[go: up one dir, main page]

EP1926916A1 - Removable impeller for fan - Google Patents

Removable impeller for fan

Info

Publication number
EP1926916A1
EP1926916A1 EP06808188A EP06808188A EP1926916A1 EP 1926916 A1 EP1926916 A1 EP 1926916A1 EP 06808188 A EP06808188 A EP 06808188A EP 06808188 A EP06808188 A EP 06808188A EP 1926916 A1 EP1926916 A1 EP 1926916A1
Authority
EP
European Patent Office
Prior art keywords
turbine
stop
hub
locking
series
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.)
Granted
Application number
EP06808188A
Other languages
German (de)
French (fr)
Other versions
EP1926916B1 (en
Inventor
Olivier Burias
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.)
Aereco
Original Assignee
Aereco
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 Aereco filed Critical Aereco
Priority to PL06808188T priority Critical patent/PL1926916T3/en
Publication of EP1926916A1 publication Critical patent/EP1926916A1/en
Application granted granted Critical
Publication of EP1926916B1 publication Critical patent/EP1926916B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/263Rotors specially for elastic fluids mounting fan or blower rotors on shafts

Definitions

  • the present invention relates to a removable turbine intended to be integrated in a fan, in particular for controlled mechanical ventilation, and made in the form of a wheel provided with a plurality of blades and equipped with locking means to enable it to be fixed. on a hub, and a hub and a latch for cooperating with said turbine.
  • a second known solution consists in the use of a removable turbine, capable of being cleaned once, disassembled.
  • Systems equipped with such a turbine provide that the latter is fixed by screwing on an axis. This step is nevertheless relatively difficult to implement, especially in the case of controlled mechanical ventilation since the occupant of the housing itself dismantles and cleans.
  • the object of the invention is to remedy these drawbacks and for this purpose consists in a removable turbine intended to be integrated in a fan, in particular for controlled mechanical ventilation, and produced in the form of a wheel provided with a plurality of blades. and equipped with locking means to allow its attachment to a hub, characterized in that it comprises projecting transmission means, positioned near a central neck whose axis of revolution is parallel to that of the wheel, and designed to alternately allow engagement or extraction of the blocking means.
  • the locking means are formed in the central neck in the form of a first series of locking clips regularly spaced from each other and each provided at the bottom of a bead radial outward.
  • each locking clip preferably has a lower radial shoulder oriented inwards.
  • the transmission means are formed in the central neck in the form of a second series of transmission clips regularly spaced from each other and interposed with the locking clips, each transmission clip being equipped with a first stop and a second abutment positioned one below the other and facing inwards, said first abutment forming a protrusion more pronounced than the second abutment.
  • the first stop is formed in the upper part, and the second stop is made in the form of a longitudinal boss, extending in the middle portion, and extended by an inclined pan at each of its upper and lower ends.
  • the present invention also relates to a hub and a closing latch designed so as to cooperate with such a turbine.
  • the hub preferably comprises a side wall in which is formed a series of notches, each of them being able to accommodate one of the turbine blocking means, and the closing lock comprises a gripping member and suitable means to slide through the central neck of the turbine.
  • the gripping member is extended by a series of longitudinal plane walls intercalated with a series of longitudinal hollow walls, said flat walls and hollow walls being regularly spaced from each other and being able to slide through the central collar of the turbine.
  • each hollow wall undergoes an elastic deformation so that the lower part of its outline is caused to slide successively along the lower inclined pan, the boss, and finally the upper inclined pan of the second stop.
  • the hollow wall then returns to its rest position in the interval between the first stop of the second stop, and the lower portion of the contour finally comes into contact with the first stop.
  • the flat walls of the lock are no longer positioned in front of the locking clips, and these can be extracted from the notches presented by the hub if the manipulator continues to exert sufficient traction on the gripping member.
  • the turbine and its lock are then disengaged from the hub, and it is possible to clean the blades of the turbine. This disassembly is done in one movement decomposed in two steps, simply, quickly and without tools.
  • the manipulator seizes the latch gripper and correctly positions the turbine on its hub. It suffices then to exert sufficient thrust on the gripping member to force the lower part of the contour of each hollow wall to slide successively along the upper inclined face, the boss, and finally the lower inclined face. In doing so, each flat wall of the lock slides along the associated locking clip, until the lower end of its contour comes into abutment against the radial shoulder of the locking clip. This then has the effect of elastically deforming the locking clip outwardly so that its radial bead is properly housed in the corresponding notch. This blocking is therefore also simple .simple, fast and without tools.
  • the turbine comprises, at the periphery of the central neck, a central wall on which are formed longitudinal ribs regularly spaced and oriented inwardly.
  • the side wall of the hub is advantageously equipped on its outer face with V-shaped indexing means.
  • the upper inclined pan is designed so that the minimum stresses to be exerted by the longitudinal ribs of the turbine on the V-shaped indexing means to force the hub to rotate until to what he are perfectly oriented are less than those necessary to cause the elastic deformation of each hollow wall due to the sliding of the lower part of its contour along said corresponding upper inclined pan.
  • the continuation of the thrust exerted by the manipulator on the gripping member then has the effect of forcing the latch to slide through the central neck, up to it comes to block the locking clips in the notches associated through its flat walls. Once the blocking of the turbine is ensured, the rotation of the turbine by the hub is then performed through the longitudinal ribs.
  • the locking means consist of at least two magnets
  • the transmission means consist of at least two links each comprising a first substantially cylindrical end having a longitudinal edge forming a stop, and connected by a rod to a second end projecting parallel to the axis of the first end.
  • the present invention also relates to a closing latch designed to cooperate / with a turbine according to the second preferred embodiment of the invention.
  • This lock advantageously comprises a gripping member extended by a longitudinal rod in which is formed a circular groove.
  • the present invention also relates to a ventilator, in particular for controlled mechanical ventilation, comprising a body forming a volute in which is fixed a rotary motor, a hub being secured to said motor and supporting a removable turbine provided with a central neck, a plurality of blades and equipped with locking means to allow its attachment to the hub, characterized in that - the locking means are formed in the central neck in the form of a first series of locking clips regularly spaced from each other and each provided at the bottom, on the one hand, with a radial bead directed towards the outside, and on the other hand, an inwardly directed radial shoulder, the turbine comprises transmission means arranged in the central neck in the form of a second series of regularly spaced clips.
  • each transmission clip being provided with a first abutment and a second abutment positioned one below the other and facing inwards, said first stop forming a protrusion more pronounced than the second stop, said first stop being formed in the upper part and said second stop being made in the form of a longitudinal boss, extending in the middle part, extended respectively by a steeply inclined pan; at its upper end and a slightly inclined pan at its lower end,
  • the hub comprises a side wall in which is formed a series of notches, each of them being adapted to accommodate one of the locking clips of the turbine,
  • a closing lock is attached to the turbine, the latch comprising a gripping member extended by a series of longitudinal plane walls interposed with a series of longitudinal hollow walls, said flat walls and hollow walls being regularly spaced from each other and being slidable through the central neck so as to each respectively disposed opposite a locking clip and a transmission clip.
  • Figure 1 is a perspective view of a fan according to the invention, with omission of the closure cap;
  • Figure 2 is a perspective view from above of a turbine according to the first preferred embodiment of the invention;
  • Figure 3 is a perspective view from below of the turbine shown in Figure 2;
  • Figure 4 is a perspective view of a locking latch according to the invention adapted to cooperate with the turbine shown in Figure 2;
  • Figure 5 is a perspective view of a hub according to the invention adapted to cooperate with the turbine shown in Figure 2;
  • Figure 6 is a perspective view of the turbine shown in Figure 2 with its lock, before fixing on its corresponding hub;
  • Figure 7 is a top view of the turbine shown in Figure 6, once fixed on its hub;
  • Figure 8 is a sectional view along the line A-A of the assembly shown in Figure 7, the latch being in the closed position;
  • Figure 9 is a sectional view along the line B-B of the assembly shown in Figure 7, the latch being in the closed position;
  • Figure 10 is a sectional view along the line A-A of the assembly shown in Figure 7, the latch being in the open position;
  • Figure 1 1 is a sectional view along the line B-B of the assembly shown in Figure 7, the latch being in the open position;
  • Figure 12 is a perspective view of a turbine according to the second preferred embodiment, with omission of the rods;
  • Figure 13 is a perspective view of a link
  • Figure 14 is a perspective view of a lock according to the invention adapted to cooperate with the turbine shown in Figure 12;
  • Figure 15 is a perspective view of a hub according to the invention adapted to cooperate with the turbine shown in Figure 12;
  • Figure 16 is a perspective view of a turbine half shown in Figure 12, cut longitudinally at the rods, before fixing on its corresponding hub;
  • Figure 17 is a perspective view of another turbine half shown in Figure 12, cut longitudinally at the magnets, before fixing on its corresponding hub.
  • a fan 1 according to the invention is intended for controlled mechanical ventilation and comprises a box 2 whose closing cap has been omitted, and in which is fixed a volute
  • the casing 2 has four air intake connectors 4, and each of them is connected to a part of the housing to be ventilated via an air duct (not shown).
  • the volute 3 is made of plastic material, and conventionally comprises an air inlet 5 and an air outlet 6, the air inlet 5 being bordered by a removable inlet 60 fixed with clips (not shown). As shown more specifically in FIGS. 1 to 3, the volute 3 contains a turbine 7, according to the first preferred embodiment of the invention, designed to create a depression in the casing 1 so as to suck stale air from the connections. air intake 4.
  • This turbine 7 is molded in plastic in the form of a wheel equipped with a plurality of blades 8, and comprises a cylindrical central wall 9 of revolution surrounding a central neck 10 whose vertical axis of revolution coincides with that of the wheel.
  • Each locking clip January 1 has in the lower part, on the one hand, a radial bead 12 oriented outwardly, and secondly, a shoulder 1.3 radially oriented inwards.
  • Each transmission clip 14 is equipped with a first stop
  • the first stop 15 is formed in the upper part of the central neck 10
  • the second stop 16 is formed in the form of a vertical boss 17, extending in the middle portion of the central neck 10, and extended by an inclined face 18, 19 to each of its upper and lower ends, the upper inclined pan 18 being more inclined than the inclined pan 19 lower.
  • four vertical ribs 20 regularly spaced from each other and oriented towards the inside are formed in the central wall 9 facing the central neck 10.
  • a closing latch 21 capable of cooperating with the turbine 7 is molded in plastic and is broken down into a discoid-shaped gripping member 22 extended by four longitudinal flat walls 24 oriented towards the external and intercalated with four longitudinal hollow walls, said planar walls 24 and hollow walls 25 being regularly spaced from each other and of the same length.
  • the flat walls 24 are in fact interconnected by plastic so as to form a rigid cross-shaped subset in cross section, which makes it possible to avoid any radial deformation of the flat walls 24.
  • this latch 21 is designed so that, on the one hand, the distance separating two flat walls or two diametrically opposite hollow walls is very slightly less than that separating two diametrically opposed clips of the turbine 7, and on the other hand, the length of said flat walls 24 and hollow walls 25 is sufficient to act respectively on the beads 12 and the shoulders 13 presented by the locking clips January 1 and the transmission clips 14 of the turbine 7 at the time of l inserting the lock 21.
  • a hub 26 adapted to cooperate with the turbine 7 is molded in plastic, and comprises a side wall in which have been formed four notches 27 regularly spaced from each other and sufficiently wide to accommodate each one of the locking clips January 1 of the turbine 7.
  • this side wall is equipped on its outer face with four indexing means 28 V-shaped, regularly spaced from each other.
  • the hub 26 is secured to a rotary motor 29 fixed in the volute 3 (not shown).
  • this lock 21 can then translate only between two extreme positions, namely, on the one hand, as shown in FIG. 11, an open position in which the lower part 30 of the contour of each hollow wall 25 is kept locked between the first stop 15 and the upper inclined face 18 of the second stop 16 of the transmission clip 14 associated, and on the other hand, as shown in Figure 9, a closed position in which the lower portion 30 of the contour of each hollow wall 25 is held blocked by the inclined pan 19 lower the second stop 16 of the transmission clip 14 associate.
  • each hollow wall 25 returns to its rest position when the lower part 30 opens into the space separating the second stop 16 from the first stop 15. The lower part 30 then comes into contact with the latter. which has been designed sufficiently protruding to constitute a stop.
  • each locking clip January 1 forces the bead 12 of each locking clip January 1 to abut against the upper edge of the notch 27 corresponding.
  • the flat wall 25 associated with each locking clip 1 1 is no longer there to act as a radial abutment, it follows that each locking clip 1 1 undergoes an elastic radial deformation oriented inwardly.
  • Each bead 12 is finally extracted from its corresponding notch 27 under the effect of traction, and the subassembly formed by the turbine 7 and the lock 21 is separated from the fan 1.
  • the user who has carried out a quick, simple and tool-less disassembly of the turbine 7, can then clean the blades 8 thereof.
  • the user reports the subassembly formed by the turbine 7 and the lock 21 on the associated hub 26, and exerts sufficient vertical thrust on the gripping member 22.
  • This vertical thrust is echoed on the upper inclined face 18 of each second abutment 16 by the lower portion 30 of the contour of the corresponding hollow wall 25 of the latch 21, and allows to automatically center the turbine 7 on the hub 26.
  • the upper inclined section 18 is designed so that the minimum stresses to be exerted by the vertical ribs of the turbine 7 on the indexing means 28 in the form of a V to force the hub 26 to pivot about its axis until 'that it is perfectly oriented are less than those necessary to cause the elastic deformation of each hollow wall 25 due to the sliding of the lower portion 30 of his contou r along said corresponding upper inclined section 18.
  • each hollow wall 25 is caused to slide successively along the upper inclined face 18, the boss 17, and finally the inclined pan 19 lower.
  • each flat wall 24 slides along the associated locking clip 11, until the lower end of its contour abuts against the radial shoulder 13 of said locking clip January 1.
  • This then has the effect of elastically deforming the locking clip 1 1 outwardly so that its radial bead 12 is properly housed in the corresponding notch 27 of the hub 26.
  • This blocking is also done in a simple manner, fast and without tools.
  • FIGS. 12 to 17 show a turbine 107 without its blades and according to the second preferred embodiment, as well as the associated locking latch 121 and hub 126.
  • the turbine 107 has a central neck 1 10 and differs mainly from the turbine 7 in that it has in the lower part two protuberances 130, arranged opposite one another on either side of the central neck 1 10, each equipped with a magnet January 1 constituting a locking means, and each provided with a longitudinal rib 120 oriented outwardly.
  • each link 1 14 has a first substantially cylindrical end 131, having a longitudinal edge 132 forming an abutment, and is connected by a rod 133. at a second end 134 projecting parallel to the axis 135 of said first end 131.
  • Each rod 1 14 is then secured to the turbine 107 through the axis 135 which is housed in two bores 137, formed in the protuberances 130 and located opposite one another.
  • the lock 121 comprises a gripping member 122 of discoid shape extended by a rod 138 in which is formed a groove 139 circular near its lower end.
  • the hub 126 is secured to a rotating motor 129, and is in the form of a metal disc 140 having a hollow circular central portion 141 in which are formed two notches 142 each intended to accommodate one of the ribs 120.
  • the factory assembly of the turbine 107 and the lock 121 in the hub 126 is made as follows. First, the second end 134 projecting from each link 1 14 is inserted into the groove 139 of the axis 140 of the lock 121 so that the lock 121 can only translate between two extreme positions, namely a closed position (not shown) and an open position shown in Figures 16 and 17. This subset thus formed is then attached to the hub
  • each link 14 pivots about its axis 135 in a direction forcing the edge 132 to move away from the bottom of the disc 140.
  • Each link 1 14 thus constitutes a transmission means enabling the magnets 1 1 1 to come into contact with the bottom of the disc 140.
  • Each link 1 14 thus constitutes a transmission means for extracting the locking means connecting the turbine 107 to the hub 126.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention concerns a removable impeller (7) designed to be integrated in a fan (1), in particular for controlled mechanical ventilation, and configured in the shape of a wheel provided with a plurality of blades (8) and equipped with locking means to enable its being fixed on a hub. The invention is characterized in that it comprises projecting transmitting means, arranged proximate a central neck whereof the axis of revolution is parallel to that of the wheel, and designed so as to enable the locking means to be alternately engaged or released. The invention also concerns a fan comprising such an impeller.

Description

TURBINE AMOVIBLE POUR VENTILATEUR REMOVABLE TURBINE FOR FAN
La présente invention se rapporte à une turbine amovible destinée à être intégrée dans un ventilateur, notamment pour la ventilation mécanique contrôlée, et réalisée sous la forme d'une roue munie d'une pluralité de pales et équipée de moyens de blocage pour permettre sa fixation sur un moyeu, ainsi qu'à un moyeu et un verrou de fermeture destinés à coopérer avec ladite turbine.The present invention relates to a removable turbine intended to be integrated in a fan, in particular for controlled mechanical ventilation, and made in the form of a wheel provided with a plurality of blades and equipped with locking means to enable it to be fixed. on a hub, and a hub and a latch for cooperating with said turbine.
De nombreux systèmes, comme par exemple les systèmes de bouches hygroréglables utilisées dans le cadre de la ventilation mécanique contrôlée, nécessitent l'emploi d'un ventilateur fournissant une dépression constante au cours du temps. Cette dépression constante peut être obtenue pour un coût réduit par régulation en vitesse d'un moteur entraînant une turbine à action. Néanmoins, l'inconvénient d'une telle turbine à action est d'être sensible à l'encrassement par la poussière et les graisses contenues dans l'air extrait. Une première solution connue pour surmonter ce problème consiste dans le fait de fixer à demeure la turbine sur le moteur associé, et de disposer un filtre en amont du ventilateur. Cependant, ce filtre crée une perte de charge défavorable au rendement du système, est encombrant, est d'un coût non négligeable, et il est nécessaire de le changer ou de le nettoyer régulièrement.Many systems, such as the humidity-controlled inlet systems used in the context of controlled mechanical ventilation, require the use of a fan providing a constant depression over time. This constant vacuum can be obtained for a reduced cost by speed regulation of a motor driving an action turbine. Nevertheless, the disadvantage of such an action turbine is to be sensitive to fouling by the dust and grease contained in the extracted air. A first known solution to overcome this problem is to permanently fix the turbine on the associated engine, and to have a filter upstream of the fan. However, this filter creates a loss of load unfavorable to the performance of the system, is cumbersome, is a significant cost, and it is necessary to change or clean it regularly.
Une deuxième solution connue consiste dans l'utilisation d'une turbine amovible, susceptible d'être nettoyée une fois, démontée. Les systèmes équipés d'une telle turbine prévoient que cette dernière est fixée par vissage sur un axe. Cette étape est néanmoins relativement délicate à mettre en oeuvre, tout particulièrement dans le cas de la ventilation mécanique contrôlée puisque l'occupant du logement procède lui-même au démontage et au nettoyage.A second known solution consists in the use of a removable turbine, capable of being cleaned once, disassembled. Systems equipped with such a turbine provide that the latter is fixed by screwing on an axis. This step is nevertheless relatively difficult to implement, especially in the case of controlled mechanical ventilation since the occupant of the housing itself dismantles and cleans.
L'invention a pour but de remédier à ces inconvénients et consiste pour cela en une turbine amovible destinée à être intégrée dans un ventilateur, notamment pour la ventilation mécanique contrôlée, et réalisée sous la forme d'une roue munie d'une pluralité de pales et équipée de moyens de blocage pour permettre sa fixation sur un moyeu, caractérisée en ce qu'elle comprend des moyens de transmission en saillie, positionnés à proximité d'un col central dont l'axe de révolution est parallèle à celui de la roue, et conçus de façon à permettre alternativement l'engagement ou l'extraction des moyens de blocage. Selon un premier mode de réalisation préféré de l'invention, les moyens de blocage sont ménagés dans le col central sous la forme d'une première série de clips de blocage régulièrement espacés les uns des autres et pourvus chacun en partie basse d'un bourrelet radial orienté vers l'extérieur. De plus, chaque clip de blocage possède de préférence en partie basse un épaulement radial orienté vers l'intérieur.The object of the invention is to remedy these drawbacks and for this purpose consists in a removable turbine intended to be integrated in a fan, in particular for controlled mechanical ventilation, and produced in the form of a wheel provided with a plurality of blades. and equipped with locking means to allow its attachment to a hub, characterized in that it comprises projecting transmission means, positioned near a central neck whose axis of revolution is parallel to that of the wheel, and designed to alternately allow engagement or extraction of the blocking means. According to a first preferred embodiment of the invention, the locking means are formed in the central neck in the form of a first series of locking clips regularly spaced from each other and each provided at the bottom of a bead radial outward. In addition, each locking clip preferably has a lower radial shoulder oriented inwards.
Avantageusement, les moyens de transmission sont ménagés dans le col central sous la forme d'une deuxième série de clips de transmission régulièrement espacés les uns des autres et intercalés avec les clips de blocage, chaque clip de transmission étant équipé d'une première butée et d'une deuxième butée positionnées l'une en dessous de l'autre et orientées vers l'intérieur, ladite première butée formant une saillie plus prononcée que la deuxième butée.Advantageously, the transmission means are formed in the central neck in the form of a second series of transmission clips regularly spaced from each other and interposed with the locking clips, each transmission clip being equipped with a first stop and a second abutment positioned one below the other and facing inwards, said first abutment forming a protrusion more pronounced than the second abutment.
Avantageusement encore, la première butée est ménagée en partie haute, et la deuxième butée est réalisée sous la forme d'un bossage longitudinal, s'étendant dans la partie médiane, et prolongé par un pan incliné à chacune de ses extrémités supérieure et inférieure.Advantageously, the first stop is formed in the upper part, and the second stop is made in the form of a longitudinal boss, extending in the middle portion, and extended by an inclined pan at each of its upper and lower ends.
La présente invention se rapporte également à un moyeu et à un verrou de fermeture conçus de façon à pouvoir coopérer avec une telle turbine. Le moyeu comprend préférentiellement une paroi latérale dans laquelle est ménagée une série d'encoches, chacune d'elles étant apte à loger l'un des moyens de blocage de la turbine, et le verrou de fermeture comprend un organe de préhension et des moyens aptes à coulisser au travers du col central de la turbine. Préférentiellement encore, l'organe de préhension est prolongé par une série de parois planes longitudinales intercalées avec une série de parois creuses longitudinales, lesdites parois planes et parois creuses étant régulièrement espacées les unes des autres et étant aptes à coulisser au travers du col central de la turbine.The present invention also relates to a hub and a closing latch designed so as to cooperate with such a turbine. The hub preferably comprises a side wall in which is formed a series of notches, each of them being able to accommodate one of the turbine blocking means, and the closing lock comprises a gripping member and suitable means to slide through the central neck of the turbine. Also preferably, the gripping member is extended by a series of longitudinal plane walls intercalated with a series of longitudinal hollow walls, said flat walls and hollow walls being regularly spaced from each other and being able to slide through the central collar of the turbine.
Dans une telle configuration, il est alors possible de procéder à une ouverture et à une fermeture séquencées.In such a configuration, it is then possible to proceed to a sequenced opening and closing.
En effet, lorsque le manipulateur exerce une traction suffisante sur l'organe de préhension du verrou, les clips de transmission présentant une rigidité radiale supérieure à celle des parois creuses, chaque paroi creuse subit une déformation élastique de sorte que la partie inférieure de son contour est amenée à glisser successivement le long du pan incliné inférieur, du bossage, et enfin du pan incliné supérieur de la deuxième butée. La paroi creuse retrouve ensuite sa position de repos dans l'intervalle séparant la première butée de la deuxième butée, et la partie inférieure du contour vient finalement au contact de la première butée. Ce faisant, les parois planes du verrou ne sont plus positionnées en face des clips de blocage, et ces derniers peuvent être extraits des encoches présentées par le moyeu si le manipulateur continue à exercer une traction suffisante sur l'organe de préhension. La turbine et son verrou sont alors désolidarisés du moyeu, et il est possible de procéder au nettoyage des pales de la turbine. Ce démontage se fait donc en un seul mouvement décomposé en deux temps, de façon simple, rapide et sans outil.Indeed, when the manipulator exerts sufficient traction on the gripping member of the latch, the transmission clips having a radial stiffness greater than that of the hollow walls, each hollow wall undergoes an elastic deformation so that the lower part of its outline is caused to slide successively along the lower inclined pan, the boss, and finally the upper inclined pan of the second stop. The hollow wall then returns to its rest position in the interval between the first stop of the second stop, and the lower portion of the contour finally comes into contact with the first stop. In doing so, the flat walls of the lock are no longer positioned in front of the locking clips, and these can be extracted from the notches presented by the hub if the manipulator continues to exert sufficient traction on the gripping member. The turbine and its lock are then disengaged from the hub, and it is possible to clean the blades of the turbine. This disassembly is done in one movement decomposed in two steps, simply, quickly and without tools.
Une fois que la turbine est correctement nettoyée, le manipulateur se saisit de l'organe de préhension du verrou et positionne correctement la turbine sur son moyeu. Il suffit alors d'exercer une poussée suffisante sur l'organe de préhension pour forcer la partie inférieure du contour de chaque paroi creuse à glisser successivement le long du pan incliné supérieur, du bossage, et enfin du pan incliné inférieur. Ce faisant, chaque paroi plane du verrou glisse le long du clip de blocage associé, jusqu'à ce que l'extrémité inférieure de son contour vienne en butée contre l'épaulement radial du clip de blocage. Ceci a alors pour effet de déformer élastiquement le clip de blocage vers l'extérieur de manière à ce que son bourrelet radial soit convenablement logé dans l'encoche correspondante. Ce blocage se fait donc également de façon .simple, rapide et sans outil.Once the turbine is properly cleaned, the manipulator seizes the latch gripper and correctly positions the turbine on its hub. It suffices then to exert sufficient thrust on the gripping member to force the lower part of the contour of each hollow wall to slide successively along the upper inclined face, the boss, and finally the lower inclined face. In doing so, each flat wall of the lock slides along the associated locking clip, until the lower end of its contour comes into abutment against the radial shoulder of the locking clip. This then has the effect of elastically deforming the locking clip outwardly so that its radial bead is properly housed in the corresponding notch. This blocking is therefore also simple .simple, fast and without tools.
Selon une variante de réalisation préférée de l'invention, la turbine comprend, en périphérie du col central, une paroi centrale sur laquelle sont ménagées des nervures longitudinales régulièrement espacées et orientées vers l'intérieur. De plus, la paroi latérale du moyeu est avantageusement équipée sur sa face extérieure de moyens d'indexage en forme de V. Ainsi, avec un tel aménagement, lorsque le verrou et la turbine sont rapportés sur le moyeu associé, une poussée suffisante exercée sur l'organe de préhension, qui est répercutée sur le pan incliné supérieur de chaque deuxième butée par la partie inférieure du contour de la paroi creuse correspondante du verrou, permet de centrer automatiquement la turbine sur le moyeu. En effet, ceci découle du fait que le pan incliné supérieur est conçu de façon à ce que les contraintes minimales devant être exercées par les nervures longitudinales de la turbine sur les moyens d'indexage en forme de V pour forcer le moyeu à pivoter jusqu'à ce qu'il soit parfaitement orienté sont inférieures à celles nécessaires pour provoquer la déformation élastique de chaque paroi creuse du fait du glissement de la partie inférieure de son contour le long dudit pan incliné supérieur correspondant. Cependant, une fois que la turbine est correctement positionnée en butée contre le moyeu, la poursuite de la poussée exercée par le manipulateur sur l'organe de préhension a alors pour effet de forcer le verrou à coulisser au travers du col central, jusqu'à ce qu'il vienne bloquer les clips de blocage dans les encoches associées par l'intermédiaire de ses parois planes. Une fois que le blocage de la turbine est assuré, la mise en rotation de la turbine par le moyeu est alors réalisée par l'intermédiaire des nervures longitudinales.According to a preferred embodiment of the invention, the turbine comprises, at the periphery of the central neck, a central wall on which are formed longitudinal ribs regularly spaced and oriented inwardly. In addition, the side wall of the hub is advantageously equipped on its outer face with V-shaped indexing means. Thus, with such an arrangement, when the lock and the turbine are attached to the associated hub, a sufficient thrust exerted on the gripping member, which is reflected on the upper inclined portion of each second abutment by the lower portion of the contour of the corresponding hollow wall of the latch, automatically centers the turbine on the hub. Indeed, this follows from the fact that the upper inclined pan is designed so that the minimum stresses to be exerted by the longitudinal ribs of the turbine on the V-shaped indexing means to force the hub to rotate until to what he are perfectly oriented are less than those necessary to cause the elastic deformation of each hollow wall due to the sliding of the lower part of its contour along said corresponding upper inclined pan. However, once the turbine is correctly positioned in abutment against the hub, the continuation of the thrust exerted by the manipulator on the gripping member then has the effect of forcing the latch to slide through the central neck, up to it comes to block the locking clips in the notches associated through its flat walls. Once the blocking of the turbine is ensured, the rotation of the turbine by the hub is then performed through the longitudinal ribs.
La turbine, le verrou et le moyeu sont avantageusement réalisés à l'aide de pièces moulées en plastique. Selon un deuxième mode réalisation préféré de l'invention, les moyens de blocage sont constitués par au moins deux aimants, et les moyens de transmission sont constitués par au moins deux biellettes comportant chacune une première extrémité sensiblement cylindrique présentant une arête longitudinale formant butée, et reliée par une tige à une seconde extrémité en saillie parallèle à l'axe de la première extrémité.The turbine, the lock and the hub are advantageously made using plastic moldings. According to a second preferred embodiment of the invention, the locking means consist of at least two magnets, and the transmission means consist of at least two links each comprising a first substantially cylindrical end having a longitudinal edge forming a stop, and connected by a rod to a second end projecting parallel to the axis of the first end.
La présente invention se rapporte également à un verrou de fermeture conçu de façon à coopère/ avec une turbine selon le deuxième mode de réalisation préféré de l'invention. Ce verrou comporte avantageusement un organe de préhension prolongé par une tige longitudinale dans laquelle est ménagée une rainure circulaire.The present invention also relates to a closing latch designed to cooperate / with a turbine according to the second preferred embodiment of the invention. This lock advantageously comprises a gripping member extended by a longitudinal rod in which is formed a circular groove.
La seconde extrémité formant saillie de chaque biellette est logée dans la rainure circulaire du verrou de façon à ce que la mise en translation de ce dernier force la première extrémité de la biellette à entrer en rotation. Par conséquent, aussi bien dans le premier que dans le deuxième mode de réalisation préféré de l'invention, il doit donc être bien compris que la turbine et le verrou peuvent être extraits et remis en place par un seul mouvement, de façon simple, rapide, sans apprentissage et sans outil. La présente invention se rapporte également à un ventilateur, notamment pour la ventilation mécanique contrôlée, comprenant un corps formant une volute dans lequel est fixé un moteur rotatif, un moyeu étant solidarisé audit moteur et supportant une turbine amovible pourvue d'un col central, d'une pluralité de pales et équipée de moyens de blocage pour permettre sa fixation sur le moyeu, caractérisé en ce que, - les moyens de blocage sont ménagés dans le col central sous la forme d'une première série de clips de blocage régulièrement espacés les uns des autres et pourvus chacun en partie basse, d'une part, d'un bourrelet radial orienté vers l'extérieur, et d'autre part, d'un épaulement radial orienté vers l'intérieur, - la turbine comprend des moyens de transmission ménagés dans le col central sous la forme d'une deuxième série de clips régulièrement espacés les uns des autres et intercalés avec les clips de blocage, chaque clip de transmission étant équipé d'une première butée et d'une deuxième butée positionnées l'une en dessous de l'autre et orientées vers l'intérieur, ladite première butée formant une saillie plus prononcée que la deuxième butée, ladite première butée étant ménagée en partie haute et ladite deuxième butée étant réalisée sous la forme d'un bossage longitudinal, s'étendant dans la partie médiane, prolongé respectivement par un pan fortement incliné à son extrémité supérieure et un pan faiblement incliné à son extrémité inférieure,The second end protruding from each link is housed in the circular groove of the lock so that the translation of the latter forces the first end of the link to rotate. Therefore, as well in the first as in the second preferred embodiment of the invention, it must be understood that the turbine and the lock can be extracted and replaced by a single movement, simply, quickly , without learning and without tools. The present invention also relates to a ventilator, in particular for controlled mechanical ventilation, comprising a body forming a volute in which is fixed a rotary motor, a hub being secured to said motor and supporting a removable turbine provided with a central neck, a plurality of blades and equipped with locking means to allow its attachment to the hub, characterized in that - the locking means are formed in the central neck in the form of a first series of locking clips regularly spaced from each other and each provided at the bottom, on the one hand, with a radial bead directed towards the outside, and on the other hand, an inwardly directed radial shoulder, the turbine comprises transmission means arranged in the central neck in the form of a second series of regularly spaced clips. the others and interposed with the locking clips, each transmission clip being provided with a first abutment and a second abutment positioned one below the other and facing inwards, said first stop forming a protrusion more pronounced than the second stop, said first stop being formed in the upper part and said second stop being made in the form of a longitudinal boss, extending in the middle part, extended respectively by a steeply inclined pan; at its upper end and a slightly inclined pan at its lower end,
- le moyeu comprend une paroi latérale dans laquelle est ménagée une série d'encoches, chacunç d'elles étant apte à loger l'un des clips de blocage de la turbine,- The hub comprises a side wall in which is formed a series of notches, each of them being adapted to accommodate one of the locking clips of the turbine,
- un verrou de fermeture est rapporté sur la turbine, ce verrou comprenant un organe de préhension prolongé par une série de parois planes longitudinales intercalées avec une série de parois creuses longitudinales, lesdites parois planes et parois creuses étant régulièrement espacées les unes des autres et étant aptes à coulisser au travers du col central de façon à être chacune respectivement disposée en regard d'un clip de blocage et d'un clip de transmission.- A closing lock is attached to the turbine, the latch comprising a gripping member extended by a series of longitudinal plane walls interposed with a series of longitudinal hollow walls, said flat walls and hollow walls being regularly spaced from each other and being slidable through the central neck so as to each respectively disposed opposite a locking clip and a transmission clip.
L'invention sera mieux comprise à l'aide de la description détaillée qui est exposée ci-dessous en regard du dessin annexé dans lequel :The invention will be better understood with the aid of the detailed description which is set out below with reference to the appended drawing in which:
La figure 1 est une vue en perspective d'un ventilateur selon l'invention, avec omission du capot de fermeture ; La figure 2 est une vue en perspective de dessus d'une turbine selon le premier mode de réalisation préféré de l'invention ;Figure 1 is a perspective view of a fan according to the invention, with omission of the closure cap; Figure 2 is a perspective view from above of a turbine according to the first preferred embodiment of the invention;
La figure 3 est une vue en perspective de dessous de la turbine représentée à la figure 2 ; La figure 4 est une vue en perspective d'un verrou de fermeture selon l'invention apte à coopérer avec la turbine représentée à la figure 2 ;Figure 3 is a perspective view from below of the turbine shown in Figure 2; Figure 4 is a perspective view of a locking latch according to the invention adapted to cooperate with the turbine shown in Figure 2;
La figure 5 est une vue en perspective d'un moyeu selon l'invention apte à coopérer avec la turbine représentée à la figure 2 ;Figure 5 is a perspective view of a hub according to the invention adapted to cooperate with the turbine shown in Figure 2;
La figure 6 est une vue en perspective de la turbine représentée à la figure 2 avec son verrou, avant fixation sur son moyeu correspondant ;Figure 6 is a perspective view of the turbine shown in Figure 2 with its lock, before fixing on its corresponding hub;
La figure 7 est une vue de dessus de la turbine représentée à la figure 6, une fois fixée sur son moyeu ;Figure 7 is a top view of the turbine shown in Figure 6, once fixed on its hub;
La figure 8 est une vue en coupe selon la ligne A-A de l'ensemble représenté à la figure 7, le verrou étant en position fermée ; La figure 9 est une vue en coupe selon la ligne B-B de l'ensemble représenté à la figure 7, le verrou étant en position fermée ;Figure 8 is a sectional view along the line A-A of the assembly shown in Figure 7, the latch being in the closed position; Figure 9 is a sectional view along the line B-B of the assembly shown in Figure 7, the latch being in the closed position;
La figure 10 est une vue en coupe selon la ligne A-A de l'ensemble représenté à la figure 7, le verrou étant en position ouverte ;Figure 10 is a sectional view along the line A-A of the assembly shown in Figure 7, the latch being in the open position;
La figure 1 1 est une vue en coupe selon la ligne B-B de l'ensemble représenté à la figure 7, le verrou étant en position ouverte ;Figure 1 1 is a sectional view along the line B-B of the assembly shown in Figure 7, the latch being in the open position;
La figure 12 est une vue en perspective d'une turbine selon le deuxième mode de réalisation préféré, avec omission des biellettes ;Figure 12 is a perspective view of a turbine according to the second preferred embodiment, with omission of the rods;
La figure 13 est une vue en perspective d'une biellette ;Figure 13 is a perspective view of a link;
La figure 14 est une vue en perspective d'un verrou selon l'invention apte à coopérer avec la turbine représentée à la figure 12 ;Figure 14 is a perspective view of a lock according to the invention adapted to cooperate with the turbine shown in Figure 12;
La figure 15 est une vue en perspective d'un moyeu selon l'invention apte à coopérer avec la turbine représentée à la figure 12 ;Figure 15 is a perspective view of a hub according to the invention adapted to cooperate with the turbine shown in Figure 12;
La figure 16 est une vue en perspective d'une moitié de turbine représentée à la figure 12, coupée longitudinalement au niveau des biellettes, avant fixation sur son moyeu correspondant ;Figure 16 is a perspective view of a turbine half shown in Figure 12, cut longitudinally at the rods, before fixing on its corresponding hub;
La figure 17 est une vue en perspective d'une autre moitié de turbine représentée à la figure 12, coupée longitudinalement au niveau des aimants, avant fixation sur son moyeu correspondant.Figure 17 is a perspective view of another turbine half shown in Figure 12, cut longitudinally at the magnets, before fixing on its corresponding hub.
Un ventilateur 1 selon l'invention, tel que représenté à la figure 1 , est destiné à la ventilation mécanique contrôlée et comprend un caisson 2 dont le capot de fermeture a été omis, et dans lequel est fixée une voluteA fan 1 according to the invention, as shown in FIG. 1, is intended for controlled mechanical ventilation and comprises a box 2 whose closing cap has been omitted, and in which is fixed a volute
3.3.
Le caisson 2 possède quatre raccords d'admission d'air 4, et chacun d'eux est mis en relation avec une pièce du logement à ventiler par l'intermédiaire d'un conduit d'aération (non représenté).The casing 2 has four air intake connectors 4, and each of them is connected to a part of the housing to be ventilated via an air duct (not shown).
La volute 3 est réalisée en matière plastique, et comporte de façon classique une entrée d'air 5 et une sortie d'air 6, l'entrée d'air 5 étant bordée par une ouïe 60 amovible fixée à l'aide de clips (non représentés). Comme représenté plus spécifiquement aux figures 1 à 3, la volute 3 contient une turbine 7, selon le premier mode de réalisation préféré de l'invention, prévue pour créer une dépression dans le caisson 1 de manière à aspirer l'air vicié provenant des raccords d'admission d'air 4.The volute 3 is made of plastic material, and conventionally comprises an air inlet 5 and an air outlet 6, the air inlet 5 being bordered by a removable inlet 60 fixed with clips ( not shown). As shown more specifically in FIGS. 1 to 3, the volute 3 contains a turbine 7, according to the first preferred embodiment of the invention, designed to create a depression in the casing 1 so as to suck stale air from the connections. air intake 4.
Cette turbine 7 est moulée en plastique sous la forme d'une roue équipée d'une pluralité de pales 8, et comprend une paroi centrale 9 cylindrique de révolution entourant un col central 10 dont l'axe de révolution vertical se confond avec celui de la roue.This turbine 7 is molded in plastic in the form of a wheel equipped with a plurality of blades 8, and comprises a cylindrical central wall 9 of revolution surrounding a central neck 10 whose vertical axis of revolution coincides with that of the wheel.
Plus précisément encore, quatre clips de blocage 1 1 verticaux régulièrement espacés les uns des autres sont ménagés dans le col central 10 de la turbine 7. Chaque clip de blocage 1 1 possède en partie basse, d'une part, un bourrelet 12 radial orienté vers l'extérieur, et d'autre part, un épaulement 1.3 radial orienté vers l'intérieur.More precisely, four vertical locking clips 1 1 regularly spaced from each other are formed in the central neck 10 of the turbine 7. Each locking clip January 1 has in the lower part, on the one hand, a radial bead 12 oriented outwardly, and secondly, a shoulder 1.3 radially oriented inwards.
De plus, quatre clips de transmission 14 verticaux régulièrement espacés les uns des autres, intercalés avec les clips de blocage 1 1 , de même longueur que ces derniers mais de largeur supérieure de façon à présenter une résistance accrue à la déformation radiale, sont également ménagés dans le col central 10.In addition, four vertical transmission clips 14 regularly spaced from each other, interposed with the locking clips January 1, of the same length as the latter but of greater width so as to have an increased resistance to radial deformation, are also provided in the central collar 10.
Chaque clip de transmission 14 est équipé d'une première butéeEach transmission clip 14 is equipped with a first stop
15 et d'une deuxième butée 16 orientées vers l'intérieur et ménagées à une certaine distance l'une en dessous de l'autre, ladite première butée 15 formant une saillie plus prononcée que la deuxième butée 16. La première butée 15 est ménagée en partie haute du col central 10, et la deuxième butée 16 est réalisée sous la forme d'un bossage 17 vertical, s'étendant dans la partie médiane du col central 10, et prolongé par un pan incliné 18, 19 à chacune de ses extrémités supérieure et inférieure, le pan incliné 18 supérieur étant plus incliné que le pan incliné 19 inférieur. Par ailleurs, quatre nervures 20 verticales régulièrement espacées les unes des autres et orientées vers l'intérieur sont ménagées dans la paroi centrale 9 en regard du col central 10.15 and a second stop 16 oriented inward and arranged at a distance one below the other, said first stop 15 forming a protrusion more pronounced than the second stop 16. The first stop 15 is formed in the upper part of the central neck 10, and the second stop 16 is formed in the form of a vertical boss 17, extending in the middle portion of the central neck 10, and extended by an inclined face 18, 19 to each of its upper and lower ends, the upper inclined pan 18 being more inclined than the inclined pan 19 lower. In addition, four vertical ribs 20 regularly spaced from each other and oriented towards the inside are formed in the central wall 9 facing the central neck 10.
Comme représenté à la figure 4, un verrou 21 de fermeture selon l'invention apte à coopérer avec la turbine 7 est moulé en plastique et se décompose en un organe de préhension 22 de forme discoïde prolongé par quatre parois planes 24 longitudinales orientées vers l'extérieur et intercalées avec quatre parois creuses 25 longitudinales, lesdites parois planes 24 et parois creuses 25 étant régulièrement espacées les unes des autres et de même longueur.As represented in FIG. 4, a closing latch 21 according to the invention capable of cooperating with the turbine 7 is molded in plastic and is broken down into a discoid-shaped gripping member 22 extended by four longitudinal flat walls 24 oriented towards the external and intercalated with four longitudinal hollow walls, said planar walls 24 and hollow walls 25 being regularly spaced from each other and of the same length.
Les parois planes 24 sont en fait reliées entre elles par de la matière plastique de manière à constituer un sous-ensemble rigide en forme de croix en section transversale, ce qui permet d'éviter toute déformation radiale des parois planes 24. De plus, il doit être bien compris que ce verrou 21 est conçu de façon à ce que, d'une part, la distance séparant deux parois planes ou deux parois creuses diamétralement opposées soit très légèrement inférieure à celle séparant deux clips diamétralement opposés de la turbine 7, et d'autre part, la longueur des desdites parois planes 24 et parois creuses 25 soit suffisante pour agir respectivement sur les bourrelets 12 et les épaulements 13 présentés par les clips de blocage 1 1 et les clips de transmission 14 de la turbine 7 lors de l'insertion du verrou 21.The flat walls 24 are in fact interconnected by plastic so as to form a rigid cross-shaped subset in cross section, which makes it possible to avoid any radial deformation of the flat walls 24. Moreover, It should be understood that this latch 21 is designed so that, on the one hand, the distance separating two flat walls or two diametrically opposite hollow walls is very slightly less than that separating two diametrically opposed clips of the turbine 7, and on the other hand, the length of said flat walls 24 and hollow walls 25 is sufficient to act respectively on the beads 12 and the shoulders 13 presented by the locking clips January 1 and the transmission clips 14 of the turbine 7 at the time of l inserting the lock 21.
Comme représenté à la figure 5, un moyeu 26 selon l'invention apte à coopérer avec la turbine 7 est moulé en plastique, et comprend une paroi latérale dans laquelle ont été ménagées quatre encoches 27 régulièrement espacées les unes des autres et suffisamment larges pour loger chacune l'un des clips de blocage 1 1 de la turbine 7. De plus, cette paroi latérale est équipée sur sa face extérieure de quatre moyens d'indexage 28 en forme de V, régulièrement espacés les uns des autres. Comme représenté schématiquement aux figures 6 à 1 1 , le moyeu 26 est rendu solidaire d'un moteur 29 rotatif fixé dans la volute 3 (non représenté).As shown in FIG. 5, a hub 26 according to the invention adapted to cooperate with the turbine 7 is molded in plastic, and comprises a side wall in which have been formed four notches 27 regularly spaced from each other and sufficiently wide to accommodate each one of the locking clips January 1 of the turbine 7. In addition, this side wall is equipped on its outer face with four indexing means 28 V-shaped, regularly spaced from each other. As shown schematically in Figures 6 to 1 1, the hub 26 is secured to a rotary motor 29 fixed in the volute 3 (not shown).
Lorsque le ventilateur 1 est installé dans le logement de l'utilisateur final, la turbine 7 et son verrou 21 ont été préalablement fixés sur le moyeu 26 en usine. Il doit être noté que ce verrou 21 ne peut alors se translater qu'entre deux positions extrêmes, à savoir, d'une part, comme représenté à la figure 1 1 , une position d'ouverture dans laquelle la partie inférieure 30 du contour de chaque paroi creuse 25 est maintenue bloquée entre la première butée 15 et le pan incliné 18 supérieur de la deuxième butée 16 du clip de transmission 14 associé, et d'autre part, comme représenté à la figure 9, une position de fermeture dans laquelle la partie inférieure 30 du contour de chaque paroi creuse 25 est maintenue bloquée par le pan incliné 19 inférieur de la deuxième butée 16 du clip de transmission 14 associé.When the fan 1 is installed in the housing of the end user, the turbine 7 and its latch 21 have been previously fixed on the hub 26 at the factory. It should be noted that this lock 21 can then translate only between two extreme positions, namely, on the one hand, as shown in FIG. 11, an open position in which the lower part 30 of the contour of each hollow wall 25 is kept locked between the first stop 15 and the upper inclined face 18 of the second stop 16 of the transmission clip 14 associated, and on the other hand, as shown in Figure 9, a closed position in which the lower portion 30 of the contour of each hollow wall 25 is held blocked by the inclined pan 19 lower the second stop 16 of the transmission clip 14 associate.
Lorsque l'utilisateur souhaite procéder au nettoyage de la turbine 7 à l'issue d'une certaine période de temps, il agit alors de la façon suivante.When the user wishes to proceed to the cleaning of the turbine 7 after a certain period of time, he then acts as follows.
Tout d'abord, il commence par décliper l'ouïe 60 amovible en tirant dessus.First, it begins by declawing the removable hearing 60 by pulling on it.
Une fois cette opération réalisée, l'utilisateur se saisit de l'organe de préhension 22 du verrou 21 et effectue une traction. Le verrou 21 qui était jusque-là en position de fermeture, comme représenté aux figures 8 et 9, est alors amené à coulisser vers le haut. En effet, la rigidité radiale des parois creuses 25 étant inférieure à celle des clips de transmission 14, la traction exercée a pour conséquence de forcer la partie inférieure 30 du contour de chaque paroi creuse 25 à se déformer élastiquement lors du glissement successif le long du pan incliné 19 inférieur, du bossage 17, et enfin du pan incliné 18 supérieur du clip de transmission 14 disposé en regard.Once this operation is performed, the user grasps the gripping member 22 of the latch 21 and pulls. The latch 21 which was hitherto in the closed position, as shown in Figures 8 and 9, is then caused to slide upwards. Indeed, since the radial rigidity of the hollow walls 25 is less than that of the transmission clips 14, the force exerted has the effect of forcing the lower part 30 of the contour of each hollow wall 25 to deform elastically during the successive sliding along the inclined pan 19 lower, the boss 17, and finally the upper inclined portion 18 of the transmission clip 14 arranged opposite.
Comme représenté aux figures 10 et 1 1 , chaque paroi creuse 25 retrouve sa position de repos lorsque la partie inférieure 30 débouche dans l'espace séparant la deuxième butée 16 de la première butée 15. La partie inférieure 30 vient alors au contact de cette dernière qui a été conçue suffisamment saillante pour constituer une butée d'arrêt.As represented in FIGS. 10 and 11, each hollow wall 25 returns to its rest position when the lower part 30 opens into the space separating the second stop 16 from the first stop 15. The lower part 30 then comes into contact with the latter. which has been designed sufficiently protruding to constitute a stop.
La poursuite du mouvement de traction force le bourrelet 12 de chaque clip de blocage 1 1 à venir buter contre le bord supérieur de l'encoche 27 correspondante. Or, la paroi plane 25 associée à chaque clip de blocage 1 1 n'étant plus là pour faire office de butée radiale, il en découle que chaque clip de blocage 1 1 subit une déformation élastique radiale orientée vers l'intérieur. Chaque bourrelet 12 est finalement extrait de son encoche 27 correspondante sous l'effet de la traction, et le sous- ensemble formé par la turbine 7 et le verrou 21 est désolidarisé du ventilateur 1 . L'utilisateur, qui a procédé à un démontage rapide, simple et sans outil de la turbine 7, peut alors nettoyer les pales 8 de celle-ci.The continuation of the traction movement forces the bead 12 of each locking clip January 1 to abut against the upper edge of the notch 27 corresponding. However, the flat wall 25 associated with each locking clip 1 1 is no longer there to act as a radial abutment, it follows that each locking clip 1 1 undergoes an elastic radial deformation oriented inwardly. Each bead 12 is finally extracted from its corresponding notch 27 under the effect of traction, and the subassembly formed by the turbine 7 and the lock 21 is separated from the fan 1. The user, who has carried out a quick, simple and tool-less disassembly of the turbine 7, can then clean the blades 8 thereof.
Une fois l'opération de nettoyage effectuée, l'utilisateur rapporte le sous-ensemble formé par la turbine 7 et le verrou 21 sur le moyeu 26 associé, et exerce une poussée verticale suffisante sur l'organe de préhension 22. Cette poussée verticale est répercutée sur le pan incliné 18 supérieur de chaque deuxième butée 16 par la partie inférieure 30 du contour de la paroi creuse 25 correspondante du verrou 21 , et permet de centrer automatiquement la turbine 7 sur le moyeu 26. En effet, ceci découle du fait que le pan incliné 18 supérieur est conçu de façon à ce que les contraintes minimales devant être exercées par les nervures 20 verticales de la turbine 7 sur les moyens d'indexage 28 en forme de V pour forcer le moyeu 26 à pivoter autour de son axe jusqu'à ce qu'il soit parfaitement orienté sont inférieures à celles nécessaires pour provoquer la déformation élastique de chaque paroi creuse 25 du fait du glissement de la partie inférieure 30 de son contour le long dudit pan incliné 18 supérieur correspondant.Once the cleaning operation has been carried out, the user reports the subassembly formed by the turbine 7 and the lock 21 on the associated hub 26, and exerts sufficient vertical thrust on the gripping member 22. This vertical thrust is echoed on the upper inclined face 18 of each second abutment 16 by the lower portion 30 of the contour of the corresponding hollow wall 25 of the latch 21, and allows to automatically center the turbine 7 on the hub 26. In fact, this follows from the fact that the upper inclined section 18 is designed so that the minimum stresses to be exerted by the vertical ribs of the turbine 7 on the indexing means 28 in the form of a V to force the hub 26 to pivot about its axis until 'that it is perfectly oriented are less than those necessary to cause the elastic deformation of each hollow wall 25 due to the sliding of the lower portion 30 of his contou r along said corresponding upper inclined section 18.
Cependant, une fois que la turbine 7 est correctement positionnée en butée contre le moyeu 26, la poursuite de la poussée verticale exercée par l'utilisateur a alors pour effet de forcer le verrou 21 à coulisser au travers du col central 10. Plus précisément, la partie inférieure 30 du contour de chaque paroi creuse 25 est amenée à glisser successivement le long du pan incliné 18 supérieur, du bossage 17, et enfin du pan incliné 19 inférieur. Ce faisant, chaque paroi plane 24 glisse le long du clip de blocage 1 1 associé, jusqu'à ce que l'extrémité inférieure de son contour vienne en butée contre l'épaulement 13 radial dudit clip de blocage 1 1 . Ceci a alors pour effet de déformer élastiquement le clip de blocage 1 1 vers l'extérieur de manière à ce que son bourrelet 12 radial soit convenablement logé dans l'encoche 27 correspondante du moyeu 26. Ce blocage se fait donc également de façon simple, rapide et sans outil.However, once the turbine 7 is properly positioned in abutment against the hub 26, the continuation of the vertical thrust exerted by the user then has the effect of forcing the latch 21 to slide through the central neck 10. More specifically, the lower part 30 of the contour of each hollow wall 25 is caused to slide successively along the upper inclined face 18, the boss 17, and finally the inclined pan 19 lower. In doing so, each flat wall 24 slides along the associated locking clip 11, until the lower end of its contour abuts against the radial shoulder 13 of said locking clip January 1. This then has the effect of elastically deforming the locking clip 1 1 outwardly so that its radial bead 12 is properly housed in the corresponding notch 27 of the hub 26. This blocking is also done in a simple manner, fast and without tools.
Une fois que le blocage de la turbine 7 est assuré, la mise en rotation de cette dernière par le moyeu 26 sous l'effet du moteur 29 est alors réalisée par l'intermédiaire des nervures 20 verticales.Once the blocking of the turbine 7 is ensured, the rotation of the latter by the hub 26 under the effect of the motor 29 is then performed through the ribs 20 vertical.
Aux figures 12 à 17 ont été représentées une turbine 107 sans ses pales et selon le second mode de réalisation préféré, ainsi que le verrou 121 de fermeture et le moyeu 126 associés. La turbine 107 possède un col central 1 10 et se différencie principalement de la turbine 7 par le fait qu'elle présente en partie basse deux protubérances 130, disposées en regard l'une de l'autre de part et d'autre du col central 1 10, équipées chacune d'un aimant 1 1 1 constituant un moyen de blocage, et pourvues chacune d'une nervure 120 longitudinale orientée vers l'extérieur.FIGS. 12 to 17 show a turbine 107 without its blades and according to the second preferred embodiment, as well as the associated locking latch 121 and hub 126. The turbine 107 has a central neck 1 10 and differs mainly from the turbine 7 in that it has in the lower part two protuberances 130, arranged opposite one another on either side of the central neck 1 10, each equipped with a magnet January 1 constituting a locking means, and each provided with a longitudinal rib 120 oriented outwardly.
Deux biellettes 1 14 sont fixées dans chaque protubérance 130 comme représenté plus spécifiquement aux figures 16 et 17. Plus précisément, chaque biellette 1 14 possède une première extrémité 131 sensiblement cylindrique, présentant une arête 132 longitudinale formant butée, et est reliée par une tige 133 à une seconde extrémité 134 en saillie parallèle à l'axe 135 de ladite première extrémité 131. Chaque biellette 1 14 est alors rendue solidaire de la turbine 107 grâce à l'axe 135 qui vient se loger dans deux alésages 137, ménagés dans les protubérances 130 et situés en regard l'un de l'autre.Two links 1 14 are fixed in each protuberance 130 as shown more specifically in FIGS. 16 and 17. More specifically, each link 1 14 has a first substantially cylindrical end 131, having a longitudinal edge 132 forming an abutment, and is connected by a rod 133. at a second end 134 projecting parallel to the axis 135 of said first end 131. Each rod 1 14 is then secured to the turbine 107 through the axis 135 which is housed in two bores 137, formed in the protuberances 130 and located opposite one another.
Le verrou 121 comporte un organe de préhension 122 de forme discoïde prolongé par une tige 138 dans laquelle est ménagée une rainure 139 circulaire à proximité de son extrémité inférieure.The lock 121 comprises a gripping member 122 of discoid shape extended by a rod 138 in which is formed a groove 139 circular near its lower end.
Le moyeu 126 est rendu solidaire d'un moteur 129 rotatif, et est réalisé sous la forme d'un disque 140 métallique possédant une partie centrale 141 circulaire creuse dans laquelle sont ménagées deux entailles 142 destinées chacune à loger l'une des nervures 120.The hub 126 is secured to a rotating motor 129, and is in the form of a metal disc 140 having a hollow circular central portion 141 in which are formed two notches 142 each intended to accommodate one of the ribs 120.
L'assemblage en usine de la turbine 107 et du verrou 121 dans le moyeu 126 est réalisé de la façon suivante. Tout d'abord, la seconde extrémité 134 formant saillie de chaque biellette 1 14 est insérée dans la rainure 139 de l'axe 140 du verrou 121 de façon à ce que le verrou 121 ne puisse se translater qu'entre deux positions extrêmes, à savoir une position de fermeture (non représentée) et une position d'ouverture représentée aux figures 16 et 17. Ce sous-ensemble ainsi formé est ensuite rapporté sur le moyeuThe factory assembly of the turbine 107 and the lock 121 in the hub 126 is made as follows. First, the second end 134 projecting from each link 1 14 is inserted into the groove 139 of the axis 140 of the lock 121 so that the lock 121 can only translate between two extreme positions, namely a closed position (not shown) and an open position shown in Figures 16 and 17. This subset thus formed is then attached to the hub
126. Lorsque le verrou 121 est abaissé pour venir en position de fermeture, chaque biellette 1 14 pivote autour de son axe 135 dans un sens forçant l'arête 132 à s'écarter du fond du disque 140. Chaque biellette 1 14 constitue ainsi un moyen de transmission permettant aux aimants 1 1 1 de venir au contact du fond du disque 140. Lorsque l'utilisateur souhaite procéder au nettoyage de la turbine 107, il se saisit de l'organe de préhension 122 et exerce une traction sur celui-ci. Chaque biellette 1 14 est alors entraînée dans un mouvement de rotation de sens contraire. L'arête 132 vient de ce fait en butée contre le fond du disque 140, ce qui a pour effet de démultiplier l'action de la traction exercée sur l'organe de préhension 122, et facilite grandement le décollement des aimants 1 1 1 du fond du disque 140. Chaque biellette 1 14 constitue ainsi un moyen de transmission permettant l'extraction des moyens de blocage reliant la turbine 107 au moyeu 126. Bien que l'invention ait été décrite en liaison avec des exemples particuliers de réalisation, il est bien évident qu'elle n'y est nullement limitée et qu'elle comprend tous les équivalents techniques des moyens décrits ainsi que leurs combinaisons si celles-ci entrent dans le cadre de l'invention. 126. When the latch 121 is lowered to come to the closed position, each link 14 pivots about its axis 135 in a direction forcing the edge 132 to move away from the bottom of the disc 140. Each link 1 14 thus constitutes a transmission means enabling the magnets 1 1 1 to come into contact with the bottom of the disc 140. When the user wishes to proceed with the cleaning of the turbine 107, he grasps the gripping member 122 and pulls on it. Each link 1 14 is then driven in a rotational movement of opposite direction. The edge 132 thus comes into abutment against the bottom of the disc 140, which has the effect of multiplying the action of the traction exerted on the gripping member 122, and greatly facilitates the separation of the magnets 1 1 1 of the The bottom of the disc 140. Each link 1 14 thus constitutes a transmission means for extracting the locking means connecting the turbine 107 to the hub 126. Although the invention has been described in connection with particular embodiments, it is it is quite obvious that it is in no way limited and that it includes all the technical equivalents of the means described and their combinations if they fall within the scope of the invention.

Claims

REVENDICATIONS
1 .- Turbine (7 ;107) amovible destinée à être intégrée dans un ventilateur (1 ), notamment pour la ventilation mécanique contrôlée, et réalisée sous la forme d'une roue munie d'une pluralité de pales (8) et équipée de moyens de blocage (1 1 ; 1 1 1 ) pour permettre sa fixation sur un moyeu (26 ; 126), caractérisée en ce qu'elle comprend des moyens de transmission (14 ;1 14) en saillie, positionnés à proximité d'un col central (10 ;1 10) dont l'axe de révolution est parallèle à celui de la roue, et conçus de façon à permettre alternativement l'engagement ou l'extraction des moyens de blocage.1 .- Turbine (7; 107) removable intended to be integrated in a fan (1), in particular for controlled mechanical ventilation, and carried out in the form of a wheel provided with a plurality of blades (8) and equipped with locking means (1 1; 1 1 1) to allow its attachment to a hub (26; 126), characterized in that it comprises projecting transmission means (14; 1 14), positioned near a central neck (10; 1 10) whose axis of revolution is parallel to that of the wheel, and designed to alternately allow the engagement or extraction of the locking means.
2.- Turbine (7) selon la revendication 1 , caractérisée en ce les moyens de blocage sont ménagés dans le col central sous la forme d'une première série de clips de blocage (1 1 ) régulièrement espacés les uns des autres et pourvus chacun en partie basse d'un bourrelet (12) radial orienté vers l'extérieur.2. Turbine (7) according to claim 1, characterized in that the locking means are formed in the central neck in the form of a first series of locking clips (1 1) regularly spaced from each other and provided with each in the lower part of a bead (12) radially oriented outwardly.
3.- Turbine (7) selon la revendication 2, caractérisée en ce que chaque clip de blocage (1 1 ) possède en partie basse un épaulement (13) radial orienté vers l'intérieur.3. Turbine (7) according to claim 2, characterized in that each locking clip (1 1) has in the lower part a shoulder (13) radially oriented inwardly.
4.- Turbine (7) selon l'une quelconque des revendications. 2 ou 3, caractérisée en ce que les moyens de transmission sont ménagés dans le col central (10) sous la forme d'une deuxième série de clips de transmission (14) régulièrement espacés les uns des autres et intercalés avec les clips de blocage (1 1 ), chaque clip de transmission étant équipé d'une première butée (15) et d'une deuxième butée (16) positionnées l'une en dessous de l'autre et orientées vers l'intérieur, ladite première butée formant une saillie plus prononcée que la deuxième butée. 4. Turbine (7) according to any one of claims. 2 or 3, characterized in that the transmission means are formed in the central neck (10) in the form of a second series of transmission clips (14) regularly spaced from each other and interposed with the locking clips ( 1 1), each transmission clip being provided with a first stop (15) and a second stop (16) positioned one below the other and facing inwards, said first stop forming a protrusion more pronounced than the second stop.
5. - Turbine (7) selon la revendication 4, caractérisée en ce que la première butée (15) est ménagée en partie haute, et en ce que la deuxième butée (16) est réalisée sous la forme d'un bossage (17) longitudinal, s'étendant dans la partie médiane, et prolongé par un pan incliné (18, 19) à chacune de ses extrémités supérieure et inférieure. 5. - Turbine (7) according to claim 4, characterized in that the first stop (15) is formed in the upper part, and in that the second stop (16) is formed as a boss (17) longitudinal, extending in the median portion, and extended by an inclined section (18, 19) at each of its upper and lower ends.
6.- Turbine (7) selon l'une quelconque des revendications 1 à 5, caractérisée en ce qu'elle comprend, en périphérie du col central (10), une paroi centrale (9) sur laquelle sont ménagées des nervures (20) longitudinales régulièrement espacées et orientées vers l'intérieur.6. Turbine (7) according to any one of claims 1 to 5, characterized in that it comprises, at the periphery of the central neck (10), a central wall (9) on which are formed longitudinal ribs (20) regularly spaced and oriented inwardly.
7.- Turbine (107) selon la revendication 1 , caractérisée en ce que les moyens de blocage sont constitués par au moins deux d'aimants (1 1 1 ), et en ce que les moyens de transmission sont constitués par au moins deux biellettes (1 14) comportant chacune une première extrémité (131 ) sensiblement cylindrique présentant une arête (132) longitudinale formant butée, et reliée par une tige (133) à une seconde extrémité (134) en saillie parallèle à l'axe de la première extrémité. 7. Turbine (107) according to claim 1, characterized in that the locking means are constituted by at least two magnets (1 1 1), and in that the transmission means are constituted by at least two links (1 14) each having a first substantially cylindrical end (131) having a longitudinal edge (132) forming a stop, and connected by a rod (133) to a second end (134) projecting parallel to the axis of the first end .
8.- Verrou (21 ;121 ) de fermeture destiné à être rapporté sur une turbine (7 ;107) selon l'une quelconque des revendications 1 à 7, caractérisé en ce qu'il comprend un organe de préhension (22 ;122) et des moyens (24, 25 ;138) aptes à coulisser au travers du col central (10 ;1 10) de la turbine. 8. Lock (21; 121) for closure to be mounted on a turbine (7; 107) according to any one of claims 1 to 7, characterized in that it comprises a gripping member (22; 122) and means (24, 25; 138) slidable through the central neck (10; 1 10) of the turbine.
9.- Verrou (21 ) selon la revendication 8, caractérisé en ce que l'organe de préhension (22) est prolongé par une série de parois planes (24) longitudinales intercalées avec une série de parois creuses (25) longitudinales, lesdites parois planes et parois creuses étant régulièrement espacées les unes des autres. 9. A latch (21) according to claim 8, characterized in that the gripping member (22) is extended by a series of longitudinal flat walls (24) interposed with a series of hollow walls (25) longitudinal, said walls planes and hollow walls being regularly spaced from each other.
10.- Verrou (121 ) selon la revendication 8, caractérisé en ce que l'organe de préhension (122) est prolongé par une tige (138) longitudinale dans laquelle est ménagée une rainure (139) circulaire.10. Lock (121) according to claim 8, characterized in that the gripping member (122) is extended by a rod (138) longitudinal in which is formed a groove (139) circular.
1 1 .- Moyeu (26) destiné à supporter une turbine (7) selon l'une quelconque des revendications 1 à 7, caractérisé en ce qu'il comprend une paroi latérale dans laquelle est ménagée une série d'encoches (27), chacune d'elles étant apte à loger l'un des moyens de blocage (1 1 ) de la turbine.1 1 .- Hub (26) for supporting a turbine (7) according to any one of claims 1 to 7, characterized in that it comprises a side wall in which is formed a series of notches (27), each of them being able to accommodate one of the locking means (1 1) of the turbine.
12.- Moyeu (26) selon la revendication 1 1 , caractérisé en ce que la paroi latérale est équipée sur sa face extérieure de moyens d'indexage (28) en forme de V.12. Hub (26) according to claim 1 1, characterized in that the side wall is equipped on its outer face with indexing means (28) V-shaped.
13,- Ventilateur (1 ), notamment pour la ventilation mécanique contrôlée, comprenant un corps formant une volute (3) dans lequel est fixé un moteur (29) rotatif, un moyeu (26) étant solidarisé audit moteur et supportant une turbine (7) amovible pourvue d'un col central (10), d'une pluralité de pales (8) et équipée de moyens de blocage pour permettre sa fixation sur le moyeu, caractérisé en ce que, - les moyens de blocage sont ménagés dans le col central sous la forme d'une première série de clips de blocage (1 1 ) régulièrement espacés les uns des autres et pourvus chacun en partie basse, d'une part, d'un bourrelet (12) radial orienté vers l'extérieur, et d'autre part, d'un épaulement (13) radial orienté vers l'intérieur,13, - Fan (1), in particular for controlled mechanical ventilation, comprising a body forming a volute (3) in which is fixed a motor (29) rotating, a hub (26) being secured to said motor and supporting a turbine (7). ) removable provided with a central neck (10), a plurality of blades (8) and equipped with locking means to allow its attachment to the hub, characterized in that, - The locking means are formed in the central neck in the form of a first series of locking clips (1 1) regularly spaced from each other and each provided at the bottom, on the one hand, with a bead ( 12) radially outwardly, and secondly, a shoulder (13) radially oriented inwardly,
- la turbine comprend des moyens de transmission ménagés dans le col central sous la forme d'une deuxième série de clips de transmission (14) régulièrement espacés les uns des autres et intercalés avec les clips de blocage, chaque clip de transmission étant équipé d'une première butée (15) et d'une deuxième butée (16) positionnées l'une en dessous de l'autre et orientées vers l'intérieur, ladite première butée formant une saillie plus prononcée que la deuxième butée, ladite première butée étant ménagée en partie haute et ladite deuxième butée étant réalisée sous la forme d'un bossage (17) longitudinal, s'étendant dans la partie médiane, prolongé par un pan incliné (18, 19) à chacune de ses extrémités supérieure et inférieure,- The turbine comprises transmission means formed in the central neck in the form of a second series of transmission clips (14) regularly spaced from each other and interposed with the locking clips, each transmission clip being equipped with a first stop (15) and a second stop (16) positioned one below the other and facing inwards, said first stop forming a protrusion more pronounced than the second stop, said first stop being provided at the top and said second stop being in the form of a boss (17) extending longitudinally in the median portion, extended by an inclined section (18, 19) at each of its upper and lower ends,
- le moyeu comprend une paroi latérale dans laquelle est ménagée une série d'encoches (27), chacune d'elles étant apte à loger l'un des clips de blocage de la turbine, - un verrou (21 ) de fermeture est rapporté sur la turbine, ce verrou comprenant un organe de préhension (22) prolongé par une série de parois planes (24) longitudinales intercalées avec une série de. parois creuses (25) longitudinales, lesdites parois planes et parois creuses étant régulièrement espacées les unes des autres et étant aptes à coulisser au travers du col central de façon à être chacune respectivement disposée en regard d'un clip de blocage et d'un clip de transmission. - The hub comprises a side wall in which is formed a series of notches (27), each of them being adapted to accommodate one of the locking clips of the turbine, - a latch (21) is closed on the turbine, this lock comprising a gripping member (22) extended by a series of longitudinal plane walls (24) interposed with a series of. hollow walls (25) longitudinal, said flat walls and hollow walls being regularly spaced from each other and being able to slide through the central neck so as to be respectively disposed opposite a locking clip and a clip of transmission.
EP06808188.4A 2005-09-22 2006-09-22 Removable impeller for fan Active EP1926916B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL06808188T PL1926916T3 (en) 2005-09-22 2006-09-22 Removable impeller for fan

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0509674A FR2891027B1 (en) 2005-09-22 2005-09-22 REMOVABLE TURBINE FOR FAN
PCT/FR2006/002170 WO2007034086A1 (en) 2005-09-22 2006-09-22 Removable impeller for fan

Publications (2)

Publication Number Publication Date
EP1926916A1 true EP1926916A1 (en) 2008-06-04
EP1926916B1 EP1926916B1 (en) 2020-05-06

Family

ID=36636485

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06808188.4A Active EP1926916B1 (en) 2005-09-22 2006-09-22 Removable impeller for fan

Country Status (8)

Country Link
US (1) US8292577B2 (en)
EP (1) EP1926916B1 (en)
JP (1) JP2009509090A (en)
CN (1) CN101268285A (en)
FR (1) FR2891027B1 (en)
HU (1) HUE050268T2 (en)
PL (1) PL1926916T3 (en)
WO (1) WO2007034086A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2891027B1 (en) * 2005-09-22 2008-01-11 Aereco Sa REMOVABLE TURBINE FOR FAN
US20110274568A1 (en) * 2010-05-10 2011-11-10 New Widetech Industries Co., Ltd. Blower for a dehumidifier
USD663411S1 (en) * 2010-05-19 2012-07-10 Panasonic Corporation Impeller of an electric fan
US9214840B2 (en) * 2010-06-14 2015-12-15 Panasonic Intellectual Property Management Co., Ltd. Fan motor, on-vehicle air conditioner using the fan motor, and method for assembling fan motor
USD667104S1 (en) * 2010-06-15 2012-09-11 Sharp Kabushiki Kaisha Cross-flow fan
USD667103S1 (en) * 2010-10-01 2012-09-11 Sharp Kabushiki Kaisha Cross-flow fan
EP3219607B1 (en) * 2014-11-10 2021-04-07 SZ DJI Technology Co., Ltd. Driving device, propeller and propulsion system
CN105134631A (en) * 2015-09-02 2015-12-09 广东美的环境电器制造有限公司 Fan heads, standing and wall-mounted fans, home appliances and blowing methods
WO2019026097A1 (en) * 2017-07-31 2019-02-07 三菱電機株式会社 Fan and indoor machine of air conditioning device provided with fan
CN110242602A (en) * 2019-06-19 2019-09-17 青岛海尔空调器有限总公司 Centrifugal fan and air conditioner with same
CN112081758B (en) * 2020-09-28 2024-12-13 珠海格力电器股份有限公司 Transmission structure and blowing device

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3870371A (en) * 1972-10-25 1975-03-11 Circle Eng Co Inc Driven plastic small vehicle wheel
JPS5553859Y2 (en) * 1977-12-20 1980-12-13
FR2420687A1 (en) * 1978-03-23 1979-10-19 Ferodo Sa DEVICE FOR FIXING A PLASTIC HUB PART ON A SHAFT
JPS6231798U (en) * 1985-08-13 1987-02-25
DE9017544U1 (en) * 1990-12-30 1991-03-21 Funken & Co. GmbH, 5202 Hennef Wheel
US5215356A (en) * 1992-10-20 1993-06-01 Lin Kuo Liang Wheel assembly for a baby carriage
US5716107A (en) * 1995-01-25 1998-02-10 Cascade Engineering, Inc. Wheel assembly
DE69836276T2 (en) * 1998-12-09 2007-09-13 Carrier Corp. Drive motor coupling for a cross-flow fan
DE69818276T2 (en) * 1998-12-10 2004-06-17 Carrier Corp. Construction of a drive shaft coupling for a cross-flow fan
DE10049341B4 (en) * 2000-10-05 2004-02-05 Pvs-Kunststofftechnik Gmbh & Co Detachable shaft-hub connection for fan wheels
FR2816380A1 (en) * 2000-11-08 2002-05-10 Faurecia Ind Cooling fan, for vehicle engine, has propeller hub mounted on primary end of shaft and secured by means of collar, rigidly fixed to shaft and securing fixing, such that collar forms axial support.
US6488474B2 (en) * 2001-01-08 2002-12-03 Wen-Hao Chuang Heat dissipating fan
US20040075356A1 (en) * 2002-10-16 2004-04-22 Sunonwealth Electric Machine Industry Co., Ltd. Fan rotor
DE202004010088U1 (en) * 2004-06-25 2004-09-09 Ebm-Papst Mulfingen Gmbh & Co. Kg Impeller, in particular for an axial fan
FR2891027B1 (en) * 2005-09-22 2008-01-11 Aereco Sa REMOVABLE TURBINE FOR FAN

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2007034086A1 *

Also Published As

Publication number Publication date
WO2007034086A1 (en) 2007-03-29
PL1926916T3 (en) 2021-04-06
US20080226447A1 (en) 2008-09-18
JP2009509090A (en) 2009-03-05
CN101268285A (en) 2008-09-17
HUE050268T2 (en) 2020-11-30
FR2891027B1 (en) 2008-01-11
FR2891027A1 (en) 2007-03-23
US8292577B2 (en) 2012-10-23
EP1926916B1 (en) 2020-05-06

Similar Documents

Publication Publication Date Title
EP1926916B1 (en) Removable impeller for fan
EP3239581B1 (en) Locking slide for fluid connector
EP1578675B1 (en) Closure cap for a bottle with controlled opening
EP1138879A1 (en) Turbine blade rotor disc assembly with fir-tree turbine blade root and assembly method therefore
EP3232887A1 (en) Cleaning appliance with airflow
EP0783928B1 (en) Method of crosspressing an at least locally cylindrical-formed workpiece into a tubular workpiece, tool for its application and use of the tool
EP2927491B1 (en) Fluid circulation pump provided with a motor which comprises two parts mounted freely in rotation
EP1021122B1 (en) Set comprising a spin drying device and a broom with a broom head and a handle
EP0491409B1 (en) Aeration device with rotatable and detachable closure element
FR2602660A1 (en) CUTTING ACCESSORY FOR A HOUSEHOLD APPLIANCE WORKING CONTAINER
FR2940198A1 (en) Head for diesel fuel filling pipe of tank of vehicle, has flap driven by tube from closed position to released position, and elongated flexible curved arms projected from periphery of ring and supported on inner surface of housing
EP1548170B1 (en) Door for rotating drum for washing machine and/or laundry dryer
FR2715543A1 (en) Case for stick of products, in particular cosmetics or pharmaceuticals and method of assembling this case.
EP2431641B1 (en) Fixing device of a connection piece of a fluid carrying pipe to a hollow wall
EP0724991A1 (en) Windscreen wiper with improved means for demounting its drive head
EP4241920B1 (en) Quick-lock roller surface renovation device
FR2652374A1 (en) HANDLE FOR A VEHICLE DOOR WITH A MOTOR.
FR2795443A1 (en) KEYS, ESPECIALLY A MOTOR VEHICLE, COMPRISING A PANNET PART AND A GRIP PART
FR2801734A1 (en) BOX WITH CLOSING DEVICES FOR LOCKING THE COVER ON THE BOX BODY AND WITH RETAINING LINK ASSOCIATED WITH ONE AT LEAST OF THESE CLOSING DEVICES, ESPECIALLY FOR ELECTRICAL EQUIPMENT
EP0213002A1 (en) Clutch bearing mounting
EP1003260A1 (en) Flush mounted box with fan foldings, in particular for electrical apparatus and its manufacturing process
FR2814090A1 (en) CENTRIFUGAL SEPARATOR AND BOWL THEREOF
EP2251554B1 (en) Attachment device between a handle rod of a roller shutter and a member rotatably connected to a shutter casing output or to the handle
EP1041350A1 (en) Fastening device for an air diffuser
FR2791945A1 (en) Water bottle carrier for bicycle has metal rod bent to form semi-circular branch and plastics frame forming mounting

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: 20080207

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20080710

DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

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: 20191018

RIN1 Information on inventor provided before grant (corrected)

Inventor name: BURIAS, OLIVIER

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

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

INTC Intention to grant announced (deleted)
INTG Intention to grant announced

Effective date: 20200121

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): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK 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

Ref country code: AT

Ref legal event code: REF

Ref document number: 1267191

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200515

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602006059390

Country of ref document: DE

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: SE

Ref legal event code: TRGR

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: AERECO

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20200506

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: 20200506

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: 20200506

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: 20200807

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: 20200906

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: 20200907

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

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: 20200506

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: 20200806

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E050268

Country of ref document: HU

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1267191

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200506

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

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: 20200506

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

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: 20200506

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: 20200506

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: 20200506

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: 20200506

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: 20200506

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: 20200506

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: 20200506

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602006059390

Country of ref document: DE

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: 20200506

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

26N No opposition filed

Effective date: 20210209

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: 20200506

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: 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: 20200506

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

Ref country code: LU

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

Effective date: 20200922

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

Ref country code: CH

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

Effective date: 20200930

Ref country code: LI

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

Effective date: 20200930

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: 20200506

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: 20200506

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

Ref country code: SE

Payment date: 20220920

Year of fee payment: 17

Ref country code: GB

Payment date: 20220921

Year of fee payment: 17

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

Ref country code: BE

Payment date: 20220909

Year of fee payment: 17

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230526

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20230930

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

Effective date: 20230922

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

Ref country code: GB

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

Effective date: 20230922

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

Ref country code: GB

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

Effective date: 20230922

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

Ref country code: SE

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

Effective date: 20230923

Ref country code: BE

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

Effective date: 20230930

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

Ref country code: DE

Payment date: 20240815

Year of fee payment: 19

Ref country code: IE

Payment date: 20240911

Year of fee payment: 19

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

Ref country code: FR

Payment date: 20240731

Year of fee payment: 19

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

Ref country code: PL

Payment date: 20240903

Year of fee payment: 19

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

Ref country code: HU

Payment date: 20240903

Year of fee payment: 19