EP0079256A1 - Static, dynamic and mechanical suction device for gases - Google Patents

Static, dynamic and mechanical suction device for gases Download PDF

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Publication number
EP0079256A1
EP0079256A1 EP82401875A EP82401875A EP0079256A1 EP 0079256 A1 EP0079256 A1 EP 0079256A1 EP 82401875 A EP82401875 A EP 82401875A EP 82401875 A EP82401875 A EP 82401875A EP 0079256 A1 EP0079256 A1 EP 0079256A1
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primary
mechanical
cap
fluid
pipe
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EP82401875A
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German (de)
French (fr)
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EP0079256B1 (en
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André Amphoux
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L17/00Inducing draught; Tops for chimneys or ventilating shafts; Terminals for flues
    • F23L17/02Tops for chimneys or ventilating shafts; Terminals for flues
    • F23L17/08Tops for chimneys or ventilating shafts; Terminals for flues with coaxial cones or louvres
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L17/00Inducing draught; Tops for chimneys or ventilating shafts; Terminals for flues
    • F23L17/005Inducing draught; Tops for chimneys or ventilating shafts; Terminals for flues using fans

Definitions

  • the invention relates to a device for vacuuming gaseous, static, dynamic and mechanical fluid, in particular gas or fumes discharged from a chimney or any outlet with a substantially vertical axis.
  • Vacuum cleaners are already known which are turrets composed of a hollow cap, a pipe which is integral with it and which is generally placed above the chimney, and means for extracting gaseous fluid.
  • these extraction means consist of one or more blades rotating around the longitudinal axis of the turret, by means of a motor, in particular an electric motor.
  • the means for extracting the gaseous fluid can be constituted by blades or a centrifugal turbine equipped for example with a two-speed motor, single-phase, etc.
  • Such turrets have several disadvantages.
  • the first drawback is that the hat has edges with a concavity directed downwards, or inclined downwards. The wind can rush in, depending on its direction, inside the cap and have an effect contrary to the device for accelerating the rejected gases, which results in a flow of the rejected gases lower than the desired flow.
  • the same drawbacks are found on turrets called "vertical jets", in the case of downwind.
  • the gas flow reje tees may vary depending on the wind direction.
  • a drawback lies in the fact that it is necessary to supply energy, for example electrical, to the motor so that it can rotate the blades or the centrifugal turbine.
  • Devices comprising a fan consisting of a first upper part formed by a conical internal surface and a rounded external surface and a second lower part formed by a conical internal surface and an external surface. rounded.
  • the first and second parts make it possible to extract the gaseous fluid statically.
  • a propeller actuated by a motor is placed in the lower part.
  • This propeller is much larger in diameter than the diameter of the fluid supply duct to be extracted.
  • this duct is cut at the level of the lower part and the fluid to be extracted spreads inside the lower part, namely between the conical internal surface and the rounded external surface.
  • this propeller rotates continuously.
  • the flow rate of extracted gas is not constant because the wind which rushes into the device can vary in speed over time.
  • an object of the invention is to provide a device aspirating gaseous fluids so that the flow rate of rejected fluids is adjusted to a desired value.
  • a device for aspirating gaseous fluid in particular of rejected gases or fumes, characterized in that it comprises in combination primary mechanical means for extracting gaseous fluid and static secondary means for extracting gaseous fluid cooperating so that the flow rate of extracted gaseous fluid is adjusted to a determined value.
  • the device comprises in combination are primary mechanical means for extracting gaseous fluid, static secondary means for extracting gaseous fluid, control means which allow the mechanical means to pass from the active state in the passive state and vice versa and adjustment means acting on the mechanical means to maintain the nominal flow rate of extracted gas flow at a minimum value.
  • the primary mechanical means for extracting fluid consist of a centrifugal or helical turbine driven by a motor.
  • the static secondary means consist of a lower element and an upper element superimposed, coaxial, rigidly fixed to one another, at a certain distance from each other by at least one spacer, the lower element comprising a bottom bottom and a bottom cap, each of them having a pseudo-frustoconical shape, the upper element comprising a top bottom, and upper cap, each of them having a pseudo-frustoconical shape, the bottom and the cap of the 'lower element being traversed coaxially by a pipe which is integral with them, which opens into the space between the two elements by an outlet orifice for gaseous fluids.
  • the primary mechanical means for extracting fluid are active as long as the flow rate of rejected fluid has not reached the desired minimum limit value and passive when the flow rate has reached this minimum value.
  • the device according to the invention therefore makes it possible to save energy which is currently becoming increasingly rare and more expensive.
  • devices of the venturi type comprising a lower element and an upper element each consisting of a cap and a bottom, make it possible to further increase the flow rate of fluid extracted by mechanical means.
  • the mechanical means are inactive, which saves money.
  • the gaseous fluid suction device comprises in combination a pipe 1, a circular hollow lower element 2, with which it is made integral.
  • the device according to the invention consists of primary mechanical means 17 for extracting fluid, means static secondary fluid extraction devices constituted by a venturi type device comprising a lower element 2 and an upper element 3.
  • the primary means 17 are more particularly constituted by a centrifugal turbine 18 (Figure 1) shown only schematically, not in itself part of the invention, within the reach of ordinary skill in the art.
  • the turbine 18 is powered by a motor 13, for example two-speed, single-phase or explosion-proof, etc.
  • the lower element 2 consists of a lower bottom 6 and a lower cap 7, each of them having a pseudo-conical shape of axis XX rigidly fixed to one another according to two large common bases 8 of circular outline.
  • the pipe 1 coaxially crosses the bottom bottom 6 and the bottom cap 7.
  • the upper element 3 consists of an upper bottom 14 and an upper cap 15, each of them having a pseudo-conical shape. These two elements are associated with each other along their large circular contour base 16. More particularly, the lower bottom 6 and the lower cap 7 have the shape of a truncated cone. The diameter of the small base of these truncated cones is substantially equal to the diameter of the pipe 1. Furthermore, the upper bottom 14 also preferably has the shape of a truncated cone, in the case of the centrifugal turbine and a conical shape in the case of the helical turbine.
  • the generatrices of the cones are inclined relative to a line perpendicular to the longitudinal axis XX of the device with an angle a of between 10 and 45 °, preferably 17 and 20 °.
  • the diameter of the large common bases 8 and 16 is between 2 to 3.5 times the diameter of pipe 1, preferably 2.5.
  • the difference d between the lower cap 7 and the upper bottom -14 calculated in line with the projection of the generator of the pipe 1 is between 0.35 and 0.8 times the diameter of the pipe 1, for example 0 , 5.
  • the spacers are joined to each other by a mesh screen, not shown, forming a cylindrical belt of axis XX.
  • the centrifugal turbine 18 sucks the gaseous fluids leaving the pipe 1 in a direction parallel to the longitudinal axis XX of the device, in the direction directed towards the inside of the device (arrow F1) and rejects the gases in a direction perpendicular to the axis XX, directed towards the outside of the device (arrow F2). Furthermore, the secondary extraction means constituted by the venturi 2,3 reject the gases in the direction of the arrow F2.
  • the control means 20 consist for example of a probe or a pressure switch. They are connected to the motor 19 to which they send pulses, in particular electrical.
  • a second embodiment of the invention is shown in Figure 2.
  • the primary means of increasing flow 17 are constituted by a propeller 21 comprising in particular two blades 22 and 23, which can pivot around the longitudinal axis XX of the device.
  • the blades 22 and 23 are driven by a motor 24 electrically connected to the control means 20 inside the pipe 1.
  • the blades 22 and 23 are arranged inside the pipe 1 so that the gaseous fluid only penetrates into the conduit 1 and does not enter the part situated between the conduit 1 and the lower bottom 6 and the lower cap 7 of the lower element. The action of the venturi is therefore not diminished by the presence of the propeller blades.
  • the blades 22, 23 of the propeller are located in the duct 1, at the level of the lower element 2.
  • the means 17 being constituted by a propeller, the latter rejects the fluids in a direction parallel to the axis XX.
  • the means 17 (namely the centrifugal turbine) if they reject the fluids in a direction perpendicular to the axis XX, are placed between the elements 2 and 3, so that the action of the primary mechanical extraction means 17 and secondary means 2 and 3 go in the same direction.
  • the means 17 namely the propeller 22, 23
  • the primary extraction means 17 are then passive.
  • the motors 19, 24 do not work, the control measuring device 20 then sending an electric control signal to these motors.
  • the primary means 17, if they are constituted by a heli-cold turbine 21, are active but are driven by the upward speed created by the depression caused by the venturi system 2, 3.
  • the propeller 21 rotates around its axis 25 .

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Centrifugal Separators (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

L'invention concerne un aspirateur de fluides gazeux. Un tel aspirateur comporte des moyens primaires mécaniques (17) d'extraction de fluide, des moyens secondaires statiques (2,3) d'extraction de fluide et éventuellement des moyens de commande (20) des moyens primaires (17). Les moyens secondaires comprennent un élément inférieur (2) et un élément supérieur (3) superposés, coaxiaux, rigidement fixés l'un à l'autre, à une certaine distance l'un de l'autre par au moins une entretoise (4) l'élément inférieur (2) comportant un fond inférieur (6) et un chapeau inférieur (7) chacun d'eux ayant une forme pseudo-tronconique, l'élément supérieur (3) comportant un fond supérieur (14) et un chapeau supérieur (15) chacun d'eux ayant une forme pseudo-tronconique, le fond (6) et le chapeau (7) de l'élément inférieur (2) étant traversés coaxialement par un tuyau (1) qui leur est solidaire. L'invention est applicable à l'extraction de gaz rejeté par une cheminée.The invention relates to a vacuum cleaner for gaseous fluids. Such a vacuum cleaner comprises mechanical primary means (17) for extracting fluid, static secondary means (2,3) for extracting fluid and possibly control means (20) for the primary means (17). The secondary means comprise a lower element (2) and an upper element (3) superimposed, coaxial, rigidly fixed to each other, at a certain distance from each other by at least one spacer (4) the lower element (2) comprising a lower bottom (6) and a lower cap (7) each of them having a pseudo-frustoconical shape, the upper element (3) comprising an upper bottom (14) and an upper cap (15) each of them having a pseudo-frustoconical shape, the bottom (6) and the cap (7) of the lower element (2) being traversed coaxially by a pipe (1) which is integral with them. The invention is applicable to the extraction of gas released from a chimney.

Description

L'invention concerne un dispositif aspirateur de fluide gazeux, statique, dynamique et mécanique, notamment de gaz ou de fumées rejetés d'une cheminée ou d'une sortie quelconque à axe sensiblement vertical.The invention relates to a device for vacuuming gaseous, static, dynamic and mechanical fluid, in particular gas or fumes discharged from a chimney or any outlet with a substantially vertical axis.

On connaît déjà des aspirateurs qui sont des tourelles composées d'un chapeau creux, d'un tuyau qui lui est solidaire et qui est placé en général au-dessus de la cheminée, et des moyens d'extraction de fluide gazeux.Vacuum cleaners are already known which are turrets composed of a hollow cap, a pipe which is integral with it and which is generally placed above the chimney, and means for extracting gaseous fluid.

En général, ces moyens d'extraction sont constitués par une ou plusieurs pales tournant autour de l'axe longitudinal de la tourelle, au moyens d'un moteur notamment électrique. Les moyens d'extraction du fluide gazeux peuvent être constitués par des pales ou une turbine centrifuge équipée par exemple d'un moteur à deux vitesses, monophasé, etc. De telles tourelles ont plusieurs inconvénients. Le premier inconvénient est que le chapeau comporte des bords à concavité dirigée vers le bas, ou inclinée vers le bas. Le vent peut s'engouffrer, selon sa direction, à l'intérieur du chapeau et avoir un effet contraire au dispositif d'accélération des gaz rejetés, ce qui entraîne un débit des gaz rejetés inférieur au débit désiré. Les mêmes inconvénients se retrouvent sur les tourelles dites "à jets verticaux", dans le cas de vent plongeant.In general, these extraction means consist of one or more blades rotating around the longitudinal axis of the turret, by means of a motor, in particular an electric motor. The means for extracting the gaseous fluid can be constituted by blades or a centrifugal turbine equipped for example with a two-speed motor, single-phase, etc. Such turrets have several disadvantages. The first drawback is that the hat has edges with a concavity directed downwards, or inclined downwards. The wind can rush in, depending on its direction, inside the cap and have an effect contrary to the device for accelerating the rejected gases, which results in a flow of the rejected gases lower than the desired flow. The same drawbacks are found on turrets called "vertical jets", in the case of downwind.

Ainsi, selon la direction du vent, le débit de gaz rejetés peut varier. Par ailleurs, un inconvénient réside dans le fait qu'il est nécessaire de fournir de l'énergie, par exemple électrique, au moteur pour qu'il puisse faire pivoter les pales ou la turbine centrifuge.Thus, depending on the wind direction, the gas flow reje tees may vary. Furthermore, a drawback lies in the fact that it is necessary to supply energy, for example electrical, to the motor so that it can rotate the blades or the centrifugal turbine.

On connaît par ailleurs des dispositifs comportant un ventilateur constitué d'une première partie supérieure formée d'une surface interne conique et d'une surface externe arrondie et d'une seconde partie inférieure formée d'une surface interne conique et d'une surface externe arrondie. La première et la seconde partie permettent d'extraire le fluide gazeux de façon statique. Un tel dispositif est décrit notamment dans les brevets américains n° 3 347 147 et n° 3 382 792. De plus, dans ces dispositifs, on place dans la partie inférieure une hélice actionnée par un moteur. Cette hélice est de diamètre beaucoup plus important que le diamètre du conduit d'amenée du fluide à extraire. Il en résulte que ce conduit est coupé au niveau de la partie inférieure et le fluide à extraire se répend à l'intérieur de la partie inférieure, à savoir entre la surface interne conique et la surface externe arrondie. Il en résulte que l'extraction de fluide se fait beaucoup moins bien, malgré la présence de l'hélice. En outre, cette hélice tourne continuellement. Ainsi, le débit de gaz extrait n'est pas constant car le vent qui s'engouffre dans le dispositif peut varier de vitesse dans le temps.Devices are also known comprising a fan consisting of a first upper part formed by a conical internal surface and a rounded external surface and a second lower part formed by a conical internal surface and an external surface. rounded. The first and second parts make it possible to extract the gaseous fluid statically. Such a device is described in particular in American patents No. 3,447,147 and No. 3,382,792. In addition, in these devices, a propeller actuated by a motor is placed in the lower part. This propeller is much larger in diameter than the diameter of the fluid supply duct to be extracted. As a result, this duct is cut at the level of the lower part and the fluid to be extracted spreads inside the lower part, namely between the conical internal surface and the rounded external surface. As a result, the extraction of fluid is much less well, despite the presence of the propeller. In addition, this propeller rotates continuously. Thus, the flow rate of extracted gas is not constant because the wind which rushes into the device can vary in speed over time.

L'invention a pour but de pallier ces inconvénients. Plus précisément, un but de l'invention est de fournir un dispositif aspirant des fluides gazeux de façon que le débit de fluides rejetés soit réglé à une valeur désirée.The invention aims to overcome these drawbacks. More specifically, an object of the invention is to provide a device aspirating gaseous fluids so that the flow rate of rejected fluids is adjusted to a desired value.

A cet effet, elle propose un dispositif aspirateur de fluide gazeux, notamment de gaz rejetés ou de fumées, caractérisé par le fait qu'il comporte en combinaison des moyens primaires mécaniques d'extraction de fluide gazeux et des moyens secondaires statiques d'extraction de fluide gazeux coopérant de façon que le débit de fluide gazeux extrait soit réglé à une valeur déterminée.To this end, it offers a device for aspirating gaseous fluid, in particular of rejected gases or fumes, characterized in that it comprises in combination primary mechanical means for extracting gaseous fluid and static secondary means for extracting gaseous fluid cooperating so that the flow rate of extracted gaseous fluid is adjusted to a determined value.

Plus particulièrement, le'dispositif comporte en combinai- sont des moyens primaires mécaniques d'extraction de fluide gazeux, des moyens secondaires statiques d'extraction de fluide gazeux, des moyens de commande qui permettent de faire passer les moyens mécaniques de l'état actif à l'état passif et inversement et des moyens de réglage agissant sur les moyens mécaniques pour maintenir le débit nominal de flux gazeux extrait à une valeur minimale.More particularly, the device comprises in combination are primary mechanical means for extracting gaseous fluid, static secondary means for extracting gaseous fluid, control means which allow the mechanical means to pass from the active state in the passive state and vice versa and adjustment means acting on the mechanical means to maintain the nominal flow rate of extracted gas flow at a minimum value.

Les moyens primaires mécaniques d'extraction de fluide sont constitués par une turbine centrifuge ou hélicoïde mue par un moteur.The primary mechanical means for extracting fluid consist of a centrifugal or helical turbine driven by a motor.

Les moyens secondaires statiques sont constitués par un élément inférieur et un élément supérieur superposés, coaxiaux, rigidement fixés l'un à l'autre, à une certaine distance l'un de l'autre par au moins une entretoise, l'élément inférieur comportant un fond inférieur et un chapeau inférieur, chacun d'eux ayant une forme pseudo-tronconique, l'élément supérieur comportant un fond supérieur, et chapeau supérieur, chacun d'eux ayant une forme pseudo-tronconique, le fond et le chapeau de l'élément inférieur étant traversés coaxialement par un tuyau qui leur est solidaire, qui débouche dans l'espace compris entre les deux éléments par un orifice dé sortie des fluides gazeux.The static secondary means consist of a lower element and an upper element superimposed, coaxial, rigidly fixed to one another, at a certain distance from each other by at least one spacer, the lower element comprising a bottom bottom and a bottom cap, each of them having a pseudo-frustoconical shape, the upper element comprising a top bottom, and upper cap, each of them having a pseudo-frustoconical shape, the bottom and the cap of the 'lower element being traversed coaxially by a pipe which is integral with them, which opens into the space between the two elements by an outlet orifice for gaseous fluids.

Les moyens de commande et de réglage des moyens primaires mécaniques se composent de moyens de détection de la valeur réelle du paramètre de commande tel que la pression du vent autour du dispositif ou la pression régnant à l'intérieur du dispositif

  • - de moyens de comparaison de cette valeur réelle et d'une valeur limite fixée.
  • - de moyens d'émission de signal de commande des moyens primaires mécaniques, en fonction de la position relative de la valeur réelle par rapport à la valeur limite.
The control and adjustment means of the mechanical primary means consist of means for detecting the real value of the control parameter such as the wind pressure around the device or the pressure prevailing inside the device
  • - means for comparing this real value and a fixed limit value.
  • - Control signal transmission means of the mechanical primary means, as a function of the relative position of the actual value with respect to the limit value.

Les moyens primaires mécaniques d'extraction de fluide sont actifs tant que le débit de fluide rejeté n'a pas atteint la valeur limite minimale désirée et passifs quand le débit a atteint cette valeur minimale.The primary mechanical means for extracting fluid are active as long as the flow rate of rejected fluid has not reached the desired minimum limit value and passive when the flow rate has reached this minimum value.

Le dispositif selon l'invention permet donc d'économiser l'énergie qui actuellement devient de plus en plus rare et plus chère. En effet, les dispositifs du type venturi comportant un élément inférieur et un élément supérieur constitués chacun d'un chapeau et d'un fond, permettent d'augmenter encore le débit de fluide extrait par les moyens mécaniques. Par ailleurs, lorsque le vent a une force suffisante, les moyens mécaniques sont inactifs, d'où une économie.The device according to the invention therefore makes it possible to save energy which is currently becoming increasingly rare and more expensive. Indeed, devices of the venturi type comprising a lower element and an upper element each consisting of a cap and a bottom, make it possible to further increase the flow rate of fluid extracted by mechanical means. In addition, when the wind has a sufficient force, the mechanical means are inactive, which saves money.

L'invention sera mieux comprise au regard des dessins annexés dans lesquels :

  • La figure 1 est une vue schématique du dispositif selon l'invention, les moyens mécaniques d'extraction de fluide étant une turbine centrifuge ; la figure 2 est une vue schématique du dispositif selon l'invention, les moyens mécaniques étant constitués par une turbine hélicoïde.
The invention will be better understood with reference to the appended drawings in which:
  • Figure 1 is a schematic view of the device according to the invention, the mechanical means for extracting fluid being a centrifugal turbine; Figure 2 is a schematic view of the device according to the invention, the mechanical means being constituted by a helical turbine.

Le dispositif aspirateur de fluide gazeux comporte en combinaison un tuyau 1, un élément inférieur 2 creux circulaire, avec lequel il est rendu solidaire.The gaseous fluid suction device comprises in combination a pipe 1, a circular hollow lower element 2, with which it is made integral.

Le dispositif selon l'invention est constitué de moyens primaires 17 mécaniques d'extraction de fluide, de moyens secondaires statiques d'extraction de fluide constitués par un dispositif du type venturi comportant un élément inférieur 2 et un élément supérieur 3.The device according to the invention consists of primary mechanical means 17 for extracting fluid, means static secondary fluid extraction devices constituted by a venturi type device comprising a lower element 2 and an upper element 3.

Les moyens primaires 17 sont constitués plus particulièrement par une turbine centrifuge 18 (figure 1) représentée seulement schématiquement, ne faisant pas en soi partie de l'invention, à la portée de l'homme de l'art. La turbine 18 est actionnée par un moteur 13 par exemple à deux vitesses, monophasé ou anti-déflagrant, etc.The primary means 17 are more particularly constituted by a centrifugal turbine 18 (Figure 1) shown only schematically, not in itself part of the invention, within the reach of ordinary skill in the art. The turbine 18 is powered by a motor 13, for example two-speed, single-phase or explosion-proof, etc.

Il comporte également des moyens secondaires d'extraction constitués par un élément supérieur 3 creux et circulaire placé à une certaine distance de l'élément inférieur 2 par une ou plusieurs tiges 4 ou entretoises. L'élément inférieur 2 est constitué d'un fond inférieur 6 et d'un chapeau inférieur 7, chacun d'eux ayant une forme pseudo-conique d'axe XX fixés rigidement l'un à l'autre suivant deux grandes bases communes 8 de contour circulaire. Le tuyau 1 traverse coaxialement le fond inférieur 6 et le chapeau inférieur 7.It also includes secondary extraction means constituted by a hollow and circular upper element 3 placed at a certain distance from the lower element 2 by one or more rods 4 or spacers. The lower element 2 consists of a lower bottom 6 and a lower cap 7, each of them having a pseudo-conical shape of axis XX rigidly fixed to one another according to two large common bases 8 of circular outline. The pipe 1 coaxially crosses the bottom bottom 6 and the bottom cap 7.

L'élément supérieur 3 est constitué d'un fond supérieur 14 et d'un chapeau supérieur 15, chacun d'eux ayant une forme pseudo-conique. Ces deux éléments sont associés l'un à l'autre suivant leur grande base de contour circulaire 16. Plus particulièrement, le fond inférieur 6 et le chapeau inférieur 7 ont une forme de cône tronqué. Le diamètre de la petite base de ces cônes tronqués est sensiblement égal au diamètre du tuyau 1. Par ailleurs, le fond supérieur 14 a lui aussi de préférence une forme de cône tronqué, dans le cas de la turbine centrifuge et une forme conique dans le cas de la turbine.hélicoïde. Les génératrices des cônes sont inclinées par rapport à une ligne perpendiculaire à l'axe longitudinal XX du dispositif d'un angle a compris entre 10 et 45° de préférence 17 et 20°. Le diamètre des grandes bases communes 8 et 16 est compris entre 2 à 3,5 fois le diamètre du tuyau 1 de préférence 2,5. De préférence, l'écart d entre le chapeau inférieur 7 et le fond supérieur-14 calculé au droit de la projection de la génératrice du tuyau 1 est compris entre 0,35 et 0,8 fois le diamètre du tuyau 1, par exemple 0,5.The upper element 3 consists of an upper bottom 14 and an upper cap 15, each of them having a pseudo-conical shape. These two elements are associated with each other along their large circular contour base 16. More particularly, the lower bottom 6 and the lower cap 7 have the shape of a truncated cone. The diameter of the small base of these truncated cones is substantially equal to the diameter of the pipe 1. Furthermore, the upper bottom 14 also preferably has the shape of a truncated cone, in the case of the centrifugal turbine and a conical shape in the case of the helical turbine. The generatrices of the cones are inclined relative to a line perpendicular to the longitudinal axis XX of the device with an angle a of between 10 and 45 °, preferably 17 and 20 °. The diameter of the large common bases 8 and 16 is between 2 to 3.5 times the diameter of pipe 1, preferably 2.5. Preferably, the difference d between the lower cap 7 and the upper bottom -14 calculated in line with the projection of the generator of the pipe 1 is between 0.35 and 0.8 times the diameter of the pipe 1, for example 0 , 5.

Les entretoises sont réunies les unes aux autres par un grillage à mailles, non représenté formant une ceinture cylindrique d'axe XX.The spacers are joined to each other by a mesh screen, not shown, forming a cylindrical belt of axis XX.

La turbine centrifuge 18 aspire les fluides gazeux sortant du tuyau 1 selon une direction parallèle à l'axe longitudinal XX du dispositif, dans le sens dirigé vers l'intérieur du dispositif (flèche Fl) et rejette les gaz selon une direction perpendiculaire à l'axe XX, dirigée vers l'extérieur du dispositif (flèche F2). Par ailleurs, les moyens secondaires d'extraction constitués par le venturi 2,3 rejettent les gaz en direction de la flèche F2.The centrifugal turbine 18 sucks the gaseous fluids leaving the pipe 1 in a direction parallel to the longitudinal axis XX of the device, in the direction directed towards the inside of the device (arrow F1) and rejects the gases in a direction perpendicular to the axis XX, directed towards the outside of the device (arrow F2). Furthermore, the secondary extraction means constituted by the venturi 2,3 reject the gases in the direction of the arrow F2.

Le dispositif comporte des moyens de commande et de réglage 20 de moyens primaires mécaniques 17 qui se composent

  • - de moyens de détection de la valeur réelle du paramètre de commande tel que la pression du vent autour du dispositif ou la pression régnant à l'intérieur du dispositif
  • - de moyens de comparaison de cette valeur réelle et d'une valeur limite fixée
  • - de moyens d'émission de signal de commande des moyens primaires mécaniques en fonction de la position relative de la valeur réelle par rapport à la valeur limite.
The device comprises control and adjustment means 20 of mechanical primary means 17 which are composed
  • - means for detecting the real value of the control parameter such as the wind pressure around the device or the pressure prevailing inside the device
  • - means of comparison of this real value and a fixed limit value
  • - Control signal transmission means of the mechanical primary means as a function of the relative position of the actual value with respect to the limit value.

Les moyens de commande 20 sont constitués par exemple d'une sonde ou d'un pressostat. Ils sont reliés au moteur 19 auquel ils envoient des impulsions, notamment électriques.The control means 20 consist for example of a probe or a pressure switch. They are connected to the motor 19 to which they send pulses, in particular electrical.

Un second mode de réalisation de l'invention est représenté sur la figure 2. Les moyens primaires d'augmentation du débit 17 sont constitués par une hélice 21 comportant notamment deux pales 22 et 23, pouvant pivoter autour de l'axe XX longitudinal du dispositif. Les pales 22 et 23 sont mues par un moteur 24 relié électriquement au moyen de commande 20 à l'intérieur du tuyau 1. Les pales 22 et 23 sont disposées à l'intérieur du tuyau 1 de sorte que le fluide gazeux ne pénètre que dans le conduit 1 et ne pénètre pas dans la partie située entre le conduit 1 et le fond inférieur 6 et le chapeau inférieur 7 de l'élément inférieur. L'action du venturi n'est donc pas diminuée par la présence despales de l'hélice. Les pales 22, 23 de l'hélice sont situées dans le conduit 1, au niveau de l'élément inférieur 2.A second embodiment of the invention is shown in Figure 2. The primary means of increasing flow 17 are constituted by a propeller 21 comprising in particular two blades 22 and 23, which can pivot around the longitudinal axis XX of the device. The blades 22 and 23 are driven by a motor 24 electrically connected to the control means 20 inside the pipe 1. The blades 22 and 23 are arranged inside the pipe 1 so that the gaseous fluid only penetrates into the conduit 1 and does not enter the part situated between the conduit 1 and the lower bottom 6 and the lower cap 7 of the lower element. The action of the venturi is therefore not diminished by the presence of the propeller blades. The blades 22, 23 of the propeller are located in the duct 1, at the level of the lower element 2.

Les moyens 17 étant constitués par une hélice, celle-ci rejette les fluides selon une direction parallèle à l'axe XX.The means 17 being constituted by a propeller, the latter rejects the fluids in a direction parallel to the axis XX.

Les moyens 17 (à savoir la turbine centrifuge) s'ils rejettent les fluides selon une direction perpendiculaire à l'axe XX, sont placés entre les éléments 2 et 3, pour que l'action des moyens primaires mécaniques d'extraction 17 et des moyens secondaires 2 et 3 aillent dans le même sens.The means 17 (namely the centrifugal turbine) if they reject the fluids in a direction perpendicular to the axis XX, are placed between the elements 2 and 3, so that the action of the primary mechanical extraction means 17 and secondary means 2 and 3 go in the same direction.

Lorsque les moyens 17 (à savoir l'hélice 22, 23) rejettent les fluides selon une direction parallèle à l'axe longitudinal XX du dispositif ils sont placés à l'intérieur du tuyau 1. Ils viennent donc augmenter le débit du fluide qui traverse le tuyau 1, tandis que les moyens 17 qui rejettent les fluides selon une direction perpendiculaire à l'axe XX, augmentent le débit des gaz sortant du tuyau 1.When the means 17 (namely the propeller 22, 23) reject the fluids in a direction parallel to the longitudinal axis XX of the device they are placed inside the pipe 1. They therefore increase the flow rate of the fluid which passes through the pipe 1, while the means 17 which reject the fluids in a direction perpendicular to the axis XX, increase the flow rate of the gases leaving the pipe 1.

Le fonctionnement est le suivant :

  • Lorsque le vent est insuffisant pour obtenir un débit désiré de fluide rejeté, les moyens 17 primaires sont actifs, c'est-à-dire que les moteurs 19, 24 fonctionnent. Le débit de fluide sortant des moyens 17 primaires est augmenté par les moyens secondaires 2, 3.
The operation is as follows:
  • When the wind is insufficient to obtain a desired flow rate of rejected fluid, the primary means 17 are active, that is to say that the motors 19, 24 operate. The flow of fluid leaving the primary means 17 is increased by secondary means 2, 3.

Lorsque le vent a une force suffisante, le débit de fluide sortant du dispositif atteint la valeur minimum désirée, et s'il la dépasse, les moyens primaires d'extraction 17 sont alors passifs. Les moteurs 19, 24 ne fonctionnent pas, le dispositif de mesure de commande 20 envoyant alors un signal électrique de commande à ces moteurs. Les moyens primaires 17, s'ils sont constitués par une turbine héli- colde 21, sont actifs mais sont entraînés par la vitesse ascensionnelle créée par la dépression provoquée par le système venturi 2, 3. L'hélice 21 tourne autour de son axe 25.When the wind has a sufficient force, the flow of fluid leaving the device reaches the minimum desired value, and if it exceeds it, the primary extraction means 17 are then passive. The motors 19, 24 do not work, the control measuring device 20 then sending an electric control signal to these motors. The primary means 17, if they are constituted by a heli-cold turbine 21, are active but are driven by the upward speed created by the depression caused by the venturi system 2, 3. The propeller 21 rotates around its axis 25 .

Les avantages de l'application du venturi aux moyens mécaniques 17 peuvent se résumer :

  • a) pour la turbine centrifuge, à un meilleur rendement de celle-ci, procuré par une amélioration de la pénétration des fluides gazeux extraits dans l'atmosphère, avec l'assurance de toujours obtenir un débit nominal déterminé. Donc, à moteur égal par rapport aux dispositifs connus, on obtient des débits plus importants correspondants.
  • b) pour la turbine hélicoïde, on obtient de même une meilleure pénétration des fluides gazeux, dont à puissance de moteur égale, des débits plus importants, et en outre, on a la possibilité d'extraire naturellement, sans faire fonctionner le moteur, dès que la vitesse du vent est suffisante pour extraire le débit nominal fixé.
The advantages of applying the venturi to mechanical means 17 can be summarized:
  • a) for the centrifugal turbine, at a better efficiency thereof, provided by an improvement in the penetration of gaseous fluids extracted into the atmosphere, with the assurance of always obtaining a determined nominal flow rate. Therefore, with an equal engine compared to known devices, corresponding higher flow rates are obtained.
  • b) for the helical turbine, we also obtain a better penetration of gaseous fluids, which at equal engine power, higher flow rates, and in addition, we have the possibility of extracting naturally, without running the engine, as soon as that the wind speed is sufficient to extract the nominal flow rate set.

Claims (9)

1. Dispositif aspirateur de fluide gazeux, notamment de gaz rejetés ou de fumées, caractérisé par le fait qu'il comporte des moyens primaires mécaniques (17) d'extraction de fluide, des moyens secondaires statiques (2,3) de fluide et éventuellement des moyens de commande et de réglage (20) permettant de rendre actifs ou passifs les moyens primaires (17) lorsque le débit de fluide gazeux atteint une valeur prédéterminée.1. Device for aspirating gaseous fluid, in particular of rejected gases or fumes, characterized in that it comprises mechanical primary means (17) of fluid extraction, static secondary means (2,3) of fluid and possibly control and adjustment means (20) making it possible to make the primary means (17) active or passive when the flow rate of gaseous fluid reaches a predetermined value. 2. Dispositif selon la revendication 1, caractérisé par le fait que les moyens secondaires statiques sont constitués par un élément inférieur (2) et un élément supérieur (3) superposés, coaxiaux, rigidement fixés l'un à l'autre, à une certaine distance l'un de l'autre par au moins une entretoise (4), l'élément inférieur (2) comportant un fond inférieur (6) et un chapeau inférieur (7), chacun d'eux ayant une forme pseudo-tronconique, l'élément supérieur (3) comportant un fond supérieur (14) et un chapeau supérieur (15) chacun ayant une forme pseudo-tronconique, le fond (6) et le chapeau (7) de l'élément inférieur (2) étant traversés coaxialement par un tuyau (1) qui leur est solidaire, qui débouche dans l'espace compris entre les deux éléments (2, 3) par un orifice de sortie de fluide gazeux.2. Device according to claim 1, characterized in that the static secondary means are constituted by a lower element (2) and an upper element (3) superimposed, coaxial, rigidly fixed to each other, to a certain distance from each other by at least one spacer (4), the lower element (2) comprising a lower bottom (6) and a lower cap (7), each of them having a pseudo-frustoconical shape, the upper element (3) comprising an upper bottom (14) and an upper cap (15) each having a pseudo-frustoconical shape, the bottom (6) and the cap (7) of the lower element (2) being traversed coaxially by a pipe (1) which is integral with them, which opens into the space between the two elements (2, 3) through a gaseous fluid outlet orifice. 3. Dispositif selon l'une quelconque des revendications 1 et 2, caractérisé par le fait que les moyens primaires mécaniques d'extraction (17) sont actifs, quand le débit désiré de fluide rejeté est inférieur à une valeur minimale désirée et sont passifs quand le débit atteint la valeur minimale.3. Device according to any one of claims 1 and 2, characterized in that the primary mechanical extraction means (17) are active, when the desired flow rate of rejected fluid is less than a minimum desired value and are passive when the flow reaches the minimum value. 4. Dispositif selon l'une quelconque des revendications 1 à 3, caractérisé par le fait que les moyens secondaires mécaniques (17) de débit sont constitués par une turbine centrifuge (18) mue par un moteur (19), la turbine centrifuge-(18) étant placée entre les éléments (2 et 3), coaxialement au dispositif.4. Device according to any one of claims 1 to 3, characterized in that the secondary mechanical means (17) of flow consist of a turbine centrifugal (18) driven by a motor (19), the centrifugal impeller (18) being placed between the elements (2 and 3), coaxially with the device. 5. Dispositif selon l'une quelconque des revendications 1 à 3, caractérisé par le fait que les moyens primaires mécaniques (17) sont constitués par une turbine hélicoïde (21) comportant au moins deux pales (22, 23.) pivotant autour de l'axe (25) coaxial à l'axe XX, les pales étant mues par un moteur (24) et étant placées à l'intérieur du tuyau (1).5. Device according to any one of claims 1 to 3, characterized in that the primary mechanical means (17) consist of a helical turbine (21) comprising at least two blades (22, 23.) pivoting around the axis (25) coaxial with axis XX, the blades being driven by a motor (24) and being placed inside the pipe (1). 6. Dispositif selon l'une quelconque des revendications 1 à 5, caractérisé par le fait que les moyens de commande et de réglage (20) des moyens primaires mécaniques (17) se composent : - de moyens de détection de la valeur réelle du paramètre décommande tel que la pression du vent autour du dispositi- ou la dépression régnant à l'intérieur du dispositif, - de moyens de comparaison de cette valeur réelle et d'une valeur limite fixée, - de moyens d'émission de signal de commande des moyens primaires mécaniques, en fonction de la position relative de la valeur réelle par rapport à la valeur limite. 6. Device according to any one of claims 1 to 5, characterized in that the control and adjustment means (20) of the mechanical primary means (17) consist of: - means for detecting the actual value of the control parameter such as the wind pressure around the device or the vacuum prevailing inside the device, - means for comparing this real value and a fixed limit value, - Control signal transmission means of the mechanical primary means, as a function of the relative position of the actual value with respect to the limit value. 7. Dispositif selon l'une quelconque des revendications 1 à 6, caractérisé par le fait que lorsque les moyens (17) sont constitués par une turbine centrifuge, le fond supérieur (14) a une forme de tronc de cône.7. Device according to any one of claims 1 to 6, characterized in that when the means (17) consist of a centrifugal turbine, the upper bottom (14) has the shape of a truncated cone. 8. Dispositif selon l'une quelconque des revendications 1 à 6, caractérisé par le fait que lorsque les moyens (17) sont constitués par une turbine hélicoïde, le fond supérieur (14) à une forme de cône et les pales de l'hélice sont situées dans le conduit 1, au niveau de l'élément inférieur 2.8. Device according to any one of claims 1 to 6, characterized in that when the means (17) consist of a helical turbine, the upper bottom (14) has a cone shape and the blades of the propeller are located in the duct 1, at the level of the lower element 2. 9. Dispositif selon l'une quelconque des revendications 1 à 8, caractérisé par le fait que l'écard d entre le chapeau inférieur (7) et le fond supérieur (14) calculé au droit de la projection de la génératrice du tuyau (1) est compris entre 0,35 et 0,8 fois le diamètre du tuyau (1), par exemple 0,5.9. Device according to any one of claims 1 to 8, characterized in that the difference d between the lower cap (7) and the upper bottom (14) calculated in line with the projection of the generator of the pipe (1 ) is between 0.35 and 0.8 times the diameter of the pipe (1), for example 0.5.
EP82401875A 1981-10-13 1982-10-12 Static, dynamic and mechanical suction device for gases Expired EP0079256B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8119229A FR2514469B1 (en) 1981-10-13 1981-10-13 STATIC, DYNAMIC AND MECHANICAL GAS FLUID VACUUM DEVICE
FR8119229 1981-10-13

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EP0079256A1 true EP0079256A1 (en) 1983-05-18
EP0079256B1 EP0079256B1 (en) 1989-09-20

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US (1) US4462305A (en)
EP (1) EP0079256B1 (en)
DE (1) DE3279952D1 (en)
FR (1) FR2514469B1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
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EP0082775A2 (en) * 1981-12-18 1983-06-29 André Amphoux Cowl for gaseous fluid
EP0196659A2 (en) * 1985-04-02 1986-10-08 Licencia Talalmanyokat Ertekesito Es Innovacios Külkereskedelmi Vallalat Draught intensifying apparatus
FR2647881A1 (en) * 1989-05-30 1990-12-07 Amphoux Andre MIXED VENTILATION DEVICE FOR A HOUSE
EP0641973A1 (en) * 1993-09-03 1995-03-08 André Amphoux Device for gaseous fluid removal
EP0641972A1 (en) * 1993-09-03 1995-03-08 André Amphoux Static dynamic device for gaseous fluid removal

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FR2651563B1 (en) * 1989-09-06 1991-12-27 Amphoux Andre GAS SUCTION DEVICE.
FR2658271B1 (en) * 1990-02-09 1995-01-06 Andre Amphoux DEVICE FOR SUCTION AND RELEASE OF GASES OR SMOKE AND INSTALLATION COMPRISING A PLURALITY OF SUCH DEVICES.
FR2740862B1 (en) 1995-11-03 1998-01-23 Amphoux Andre DEVICE FOR SUCTION OF A GASEOUS FLUID THROUGH A CONDUIT TO REJECT IT OUTSIDE THE SAME
FR2749930B1 (en) 1996-06-18 1998-09-04 Amphoux Andre EXTRACTION MOUTH FOR VENTILATION OF A ROOM AND STATIC OR STATOMECHANICAL SYSTEM INCLUDING SUCH A MOUTH
FR2755505B1 (en) 1996-11-05 1999-01-15 Amphoux Andre AIR EXTRACTOR FOR VENTILATION
FR2763387B1 (en) 1997-05-13 1999-07-23 Andre Amphoux GAS INJECTION DEVICE FOR DRAFT ASSISTANCE IN A GAS FLUID TRANSPORT SYSTEM
FR2763390B1 (en) 1997-05-13 1999-07-23 Andre Amphoux VENTILATION SYSTEM WITH ADDITIONAL AIR INJECTION FOR DRAFT ASSISTANCE
FR2782781B1 (en) 1998-09-02 2000-09-29 Andre Amphoux SAFETY DEVICE FOR GAS EVACUATION SYSTEMS
PL368953A1 (en) * 2004-07-06 2006-01-09 Przedsiębiorstwo Usługowo-Produkcyjne i WdrażaniaPostępu Technicznego UNIWERSAL Sp.z o.o. Hybrid ventilation cap
FR2892499B1 (en) * 2005-10-20 2008-01-11 Astato Soc Par Actions Simplif STATO-DYNAMIC AIR EXTRACTOR COMPRISING SENSOR FOR OPERATING THE BLADES OF SAID EXTRACTOR
ES2306596B1 (en) * 2007-02-15 2009-10-27 Sistemas Shunt De Baleares, S.L. VACUUM CLEANER APPLICABLE TO THE OUTLET IN VENTILATION DUCTS.

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FR2474651A1 (en) * 1980-01-25 1981-07-31 Amphoux Andre INSTALLATION OF REJECTION IN THE AMBIENT ATMOSPHERE OF A HIGH SPEED PRESSURE GASEOUS FLUID

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US3382792A (en) * 1965-08-16 1968-05-14 Ben O. Howard Omnidirectional exhaust ventilator
DE2209301B1 (en) * 1972-02-28 1973-07-05 Buettner-Schilde-Haas Ag, 4150 Krefeld Roof fan
DE2318885A1 (en) * 1973-04-14 1974-10-24 Gal Ges Fuer Angewandte Luftte ROOF VENTILATOR
FR2438795A2 (en) * 1978-10-13 1980-05-09 Amphoux Andre Gas and noise absorber for factory chimney - has perforated steel sections holding glass fibre or rock wool acoustic absorbers
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0082775A2 (en) * 1981-12-18 1983-06-29 André Amphoux Cowl for gaseous fluid
EP0082775A3 (en) * 1981-12-18 1984-07-18 Andre Amphoux Cowl for gaseous fluid
EP0196659A2 (en) * 1985-04-02 1986-10-08 Licencia Talalmanyokat Ertekesito Es Innovacios Külkereskedelmi Vallalat Draught intensifying apparatus
EP0196659A3 (en) * 1985-04-02 1987-02-04 Licencia Talalmanyokat Ertekesito Es Innovacios Külkereskedelmi Vallalat Draught intensifying apparatus
FR2647881A1 (en) * 1989-05-30 1990-12-07 Amphoux Andre MIXED VENTILATION DEVICE FOR A HOUSE
EP0404615A1 (en) * 1989-05-30 1990-12-27 André Amphoux Combined ventilation appliance for a living room
EP0641973A1 (en) * 1993-09-03 1995-03-08 André Amphoux Device for gaseous fluid removal
EP0641972A1 (en) * 1993-09-03 1995-03-08 André Amphoux Static dynamic device for gaseous fluid removal
FR2709534A1 (en) * 1993-09-03 1995-03-10 Amphoux Andre Static / dynamic device for evacuating gaseous fluid.
FR2709533A1 (en) * 1993-09-03 1995-03-10 Amphoux Andre Device for discharging gaseous fluid.

Also Published As

Publication number Publication date
EP0079256B1 (en) 1989-09-20
US4462305A (en) 1984-07-31
DE3279952D1 (en) 1989-10-26
FR2514469B1 (en) 1986-04-04
FR2514469A1 (en) 1983-04-15

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