EP3064778B1 - Ventilateur radial avec dispositif de mélange air-gaz - Google Patents

Ventilateur radial avec dispositif de mélange air-gaz Download PDF

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Publication number
EP3064778B1
EP3064778B1 EP16158639.1A EP16158639A EP3064778B1 EP 3064778 B1 EP3064778 B1 EP 3064778B1 EP 16158639 A EP16158639 A EP 16158639A EP 3064778 B1 EP3064778 B1 EP 3064778B1
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EP
European Patent Office
Prior art keywords
housing
air intake
gas inlet
opening
impeller
Prior art date
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Application number
EP16158639.1A
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German (de)
English (en)
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EP3064778A1 (fr
Inventor
Francesco Trabalzi
Marco Pallotta
Leonardo Vitaletti
Stefano Torregiani
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.)
Emc Fime SRL
Original Assignee
Elica SpA
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Priority to PL16158639T priority Critical patent/PL3064778T3/pl
Publication of EP3064778A1 publication Critical patent/EP3064778A1/fr
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Publication of EP3064778B1 publication Critical patent/EP3064778B1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226—Fan casings
    • F04D29/424—Double entry casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/16—Centrifugal pumps for displacing without appreciable compression
    • F04D17/162—Double suction pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/34—Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
    • F23D14/36—Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air in which the compressor and burner form a single unit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/62—Mixing devices; Mixing tubes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps

Definitions

  • the present invention relates to a housing for a radial fan and to a radial fan provided with such a housing.
  • DE102011014117A , EP2597370A1 , EP2597369A1 describe closest prior art fans in relation with the present invention.
  • EP1482245A1 discloses a prior art fan according to the preamble of claim 1.
  • radial fans intended to send a mixture of air and gas to boilers comprise a housing provided with an air intake opening and an air exhaust opening.
  • An impeller is arranged inside the housing, capable of rotating about a rotation axis. The air enters into the housing through the intake opening in axial direction, crosses the impeller, and is exhausted therefrom in radial direction into a spiral portion of the housing, from where the air reaches the exhaust opening.
  • the impeller is provided with a plurality of blades arranged about the rotation axis of the impeller and having an arc-shaped profile in transverse direction to the rotation axis.
  • Radial fans must be able to make available suitable heads in clearly defined intervals (the so-called “working curves") in order to ensure the correct operation of the condensation boiler, for example, to which they are connected.
  • a further particularly felt need, to which the research in the radial fan industry dedicates considerable efforts, is to obtain size reductions without worsening performance.
  • a premixing assembly e.g. a Venturi effect mixer, arranged upstream of the intake opening of the housing and in all cases necessarily inside e.g. a boiler.
  • Fan 1 is adapted to convey air and gas towards a burner or a boiler or a general heating system. Fan 1 is particularly suited for conveying a mixture of air and gas towards a condensation boiler.
  • Fan 1 comprises a housing 3 adapted to accommodate an impeller 2 capable of rotating about a rotation axis A.
  • the words “axial” and “radial” refer to the rotation axis A of impeller 2, unless otherwise specified.
  • Housing 3 preferably comprises two mutually distinct, connectable parts, e.g. a half-shell 4, which delimits an impeller space 6 adapted to accommodate the impeller 2 therein and a lid 5 adapted to close the impeller space 6.
  • the half-shell 4 and the lid 5 can be connected to each other by means of connecting members, e.g. screws 7.
  • Lid 5 may further comprise a protruding portion 5' adapted to be inserted with shape connection into the impeller space 6 delimited by the half-shell 4, advantageously substantially complementary thereto.
  • Lid 5 is adapted to support a motor 8, preferably an electric motor, intended to move impeller 2 by means of a shaft 9 thereof which, in the assembled condition of fan 1, is coaxial to the rotation axis A.
  • Motor 8 may be connected to lid 5 by means of an intermediate support 10 arranged for connecting the lid 5, e.g. by means of screws 11 to be inserted into corresponding screw seats 12 of lid 5.
  • the screw seats 12 are preferably arranged along a circumference at constant angular distances.
  • the screw seats 12 may be three in number and spaced apart by 120°.
  • the intermediate support 10 may be provided with a corresponding number of radial brackets 15 distributed in a manner corresponding to the screw seats 12 of lid 5.
  • Fan 1 may comprise vibration damping means in order to limit the vibration transmission between motor 8 and lid 5.
  • vibration damping means comprise first dampers 13 adapted to act between the intermediate support 10 and the lid 5, e.g. rubber elements provided with a through opening for allowing the screws 11 to extend therethrough, so as to damp the vibrations parallel to the rotation axis A.
  • fan 1 may further comprise second dampers 14 acting between the intermediate support 10 and the lid 5 which are oriented and shaped so as to damp the vibrations which are transmitted from motor 8 to housing 3 along radial directions.
  • rubber elements may be inserted into shelves 16 either consisting of or connected to lid 5 and preferably arranged along a circumference inside the circumference along which the screw seats 12 are arranged. Even more preferably, such shelves 16 are three in number and arranged at 120° with respect to one another.
  • the second dampers 14 may be arranged laterally in contact with the intermediate support 10, so as to act radially between the latter and the shelves 16.
  • the latter may comprise a covering element 17 connectable to motor 8, e.g. by means of screws 18.
  • a covering element 17 is preferably cup-shaped so as not to make motor 8 accessible once fan 1 has been assembled.
  • the covering element 17 may have the function of protecting one or more auxiliary elements 48, such as for example electronic control circuits of motor 8, in addition to the motor 8 itself.
  • Lid 5 advantageously comprises a passage opening 19 in order to allow the shaft 9 of motor 8 to pass through lid 5 and to be connected to the impeller 2 accommodated in the impeller space 6.
  • the housing 3 of fan 1 forms an air intake opening 20 and an exhaust opening 21 for the air-gas mixture.
  • the intake opening 20 and the exhaust opening 21 are formed in the half-shell 4.
  • the intake opening 20 is preferably arranged in the half-shell 4 and shaped so that the incoming air enters into the impeller shape 6 and reaches the impeller 2 along a substantially axial direction.
  • the exhaust opening 21 is preferably formed by an end 23 of an exhaust portion 22 of the half-shell 4 which is developed in a direction substantially tangential to housing 3 ( figures 1, 2 , 3 ), so that the mixed air and gas (or mixed generic fluids) conveyed by impeller 2 circulate in the impeller space 6 according to flow lines which are substantially tangential, and are exhausted by fan 1 through the exhaust opening 21 without their motion being excessively diverted.
  • a flange 24 adapted to connect fan 1 to outer support elements (not shown in the figures), e.g. by means of threaded connecting members.
  • housing 3 forms, in addition to the air intake opening 20, a gas intake opening 25 which is separate (and preferably spaced apart) from the air intake opening 20 and in direct communication with the impeller space 6.
  • the impeller space 6 inside housing 3 may be utilized for mixing the gas with the air, so as to completely avoid the need for a premixing assembly positioned upstream of the intake opening 20, and to connect (the gas tube to) the gas valve 26 directly at the gas inlet opening 25 of housing 3. This considerably reduces the dimensions of the entire mixing and conveying assembly of the fuel mixture in a boiler or in another similar application.
  • the air intake opening 20 and the gas inlet opening 25 are both formed (in one piece) in the same portion of housing 3, preferably in the half-shell 4.
  • Housing 3 in particular the half-shell 4, forms an air intake duct 27 extending from the air intake opening 20 (which opens to the outside of housing 3) to an inner end 28 which opens in the impeller space 6, as well as a gas inlet duct 29 extending from the gas inlet opening 25 (which opens to the outside of housing 3) to an inner opening zone 30 which opens into the impeller space 6 at a distance from the inner end 28 of the air intake channel 27.
  • the air intake duct 27 is parallel to the rotation axis A and the gas inlet duct 29 has an annular portion 34 extending all around the air intake duct (27) and which forms the inner opening zone 30.
  • the inner opening zone 30 is formed by one or more openings 31 passing from the inside of the gas inlet duct 29 directly into the impeller space 6 (bypassing the air intake duct 27) and extending or distributed along a circumference around the air intake duct 27, possibly along a circumference which is coaxial to the rotation axis A.
  • the inner end 28 of the air intake duct 27 axially protrudes into the impeller space 6 and faces the impeller 2, while the inner opening zone 30 is formed in a portion of the gas inlet duct 29 protruding towards the outside of housing 3 and/or facing away from impeller 2. Furthermore, the inner opening zone 30 of the gas inlet duct 29 is axially spaced apart from the inner end 28 of the air intake duct 27 and more retracted (more distant) with respect to impeller 2 ( figures 4 , 6, 7 ). More in general, the gas inlet duct (29) and the air intake duct (27) are configured (e.g.
  • an inner end 28 of the air intake duct 27 and the inner opening zone 30 are dimensioned and spaced apart in the flow direction and in a direction transversal to the flow direction) so as to prevent the establishment of a Venturi effect between the air flow (31) and the gas flow (32) entering into the impeller space (6).
  • the configuration of claim prevents or at least considerably reduces the establishment of a Venturi effect between the intake air flow 31 and the gas flow 32 entering into the impeller space 6.
  • the flow rates of both flows 31, 32 are mainly controlled by the rotation speed of impeller 2, the flow resistance (backpressure) downstream of the fan, and the individual and independent flow resistances of the two pipes, air duct 27 and gas duct 29. This allows to control and modulate the air and gas mixture in a wide modulation range and to operate at low pressures and with slow air flow speeds which would not be suitable for a primary air intake by means of Venturi effect.
  • a front wall 43 of housing 3 (e.g. of the half-shell 4 or alternatively of the lid 5) forms a truncated-cone-shaped portion 33 which protrudes towards the outside of housing 3 and externally delimits (with reference to housing 3) the annular portion 34 of the gas inlet duct 29.
  • To the smaller base (outer end) of the truncated-cone-shaped portion 33 is connected a first externally cylindrical tubular portion 35 protruding towards the outside of housing 3, wherein the first externally cylindrical tubular portion 35 delimits the air intake opening 20 and an axially outer portion 36 of the air intake duct 27.
  • the air intake duct 27 has a converging profile in the direction of the impeller space 6. Moreover, such a convergence is characterized by a concave curve-shape or progression in the outer portion 36 and by a convex curve-shape or progression in the inner portion 38 of the air intake duct 27 ( figures 4 , 6, 7 ).
  • the aforesaid convergence, concavity and convexity refer to the shape of the inner surface of duct 27 on a longitudinal section plane which comprises the longitudinal axis A of the air intake duct 27.
  • Such a converging shape with double curvature is optimal (according to experimental tests and numeric simulations) to connect the diameter of the outer cylindrical portion 35 (indispensable for connecting an air duct and/or a possible muffler, e.g. of a boiler) to the diameter of the inner end 28.
  • the diameter of the inner end 28 has a two-fold function: it determines the required amount of air which must transit for a correct combustion in the entire operating range and also forms a maximal local vacuum zone within the impeller space 6 which contributes to the required intake and mixing of the gas in an operating range that is as wide as possible.
  • the front wall 43 of housing 3 further forms a third tubular portion 39 spaced apart from the truncated-cone-shaped portion 33 and protruding towards the outside of housing 3, and a connecting portion 40 shaped as a channel which is open towards the inside of housing 3 which connects the third tubular portion 39 and the truncated-cone-shaped portion 33 and externally delimits a corresponding intermediate portion 42 of the gas inlet channel 29.
  • the third tubular portion 39 forms the gas inlet opening 25 and may be preferably cylindrical and substantially parallel to the longitudinal axis A of the air intake duct 27.
  • the connecting portion 40 may have an arc-shaped or rectangular cross section (open channel section) and may extend in a radial direction to the longitudinal axis A of the air intake duct 27 ( figures 2 , 6 ).
  • the distance between the first tubular portion 35 and the third tubular portion 39 facilitates the assembly of the gas valve 26 to the gas inlet opening 25 ( figure 1 ) without obstructing the feeding of air to the air intake opening 20.
  • Housing 3 further comprises an inner wall 41 which delimits the annular portion 34 and the intermediate portion 42 of the gas inlet duct 29 from the inside of housing 3 so as to embody the gas inlet duct 29 as a closed channel ( figure 6 ).
  • the inner opening zone 30 of the gas inlet channel 29 is formed along a first meeting line between the inner wall 41 and the front wall 43 at the smaller base of the truncated-cone-shaped portion 33.
  • the opening zone 30 is thus formed along the bottom of a groove formed between the annular portion 34 of the gas inlet duct 29 and the converging inner portion 37 of the air intake duct 27.
  • An annular part 44 of the inner wall 41 preferably extends from the inner opening zone 30 in a diverging manner towards a second meeting line with the front wall 43 at the larger base of the truncated-cone-shaped portion 33.
  • an annular surface of the inner wall 41 facing towards the inside of housing 3 forms a guide or diffusion surface which is diverging in the direction of impeller 2.
  • the guide surface has a rotational symmetry shape with respect to the longitudinal axis A of the air intake duct 27 which is parallel to the rotation axis A of the impeller.
  • Such a rotational symmetry shape may be, for example, similar to a cone (substantially straight generatrix line), a bell (generatrix line with double curvature) or a trumpet (arcuate generatrix line with simple curvature).
  • the inner wall 41 also forms a side appendix 45 which protrudes, e.g. in radial direction, from the annular part 44 and covers the intermediate portion 42 of the gas inlet duct 29 from the inside of housing 3, and possibly also at least part of the third tubular portion 39.
  • the inner wall 41 is an insert which is separately manufactured ( figures 8, 9, 10 ) and then applied to the front wall 43, from the inside of housing 3, to jointly delimit the gas inlet duct 29.
  • the front wall 43 is an insert separately manufactured and then applied to the inner wall 41 from the outside of housing 3, to jointly delimit the gas inlet duct 29.
  • housing 3 This facilitates the manufacturing of housing 3, e.g. by making the plastic insert by injection molding and the wall of housing 3 by means of aluminum molding, casting or die-casting.
  • the insert forming the inner wall 41 may have a fitting edge 46 formed along the annular part 44 and configured to engage by force fitting, press fitting or snap fitting a corresponding annular seat (e.g. a negative step) of the front wall 43 at the larger base of the truncated-cone-shaped portion 33. Furthermore, the insert forming the inner wall 41 may have a detent or retaining hook 47 adapted to engage a bottom of the third tubular portion 39 formed by the front wall 43.
  • the insert forming the inner wall 41 has a crenellation 50 or notching formed along the annular part 44 (at the annular edge opposite to the fitting edge) and resting (freely or with elastic engagement, press-fitting or snap-fitting) against the front wall 43 so as to jointly delimit said through openings for the release of the gas ( figures 6 , 9, 10 ).
  • a crenellation 50 or notching formed along the annular part 44 (at the annular edge opposite to the fitting edge) and resting (freely or with elastic engagement, press-fitting or snap-fitting) against the front wall 43 so as to jointly delimit said through openings for the release of the gas ( figures 6 , 9, 10 ).
  • impeller 2 comprises a plurality of blades 49 arranged in sequence about the rotation axis A ( figure 5 ).
  • Each of the blades 49 has a radially outermost inlet end and a radially outermost outlet end.
  • the inlet end has the function of taking in and capturing the air and gas coming in axial direction from the intake opening 20 and from the gas inlet opening 25, and the outlet end has the function of guiding the gas-air mixture from impeller 2 radially outwards and tangentially towards the exhaust opening 21.
  • the total ratio of the axial extension La to the diametrical or radial extension Ld of housing 3 is La/Ld ⁇ 0.75, preferably 0,38 ⁇ La/Ld ⁇ 0.75, even more preferably 0.42 ⁇ La/Ld ⁇ 0.46.
  • the fan 1 thus configured is able to achieve the objects of the invention.
  • the overall dimensions of the fan-mixer on which the axial and radial dimensions of the housing depend, are suited to the applications for which the fans according to the invention are intended, in particular for feeding air and/or gas to condensation boilers.
  • housing and fan according to the invention allow to obtain small dimensions, wide modularity ranges, and high gas-air mixing efficiency.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Claims (12)

  1. Carter (3) pour un ventilateur radial (1), dans lequel le carter (3) forme :
    - intérieurement un espace d'hélice (6) accueillant une hélice (2) pouvant tourner autour d'un axe de rotation (A),
    - une ouverture d'admission d'air (20) en communication directe avec l'espace d'hélice (6),
    - une ouverture d'évacuation (21) destinée à évacuer un mélange air-gaz de l'espace d'hélice vers l'extérieur du carter (3),
    - une ouverture d'entrée de gaz (25) espacée de l'ouverture d'admission d'air (20) et en communication directe avec l'espace d'hélice (6),
    de sorte que l'espace d'hélice (6) forme un espace pour mélanger une veine d'air (31) provenant de l'ouverture d'admission d'air (20) avec une veine de gaz (32) provenant de l'ouverture d'entrée de gaz (25),
    - un conduit d'admission d'air (27) s'étendant depuis l'ouverture d'admission d'air (20) qui débouche à l'extérieur du carter (3) vers une extrémité interne (28) qui débouche dans l'espace d'hélice (6),
    - un conduit d'entrée de gaz (29) s'étendant depuis l'ouverture d'entrée de gaz (25) qui débouche à l'extérieur du carter (3) vers une zone d'ouverture interne (30) qui débouche dans l'espace d'hélice (6) à une distance de l'extrémité interne (28) du conduit d'admission d'air (27), contournant le conduit d'admission d'air (27),
    dans lequel le conduit d'admission d'air (27) est parallèle à l'axe de rotation (A) et le conduit d'entrée de gaz (29) comporte une portion annulaire (34) s'étendant tout autour du conduit d'admission d'air (27) et qui forme la zone d'ouverture interne (30), ladite zone d'ouverture interne (30) comprenant une ou plusieurs ouvertures de gaz (32) s'étendant ou réparties le long d'une circonférence autour du conduit d'admission d'air (27),
    dans lequel
    - une paroi avant (43) du carter (3) forme :
    - une portion en forme de cône tronqué (33) qui dépasse vers l'extérieur du carter (3) et délimite extérieurement la portion annulaire (34) du conduit d'entrée de gaz (29), et
    - une portion tubulaire dépassante supplémentaire (37) convergeant depuis une plus petite base, c'est-à-dire une extrémité externe de la portion en forme de cône tronqué (33) vers l'intérieur du carter (3) et formant une portion interne (38) du conduit d'admission d'air (27) et ladite extrémité interne (28),
    - le carter (3) comprenant en outre une paroi interne (41) qui délimite le conduit d'entrée de gaz (29) depuis l'intérieur du carter (3), caractérisé en ce que
    - la zone d'ouverture interne (30) du canal d'entrée de gaz (29) est formée le long d'une première ligne de croisement entre la paroi interne (41) et la paroi avant (43) au niveau de la plus petite base de la portion en forme de cône tronqué (33), de façon à empêcher l'établissement d'un effet Venturi entre la veine d'air (31) et la veine de gaz (32) entrant dans l'espace d'hélice (6).
  2. Carter (3) selon la revendication 1, dans lequel l'ouverture d'admission d'air (20) et l'ouverture d'entrée de gaz (25) sont toutes deux formées d'un seul tenant dans une même paroi avant (43) du carter (3).
  3. Carter (3) selon l'une quelconque des revendications précédentes, dans lequel l'extrémité interne (28) dépasse axialement dans l'espace d'hélice (2), tandis que la zone d'ouverture interne (30) est formée dans une portion d'entrée de gaz (29) tournant axialement le dos à l'espace d'hélice (2).
  4. Carter (3) selon l'une quelconque des revendications précédentes, dans lequel l'ouverture interne (30) du conduit d'entrée de gaz (29) est espacée axialement de l'extrémité interne (28) du conduit d'admission d'air (27) et est plus distante de l'hélice (2) que ladite extrémité interne (28).
  5. Carter (3) selon la revendication 1 ou 2, dans lequel une paroi avant (43) du carter (3) forme :
    - une portion tubulaire extérieurement cylindrique (35), dépassant d'une plus petite base de la portion en forme de cône tronqué (33) vers l'extérieur du carter (3) et délimitant l'ouverture d'admission d'air (20) et une portion axialement interne (36) du conduit d'admission d'air (27),
    - une portion tubulaire supplémentaire (39) espacée de la portion en forme de cône tronqué (33) et dépassant vers l'extérieur du carter (3), ladite portion tubulaire supplémentaire (39) formant l'ouverture d'entrée de gaz (25),
    - une portion de raccordement (40) en forme de canal débouchant vers l'intérieur du carter (3) qui raccorde la portion tubulaire supplémentaire (39) à la portion en forme de cône tronqué (33) et délimite extérieurement une portion intermédiaire (42) du canal d'entrée de gaz (29).
  6. Carter (3) selon l'une quelconque des revendications précédentes, dans lequel le conduit d'admission d'air (27) a un profil convergeant dans la direction de l'espace d'hélice (6) avec une forme convergente concave dans une portion externe (36) et une forme convergente convexe dans une portion interne (38) du conduit d'admission d'air (27) observé sur un plan de coupe longitudinale qui comprend un axe longitudinal (A) du conduit d'admission d'air (27).
  7. Carter (3) selon la revendication 5, dans lequel :
    - une partie annulaire (44) de la paroi interne (41) s'étend depuis la zone d'ouverture interne (30) de manière divergente vers une seconde ligne de croisement avec la roue avant (43) au niveau de la plus grande base de la portion en forme de cône tronqué (33) et forme une surface guide avec symétrie de rotation et divergeant dans la direction de l'hélice (2),
    - la paroi interne (41) forme un appendice latéral (45) qui dépasse latéralement de la partie annulaire (44) et couvre une portion intermédiaire (42) du conduit d'entrée de gaz (29) depuis l'intérieur du carter (3).
  8. Carter (3) selon la revendication 7, dans lequel la paroi interne (41) est une pièce rapportée qui est fabriquée séparément puis appliquée sur une paroi avant (43) du carter (3).
  9. Carter (3) selon l'une des revendications 7 et 8, dans lequel la paroi interne (41) est faite de plastique et la paroi avant (43) du carter (3) est faite d'aluminium moulé sous pression.
  10. Carter (3) selon l'une des revendications 7 à 9, dans lequel la pièce rapportée formant la paroi interne (41) comporte un crénelage (50) reposant contre la paroi avant (43) et qui forme les ouvertures traversantes dans la zone d'ouverture interne (30).
  11. Carter (3) selon l'une des revendications précédentes, dans lequel le rapport (La/Ld) entre une extension axiale (La) et une extension diamétrale (Ld) du carter (3) est inférieur à 0,75, de préférence 0,38 < (La/Ld) < 0,75, de manière davantage préférée 0,42 < (La/Ld) < 0,46.
  12. Ventilateur radial (1) comprenant un carter (3) selon l'une quelconque des revendications précédentes, un moteur électrique et ladite hélice (2).
EP16158639.1A 2015-03-06 2016-03-04 Ventilateur radial avec dispositif de mélange air-gaz Active EP3064778B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL16158639T PL3064778T3 (pl) 2015-03-06 2016-03-04 Wentylator promieniowy z układem mieszania powietrza z gazem

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI20150336 2015-03-06

Publications (2)

Publication Number Publication Date
EP3064778A1 EP3064778A1 (fr) 2016-09-07
EP3064778B1 true EP3064778B1 (fr) 2022-02-16

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EP16158639.1A Active EP3064778B1 (fr) 2015-03-06 2016-03-04 Ventilateur radial avec dispositif de mélange air-gaz

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DE102016219418A1 (de) 2016-10-06 2018-04-12 Mahle International Gmbh Flüssigkeitspumpe
JP6747402B2 (ja) * 2017-08-11 2020-08-26 株式会社デンソー 送風機
DE102019109369A1 (de) * 2019-04-09 2020-10-15 Ebm-Papst Landshut Gmbh Adaptervorrichtung ausgeführt zur befestigten Anordnung an einer Ansaugöffnung eines Gasgebläses
DE102019112645A1 (de) * 2019-05-14 2020-11-19 Ebm-Papst Landshut Gmbh Einströmvorrichtung für ein Gasgebläse
IT202000012616A1 (it) * 2020-05-27 2021-11-27 Sit Spa Ventilatore per sistemi di miscelazione aria-gas in bruciatori di apparecchi di riscaldamento
CN115483413A (zh) * 2022-09-26 2022-12-16 平原滤清器有限公司 一种燃料电池发动机用分水器

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JPH1089628A (ja) * 1996-09-12 1998-04-10 Tokyo Gas Co Ltd 元混合型ガス燃焼装置
EP1482245A1 (fr) * 2003-05-30 2004-12-01 Hovalwerk AG Dispositif de réglage du rapport air/carburant d'un appareil de combustion à prémélange
EP2597369A1 (fr) * 2011-11-24 2013-05-29 LN 2 S.R.L. a socio unico Dispositif de mélange air-gaz pour brûleurs à gaz avec prémélange

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DE102011014117A1 (de) * 2011-03-15 2012-09-20 Ebm-Papst Landshut Gmbh Mischvorrichtung zur Mischung von Verbrennungsluft und Gas für ein Gasgerät
ITPD20110373A1 (it) * 2011-11-24 2013-05-25 Ln 2 Srl Socio Unico Dispositivo miscelatore aria-gas per bruciatori a gas combustibile con pre-miscelazione
EP2927584A1 (fr) * 2014-04-02 2015-10-07 Honeywell Technologies Sarl Dispositif mélangeur intégrale de gaz combustible/aire pour un brûleur à gaz

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Publication number Priority date Publication date Assignee Title
JPH1089628A (ja) * 1996-09-12 1998-04-10 Tokyo Gas Co Ltd 元混合型ガス燃焼装置
EP1482245A1 (fr) * 2003-05-30 2004-12-01 Hovalwerk AG Dispositif de réglage du rapport air/carburant d'un appareil de combustion à prémélange
EP2597369A1 (fr) * 2011-11-24 2013-05-29 LN 2 S.R.L. a socio unico Dispositif de mélange air-gaz pour brûleurs à gaz avec prémélange

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PL3064778T3 (pl) 2022-05-23

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