WO2018078239A1 - Impeller for centrifugal pump, centrifugal pump and manufacturing method - Google Patents

Impeller for centrifugal pump, centrifugal pump and manufacturing method Download PDF

Info

Publication number
WO2018078239A1
WO2018078239A1 PCT/FR2017/052832 FR2017052832W WO2018078239A1 WO 2018078239 A1 WO2018078239 A1 WO 2018078239A1 FR 2017052832 W FR2017052832 W FR 2017052832W WO 2018078239 A1 WO2018078239 A1 WO 2018078239A1
Authority
WO
WIPO (PCT)
Prior art keywords
wheel
hub
web
annular bead
axial direction
Prior art date
Application number
PCT/FR2017/052832
Other languages
French (fr)
Inventor
Laurent Fabbri
Alban Lemaitre
Antoine Alain Gaston MERY
Original Assignee
Arianegroup Sas
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 Arianegroup Sas filed Critical Arianegroup Sas
Priority to EP17793718.2A priority Critical patent/EP3532732B1/en
Publication of WO2018078239A1 publication Critical patent/WO2018078239A1/en

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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2261Rotors specially for centrifugal pumps with special measures
    • F04D29/2266Rotors specially for centrifugal pumps with special measures for sealing or thrust balance
    • 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
    • F04D29/02Selection of particular materials
    • F04D29/026Selection of particular materials especially adapted for liquid pumps
    • 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
    • F04D29/04Shafts or bearings, or assemblies thereof
    • F04D29/043Shafts
    • 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
    • F04D29/18Rotors
    • F04D29/20Mounting rotors on shafts
    • 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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2261Rotors specially for centrifugal pumps with special measures
    • F04D29/2277Rotors specially for centrifugal pumps with special measures for increasing NPSH or dealing with liquids near boiling-point
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material

Definitions

  • the present disclosure relates to a centrifugal pump, in particular for a turbomachine.
  • the wheel is shrunk on the shaft by an element of the wheel called tail rotor which must ensure the good transmission of torque between the wheel and the shaft even at high speeds of rotation undergone by the wheel of the centrifugal pump.
  • the present disclosure aims to provide a centrifugal pump whose mass is reduced compared to known centrifugal pumps and which has hydraulic performance and mechanical strength at least equivalent to known centrifugal pumps.
  • the present disclosure relates to a wheel for centrifugal pump having an axial direction, the wheel comprising a hub, a veil having a shape of revolution comprising a fixing part. of the web with the hub, the web flaring from the fastening portion in the axial direction, and an annular bead disposed between the web and the hub, the annular bead being attached to the web while an annular space is provided between the hub and the annular bead.
  • the hub does not undergo centrifugal force exerted by the web on the hub when the wheel is rotating. Also, when the wheel is rotating about the axial direction, the deformation undergone by the hub is relatively small and less important than the deformation undergone by a hub on which a web would be directly attached.
  • the annular bead is disposed between a central axis of the wheel and the web, the annular space being present between the annular bead. , and therefore a part of the veil, and the hub or a projection of the hub on the perpendicular plane.
  • annular bead fixed on the web, between the web and the hub.
  • This annular bead has a dimension in the axial direction which is greater than the thickness of the veil, the thickness of the veil being measured perpendicularly to the main surfaces of the veil.
  • This annular bead therefore makes it possible to limit the displacements in a radial direction at the output of the wheel and also makes it possible to control the displacements in the axial direction.
  • the annular bead corresponds to a thickening in the ring-shaped material direction. It is understood that the shape and / or the dimensions of the annular bead can be modified in order to adapt the rotational behavior of the wheel, in particular as a function of rotational speeds in operation of the wheel. Indeed, if the maximum displacements in service in the radial and axial directions are of low amplitude, for example less than 100 ⁇ , it is possible to reduce the dimensions of the annular bead.
  • Displacements in the radial and axial directions may depend for example on the diameter of the wheel, the speed of rotation, the intrinsic properties of the material in which the wheel is made, such as the density.
  • simulation software for example by finite element
  • the web is attached to the hub by the fastening portion of the web and that the fastening portion of the web and the hub forms the bottom of the open cavity, the bottom of the open cavity being disposed downstream the annular space between the hub and the annular bead.
  • the wheel is made in one piece, that is to say that the hub, the web and the bead are not assembled to each other.
  • the wheel may comprise an upstream end and a downstream end, the fixing portion of the web with the hub being disposed at the upstream end of the wheel and the annular bead being disposed at the downstream end of the wheel.
  • upstream and downstream are defined relative to the normal flow direction of the fluid in the centrifugal pump.
  • upstream end of the wheel is meant a portion of the wheel located upstream of the wheel and whose dimension, in the axial direction, is less than or equal to 50% of the total length of the wheel, in the axial direction.
  • downstream end of the wheel is understood to mean a part of the wheel located downstream of the wheel and whose dimension, in the axial direction, is less than or equal to 50% of the total length of the wheel, in the axial direction.
  • the hub may comprise an inner shrinking surface configured to shrink the hub on a shaft, the inner hooping surface being arranged, at least in part, in the axial direction, to the right of the annular space formed between the hub and the annular bead.
  • the inner surface of the hub shrinking is disposed downstream of the web so that the centrifugal forces exerted by the mass of the wheel on the inner surface of the hub , in particular by the end of the wheel farthest radially from the axis of rotation of the wheel, do not deform the internal hooping surface.
  • the internal shrinking surface being little or no deformed during the rotation of the wheel, the shrinking of the wheel on the shaft is facilitated.
  • the inner diameter of the inner hooping surface is dimensioned at rest taking into account the maximum deformation under stress experienced by the inner hooping surface. Since this deformation is small, the inside diameter of the inner hoop-resting surface is therefore slightly smaller than the inside diameter of the inner hooping surface during the rotation of the wheel.
  • the force required to assemble the shaft and the wheel is therefore limited with respect to the force required to assemble a wheel having no annular space formed between the annular bead and the hub and whose difference in internal diameter of the inner surface of hooping between the rest and the rotation of the wheel is significant.
  • the maximum displacement in use can reach 0.2 mm in the shrinking zone, whereas with a wheel as defined above, the maximum displacement in use is only 0.02 mm in the hooping zone.
  • the inner hooping surface may be substantially completely disposed in the axial direction to the right of the annular space formed between the hub and the annular bead.
  • the right of the annular space formed between the hub and the annular bead means that the inner shrinking surface is included in the radial projection of the annular bead on the inner surface of the hub, at plus or minus 5% the radial projection of the annular bead on the inner surface of the hub.
  • the inner hooping surface may be smaller than the radial projection of the annular bead on the inner surface of the hub but slightly exceed, less than 5% of the dimension, in the axial direction of the annular bead.
  • the hub may comprise an inner shrinking surface (38) configured to shroud the hub on a shaft, the inner hooping surface being arranged, in the axial direction, upstream of the annular space formed between the hub and the annular bead.
  • the wheel may comprise a plurality of reinforcing ribs disposed between the web and the hub.
  • These reinforcing ribs increase the mechanical strength of the wheel while limiting the overall mass of the wheel.
  • These reinforcing ribs may have a purely radial direction, they may also be inclined relative to the radial direction. Thus, by modifying the number, the location and / or the dimensions of the reinforcing ribs, it is possible to modify the rigidity of the wheel.
  • These reinforcing ribs may also allow the transmission of torque between the shaft and the wheel, in particular between the shaft and the wheel web.
  • the web may comprise a plurality of through orifices. These through holes allow a pressure equalization between an upstream surface of the web and a downstream surface of the web. It is thus possible to balance the forces on the shaft upstream and downstream of the wheel and thus reduce the sudden forces by stops of the centrifugal pump.
  • the wheel may comprise an inductor and an impeller and the through orifices are disposed between the inductor and the impeller allowing orientation of the fluid in the axis of the flow.
  • the wheel can be made of metal or metal alloy.
  • the present disclosure also relates to a centrifugal pump comprising a wheel as defined above.
  • the present disclosure also relates to a method of manufacturing a wheel as defined above, the wheel being made by an additive manufacturing process.
  • This additive manufacturing process allows great flexibility in the shapes produced and also makes it easy to produce parts with cavities and / or internal ducts.
  • FIG. 1 is a schematic axial sectional view of a centrifugal pump
  • FIGS. 2A and 2B are views in axial section of a wheel for a centrifugal pump according to two embodiments
  • FIG. 3 is a perspective view of the wheel of FIG. 2A, seen from the upstream side;
  • FIG. 4 is a partial perspective view of the wheel of Figure 2A, seen from the downstream side.
  • FIG. 1 represents an axial sectional view of a centrifugal pump 100 comprising a shaft 12, defining an axis X, on which are mounted a wheel 10, an impeller turbine nozzle 116 and a turbine disk 102.
  • a pump housing 104 which has a front housing 106, a central housing 108 and an exhaust housing 110.
  • the pump housing 104 defines a pump volute 112 and a turbine inlet core 114.
  • the pump 100 also comprises locking means along the axis X of the elements of the pump 100 on the shaft 12. These elements are for example nuts 14 and 118.
  • the wheel 10 and the turbine disc 102 are mounted on the shaft 12 and in the pump casing 104 by bearings 18, the wheel 10 and the turbine disc 102 being each spaced from their respective bearing 18 by a shim 16.
  • FIG. 2A shows an embodiment of a wheel 10 for a centrifugal pump 100.
  • the arrow F represents the normal flow direction of a fluid in the centrifugal pump 100 and therefore around the wheel 10. Thereafter, the terms “upstream” and “downstream” are defined relative to the direction of normal circulation of the fluid in the centrifugal pump.
  • the wheel 10 is shown mounted on the shaft 12. It is fixed on the shaft 12, at its upstream end, by the nut 14 and, at its downstream end, by the shim 16 and the bearing 18.
  • the wheel 10 of FIG. 2A comprises an inductor 20 and an impeller 22.
  • the wheel 10 comprises an axis of rotation X defining an axial direction X of the wheel 10.
  • the wheel 10 comprises a hub 24 and a sail 26 having a shape of revolution comprising an attachment portion 28 of the web 26 with the hub 24.
  • the web 24 flares from the fastening portion 28 according to the X axial direction, that is to say that the web 26 flares from the fastening portion 28, disposed at an upstream end of the wheel 10 to a downstream end of the wheel 10.
  • the veil 26 has a first portion of substantially cylindrical shape which then flares downstream of the wheel 10, so that a free end 26A of the web extends substantially in a radial plane, that is to say in a plane perpendicular to the axial direction X.
  • the wheel 10 also comprises an annular bead 30 disposed between the web 26 and the hub 24, at the downstream end of the wheel 10, to the right, in the axial direction X, of the free end 26A of the sail 26
  • the annular bead 30 is fixed to the web 26 while an annular space 32 is formed between the hub 24 and the annular bead 30.
  • the hub 24 has an inner surface 36.
  • This inner surface 36 has a portion which forms an inner shrinking surface 38 of the hub 24 and thus the wheel 10 on the shaft 12.
  • This inner hooping surface 38 is disposed at the downstream end of the wheel 10.
  • the inside hooping surface 36 is arranged substantially completely, in the axial direction X, at the level of the annular space 32 formed between the hub 24 and the annular bead 30.
  • the inner hooping surface 38 is included in the radial projection of the annular bead 30 on the inner surface 36 of the hub 24, plus or minus 5% the radial projection of the annular bead 30 on the inner surface 36 of the hub 24.
  • the internal hooping surface 38 may be smaller than the radial projection of the annular bead 30 on the inner surface 36 of the hub 24 but slightly exceed, by less than 5% of the dimension, in the axial direction X of the annular bead. 30.
  • the wheel 10 comprises a plurality of reinforcing ribs 40 for reinforcing disposed between the web 26 and the hub 24 in the cavity 34. These radial ribs 40 are also visible in FIG. 4. 17 052832
  • the web 26 has a plurality of through holes 42 disposed between the inductor 20 and the impeller 22. These through holes 42 allow the passage of liquid from the upstream of the wheel 10 in the cavity 34. As shown in Figure 4, each through hole 42 opens between two reinforcing ribs 40.
  • the inductor 20 comprises fins 44, in this embodiment the inductor 20 comprises four fins 44 and the impeller 22 comprises fins 46, in this embodiment the wheel comprises twelve fins 46.
  • reinforcing ribs 40 are also 12 in number and that they are arranged vis-à-vis on both sides of the web 26.
  • the inner surface 36 of the hub 24 has projections 48 also allowing the passage of the torque between the shaft 12 and the hub 24.
  • the inner hooping surface 36 is arranged substantially completely, in the axial direction X, upstream of the annular space 32 formed between the hub 24 and the annular bead 30.
  • the wheel 10 is manufactured by an additive manufacturing process, for example by using a laser beam on a bed of powder.
  • the powder bed is formed by the powder that will constitute the wheel 10.
  • the powder may comprise titanium or be a metal alloy commonly referred to by the trademark Inconel TM.
  • Inconel is later referred to as an alloy based on iron alloyed with nickel and chromium.
  • the wheel 10 is manufactured by superposition of layers in the axial direction X from its downstream end and ending with its upstream end.
  • the outer surfaces of the wheel 10 are then machined in a conventional manner and known so that the surface condition of the web 26, the fins 44, 46 and the inner surface 36 of the hub is in accordance with the 52832
  • the number of fins 44 carried by the inductor 20 may vary, the same is true of the number of fins 46 carried by the impeller 22.
  • the number of reinforcing ribs 40 may be different from the number of fins 46 carried by the impeller 22.
  • the number of through holes 42 may be different from the number of reinforcing ribs 40.
  • the fins 44, 46 are straight fins, these fins may also be inclined relative to the radial direction, or even have a certain curvature.
  • the reinforcing ribs 40 shown are radial ribs. However, these ribs may also be inclined relative to the radial direction, or even have a certain curvature.
  • the wheel 10 comprises an inductor 20 and an impeller 22.
  • the wheel 10 could comprise only one impeller 22.

Landscapes

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

Abstract

The invention relates to an impeller (10) for a centrifugal pump having an axial direction (X), the impeller (10) comprising a hub (24), a web (26) having a rotationally symmetrical shape comprising an attachment part (28) for attaching the web (26) to the hub (24), the web (26) widening from the attachment part (28) in the axial direction (X), and an annular bead (30) arranged between the web (26) and the hub (24), the annular bead (30) being attached to the web (26) while an annular space (32) is created between the hub (24) and the annular bead (30). The invention also relates to a centrifugal pump comprising the impeller (10) and a method for manufacturing the impeller (10).

Description

ROUE POUR POMPE CENTRIFUGE, POMPE CENTRIFUGE ET PROCEDE DE  CENTRIFUGAL PUMP WHEEL, CENTRIFUGAL PUMP AND METHOD OF
FABRICATION  MANUFACTURING
Arrière-plan de l'invention Background of the invention
[0001] Le présent exposé concerne une pompe centrifuge, notamment pour turbomachine. The present disclosure relates to a centrifugal pump, in particular for a turbomachine.
[0002] Dans les moteurs de fusée, d'avion ou d'hélicoptère, un aspect important est la masse des différents éléments constitutifs du moteur.  In rocket engines, aircraft or helicopter, an important aspect is the mass of the various constituent elements of the engine.
[0003] Toutefois, la réduction de masse se fait souvent au détriment de la résistance mécanique ou de la résistance à la fatigue des différents éléments, si bien que chaque élément est généralement un compromis entre la masse et la tenue mécanique de l'élément.  However, the mass reduction is often to the detriment of the mechanical strength or fatigue strength of the various elements, so that each element is generally a compromise between the mass and the mechanical strength of the element.
[0004] C'est le cas par exemple d'une roue de pompe centrifuge qui doit avoir de bonnes performances hydrauliques et également une bonne tenue mécanique sur l'arbre afin que le couple puisse être transmis de l'arbre en rotation à la roue de la pompe centrifuge.  This is the case for example of a centrifugal pump wheel which must have good hydraulic performance and also good mechanical strength on the shaft so that the torque can be transmitted from the rotating shaft to the wheel centrifugal pump.
[0005] A cette fin, typiquement, la roue est frettée sur l'arbre par un élément de la roue appelé queue de rouet qui doit assurer la bonne transmission du couple entre la roue et l'arbre même aux vitesses élevées de rotation subies par la roue de la pompe centrifuge.  For this purpose, typically, the wheel is shrunk on the shaft by an element of the wheel called tail rotor which must ensure the good transmission of torque between the wheel and the shaft even at high speeds of rotation undergone by the wheel of the centrifugal pump.
[0006] Aussi, lorsque certaines pièces ont plusieurs fonctions, on comprend que leur optimisation peut devenir difficile.  Also, when some parts have several functions, we understand that their optimization can become difficult.
[0007] Toutefois, on cherche encore à optimiser de telles pompes centrifuges afin notamment de réduire leur masse tout en conservant leurs performances hydrauliques et leur tenue mécanique.  However, it is still sought to optimize such centrifugal pumps in particular to reduce their mass while maintaining their hydraulic performance and mechanical strength.
Objet et résumé de l'invention Object and summary of the invention
[0008] Le présent exposé vise à proposer une pompe centrifuge dont la masse est réduite par rapport aux pompes centrifuges connues et qui présente des performances hydrauliques et une tenue mécanique au moins équivalente aux pompes centrifuges connues. The present disclosure aims to provide a centrifugal pump whose mass is reduced compared to known centrifugal pumps and which has hydraulic performance and mechanical strength at least equivalent to known centrifugal pumps.
[0009] A cet effet, le présent exposé concerne une roue pour pompe centrifuge présentant une direction axiale, la roue comprenant un moyeu, un voile ayant une forme de révolution comprenant une partie de fixation du voile avec le moyeu, le voile s'évasant depuis la partie de fixation selon la direction axiale, et un bourrelet annulaire disposé entre le voile et le moyeu, le bourrelet annulaire étant fixé au voile tandis qu'un espace annulaire est ménagé entre le moyeu et le bourrelet annulaire. For this purpose, the present disclosure relates to a wheel for centrifugal pump having an axial direction, the wheel comprising a hub, a veil having a shape of revolution comprising a fixing part. of the web with the hub, the web flaring from the fastening portion in the axial direction, and an annular bead disposed between the web and the hub, the annular bead being attached to the web while an annular space is provided between the hub and the annular bead.
[0010] Grâce à cet espace annulaire ménagé entre le moyeu et le bourrelet annulaire, le moyeu ne subit pas d'effort centrifuge exercé par le voile sur le moyeu lorsque la roue est en rotation. Aussi, lorsque la roue est en rotation autour de la direction axiale, la déformation subie par le moyeu est relativement faible et moins importante que la déformation subie par un moyeu sur lequel un voile serait directement attaché.  With this annular space between the hub and the annular bead, the hub does not undergo centrifugal force exerted by the web on the hub when the wheel is rotating. Also, when the wheel is rotating about the axial direction, the deformation undergone by the hub is relatively small and less important than the deformation undergone by a hub on which a web would be directly attached.
[0011] On comprend donc que dans un plan perpendiculaire à la direction axiale passant par le voile et le bourrelet annulaire, le bourrelet annulaire est disposé entre un axe central de la roue et le voile, l'espace annulaire étant présent entre le bourrelet annulaire, et donc une partie du voile, et le moyeu ou une projection du moyeu sur le plan perpendiculaire.  It is therefore understood that in a plane perpendicular to the axial direction passing through the web and the annular bead, the annular bead is disposed between a central axis of the wheel and the web, the annular space being present between the annular bead. , and therefore a part of the veil, and the hub or a projection of the hub on the perpendicular plane.
[0012] Par ailleurs, l'intégrité structurelle du voile et de la roue est assurée par la présence du bourrelet annulaire fixé sur le voile, entre le voile et le moyeu. Ce bourrelet annulaire présente une dimension selon la direction axiale qui est supérieure à l'épaisseur du voile, l'épaisseur du voile étant mesurée perpendiculairement aux surfaces principales du voile.  Furthermore, the structural integrity of the web and the wheel is ensured by the presence of the annular bead fixed on the web, between the web and the hub. This annular bead has a dimension in the axial direction which is greater than the thickness of the veil, the thickness of the veil being measured perpendicularly to the main surfaces of the veil.
[0013] Ce bourrelet annulaire permet donc de limiter les déplacements selon une direction radiale en sortie de la roue et permet également de contrôler les déplacements selon la direction axiale. Le bourrelet annulaire correspond à un épaississement dans la direction de matière en forme d'anneau On comprend que l'on peut modifier la forme et/ou les dimensions du bourrelet annulaire afin d'adapter le comportement en rotation de la roue, notamment en fonction des vitesses de rotation en fonctionnement de la roue. En effet, si les déplacements maximaux en service selon les directions radiales et axiales sont de faible amplitude, par exemple inférieurs à 100 μπι, il est possible de réduire les dimensions du bourrelet annulaire. Les déplacements selon les directions radiales et axiales peuvent dépendre par exemple du diamètre de la roue, de la vitesse de rotation, des propriétés intrinsèques du matériau dans lequel la roue est réalisée, telles que la densité. Cependant, notamment grâce à des logiciels de simulation (par exemple par éléments finis), il est possible de modifier la forme et/ou les dimensions du bourrelet annulaire. [0014] Le voile s'évasant depuis la partie d'attache du voile selon la direction axiale, il existe une cavité formée entre le moyeu, le voile et le bourrelet annulaire. Cette cavité est au moins ouverte vers l'extérieur du fait de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire. De ce fait, la masse de la roue est inférieure à la masse d'une roue ne présentant pas cette cavité ouverte. This annular bead therefore makes it possible to limit the displacements in a radial direction at the output of the wheel and also makes it possible to control the displacements in the axial direction. The annular bead corresponds to a thickening in the ring-shaped material direction. It is understood that the shape and / or the dimensions of the annular bead can be modified in order to adapt the rotational behavior of the wheel, in particular as a function of rotational speeds in operation of the wheel. Indeed, if the maximum displacements in service in the radial and axial directions are of low amplitude, for example less than 100 μπι, it is possible to reduce the dimensions of the annular bead. Displacements in the radial and axial directions may depend for example on the diameter of the wheel, the speed of rotation, the intrinsic properties of the material in which the wheel is made, such as the density. However, in particular thanks to simulation software (for example by finite element), it is possible to modify the shape and / or the dimensions of the annular bead. The veil flaring from the attachment portion of the web in the axial direction, there is a cavity formed between the hub, the web and the annular bead. This cavity is at least open towards the outside because of the annular space formed between the hub and the annular bead. As a result, the mass of the wheel is less than the mass of a wheel that does not have this open cavity.
[0015] On comprend que le voile est attaché au moyeu par la partie d'attache du voile et que la partie d'attache du voile et du moyeu forme le fond de la cavité ouverte, le fond de la cavité ouverte étant disposé en aval de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire.  It is understood that the web is attached to the hub by the fastening portion of the web and that the fastening portion of the web and the hub forms the bottom of the open cavity, the bottom of the open cavity being disposed downstream the annular space between the hub and the annular bead.
[0016] On comprend que la roue est faite d'une seule pièce, c'est-à- dire que le moyeu, le voile et le bourrelet ne sont pas assemblés les uns aux autres.  It is understood that the wheel is made in one piece, that is to say that the hub, the web and the bead are not assembled to each other.
[0017] La roue peut comprendre une extrémité amont et une extrémité aval, la partie de fixation du voile avec le moyeu étant disposé à l'extrémité amont de la roue et le bourrelet annulaire étant disposé à l'extrémité aval de la roue.  The wheel may comprise an upstream end and a downstream end, the fixing portion of the web with the hub being disposed at the upstream end of the wheel and the annular bead being disposed at the downstream end of the wheel.
[0018] Par la suite, les termes « amont » et « aval » sont définis par rapport au sens de circulation normal du fluide dans la pompe centrifuge.  Subsequently, the terms "upstream" and "downstream" are defined relative to the normal flow direction of the fluid in the centrifugal pump.
[0019] On entend par extrémité amont de la roue, une partie de la roue située à l'amont de la roue et dont la dimension, selon la direction axiale, est inférieure ou égale à 50% de la longueur totale de la roue, selon la direction axiale. De même, on entend par extrémité aval de la roue, une partie de la roue située à l'aval de la roue et dont la dimension, selon la direction axiale, est inférieure ou égale à 50% de la longueur totale de la roue, selon la direction axiale.  By upstream end of the wheel is meant a portion of the wheel located upstream of the wheel and whose dimension, in the axial direction, is less than or equal to 50% of the total length of the wheel, in the axial direction. Similarly, the term "downstream end of the wheel" is understood to mean a part of the wheel located downstream of the wheel and whose dimension, in the axial direction, is less than or equal to 50% of the total length of the wheel, in the axial direction.
[0020] Le moyeu peut comporter une surface intérieure de frettage configurée pour fretter le moyeu sur un arbre, la surface intérieure de frettage étant disposée, au moins en partie, selon la direction axiale, au droit de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire.  The hub may comprise an inner shrinking surface configured to shrink the hub on a shaft, the inner hooping surface being arranged, at least in part, in the axial direction, to the right of the annular space formed between the hub and the annular bead.
[0021] On comprend que dans une vue en coupe axiale de la roue, lorsque l'on projette la section du bourrelet annulaire sur la surface intérieure du moyeu selon une direction radiale, on définit une section de la surface intérieure du moyeu qui est, selon la direction axiale, au droit de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire et donc, selon la direction axiale, au droit du bourrelet annulaire. It is understood that in an axial sectional view of the wheel, when projecting the section of the annular bead on the inner surface of the hub in a radial direction, defining a section of the inner surface of the hub which is, according to the axial direction, to the right the annular space formed between the hub and the annular bead and therefore, in the axial direction, to the right of the annular bead.
[0022] De ce fait, même lorsque la roue est montée sur l'arbre et tourne à grande vitesse, le frettage entre l'arbre et le moyeu subit peu ou pas de déformations.  Therefore, even when the wheel is mounted on the shaft and rotates at high speed, the hoop between the shaft and the hub undergoes little or no deformation.
[0023] Aussi, contrairement aux roues connues, il n'est plus nécessaire de prévoir une queue de rouet aussi longue selon la direction axiale et décalée par rapport au voile vers l'aval de la roue selon la direction axiale. En effet, dans des roues ne présentant pas d'espace annulaire ménagé autour du moyeu, la surface intérieure de frettage du moyeu est disposée en aval du voile de sorte que les forces centrifuges exercées par la masse de la roue sur la surface intérieure du moyeu, en particulier par l'extrémité de la roue la plus éloignée radialement de l'axe de rotation de la roue, ne déforment pas la surface intérieure de frettage.  Also, unlike known wheels, it is no longer necessary to provide a tail wheel as long in the axial direction and offset from the web downstream of the wheel in the axial direction. Indeed, in wheels having no annular space around the hub, the inner surface of the hub shrinking is disposed downstream of the web so that the centrifugal forces exerted by the mass of the wheel on the inner surface of the hub , in particular by the end of the wheel farthest radially from the axis of rotation of the wheel, do not deform the internal hooping surface.
[0024] Il est donc possible de déplacer la surface de frettage vers l'amont de la roue. On peut ainsi réduire la longueur de la queue de rouet, réduire la masse de la roue et son encombrement, c'est-à-dire la dimension totale de la roue selon la direction axiale. De ce fait, le gain en masse va au-delà du gain en masse de la roue. En effet, on peut également réduire la masse des carters de la pompe centrifuge ainsi que la masse des carters entourant la pompe centrifuge.  It is therefore possible to move the hooping surface upstream of the wheel. It is thus possible to reduce the length of the wheel shank, to reduce the mass of the wheel and its bulk, ie the total dimension of the wheel in the axial direction. As a result, the mass gain goes beyond the mass gain of the wheel. In fact, it is also possible to reduce the mass of the casings of the centrifugal pump as well as the mass of the casings surrounding the centrifugal pump.
[0025] Par ailleurs, la surface intérieure de frettage étant peu ou pas déformée lors de la rotation de la roue, le frettage de la roue sur l'arbre est facilité. En effet, le diamètre intérieur de la surface intérieure de frettage est dimensionné au repos en tenant compte de la déformation maximale sous effort subie par la surface intérieure de frettage. Cette déformation étant faible, le diamètre intérieur de la surface intérieure de frettage au repos est donc légèrement plus petit que le diamètre intérieur de la surface intérieure de frettage lors de la rotation de la roue. L'effort requis pour assembler l'arbre et la roue est donc limité par rapport à l'effort nécessaire pour assembler une roue ne comportant pas d'espace annulaire ménagé entre le bourrelet annulaire et le moyeu et dont la différence de diamètre intérieur de la surface intérieure de frettage entre le repos et la rotation de la roue est significative. Par exemple, pour un moyeu présentant un diamètre de 27 mm (millimètre), avec une roue classique, le déplacement maximal en service peut atteindre 0.2 mm dans la zone de frettage, alors qu'avec une roue telle que définie ci-dessus, le déplacement maximal en service n'est que de 0.02 mm dans la zone de frettage. Moreover, the internal shrinking surface being little or no deformed during the rotation of the wheel, the shrinking of the wheel on the shaft is facilitated. Indeed, the inner diameter of the inner hooping surface is dimensioned at rest taking into account the maximum deformation under stress experienced by the inner hooping surface. Since this deformation is small, the inside diameter of the inner hoop-resting surface is therefore slightly smaller than the inside diameter of the inner hooping surface during the rotation of the wheel. The force required to assemble the shaft and the wheel is therefore limited with respect to the force required to assemble a wheel having no annular space formed between the annular bead and the hub and whose difference in internal diameter of the inner surface of hooping between the rest and the rotation of the wheel is significant. For example, for a hub having a diameter of 27 mm (millimeter), with a conventional wheel, the maximum displacement in use can reach 0.2 mm in the shrinking zone, whereas with a wheel as defined above, the maximum displacement in use is only 0.02 mm in the hooping zone.
[0026] La surface intérieure de frettage peut être sensiblement complètement disposée, selon la direction axiale, au droit de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire.  The inner hooping surface may be substantially completely disposed in the axial direction to the right of the annular space formed between the hub and the annular bead.
[0027] On peut donc concevoir une roue ne comprenant pas de queue de rouet.  We can design a wheel does not include spinning wheel.
[0028] Par sensiblement complètement disposée, selon la direction axiale, au droit de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire, on entend que la surface intérieure de frettage est comprise dans la projection radiale du bourrelet annulaire sur la surface intérieure du moyeu, à plus ou moins 5% la projection radiale du bourrelet annulaire sur la surface intérieure du moyeu.  By substantially completely arranged, in the axial direction, the right of the annular space formed between the hub and the annular bead means that the inner shrinking surface is included in the radial projection of the annular bead on the inner surface of the hub, at plus or minus 5% the radial projection of the annular bead on the inner surface of the hub.
[0029] Ainsi, la surface intérieure de frettage peut être de dimension inférieure à la projection radiale du bourrelet annulaire sur la surface intérieure du moyeu mais dépasser légèrement, de moins de 5% de la dimension, selon la direction axiale du bourrelet annulaire.  Thus, the inner hooping surface may be smaller than the radial projection of the annular bead on the inner surface of the hub but slightly exceed, less than 5% of the dimension, in the axial direction of the annular bead.
[0030] Le moyeu peut comporter une surface intérieure de frettage (38) configurée pour fretter le moyeu sur un arbre, la surface intérieure de frettage étant disposée, selon la direction axiale, en amont de l'espace annulaire ménagé entre le moyeu et le bourrelet annulaire.  The hub may comprise an inner shrinking surface (38) configured to shroud the hub on a shaft, the inner hooping surface being arranged, in the axial direction, upstream of the annular space formed between the hub and the annular bead.
[0031] On peut ainsi réduire la masse de la roue.  It is thus possible to reduce the mass of the wheel.
[0032] La roue peut comporter une pluralité de nervures de renforcement disposées entre le voile et le moyeu.  The wheel may comprise a plurality of reinforcing ribs disposed between the web and the hub.
[0033] Ces nervures de renforcement permettent d'accroître la tenue mécanique de la roue tout en limitant la masse globale de la roue. Ces nervures de renforcement peuvent avoir une direction purement radiale, elles peuvent également être inclinées par rapport à la direction radiale. Ainsi, en modifiant le nombre, l'emplacement et/ou les dimensions des nervures de renforcement, il est possible de modifier la rigidité de la roue. Ces nervures de renforcement peuvent également permettre la transmission du couple entre l'arbre et la roue, en particulier entre l'arbre et le voile de la roue.  These reinforcing ribs increase the mechanical strength of the wheel while limiting the overall mass of the wheel. These reinforcing ribs may have a purely radial direction, they may also be inclined relative to the radial direction. Thus, by modifying the number, the location and / or the dimensions of the reinforcing ribs, it is possible to modify the rigidity of the wheel. These reinforcing ribs may also allow the transmission of torque between the shaft and the wheel, in particular between the shaft and the wheel web.
[0034] Le voile peut comporter une pluralité d'orifices traversants. [0035] Ces orifices traversant permettent un équilibrage de pression entre une surface amont du voile et une surface aval du voile. On peut ainsi équilibrer les efforts sur l'arbre en amont et en aval de la roue et ainsi réduire les efforts subits par des butées de la pompe centrifuge. The web may comprise a plurality of through orifices. These through holes allow a pressure equalization between an upstream surface of the web and a downstream surface of the web. It is thus possible to balance the forces on the shaft upstream and downstream of the wheel and thus reduce the sudden forces by stops of the centrifugal pump.
[0036] La roue peut comprendre un inducteur et un impulseur et les orifices traversants sont disposés entre l'inducteur et l'impulseur permettant une orientation du fluide dans l'axe de l'écoulement.  The wheel may comprise an inductor and an impeller and the through orifices are disposed between the inductor and the impeller allowing orientation of the fluid in the axis of the flow.
[0037] La roue peut être réalisée en métal ou en alliage métallique.  The wheel can be made of metal or metal alloy.
[0038] Le présent exposé concerne également une pompe centrifuge comprenant une roue telle que définie précédemment.  The present disclosure also relates to a centrifugal pump comprising a wheel as defined above.
[0039] Le présent exposé concerne aussi un procédé de fabrication d'une roue tel que défini précédemment, la roue étant réalisé par un procédé de fabrication additive.  The present disclosure also relates to a method of manufacturing a wheel as defined above, the wheel being made by an additive manufacturing process.
[0040] Ce procédé de fabrication additive permet une grande souplesse dans les formes produites et permet également de réaliser de manière aisée des pièces présentant des cavités et/ou des conduits internes.  This additive manufacturing process allows great flexibility in the shapes produced and also makes it easy to produce parts with cavities and / or internal ducts.
Brève description des dessins Brief description of the drawings
[0041] D'autres caractéristiques et avantages de l'invention ressortiront de la description suivante de modes de réalisation de l'invention, donnés à titre d'exemples non limitatifs, en référence aux figures annexées, sur lesquelles : Other features and advantages of the invention will emerge from the following description of embodiments of the invention, given by way of non-limiting examples, with reference to the appended figures, in which:
- la figure 1 est une vue schématique en coupe axiale d'une pompe centrifuge ;  - Figure 1 is a schematic axial sectional view of a centrifugal pump;
- les figures 2A et 2B sont des vues en coupe axiale d'une roue pour une pompe centrifuge selon deux modes de réalisation ;  - Figures 2A and 2B are views in axial section of a wheel for a centrifugal pump according to two embodiments;
- la figure 3 est une vue en perspective de la roue de la figure 2A, vu du côté amont ; et  FIG. 3 is a perspective view of the wheel of FIG. 2A, seen from the upstream side; and
- la figure 4 est une vue partielle en perspective de la roue de la figure 2A, vu du côté aval.  - Figure 4 is a partial perspective view of the wheel of Figure 2A, seen from the downstream side.
Description détaillée de l'invention [0042] La figure 1 représente une vue en coupe axiale d'une pompe centrifuge 100 comprenant un arbre 12, définissant un axe X, sur lequel sont monté une roue 10, un distributeur de turbine aubé 116 et un disque de turbine 102. Ces éléments sont compris dans un carter de pompe 104 qui comporte un carter avant 106, un carter central 108 et un carter d'échappement 110. Le carter de pompe 104 définit une volute de pompe 112 et un tore d'admission de turbine 114. Detailed description of the invention FIG. 1 represents an axial sectional view of a centrifugal pump 100 comprising a shaft 12, defining an axis X, on which are mounted a wheel 10, an impeller turbine nozzle 116 and a turbine disk 102. These FIG. elements are included in a pump housing 104 which has a front housing 106, a central housing 108 and an exhaust housing 110. The pump housing 104 defines a pump volute 112 and a turbine inlet core 114.
[0043] La pompe 100 comporte également des moyens de blocage selon l'axe X des éléments de la pompe 100 sur l'arbre 12. Ces éléments sont par exemple des écrous 14 et 118. La roue 10 et le disque de turbine 102 sont montés sur l'arbre 12 et dans le carter de pompe 104 par des roulements 18, la roue 10 et le disque de turbine 102 étant chacun espacé de leur roulement 18 respectif par une cale de réglage 16.  The pump 100 also comprises locking means along the axis X of the elements of the pump 100 on the shaft 12. These elements are for example nuts 14 and 118. The wheel 10 and the turbine disc 102 are mounted on the shaft 12 and in the pump casing 104 by bearings 18, the wheel 10 and the turbine disc 102 being each spaced from their respective bearing 18 by a shim 16.
[0044] La figure 2A représente un mode de réalisation d'une roue 10 pour une pompe centrifuge 100. Sur la figure 2A, la flèche F représente le sens de circulation normal d'un fluide dans la pompe centrifuge 100 et donc autour de la roue 10. Par la suite, les termes « amont » et « aval » sont définis par rapport au sens de circulation normal du fluide dans la pompe centrifuge.  FIG. 2A shows an embodiment of a wheel 10 for a centrifugal pump 100. In FIG. 2A, the arrow F represents the normal flow direction of a fluid in the centrifugal pump 100 and therefore around the wheel 10. Thereafter, the terms "upstream" and "downstream" are defined relative to the direction of normal circulation of the fluid in the centrifugal pump.
[0045] La roue 10 est représenté montée sur l'arbre 12. Elle est fixée sur l'arbre 12, à son extrémité amont, par l'écrou 14 et, à son extrémité aval, par la cale de réglage 16 et le roulement 18.  The wheel 10 is shown mounted on the shaft 12. It is fixed on the shaft 12, at its upstream end, by the nut 14 and, at its downstream end, by the shim 16 and the bearing 18.
[0046] D'une manière générale, la roue 10 de la figure 2A comprend un inducteur 20 et un impulseur 22.  In general, the wheel 10 of FIG. 2A comprises an inductor 20 and an impeller 22.
[0047] La roue 10 comprend un axe de rotation X définissant une direction axiale X de la roue 10.  The wheel 10 comprises an axis of rotation X defining an axial direction X of the wheel 10.
[0048] La roue 10 comprend un moyeu 24 et un voile 26 ayant une forme de révolution comprenant une partie de fixation 28 du voile 26 avec le moyeu 24. Comme représenté, le voile 24 s'évase depuis la partie de fixation 28 selon la direction axiale X, c'est-à-dire que le voile 26 s'évase depuis la partie de fixation 28, disposée à une extrémité amont de la roue 10 vers une extrémité aval de la roue 10. Sur la figure 2A, le voile 26 a une première partie de forme sensiblement cylindrique qui s'évase ensuite vers l'aval de la roue 10, de sorte qu'une extrémité libre 26A du voile s'étend sensiblement dans un plan radial, c'est-à-dire dans un plan perpendiculaire à la direction axiale X. [0049] La roue 10 comprend également un bourrelet annulaire 30 disposé entre le voile 26 et le moyeu 24, à l'extrémité aval de la roue 10, au droit, selon la direction axiale X, de l'extrémité libre 26A du voile 26. Le bourrelet annulaire 30 est fixé au voile 26 tandis qu'un espace annulaire 32 est ménagé entre le moyeu 24 et le bourrelet annulaire 30. The wheel 10 comprises a hub 24 and a sail 26 having a shape of revolution comprising an attachment portion 28 of the web 26 with the hub 24. As shown, the web 24 flares from the fastening portion 28 according to the X axial direction, that is to say that the web 26 flares from the fastening portion 28, disposed at an upstream end of the wheel 10 to a downstream end of the wheel 10. In Figure 2A, the veil 26 has a first portion of substantially cylindrical shape which then flares downstream of the wheel 10, so that a free end 26A of the web extends substantially in a radial plane, that is to say in a plane perpendicular to the axial direction X. The wheel 10 also comprises an annular bead 30 disposed between the web 26 and the hub 24, at the downstream end of the wheel 10, to the right, in the axial direction X, of the free end 26A of the sail 26 The annular bead 30 is fixed to the web 26 while an annular space 32 is formed between the hub 24 and the annular bead 30.
[0050] Le voile 26 s'évasant depuis la partie d'attache 28 du voile 26 selon la direction axiale X, une cavité 34 est ainsi formée entre le moyeu 24, le voile 26 et le bourrelet annulaire 30. Cette cavité 34 est au moins ouverte du fait de l'espace annulaire 32 ménagé entre le moyeu 24 et le bourrelet annulaire 30.  The web 26 flaring from the attachment portion 28 of the web 26 in the axial direction X, a cavity 34 is thus formed between the hub 24, the web 26 and the annular bead 30. This cavity 34 is at less open because of the annular space 32 formed between the hub 24 and the annular bead 30.
[0051] Par ailleurs, dans le mode de réalisation de la figure 2A, le moyeu 24 présente une surface intérieure 36. Cette surface intérieure 36 comporte une portion qui forme une surface intérieure de frettage 38 du moyeu 24 et donc de la roue 10 sur l'arbre 12. Cette surface intérieure de frettage 38 est disposée à l'extrémité aval de la roue 10.  Furthermore, in the embodiment of Figure 2A, the hub 24 has an inner surface 36. This inner surface 36 has a portion which forms an inner shrinking surface 38 of the hub 24 and thus the wheel 10 on the shaft 12. This inner hooping surface 38 is disposed at the downstream end of the wheel 10.
[0052] La projection radiale, c'est-à-dire selon une direction radiale R, de la section du bourrelet annulaire 30 sur le moyeu 24, en particulier sur la surface intérieure 36 du moyeu 24, définit une portion de la surface intérieure 36, selon la direction axiale X, au droit de l'espace annulaire 32 ménagé entre le moyeu 24 et le bourrelet annulaire 30.  The radial projection, that is to say in a radial direction R, of the section of the annular bead 30 on the hub 24, in particular on the inner surface 36 of the hub 24, defines a portion of the inner surface. 36, in the axial direction X, to the right of the annular space 32 formed between the hub 24 and the annular bead 30.
[0053] Dans le mode de réalisation de la figure 2A, la surface intérieure de frettage 36 est disposée sensiblement complètement, selon la direction axiale X, au droit de l'espace annulaire 32 ménagé entre le moyeu 24 et le bourrelet annulaire 30.  In the embodiment of FIG. 2A, the inside hooping surface 36 is arranged substantially completely, in the axial direction X, at the level of the annular space 32 formed between the hub 24 and the annular bead 30.
[0054] La surface intérieure de frettage 38 est comprise dans la projection radiale du bourrelet annulaire 30 sur la surface intérieure 36 du moyeu 24, à plus ou moins 5% la projection radiale du bourrelet annulaire 30 sur la surface intérieure 36 du moyeu 24. Ainsi, la surface intérieure de frettage 38 peut être de dimension inférieure à la projection radiale du bourrelet annulaire 30 sur la surface intérieure 36 du moyeu 24 mais dépasser légèrement, de moins de 5% de la dimension, selon la direction axiale X du bourrelet annulaire 30.  The inner hooping surface 38 is included in the radial projection of the annular bead 30 on the inner surface 36 of the hub 24, plus or minus 5% the radial projection of the annular bead 30 on the inner surface 36 of the hub 24. Thus, the internal hooping surface 38 may be smaller than the radial projection of the annular bead 30 on the inner surface 36 of the hub 24 but slightly exceed, by less than 5% of the dimension, in the axial direction X of the annular bead. 30.
[0055] La roue 10 comporte une pluralité de nervures de renforcement 40 de renforcement disposées entre le voile 26 et le moyeu 24 dans la cavité 34. Ces nervures radiales 40 sont visibles également sur la figure 4. 17 052832 The wheel 10 comprises a plurality of reinforcing ribs 40 for reinforcing disposed between the web 26 and the hub 24 in the cavity 34. These radial ribs 40 are also visible in FIG. 4. 17 052832
9  9
[0056] Comme représenté sur les figures 2 à 4, le voile 26 comporte une pluralité d'orifices traversants 42 disposés entre l'inducteur 20 et l'impulseur 22. Ces orifices traversants 42 permettent le passage de liquide de l'amont de la roue 10 dans la cavité 34. Comme représenté sur la figure 4, chaque orifice traversant 42 débouche entre deux nervures de renforcement 40. As shown in Figures 2 to 4, the web 26 has a plurality of through holes 42 disposed between the inductor 20 and the impeller 22. These through holes 42 allow the passage of liquid from the upstream of the wheel 10 in the cavity 34. As shown in Figure 4, each through hole 42 opens between two reinforcing ribs 40.
[0057] Par ailleurs, l'inducteur 20 comporte des ailettes 44, dans ce mode de réalisation l'inducteur 20 comporte quatre ailettes 44 et l'impulseur 22 comporte des ailettes 46, dans ce mode de réalisation la roue comporte douze ailettes 46.  Furthermore, the inductor 20 comprises fins 44, in this embodiment the inductor 20 comprises four fins 44 and the impeller 22 comprises fins 46, in this embodiment the wheel comprises twelve fins 46.
[0058] On notera que les nervures de renforcement 40 sont également au nombre de 12 et qu'elles sont disposées en vis-à-vis de part et d'autre du voile 26.  Note that the reinforcing ribs 40 are also 12 in number and that they are arranged vis-à-vis on both sides of the web 26.
[0059] Par ailleurs, la surface intérieure 36 du moyeu 24 comporte des saillies 48 permettant également le passage du couple entre l'arbre 12 et le moyeu 24.  Furthermore, the inner surface 36 of the hub 24 has projections 48 also allowing the passage of the torque between the shaft 12 and the hub 24.
[0060] Dans ce qui suit, les éléments communs aux différents modes de réalisation sont identifiés par les mêmes références numériques.  In the following, the elements common to the various embodiments are identified by the same reference numerals.
[0061] Dans le mode de réalisation de la figure 2B, la surface intérieure de frettage 36 est disposée sensiblement complètement, selon la direction axiale X, en amont de l'espace annulaire 32 ménagé entre le moyeu 24 et le bourrelet annulaire 30.  In the embodiment of FIG. 2B, the inner hooping surface 36 is arranged substantially completely, in the axial direction X, upstream of the annular space 32 formed between the hub 24 and the annular bead 30.
[0062] La roue 10 est fabriquée par un procédé de fabrication additive, par exemple par utilisation d'un faisceau laser sur un lit de poudre. Le lit de poudre est formé par la poudre qui constituera la roue 10. Par exemple, la poudre peut comprendre du titane ou être en alliage métallique communément désigné par la marque déposée Inconel™. On parle par la suite d'Inconel pour désigner un alliage à base de fer alliés avec du nickel et du chrome.  The wheel 10 is manufactured by an additive manufacturing process, for example by using a laser beam on a bed of powder. The powder bed is formed by the powder that will constitute the wheel 10. For example, the powder may comprise titanium or be a metal alloy commonly referred to by the trademark Inconel ™. Inconel is later referred to as an alloy based on iron alloyed with nickel and chromium.
[0063] La roue 10 est fabriquée par superposition de couches selon la direction axiale X en partant de son extrémité aval et en terminant par son extrémité amont.  The wheel 10 is manufactured by superposition of layers in the axial direction X from its downstream end and ending with its upstream end.
[0064] Les surfaces extérieures de la roue 10 sont ensuite usinées de manière classique et connue de sorte que l'état de surface du voile 26, des ailettes 44, 46 et de la surface interne 36 du moyeu est conforme au 52832 The outer surfaces of the wheel 10 are then machined in a conventional manner and known so that the surface condition of the web 26, the fins 44, 46 and the inner surface 36 of the hub is in accordance with the 52832
10  10
cahier des charges. Il n'est par contre pas nécessaire d'usiner les surfaces de la cavité 34. Specifications. It is not necessary to machine the surfaces of the cavity 34.
[0065] Quoique le présent exposé ait été décrit en se référant à un exemple de réalisation spécifique, il est évident que des différentes modifications et changements peuvent être effectués sur ces exemples sans sortir de la portée générale de l'invention telle que définie par les revendications. En outre, des caractéristiques individuelles des différents modes de réalisation évoqués peuvent être combinées dans des modes de réalisation additionnels. Par conséquent, la description et les dessins doivent être considérés dans un sens illustratif plutôt que restrictif.  Although the present description has been described with reference to a specific embodiment, it is obvious that various modifications and changes can be made to these examples without departing from the general scope of the invention as defined by the claims. In addition, individual features of the various embodiments mentioned can be combined in additional embodiments. Therefore, the description and drawings should be considered in an illustrative rather than restrictive sense.
[0066] Par exemple, le nombre d'ailettes 44 portées par l'inducteur 20 peut varier, il en va de même du nombre d'ailettes 46 portées par l'impulseur 22. Le nombre de nervures de renforcement 40 peut être différent du nombre d'ailettes 46 portées par l'impulseur 22. De même, le nombre d'orifices traversants 42 peut être différent du nombre de nervures de renforcement 40.  For example, the number of fins 44 carried by the inductor 20 may vary, the same is true of the number of fins 46 carried by the impeller 22. The number of reinforcing ribs 40 may be different from the number of fins 46 carried by the impeller 22. Similarly, the number of through holes 42 may be different from the number of reinforcing ribs 40.
[0067] On notera par ailleurs, que les ailettes 44, 46 sont des ailettes droites, ces ailettes peuvent également être inclinées par rapport à la direction radiale, voire présenter une certaine courbure. Il en va de même des nervures de renforcement 40. Les nervures de renforcement 40 représentées sont des nervures radiales. Toutefois, ces nervures peuvent également être inclinées par rapport à la direction radiale, voire présenter une certaine courbure. La roue 10 comporte un inducteur 20 et un impulseur 22. La roue 10 pourrait ne comporter qu'un impulseur 22.  Note also that the fins 44, 46 are straight fins, these fins may also be inclined relative to the radial direction, or even have a certain curvature. The same is true of the reinforcing ribs 40. The reinforcing ribs 40 shown are radial ribs. However, these ribs may also be inclined relative to the radial direction, or even have a certain curvature. The wheel 10 comprises an inductor 20 and an impeller 22. The wheel 10 could comprise only one impeller 22.

Claims

REVENDICATIONS
1. Roue (10) pour pompe centrifuge présentant une direction axiale (X), la roue (10) comprenant un moyeu (24), un voile (26) ayant une forme de révolution comprenant une partie de fixation (28) du voile (26) avec le moyeu (24), le voile (26) s'évasant depuis la partie de fixation (28) selon la direction axiale (X), et un bourrelet annulaire (30) disposé entre le voile (26) et le moyeu (24), le bourrelet annulaire (30) étant fixé au voile (26) tandis qu'un espace annulaire (32) est ménagé entre le moyeu (24) et le bourrelet annulaire (30). A centrifugal pump wheel (10) having an axial direction (X), the wheel (10) comprising a hub (24), a web (26) having a shape of revolution comprising an attachment portion (28) of the web ( 26) with the hub (24), the web (26) flaring from the fastening portion (28) in the axial direction (X), and an annular bead (30) disposed between the web (26) and the hub (24), the annular bead (30) being attached to the web (26) while an annular space (32) is provided between the hub (24) and the annular bead (30).
2. Roue (10) selon la revendication 1, dans laquelle la roue (10) comprend une extrémité amont et une extrémité aval, la partie de fixation du voile (28) avec le moyeu (24) étant disposé à l'extrémité amont de la roue (10) et le bourrelet annulaire (30) étant disposé à l'extrémité aval de la roue (10).  The wheel (10) of claim 1, wherein the wheel (10) includes an upstream end and a downstream end, the veil attachment portion (28) with the hub (24) being disposed at the upstream end of the wheel (10). the wheel (10) and the annular bead (30) being disposed at the downstream end of the wheel (10).
3. Roue (10) selon la revendication 1 ou 2, dans laquelle le moyeu (24) comporte une surface intérieure de frettage (38) configurée pour fretter le moyeu (24) sur un arbre (12), la surface intérieure de frettage (38) étant disposée, au moins en partie, selon la direction axiale (X), au droit de l'espace annulaire (32) ménagé entre le moyeu (24) et le bourrelet annulaire (30).  A wheel (10) according to claim 1 or 2, wherein the hub (24) has an inner shrinking surface (38) configured to shroud the hub (24) on a shaft (12), the inner hooping surface ( 38) being arranged, at least in part, in the axial direction (X), to the right of the annular space (32) formed between the hub (24) and the annular bead (30).
4. Roue (10) selon la revendication 3, dans laquelle la surface intérieure de frettage (38) est sensiblement complètement disposée, selon la direction axiale (X), au droit de l'espace annulaire (32) ménagé entre le moyeu (24) et le bourrelet annulaire (30).  A wheel (10) according to claim 3, wherein the inner hooping surface (38) is substantially completely disposed in the axial direction (X) to the right of the annular space (32) between the hub (24). ) and the annular bead (30).
5. Roue (10) selon la revendication 1 ou 2, dans laquelle le moyeu (24) comporte une surface intérieure de frettage (38) configurée pour fretter le moyeu (24) sur un arbre (12), la surface intérieure de frettage (38) étant disposée, selon la direction axiale (X), en amont de l'espace annulaire (32) ménagé entre le moyeu (24) et le bourrelet annulaire (30).  The wheel (10) according to claim 1 or 2, wherein the hub (24) has an inner shrinking surface (38) configured to shroud the hub (24) on a shaft (12), the inner hooping surface ( 38) being arranged, in the axial direction (X), upstream of the annular space (32) formed between the hub (24) and the annular bead (30).
6. Roue (10) selon l'une quelconque des revendications 1 à 5, dans laquelle la roue (10) comporte une pluralité de nervures de renforcement (40) disposées entre le voile (26) et le moyeu (24).  Wheel (10) according to any one of claims 1 to 5, wherein the wheel (10) has a plurality of reinforcing ribs (40) disposed between the web (26) and the hub (24).
7. Roue (10) selon l'une quelconque des revendications 1 à 6, dans laquelle le voile (26) comporte une pluralité d'orifices traversants (42). Wheel (10) according to any one of claims 1 to 6, wherein the web (26) has a plurality of through holes (42).
8. Roue (10) selon la revendication 7, dans laquelle la roue (10) comprend un inducteur (20) et un impulseur (22) et dans laquelle les orifices traversants (42) sont disposés entre l'inducteur (20) et l'impulseur (22). Wheel (10) according to claim 7, wherein the wheel (10) comprises an inductor (20) and an impeller (22) and in which the through holes (42) are arranged between the inductor (20) and the impeller (22).
9. Pompe centrifuge comprenant une roue (10) selon l'une quelconque des revendications 1 à 8.  9. Centrifugal pump comprising a wheel (10) according to any one of claims 1 to 8.
10. Procédé de fabrication d'une roue (10) selon l'une quelconque des revendications 1 à 8, la roue (10) étant réalisée par un procédé de fabrication additive.  10. A method of manufacturing a wheel (10) according to any one of claims 1 to 8, the wheel (10) being performed by an additive manufacturing process.
PCT/FR2017/052832 2016-10-27 2017-10-16 Impeller for centrifugal pump, centrifugal pump and manufacturing method WO2018078239A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP17793718.2A EP3532732B1 (en) 2016-10-27 2017-10-16 Impeller for centrifugal pump, centrifugal pump and manufacturing method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1660434A FR3058190B1 (en) 2016-10-27 2016-10-27 IMPELLER FOR CENTRIFUGAL PUMP, CENTRIFUGAL PUMP AND MANUFACTURING PROCESS
FR1660434 2016-10-27

Publications (1)

Publication Number Publication Date
WO2018078239A1 true WO2018078239A1 (en) 2018-05-03

Family

ID=58314352

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2017/052832 WO2018078239A1 (en) 2016-10-27 2017-10-16 Impeller for centrifugal pump, centrifugal pump and manufacturing method

Country Status (3)

Country Link
EP (1) EP3532732B1 (en)
FR (1) FR3058190B1 (en)
WO (1) WO2018078239A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024076496A1 (en) * 2022-10-04 2024-04-11 Atlas Copco Comptec, Llc Adapter for torque transmission between two rotatable components

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3589827A (en) * 1969-08-12 1971-06-29 Sergei Stepanovich Gerasimenko Centrifugal leakproof fluid pump
GB1386937A (en) * 1972-04-17 1975-03-12 Mecanique Ind Int Impellers of pumps for cooling systems of internal combustion engines
DE19918286A1 (en) * 1999-04-22 2000-10-26 Ksb Ag Inducer for centrifugal pump is assembled from individual parts, and has blades fitted into and welded to grooves in inducer hub
FR3008749A1 (en) * 2013-07-22 2015-01-23 Snecma CENTRIFUGAL PUMP, ESPECIALLY FOR FEEDER ENGINES
DE102014009735A1 (en) * 2014-07-02 2016-01-07 Rosswag Gmbh Blade and impeller of a turbomachine, as well as manufacturing process for it

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3589827A (en) * 1969-08-12 1971-06-29 Sergei Stepanovich Gerasimenko Centrifugal leakproof fluid pump
GB1386937A (en) * 1972-04-17 1975-03-12 Mecanique Ind Int Impellers of pumps for cooling systems of internal combustion engines
DE19918286A1 (en) * 1999-04-22 2000-10-26 Ksb Ag Inducer for centrifugal pump is assembled from individual parts, and has blades fitted into and welded to grooves in inducer hub
FR3008749A1 (en) * 2013-07-22 2015-01-23 Snecma CENTRIFUGAL PUMP, ESPECIALLY FOR FEEDER ENGINES
DE102014009735A1 (en) * 2014-07-02 2016-01-07 Rosswag Gmbh Blade and impeller of a turbomachine, as well as manufacturing process for it

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024076496A1 (en) * 2022-10-04 2024-04-11 Atlas Copco Comptec, Llc Adapter for torque transmission between two rotatable components

Also Published As

Publication number Publication date
EP3532732A1 (en) 2019-09-04
EP3532732B1 (en) 2022-03-09
FR3058190B1 (en) 2021-01-29
FR3058190A1 (en) 2018-05-04

Similar Documents

Publication Publication Date Title
EP3732384B1 (en) Planet carrier for an epicyclic speed reduction gear
EP2530298B1 (en) Propeller for a hydraulic machine, hydraulic machine provided with such a propeller and method for assembling such a propeller
EP4185519B1 (en) Aircraft turbine engine comprising variable-pitch propeller blades
EP4034776B1 (en) Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contact
FR2901843A1 (en) Radial-flow impeller driving mechanism for motor vehicle cooling water pump, has drum with outer track placed with respect to inner track, balls placed on tracks to form bearing, and shaft fixed to drum by using annular cup
EP3124795B1 (en) Turbojet engine fan with engine fan disc and turbojet
FR3112819A1 (en) AIRCRAFT TURBOMACHINE COMPRISING VARIABLE-PITCHED PROPELLER BLADE
EP3927989B1 (en) Drive shaft comprising a fusible section and method for protecting such a drive shaft against an overtorque
WO2013083937A1 (en) Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element
EP3532732B1 (en) Impeller for centrifugal pump, centrifugal pump and manufacturing method
FR2976615A1 (en) ROTOR STRUCTURE COMPRISING AN INTERNAL HYDRAULIC VOLTAGE DEVICE
EP2435662B1 (en) Low-pressure turbine
EP3648926B1 (en) Assembly of a shaft and an element intended to form a rotor and manufacturing method
EP2053248A2 (en) Belt drive mechanism and its manufacturing method
FR3112820A1 (en) AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE
FR2949858A1 (en) EQUILIBRATION DEVICE AND METHOD
EP4308800A1 (en) Device for centring and guiding a shaft of an aircraft turbine engine
EP4308799A1 (en) Device for centring and guiding a shaft of an aircraft turbine engine
WO2024033590A1 (en) Propeller for an aircraft turbine engine
FR3045711A1 (en) ATTACK SHIELD
EP4308798A1 (en) Device for centring and guiding a shaft of an aircraft turbine engine
WO2021058898A1 (en) Assembly for a turbine engine
FR3121473A1 (en) Fixing shells in a turbomachine
FR2681094A1 (en) Vane wheel made in three parts
FR3135303A1 (en) Pre-assembly process for an aircraft turbomachine

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17793718

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2017793718

Country of ref document: EP

Effective date: 20190527