to train the agitator propeller with sufficient force.
- it is sometimes necessary method of disassembling the propeller in particular for reasons maintenance or inspection of the container in which is formed the mixture. It is thus common to plan to clean the propeller of an agitator and / or sterilize it outside the container at the end of each manufacturing batch. He's sometimes necessary to dismantle the propeller to proceed with the exchange standard of wearing parts such as bearings.
- a propeller When a propeller has been dismantled, it must be replaced with the greater precautions on its support, avoiding the most possible impacts that could damage the blades, bearings and / or the surface of the container.
- the magnetic forces necessary for the drive of the propeller of an industrial agitator are such that the effort that must exercise an operator to remove the propeller is very important, because this effort must overcome both the weight of the helix and the magnetic coupling force required to training. This is even more critical when handing over in place of the propeller, insofar as, during the presentation of it, it happens that the magnetic force is so intense that the propeller escapes the operator and comes to tackle violently against its support, which has the consequence damage the bearings, or even injure the operator.
- the invention relates to a stirrer with magnetic drive which includes a flange adapted to be tightly mounted in a wall of a container and provided with a blind sleeve inside which is housed a rotor supporting a first magnetic coupling means, then that a propeller arranged around this sleeve is equipped with a second magnetic coupling means for driving this helix around an axis of rotation.
- This agitator is characterized in that the rotor is movable in translation, parallel to this axis inside the sleeve, between a first position where the first and second coupling means are next to each other, so that they cooperate for training in rotation of this propeller, and a second position where they interact little or no, so that this propeller can be moved relative to the sleeve without interaction notable first and second coupling means.
- the movable nature of the rotor in translation it can be retracted during assembly and disassembly of the propeller, so that the coupling means magnetic that it supports, such as permanent magnets, is removed from the coupling means which equip the propeller with a sufficient distance to prevent the magnetic force between these coupling means does not disturb the mounting or the disassembly of the propeller.
- the displacement of the rotor inside the sleeve takes place in a direction corresponding to shear the air gap between the magnetic coupling means, that is to say in practice between the permanent magnets respectively associated with the rotor and the propeller. This shear perpendicular to the magnetic force created between these magnets does not require significant effort as far where this magnetic force does not oppose this shearing.
- the magnetic coupling between the magnets of the rotor and propeller is annihilated without this magnetic coupling strongly opposes the translation of the rotor.
- the invention therefore makes it possible to set up the propeller without interference with the magnets of the rotor, then move it until it can drive the propeller, this displacement being carried out in a direction such that it it is not necessary to overcome an intense magnetic effort.
- the rotor is moved in rotation around its axis and in translation parallel to this axis, by a drive shaft itself mobile in rotation around this axis and in translation parallel to this axis, between two positions corresponding to first and second rotor positions.
- a drive shaft itself mobile in rotation around this axis and in translation parallel to this axis, between two positions corresponding to first and second rotor positions.
- the rotor is provided with a central recess for receiving a screw for mounting the rotor on the shaft, this screw being arranged substantially along the aforementioned axis.
- the rotor and / or the drive shaft are able to be immobilized, in their translational movement parallel to the axis above, in an intermediate position between the first and second positions.
- This aspect of the invention makes it possible to envisage to use the agitator while the magnetic coupling effort between the rotor and the propeller is decreased compared to the position where the respective coupling means are opposite, so that the drive torque of the propeller is limited.
- This is advantageous when you want to use the agitator with a mixture whose viscosity is variable, for example made of a chemical reaction. In this case, the agitator is blocked when the viscosity of the mixture is such that the torque that can be transmitted to the propeller is less than that which would be necessary to set it in motion in this mixture.
- the tree drive is slidably mounted inside a shaft output hollow of a reducer, these drive shafts and hollow shaft being integral in rotation.
- reducer we hears any device for transmitting a movement of rotation, whatever its reduction ratio. He can particular be a 1/1 ratio angle gear.
- the hollow shaft carries a nut whose internal thread is able to cooperate with an external thread of a threaded rod integral with the drive shaft. This creates a system, with nut and worm, for adjusting the position in translation of the drive shaft and the rotor.
- the rod threaded is advantageously provided, at one of its ends protruding outside the hollow shaft, means control of its rotation around its axis. In this case, a protective cover for this end of the threaded rod and these control means can be provided, this cover being mounted removable on the reducer.
- the rotor can be controlled in translation along the above axis by a pneumatic or hydraulic cylinder.
- the invention also relates to a method for adjusting the force transmission torque limit of an agitator such as previously described, which consists in adjusting the position of the rotor along this axis, so that the first and second magnetic coupling means are more or less opposite. Thanks to the process of the invention, the transmissible torque between the rotor and the propeller is more or less important, as indicated above.
- a container 1 is formed from a tank 2 in which is arranged a mixture 3, while a cover 4 is designed to close an upper opening of the tank.
- a propeller 8 is disposed inside the tank 2, in the mixture 3. The rotation of the propeller 8 by the motor 7 results in a displacement of its blades 8 a , two of which are visible in the figures, around an axis of rotation XX ' , which has the effect of mixing the mixture 3.
- the flange 5 forms a blind sleeve 10 which extends inside the tank 2.
- a bearing 11 is mounted on the end 10 a of the sleeve 10 by means of an axis 12 whose threaded end 12 a is received in a tapping 10 b of the end 10 a of the sleeve 10.
- the bearing 11 supports a bush 13 whose outer surface 13 a constitutes a bearing surface.
- the propeller 8 comprises a head 14 formed of a ring 15 whose internal circular surface 15 a is intended to fit around the surface 13 a of the sleeve 13.
- a smooth bearing is thus produced by contact, for example metal -metal, between surfaces 13 a and 15 a .
- Three branches two of which are visible in the figures with the reference 15b , and which are regularly distributed around the periphery of the ring 15, extend outwards from the latter and support a sheath 16 disposed around the blind sleeve 10.
- the blades 8a of the impeller 8 are welded to the outside of the sheath 16.
- This sheath 16 carries on its inner surface 16a facing the sleeve 10, two rows of permanent magnets 17 whose polarity north-south is directed in directions AA 'and BB' generally perpendicular to the axis X-X '.
- a rotor 20 is disposed inside the sleeve 10 and comprises a first sleeve-shaped part 20 a on the external surface 20 b of which are mounted permanent magnets 21 aligned with the magnets 17, in the configuration of FIG. 2 In this configuration, the directions CC ′ and DD ′ of polarity of the magnets 21 are substantially aligned with the directions AA ′ and B-B ′.
- the rotor 20 is provided to rotate around the axis XX 'and cause, thanks to the magnetic coupling produced between the magnets 21 and 17, the propeller 8 in rotation about this axis.
- the rotor 20 is made integral with a drive shaft 22 by means of a screw 23 disposed in the central recess 20 c of the sleeve 20 a along the axis XX 'and penetrating into an end thread 22 a of l 'shaft 22.
- the rotor 20 is provided with an axial bore 20 d for receiving the end 22 b of the shaft 22 in which is formed the thread 22 a .
- a screw 24 is disposed in a radial bore in the part of the rotor 20 in which the bore 20 d is formed, so as to come into abutment against the external radial surface of the end 22b of the shaft 22, so as to immobilize elements 20 and 22 in rotation.
- the flange 5 is integral with a spacer 25 on which is mounted the reducer 6.
- the spacer 25 defines a housing cylindrical 26 for receiving the shaft 22.
- An output shaft 27 of the reduction gear 6 is driven by pinions 28 and 29, the pinion 29 being engaged, thanks to a shaft 30, with the output shaft 31 of the motor 7.
- the shaft 27 is hollow and defines a internal volume in which the shaft 22 can slide, the shafts 22 and 27 being integral in rotation by means of a key 32.
- the shaft 22 can slide inside the shaft 27 and be driven in rotation by that -this, thanks to the key 32.
- Note 27 has a longitudinal groove in the shaft 27 in which the key 32 can slide.
- the end 22 c of the shaft 22 opposite the rotor 20 is integral with a threaded rod 33, a first end 33 a is provided for entering a housing 22 d of the end 22 c .
- Two screws 34 serve to axially immobilize the end 33 a of the rod 33 inside the housing 22 d .
- the second end 33 b of the rod 33 cooperates with a nut 35 fixed to the end of the shaft 27 opposite the spacer 25.
- a nut 36 is immobilized on the end 32 b of the rod 33 by means of a pin 37. It is thus possible to rotate the threaded rod 33 inside the nut 35 thanks to the nut 36.
- a screw-nut system has thus been formed which, due to the fixed position in translation of the nut 35 relative to the axis XX ′, makes it possible to control the displacement in translation of the rod 33, of the shaft 22 and of the rotor 20 between the two positions respectively shown in FIGS. 2 and 3.
- L 'nut 36 therefore constitutes a means of controlling the movement of these elements along the axis X-X'.
- a cover 38 is mounted on the reduction gear 6 around the end 33 b of the threaded rod 33 in order to protect the elements 35 to 37.
- the cover 38 made of metal or plastic, can be screwed or clipped onto the reduction gear 6.
- the directions of polarity CC 'and DD' of the magnets 21 are offset with respect to the directions of polarity AA and BB 'of the magnets 17 by a distance d such that the magnetic coupling force between these magnets is practically zero. In other words, there is then no significant magnetic interaction between the magnets 17 and 21.
- the propeller 8 can therefore be removed, without the magnetic forces exerted between the magnets 17 and 21 being opposed to it. in a sensitive way.
- propeller 8 can be replaced without exerting on the magnets 17 too great an attraction force due to the magnets 21.
- the maximum torque value transmissible depends on the proportion of magnets 17 and 21 which are facing each other and create a magnetic coupling effort partial. It is possible to calibrate the agitator of the invention to determine the maximum transmissible torque as a function of the position of rotor 20. After this calibration, you can scale the rod 33, which allows a user to move it towards inside the tube 27 as a function of the limit or maximum torque wish.
- a device (not shown) for detecting movement propeller size 8 can be combined with the agitator the invention so that the operator is notified when the propeller 8 no longer turns while the motor 6 is running, such situation corresponding to a predetermined viscosity value for mixing 3.
- the engine 7 can be stopped in These conditions.
- the agitator of this second embodiment differs from the previous one essentially in that the end 33b of a rod 33 ', which is not threaded, is integral with a piston 50 movable in translation along the axis XX ′ inside a cylinder 51, the elements 50 and 51 belonging to a pneumatic cylinder 52 supplied with air through two conduits 53 and 54.
- the rod 33 is moved along the axis XX ′, which makes it possible to move the magnets 21 of the rotor 20 relative to the magnets 17 sheath 16, as in the first embodiment.
- the cylinder 52 could also be a cylinder hydraulic.
- a jack allows rapid maneuvering of the rotor 20 inside the sleeve 10, such an operation can be automated.
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mixers With Rotating Receptacles And Mixers With Vibration Mechanisms (AREA)
- Accessories For Mixers (AREA)
- Mixers Of The Rotary Stirring Type (AREA)
- Toys (AREA)
- Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)
Abstract
Description
L'invention a trait à un agitateur à entraínement magnétique et à un procédé de réglage du couple limite de transmission d'effort d'un tel agitateur.The invention relates to a stirrer with magnetic drive and a method for adjusting the transmission limit torque effort of such an agitator.
Des agitateurs sont classiquement utilisés pour brasser un mélange situé à l'intérieur d'un récipient afin d'éviter une décantation ou toute autre altération du mélange au cours du temps. Un agitateur à entraínement magnétique présente l'avantage que la mise en mouvement de l'hélice qu'il comprend est réalisée par un couplage magnétique qui a lieu sans contact physique entre deux parties tournantes dont l'une est entraínée par l'arbre de sortie d'un moteur électrique alors que l'autre est constituée par une hélice. Ceci permet de disposer la partie associée à l'arbre du moteur électrique à l'extérieur du récipient alors que l'hélice est installée à l'intérieur du récipient. Tout danger de fuite au niveau de l'agitateur peut ainsi être écarté. Ceci est particulièrement utile lorsque le mélange est toxique ou lorsqu'une pollution de celui-ci par des agents extérieurs doit être évitée comme, par exemple, dans le cas d'une composition médicamenteuse.Agitators are conventionally used for brewing a mixture located inside a container to avoid decantation or any other alteration of the mixture during time. The advantage of a stirrer with magnetic drive that the setting in motion of the propeller which it comprises is realized by a magnetic coupling which takes place without contact physics between two rotating parts, one of which is driven by the output shaft of an electric motor while the other consists of a propeller. This allows the part associated with the electric motor shaft outside the container while the propeller is installed inside the container. Any danger of leakage from the agitator can thus be dismissed. This is particularly useful when the mixture is toxic or when pollution of it by external agents should be avoided as, for example, in the case of a drug composition.
Le couplage magnétique utilisé pour un agitateur industriel doit être intense afin d'entraíner l'hélice de l'agitateur avec une force suffisante. Or, il est parfois nécessaire de procédé au démontage de l'hélice, notamment pour des raisons de maintenance ou d'inspection du récipient dans lequel est formé le mélange. Il est ainsi courant de prévoir de nettoyer l'hélice d'un agitateur et/ou de la stériliser à l'extérieur du récipient à la fin de chaque lot de fabrication. Il est parfois nécessaire de démonter l'hélice pour procéder à l'échange standard de pièces d'usure telles que des paliers. Lorsqu'une hélice à été démontée, elle doit être remise en place avec les plus grandes précautions sur son support en évitant le plus possible les heurts susceptibles d'endommager les pales, les paliers et/ou la surface du récipient.The magnetic coupling used for an industrial stirrer must be intense in order to train the agitator propeller with sufficient force. However, it is sometimes necessary method of disassembling the propeller, in particular for reasons maintenance or inspection of the container in which is formed the mixture. It is thus common to plan to clean the propeller of an agitator and / or sterilize it outside the container at the end of each manufacturing batch. He's sometimes necessary to dismantle the propeller to proceed with the exchange standard of wearing parts such as bearings. When a propeller has been dismantled, it must be replaced with the greater precautions on its support, avoiding the most possible impacts that could damage the blades, bearings and / or the surface of the container.
Les forces magnétiques nécessaires à l'entraínement de l'hélice d'un agitateur industriel sont telles que l'effort que doit exercer un opérateur pour retirer l'hélice est très important, car cet effort doit vaincre à la fois le poids de l'hélice et la force de couplage magnétique nécessaire à l'entraínement. Ceci est encore plus critique lors de la remise en place de l'hélice, dans la mesure où, lors de la présentation de celle-ci, il arrive que l'effort magnétique soit si intense que l'hélice échappe à l'opérateur et vienne se plaquer violemment contre son support, ce qui a pour conséquence d'endommager les paliers, voire de blesser l'opérateur.The magnetic forces necessary for the drive of the propeller of an industrial agitator are such that the effort that must exercise an operator to remove the propeller is very important, because this effort must overcome both the weight of the helix and the magnetic coupling force required to training. This is even more critical when handing over in place of the propeller, insofar as, during the presentation of it, it happens that the magnetic force is so intense that the propeller escapes the operator and comes to tackle violently against its support, which has the consequence damage the bearings, or even injure the operator.
En outre, il est particulièrement délicat pour un opérateur de présenter l'hélice parfaitement alignée avec l'axe de rotation de son rotor, de sorte que si celle-ci échappe à l'opérateur du fait de la force magnétique qu'elle subit, elle a tendance à être plaquée en biais sur son support, ce qui peut conduire à la destruction d'une de ses pales, au marquage de la surface interne de la cuve et/ou à l'endommagement d'un des paliers. Pour pallier cet inconvénient, on peut envisager de démonter systématiquement l'ensemble d'entraínement de l'hélice situé à l'extérieur du récipient, c'est-à-dire son moteur d'entraínement et éventuellement le réducteur qui lui est associé, afin de supprimer les efforts magnétiques exercés sur l'hélice en cours de montage ou de démontage. Une telle approche nécessite la manipulation par un opérateur de pièces lourdes et encombrantes, ces pièces étant généralement situées sous les cuves ou récipients de fabrication et d'accès difficile. En outre, un tel démontage de ces systèmes d'entraínement doit être suivi d'un remontage au cours duquel les axes des pièces tournantes doivent être très précisément alignés, ce qui n'est pas toujours possible compte tenu des difficultés d'accès aux zones de remontage du moteur et de son éventuel réducteur. De plus, le démontage de la partie extérieure de l'agitateur revient à exposer à l'air libre le rotor d'entraínement magnétique, ce rotor étant pourvu d'aimants permanents dont les surfaces externes peuvent se couvrir d'impuretés magnétiques. Compte tenu du faible jeu présent autour du rotor, ces impuretés peuvent conduire à un usinage des aimants et à un blocage de l'agitateur.In addition, it is particularly delicate for an operator to present the propeller perfectly aligned with the axis of rotation of its rotor, so that if it escapes the operator because of the magnetic force which it undergoes, it tends to be biased on its support, which can lead to the destruction of one of its blades, to the marking of the internal surface of the tank and / or damage to one of the bearings. To overcome this drawback, we can consider systematically disassemble the propeller drive assembly located outside the container, i.e. its motor drive and possibly the reduction gear which is its associated, in order to remove the magnetic forces exerted on the propeller during assembly or disassembly. Such a approach requires manipulation by a parts operator heavy and bulky, these parts being generally located under tanks or containers that are difficult to manufacture and access. In addition, such disassembly of these drive systems must be followed by a reassembly during which the axes of the rotating parts must be very precisely aligned, which is not always possible given the difficulties of access to the reassembly areas of the engine and its possible reduction gear. In addition, the disassembly of the external part of the agitator is to expose the drive rotor to the air magnetic, this rotor being provided with permanent magnets whose external surfaces may be covered with magnetic impurities. Given the small clearance present around the rotor, these impurities can lead to magnet processing and blockage of the agitator.
C'est à ces inconvénients qu'entend plus particulièrement remédier l'invention en proposant un agitateur à entraínement magnétique dont l'hélice peut être aisément démontée et remise en place, sans risque que les forces magnétiques qu'elle subit ne viennent perturber ces opérations et sans nécessiter le démontage complet de la partie de l'agitateur extérieure au récipient sur lequel il est monté.It is to these disadvantages that we hear more particularly remedy the invention by proposing a drive agitator magnetic whose propeller can be easily disassembled and put back in place, without risk that the magnetic forces it undergoes do not interfere with these operations and without requiring the complete disassembly of the agitator part outside the container on which it is mounted.
Dans cet esprit, l'invention concerne un agitateur à entraínement magnétique qui comprend une bride apte à être montée de façon étanche dans une paroi d'un récipient et pourvue d'un manchon borgne à l'intérieur duquel est logé un rotor supportant un premier moyen de couplage magnétique, alors qu'une hélice disposée autour de ce manchon est équipée d'un second moyen de couplage magnétique pour l'entraínement de cette hélice autour d'un axe de rotation. Cet agitateur est caractérisé en ce que le rotor est mobile en translation, parallèlement à cet axe à l'intérieur du manchon, entre une première position où les premier et second moyens de couplage sont en regard, de telle façon qu'ils coopèrent pour l'entraínement en rotation de cette hélice, et une seconde position où ils n'interagissent pas ou peu, de telle façon que cette hélice peut être déplacée par rapport au manchon sans interaction notable des premier et second moyens de couplage.In this spirit, the invention relates to a stirrer with magnetic drive which includes a flange adapted to be tightly mounted in a wall of a container and provided with a blind sleeve inside which is housed a rotor supporting a first magnetic coupling means, then that a propeller arranged around this sleeve is equipped with a second magnetic coupling means for driving this helix around an axis of rotation. This agitator is characterized in that the rotor is movable in translation, parallel to this axis inside the sleeve, between a first position where the first and second coupling means are next to each other, so that they cooperate for training in rotation of this propeller, and a second position where they interact little or no, so that this propeller can be moved relative to the sleeve without interaction notable first and second coupling means.
Grâce au caractère mobile en translation du rotor, celui-ci peut être escamoté lors des opérations de montage et de démontage de l'hélice, de telle façon que le moyen de couplage magnétique qu'il supporte, tel que des aimants permanents, est écarté des moyens de couplage qui équipent l'hélice d'une distance suffisante pour éviter que la force magnétique entre ces moyens de couplage ne vienne perturber le montage ou le démontage de l'hélice. Le déplacement du rotor à l'intérieur du manchon a lieu selon une direction correspondant au cisaillement de l'entrefer entre les moyens de couplage magnétique, c'est-à-dire en pratique entre les aimants permanents respectivement associés au rotor et à l'hélice. Ce cisaillement perpendiculaire à la force magnétique créée entre ces aimants ne nécessite pas d'exercer un effort important dans la mesure où cette force magnétique ne s'oppose pas à ce cisaillement. En d'autres termes, le couplage magnétique entre les aimants du rotor et de l'hélice est annihilé sans que ce couplage magnétique s'oppose de façon importante à la translation du rotor. Lors du montage ou du remontage de l'hélice, il suffit de placer celle-ci sur le manchon, puis de déplacer le rotor en translation à l'intérieur du manchon jusqu'à ce que les aimants qu'il porte soient au niveau ou en regard des aimants portés par l'hélice. L'invention permet donc de mettre en place l'hélice sans interférence avec les aimants du rotor, puis de déplacer celui-ci jusqu'à ce qu'il puisse entraíner l'hélice, ce déplacement étant réalisé selon une direction telle qu'il n'est pas nécessaire de vaincre un effort magnétique intense.Thanks to the movable nature of the rotor in translation, it can be retracted during assembly and disassembly of the propeller, so that the coupling means magnetic that it supports, such as permanent magnets, is removed from the coupling means which equip the propeller with a sufficient distance to prevent the magnetic force between these coupling means does not disturb the mounting or the disassembly of the propeller. The displacement of the rotor inside the sleeve takes place in a direction corresponding to shear the air gap between the magnetic coupling means, that is to say in practice between the permanent magnets respectively associated with the rotor and the propeller. This shear perpendicular to the magnetic force created between these magnets does not require significant effort as far where this magnetic force does not oppose this shearing. In in other words, the magnetic coupling between the magnets of the rotor and propeller is annihilated without this magnetic coupling strongly opposes the translation of the rotor. When mounting or reassembling the propeller, simply place it on the sleeve, then move the rotor in translation inside the sleeve until the magnets he wears are at or near the magnets worn by the propeller. The invention therefore makes it possible to set up the propeller without interference with the magnets of the rotor, then move it until it can drive the propeller, this displacement being carried out in a direction such that it it is not necessary to overcome an intense magnetic effort.
Selon un premier aspect avantageux de l'invention, le rotor est déplacé en rotation autour de son axe et en translation parallèlement de cet axe, par un arbre d'entraínement lui-même mobile en rotation autour de cet axe et en translation parallèlement à cet axe, entre deux positions correspondant aux première et seconde positions du rotor. On peut prévoir que le rotor est pourvu d'un évidement central de réception d'une vis de montage du rotor sur l'arbre, cette vis étant disposée sensiblement selon l'axe précité.According to a first advantageous aspect of the invention, the rotor is moved in rotation around its axis and in translation parallel to this axis, by a drive shaft itself mobile in rotation around this axis and in translation parallel to this axis, between two positions corresponding to first and second rotor positions. We can predict that the rotor is provided with a central recess for receiving a screw for mounting the rotor on the shaft, this screw being arranged substantially along the aforementioned axis.
Selon un autre aspect avantageux de l'invention, le rotor et/ou l'arbre d'entraínement sont aptes à être immobilisés, dans leur mouvement de translation parallèlement à l'axe précité, dans une position intermédiaire entre les première et seconde positions. Cet aspect de l'invention permet d'envisager d'utiliser l'agitateur alors que l'effort de couplage magnétique entre le rotor et l'hélice est diminué par rapport à la position où les moyens de couplage respectifs sont en regard, de sorte que le couple d'entraínement de l'hélice est limité. Ceci est avantageux lorsqu'on souhaite utiliser l'agitateur avec un mélange dont la viscosité est variable, par exemple du fait d'une réaction chimique. Dans ce cas, l'agitateur est bloqué lorsque la viscosité du mélange est telle que le couple pouvant être transmis à l'hélice est inférieur à celui qui serait nécessaire pour la mettre en mouvement dans ce mélange.According to another advantageous aspect of the invention, the rotor and / or the drive shaft are able to be immobilized, in their translational movement parallel to the axis above, in an intermediate position between the first and second positions. This aspect of the invention makes it possible to envisage to use the agitator while the magnetic coupling effort between the rotor and the propeller is decreased compared to the position where the respective coupling means are opposite, so that the drive torque of the propeller is limited. This is advantageous when you want to use the agitator with a mixture whose viscosity is variable, for example made of a chemical reaction. In this case, the agitator is blocked when the viscosity of the mixture is such that the torque that can be transmitted to the propeller is less than that which would be necessary to set it in motion in this mixture.
Selon un autre aspect avantageux de l'invention, l'arbre d'entraínement est monté coulissant à l'intérieur d'un arbre creux de sortie d'un réducteur, ces arbres d'entraínement et arbre creux étant solidaires en rotation. Par réducteur, on entend tout dispositif de transmission d'un mouvement de rotation, quel que soit son rapport de réduction. Il peut en particulier s'agir d'un renvoi d'angle de rapport 1/1. On peut prévoir que l'arbre creux porte un écrou dont le filet interne est apte à coopérer avec un filet externe d'une tige filetée solidaire de l'arbre d'entraínement. Ceci permet de créer un système, à écrou et vis sans fin, de réglage de la position en translation de l'arbre d'entraínement et du rotor. La tige filetée est avantageusement pourvue, au niveau d'une de ses extrémités dépassant à l'extérieur de l'arbre creux, de moyens de commande de sa rotation autour de son axe. Dans ce cas, un capot de protection de cette extrémité de la tige filetée et de ces moyens de commande peut être prévu, ce capot étant monté de façon amovible sur le réducteur.According to another advantageous aspect of the invention, the tree drive is slidably mounted inside a shaft output hollow of a reducer, these drive shafts and hollow shaft being integral in rotation. By reducer, we hears any device for transmitting a movement of rotation, whatever its reduction ratio. He can particular be a 1/1 ratio angle gear. We can provide that the hollow shaft carries a nut whose internal thread is able to cooperate with an external thread of a threaded rod integral with the drive shaft. This creates a system, with nut and worm, for adjusting the position in translation of the drive shaft and the rotor. The rod threaded is advantageously provided, at one of its ends protruding outside the hollow shaft, means control of its rotation around its axis. In this case, a protective cover for this end of the threaded rod and these control means can be provided, this cover being mounted removable on the reducer.
Selon une variante de réalisation de l'invention, le rotor peut être commandé en translation selon l'axe précité par un vérin pneumatique ou hydraulique.According to an alternative embodiment of the invention, the rotor can be controlled in translation along the above axis by a pneumatic or hydraulic cylinder.
L'invention concerne également un procédé de réglage du couple limite de transmission d'effort d'un agitateur tel que précédemment décrit, qui consiste à régler la position du rotor le long de cet axe, de telle sorte que les premier et second moyens de couplage magnétique soient plus ou moins en regard. Grâce au procédé de l'invention, le couple transmissible entre le rotor et l'hélice est plus ou moins important, comme indiqué ci-dessus.The invention also relates to a method for adjusting the force transmission torque limit of an agitator such as previously described, which consists in adjusting the position of the rotor along this axis, so that the first and second magnetic coupling means are more or less opposite. Thanks to the process of the invention, the transmissible torque between the rotor and the propeller is more or less important, as indicated above.
L'invention sera mieux comprise et d'autres avantages de celle-ci apparaítront plus clairement à la lumière de la description qui va suivre de deux modes de réalisation d'un agitateur à entraínement magnétique conforme à son principe et de leur procédé de réglage, donnée uniquement à titre d'exemple et faite en référence aux dessins annexés dans lesquels :
- la figure 1 est une représentation schématique de principe d'un récipient pour mélange équipé d'un agitateur conforme à l'invention ;
- la figure 2 est une vue à plus grande échelle du détail II à la figure 1, l'agitateur étant représenté en coupe, dans une première position ;
- la figure 3 est une vue analogue à la figure 2, alors que l'agitateur est dans une seconde position et
- la figure 4 est une vue partielle de la partie inférieure d'un agitateur conforme à un second mode de réalisation de l'invention.
- Figure 1 is a schematic representation of the principle of a mixing container equipped with an agitator according to the invention;
- Figure 2 is an enlarged view of detail II in Figure 1, the agitator being shown in section, in a first position;
- FIG. 3 is a view similar to FIG. 2, while the agitator is in a second position and
- Figure 4 is a partial view of the lower part of an agitator according to a second embodiment of the invention.
A la figure 1, un récipient 1 est formé d'une cuve 2 dans
laquelle est disposé un mélange 3, alors qu'un couvercle 4 est
prévu pour obturer une ouverture supérieure de la cuve.In FIG. 1, a container 1 is formed from a
Dans la paroi de fond 2a de la cuve 2 est disposée une
bride 5 en matériau amagnétique supportant un réducteur 6 et un
moteur électrique 7, situés à l'extérieur de la cuve 2. Une
hélice 8 est disposée à l'intérieur de la cuve 2, dans le
mélange 3. La mise en rotation de l'hélice 8 par le moteur 7
résulte dans un déplacement de ses pales 8a, dont deux sont
visibles sur les figures, autour d'un axe de rotation X-X', ce
qui a pour effet de brasser le mélange 3.In the bottom wall 2 a of the
La bride 5 forme un manchon borgne 10 qui se prolonge à
l'intérieur de la cuve 2. Un palier 11 est monté sur l'extrémité
10a du manchon 10 grâce à un axe 12 dont l'extrémité
filetée 12a est reçue dans un taraudage 10b de l'extrémité 10a
du manchon 10. Le palier 11 supporte une douille 13 dont la
surface extérieure 13a constitue une surface de palier.
L'hélice 8 comprend une tête 14 formée d'une bague 15 dont la
surface circulaire interne 15a est destinée à s'emboíter autour
de la surface 13a de la douille 13. Un palier lisse est ainsi
réalisé par contact, par exemple métal-métal, entre les
surfaces 13a et 15a.The
Trois branches, dont deux sont visibles sur les figures
avec la référence 15b, et qui sont régulièrement réparties à la
périphérie de la bague 15, s'étendent vers l'extérieur à partir
de celle-ci et supportent un fourreau 16 disposé autour du
manchon borgne 10. Les pales 8a de l'hélice 8 sont soudées sur
l'extérieur du fourreau 16. Ce fourreau 16 porte, sur sa
surface interne 16a dirigée vers le manchon 10, deux rangées
d'aimants permanents 17 dont la polarité nord-sud est dirigée
selon des directions A-A' et B-B' globalement perpendiculaires
à l'axe X-X'.Three branches, two of which are visible in the figures with the
Un rotor 20 est disposé à l'intérieur du manchon 10 et
comprend une première partie en forme de douille 20a sur la
surface externe 20b de laquelle sont montés des aimants
permanents 21 alignés avec les aimants 17, dans la configuration
de la figure 2. Dans cette configuration, les directions
C-C' et D-D' de polarité des aimants 21 sont sensiblement
alignées avec les directions A-A' et B-B'. Le rotor 20 est
prévu pour tourner autour de l'axe X-X' et entraíner, grâce au
couplage magnétique réalisé entre les aimants 21 et 17,
l'hélice 8 en rotation autour de cet axe.A
Le rotor 20 est rendu solidaire d'un arbre d'entraínement
22 grâce à une vis 23 disposée dans l'évidement central 20c de
la douille 20a selon l'axe X-X' et pénétrant dans un taraudage
d'extrémité 22a de l'arbre 22. Le rotor 20 est pourvu d'un
alésage axial 20d de réception de l'extrémité 22b de l'arbre 22
dans laquelle est ménagé le taraudage 22a. Une vis 24 est
disposée dans un perçage radial de la partie du rotor 20 dans
laquelle est ménagé l'alésage 20d, de façon à venir en appui
contre la surface radiale externe de l'extrémité 22b de l'arbre
22, de façon à immobiliser en rotation les éléments 20 et 22.The
La bride 5 est solidaire d'une entretoise 25 sur laquelle
est monté le réducteur 6. L'entretoise 25 définit un logement
cylindrique 26 de réception de l'arbre 22.The
Un arbre de sortie 27 du réducteur 6 est entraíné par des
pignons 28 et 29, le pignon 29 étant en prise, grâce à un arbre
30, avec l'arbre de sortie 31 du moteur 7. L'arbre 27 est creux
et définit un volume interne dans lequel peut coulisser l'arbre
22, les arbres 22 et 27 étant solidaires en rotation grâce à
une clavette 32. Ainsi, l'arbre 22 peut coulisser à l'intérieur
de l'arbre 27 et être entraíné en rotation par celui-ci, grâce
à la clavette 32. On note 27a une rainure longitudinale de
l'arbre 27 dans laquelle peut coulisser la clavette 32.An
L'extrémité 22c de l'arbre 22 opposée au rotor 20 est
solidaire d'une tige filetée 33 dont une première extrémité 33a
est prévue pour pénétrer dans un logement 22d de l'extrémité
22c. Deux vis 34 servent à immobiliser axialement l'extrémité
33a de la tige 33 à l'intérieur du logement 22d.The
La seconde extrémité 33b de la tige 33 coopère avec un
écrou 35 fixé à l'extrémité de l'arbre 27 opposée à l'entretoise
25. Un écrou 36 est immobilisé sur l'extrémité 32b de la
tige 33 grâce à une goupille 37. Il est ainsi possible d'entraíner
en rotation la tige filetée 33 à l'intérieur de l'écrou
35 grâce à l'écrou 36. On a ainsi constitué un système vis-écrou
qui, du fait de la position fixe en translation de
l'écrou 35 par rapport à l'axe X-X', permet de commander le
déplacement en translation de la tige 33, de l'arbre 22 et du
rotor 20 entre les deux positions respectivement représentées
aux figures 2 et 3. L'écrou 36 constitue donc un moyen de
commande du déplacement de ces éléments selon l'axe X-X'.The second end 33 b of the
Un capot 38 est monté sur le réducteur 6 autour de
l'extrémité 33b de la tige filetée 33 afin de protéger les
éléments 35 à 37. Le capot 38, réalisé en métal ou en matière
plastique, peut être vissé ou clipsé sur le réducteur 6.A
Le fonctionnement est le suivant :The operation is as follows:
A partir de la position de la figure 2, et lorsqu'il est
nécessaire de démonter l'hélice 8, on retire le capot 38 et on
manoeuvre l'écrou 36 avec un clé dans un sens de dévissage de
la tige 33 par rapport à l'écrou 35, de telle sorte que cette
tige est progressivement extraite à l'extérieur du tube 27, ce
qui a pour conséquence d'entraíner l'arbre 22 en direction de
l'écrou 35 jusqu'à la position représentée à la figure 3. Dans
cette position, les aimants 17 et 21 ne sont plus en regard,
puisque la douille 20a du rotor 20 est parvenue dans une partie
du volume intérieur du manchon 10 situé à l'extérieur de la
cuve 2. Dans cette position, les directions de polarité C-C' et
D-D' des aimants 21 sont décalées par rapport aux directions de
polarité A-A et B-B' des aimants 17 d'une distance d telle que
l'effort de couplage magnétique entre ces aimants est pratiquement
nul. En d'autres termes, il n'existe alors pas d'interaction
magnétique notable entre les aimants 17 et 21. L'hélice 8
peut donc être retirée, sans que les forces magnétiques
exercées entre les aimants 17 et 21 ne s'y opposent de façon
sensible.From the position of FIG. 2, and when it is necessary to disassemble the
A la fin des opérations de nettoyage et/ou de maintenance,
l'hélice 8 peut être remise en place sans que ne s'exerce sur
les aimants 17 un effort d'attraction trop important dû aux
aimants 21.At the end of cleaning and / or maintenance operations,
Il est alors possible de manoeuvrer l'écrou 36 dans le
sens inverse de celui évoqué précédemment, de telle sorte que
la tige filetée 33 pénètre à nouveau à l'intérieur du tube 27
et que le rotor 20 est poussé par l'arbre 22 jusqu'à la
position de la figure 2 dans laquelle les aimants 17 et 21 sont
à nouveau en regard.It is then possible to operate the
Le déplacement des aimants 21 par rapport aux aimants 17
a lieu perpendiculairement aux efforts d'attraction magnétique
qui s'exercent entre ces éléments de couplage magnétique, de
sorte que ces efforts ne doivent pas être vaincus alors qu'ils
peuvent être particulièrement importants si l'entrefer entre
les aimants est réduit. On travaille ici en cisaillement de ces
efforts et la manoeuvre du rotor 20 entre les positions des
figures 2 et 3 est relativement aisée. De plus, une démultiplication
importante peut être obtenue en fonction du pas du
filet de la tige 33 et de l'écrou 35.The displacement of the
Lors de la remontée du rotor 20 à l'intérieur du manchon
10, il est possible d'interrompre la rotation de la tige
filetée 33 dans une position intermédiaire entre celles des
figures 2 et 3, une fraction seulement des aimants 21 parvenant
au niveau des aimants 17 les plus près du fond de la cuve 2.
Dans ces conditions, le couple maximum qui peut être transmis
entre le rotor 20 et le fourreau 16 de l'hélice 8 est moins
important que dans la position de la figure 2, ce qui s'avère
utile lorsqu'on veut limiter le couple pouvant être transmis à
l'hélice 8, notamment dans le cas d'un mélange 3 dont la
viscosité évolue en fonction du temps, par exemple du fait
d'une réaction chimique modifiant cette viscosité. Il est ainsi
possible d'éviter l'agitation du mélange à la fin d'une
réaction chimique, c'est-à-dire lorsque cette viscosité a
atteint une valeur prédéterminée. La valeur du couple maximum
transmissible dépend de la proportion des aimants 17 et 21 qui
sont en regard et créent un effort de couplage magnétique
partiel. Il est possible d'étalonner l'agitateur de l'invention
pour déterminer le couple maximum transmissible en fonction de
la position du rotor 20. Après cet étalonnage, on peut graduer
la tige 33, ce qui permet à un utilisateur de la déplacer vers
l'intérieur du tube 27 en fonction du couple limite ou maximum
souhaité.When the
Un dispositif non représenté de détection du mouvement
effectif de l'hélice 8 peut être associé à l'agitateur de
l'invention pour que l'opérateur soit prévenu lorsque l'hélice
8 ne tourne plus alors que le moteur 6 fonctionne, une telle
situation correspondant à une valeur prédéterminée de viscosité
pour le mélange 3. L'arrêt du moteur 7 peut être programmé dans
ces conditions.A device (not shown) for detecting
Lorsque le rotor est positionné dans sa position d'entraínement
de l'hélice 8, qu'il s'agisse de la position de la
figure 2 ou d'une position intermédiaire, le capot 38 est
remonté sur le réducteur 6.When the rotor is positioned in its
Dans le mode de réalisation de l'invention représenté à la
figure 4, les éléments analogues à ceux du mode de réalisation
des figures 1 à 3 portent des références identiques. L'agitateur
de ce second mode de réalisation diffère du précédent
essentiellement en ce que l'extrémité 33b d'une tige 33', qui
n'est pas filetée, est solidaire d'un piston 50 mobile en
translation selon l'axe X-X' à l'intérieur d'un cylindre 51,
les éléments 50 et 51 appartenant à un vérin pneumatique 52
alimenté en air grâce à deux conduits 53 et 54. En fonction des
pressions régnant respectivement dans les chambres définies à
l'intérieur du cylindre 51 de part et d'autre du piston 50, la
tige 33 est déplacée selon l'axe X-X', ce qui permet de
déplacer les aimants 21 du rotor 20 par rapport aux aimants 17
du fourreau 16, comme dans le premier mode de réalisation.In the embodiment of the invention shown in
Figure 4, elements similar to those of the embodiment
Figures 1 to 3 bear identical references. The agitator
of this second embodiment differs from the previous one
essentially in that the end 33b of a rod 33 ', which
is not threaded, is integral with a
Bien entendu, le vérin 52 pourrait également être un vérin
hydraulique.Of course, the
L'utilisation d'un vérin permet une manoeuvre rapide du
rotor 20 à l'intérieur du manchon 10, une telle manoeuvre
pouvant être automatisée.The use of a jack allows rapid maneuvering of the
D'autres systèmes de commande du déplacement du rotor 20
à l'intérieur du manchon 10 peuvent être envisagés, notamment
un système à ressorts où à cames.Other systems for controlling the movement of the
Dans tous les cas, le procédé de réglage du couple limite de transmission d'effort précédemment décrit demeure applicable.In all cases, the process for adjusting the limit torque transmission of force described above remains applicable.
Claims (10)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9901130 | 1999-01-28 | ||
FR9901130A FR2788995B1 (en) | 1999-01-28 | 1999-01-28 | MAGNETICALLY DRIVEN AGITATOR AND METHOD FOR ADJUSTING THE LIMIT TORQUE FOR THE TRANSMISSION OF EFFORT OF SUCH AN AGITATOR |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1023936A1 true EP1023936A1 (en) | 2000-08-02 |
EP1023936B1 EP1023936B1 (en) | 2003-01-08 |
EP1023936B2 EP1023936B2 (en) | 2007-03-07 |
Family
ID=9541461
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP99420233A Expired - Lifetime EP1023936B2 (en) | 1999-01-28 | 1999-11-26 | Method for adjusting the torque for force transmission of a magnetic drive agitator |
Country Status (6)
Country | Link |
---|---|
US (1) | US6206562B1 (en) |
EP (1) | EP1023936B2 (en) |
AT (1) | ATE230628T1 (en) |
CA (1) | CA2291500C (en) |
DE (1) | DE69904803D1 (en) |
FR (1) | FR2788995B1 (en) |
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- 1999-11-26 EP EP99420233A patent/EP1023936B2/en not_active Expired - Lifetime
- 1999-11-26 AT AT99420233T patent/ATE230628T1/en not_active IP Right Cessation
- 1999-12-02 CA CA002291500A patent/CA2291500C/en not_active Expired - Fee Related
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1475566A2 (en) * | 2003-05-07 | 2004-11-10 | Ashland Inc. | Fuel processing device having magnetic coupling and method of operating thereof |
FR2854663A1 (en) * | 2003-05-07 | 2004-11-12 | Ashland Inc | FUEL TREATMENT APPARATUS COMPRISING A HOMOGENIZER |
EP1475566A3 (en) * | 2003-05-07 | 2010-05-19 | Ashland Licensing and Intellectual Property LLC | Fuel processing device having magnetic coupling and method of operating thereof |
CN110098537A (en) * | 2019-05-16 | 2019-08-06 | 程少云 | A kind of convenient socket of plug |
Also Published As
Publication number | Publication date |
---|---|
US6206562B1 (en) | 2001-03-27 |
CA2291500A1 (en) | 2000-07-28 |
ATE230628T1 (en) | 2003-01-15 |
FR2788995B1 (en) | 2001-04-06 |
EP1023936B2 (en) | 2007-03-07 |
CA2291500C (en) | 2008-05-27 |
EP1023936B1 (en) | 2003-01-08 |
DE69904803D1 (en) | 2003-02-13 |
FR2788995A1 (en) | 2000-08-04 |
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