EP3807500B1 - Holding system for the dismantling of a blade wheel - Google Patents

Holding system for the dismantling of a blade wheel Download PDF

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Publication number
EP3807500B1
EP3807500B1 EP19735372.5A EP19735372A EP3807500B1 EP 3807500 B1 EP3807500 B1 EP 3807500B1 EP 19735372 A EP19735372 A EP 19735372A EP 3807500 B1 EP3807500 B1 EP 3807500B1
Authority
EP
European Patent Office
Prior art keywords
blade
inserts
blades
inter
insert
Prior art date
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Active
Application number
EP19735372.5A
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German (de)
French (fr)
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EP3807500A1 (en
Inventor
Nicolas Daniel DELAPORTE
Alain Dominique Gendraud
Emmanuel Bernard Marie CHARRIER
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.)
Safran Aircraft Engines SAS
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Safran Aircraft Engines SAS
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Publication date
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Publication of EP3807500A1 publication Critical patent/EP3807500A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • F05D2230/70Disassembly methods
    • 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
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position

Definitions

  • This presentation relates to a holding system for removing a paddle wheel and a method for removing a paddle wheel.
  • a turbine rotor comprising a movable blade wheel 1, that is to say configured to be driven in rotation around the axis of the rotor, shown in figure 1 , forming a crown, and which comprises a disc 2 around which are circumferentially mounted a set of blades 3. It is also known to hold the blades 3 axially by means of a retaining ring 17.
  • the retaining ring 17 is subject to faster wear than disk 2. It must therefore be replaced more regularly.
  • the axis of the paddle wheel is called the axis of symmetry (or quasi-symmetry) thereof.
  • This axis corresponds to the axis of rotation of the paddle wheel.
  • the axial direction corresponds to the direction of the axis of the blade wheel and a radial direction is a direction perpendicular to the axis of the blade wheel and intersecting this axis.
  • an axial plane is a plane containing the axis of the impeller and a radial plane is a plane perpendicular to this axis.
  • a circumference is understood as a circle belonging to a radial plane and whose center belongs to the axis of the paddle wheel.
  • a circumferential direction is a direction following a circumference.
  • interior/internal and exterior/external are used with reference to a radial direction so that the interior part of an element is, in a radial direction, closer to the axis of the impeller than the outer part of the same element.
  • the holding position is at a determined height of the inter-blade space in the radial direction.
  • the center of the insert in the radial direction is at the determined height.
  • the position for holding the inserts is preferably as close as possible to the disk, in order to hold the blades as well as possible.
  • the blade wheel further includes a retainer ring configured to axially retain the blades to the disk.
  • each vane of the plurality of vanes comprises a root, a blade and a head, arranged in this order along a longitudinal direction of the vane.
  • the longitudinal direction of the blade corresponds to the radial direction.
  • the position for holding the inserts is at an internal portion of the inter-blade space, defined between the blade root and the center of the inter-blade space in a radial direction.
  • each insert has a shape corresponding to the inter-blade space, defined between two adjacent blades.
  • at least a portion of the inserts matches the shape of a portion of the blades of two adjacent blades.
  • each insert in the holding position, is placed against, and preferably directly against, each of the adjacent blades defining the inter-blade space.
  • each of the inserts comprises at least one portion made of an aluminum-based alloy, and/or a polymer having a shore A hardness of between 75 and 100.
  • the inserts could comprise a portion comprising an aluminum-based alloy covered with a polymer.
  • the polymer is a resin.
  • the at least one portion comprising aluminum, or a polymer having a Shore A hardness of between 75 and 100 is a portion in contact with a blade.
  • the at least one portion consists of an alloy based on aluminium, and/or a polymer having a shore A hardness of between 75 and 100.
  • the material forming the blade is less soft than the aluminum-based alloy and/or the polymer having a Shore A hardness of between 75 and 100.
  • the inserts have a thickness in a radial direction greater than or equal to 10% of the height of a blade of a vane in the radial direction.
  • height of a blade of a blade is meant the greatest distance between a platform of the blade root and a platform of the blade tip.
  • the thickness is about 10 mm, for a blade height of about 100 mm.
  • the insert comprises a first part and a second part.
  • the first part is the part of the insert intended to be inserted into the inter-blade space.
  • the second part is used, for example, for mounting the insert.
  • the greatest length in an axial direction of the first part is between 10 mm and 20 mm, that is to say represents between 70% and 100% of the length of the blade of the blade in the axial direction.
  • the holding system includes a gripping portion configured to be mounted on an insert of the plurality of inserts, the gripping portion being configured to allow the gripping of the insert and to facilitate the mounting of the insert in an inter-blade space.
  • the gripping portion can make it possible to mount the inserts directly at their holding position, by a movement which follows the shape of the insert.
  • the gripping portion can form a lever arm which thus makes it possible to be able to exert sufficient force on the insert to insert it directly into the holding position.
  • the holding system comprises a device for positioning the plurality of inserts, each insert of the plurality of inserts being configured to be attached to the positioning device so as to hold the inserts in position, c 'that is to say so that the inserts are arranged in the holding position.
  • the inserts are substantially aligned in a circumferential direction, which makes it possible to balance the forces exerted on the blades, and thus to more effectively maintain the position of the blades with respect to each other, and will facilitate the dismantling of the disc.
  • the positioning device allows slightly different insert holding positions in the radial direction, so as to compensate for the dimensional tolerances/dispersions of the blades.
  • substantially or “slightly” is meant that the actual height in the radial direction of the inserts in their holding position differs by at most 5% relative to the determined height.
  • the positioning device allows radial blocking of the inserts which makes it possible to guarantee the integrity of the assembly comprising the blades and the inserts, in particular when the disc is disassembled.
  • the positioning device includes a positioning ring, the positioning ring including fasteners to allow attachment of the inserts to the positioning ring.
  • the inserts are held in their holding position, which makes it possible to more effectively maintain the relative position of the blades.
  • the positioning device is annular.
  • the fasteners allow attachment of the inserts to the positioning ring.
  • the fixing elements of the positioning device are intended to be arranged opposite the inserts when the inserts are in the holding position, to allow the fixing of the inserts on the positioning device.
  • the fixing elements comprise oblong openings each emerging facing an inter-blade space.
  • the oblong slots extend in the radial direction so as to allow a slightly different positioning of the inserts relative to each other in the radial direction.
  • the inserts each comprise a blind hole extending in the axial direction.
  • the blind hole is intended to come opposite the oblong slot when the insert is in the holding position.
  • a fixing member makes it possible to fix the insert on the positioning ring, cooperating with the blind hole.
  • the blind hole is reamed and the fastener is threaded.
  • the fasteners are threaded and are configured to cooperate with the reamed blind holes present in each of the inserts.
  • the fixing members are configured to hold the inserts against the positioning ring, for example thanks to a stop element, such as a screw head.
  • the inserts each comprise a first member and a second member, the first and second members being configured to be placed in an inter-blade space, the first member being placed against a first blade, and the second member being disposed against a second vane circumferentially adjacent to the first vane; and a clamp, configured to be inserted between the first and second bodies so as to maintain the insert between the first and second blades.
  • the clamping piece is configured to be inserted between the first and second members in the axial direction.
  • the mounting of the inserts can be carried out axially in particular when the radial mounting is difficult to achieve in certain circumstances.
  • This embodiment of the inserts also makes it possible to adapt the clamping to each inter-blade space, depending on the insertion of the clamping part.
  • the holding system includes a stop disk, allowing the positioning of the inserts.
  • At least one of the first and second members comprises a guide surface, configured to guide the clamping part during its insertion between the first and second members and to avoid the radial displacement of the clamping piece.
  • the clamping part comprises an abutment configured to come into contact with the first and second members when the clamping part is mounted between the first and second members.
  • the clamping piece has a wedge, bevel, conical or rectangular shape.
  • the inserts are inserted directly at their holding position, thanks to a gripping portion, by a movement which follows the shape of the insert.
  • the gripping portion can form a lever arm which thus makes it possible to be able to exert sufficient force on the insert to insert it directly into the holding position.
  • the mounting of the inserts can be carried out axially if the radial mounting is difficult to carry out in certain circumstances.
  • a positioning device for example, to position and hold the inserts in the holding position, it is possible to arrange a positioning device at the level of the holding position of the inserts.
  • the figure 1 represents a blade wheel 1.
  • the blade wheel 1 is installed at the level of the low pressure turbine of a turbomachine.
  • the paddle wheel 1 comprises a disc 2 and a plurality of vanes 3.
  • the plurality of vanes 3 are mounted on the disc 2 around its circumference.
  • the picture 2 is a section of the bladed wheel 1 according to the plane II-II shown in figure 1 .
  • Dawn 3 represented on the figure 2 comprises a blade 5, a blade root 7 and a blade tip 9.
  • the blade root 7 comprises a radially inner platform 11.
  • the blade tip 9 comprises a radially outer platform 13.
  • the blade 5 extends radially between the platforms 11, 13. All the blades 3 of the plurality of blades are similar to the blade shown in figure 1 .
  • the blades 5 of the blades 3 each have a concave face and a convex face.
  • the vanes 3 When they are mounted on the disc 2, the vanes 3 extend in a radial direction DR and are spaced apart from each other so as to define inter-vane spaces 15, visible on the figure 1 for example. It is understood that an inter-blade space 15 is defined between two adjacent blades 3. The distance between two blades 5 of adjacent blades 3 is greater near the blade tips 9 than at proximity of the blade roots 7. Thus, the distance between two blade blades decreases between the blade tips 9 and the blade roots 7.
  • the vanes 3 are mounted on the disc 2 in a nominal operating position.
  • the figure 1 and 2 also represent a retaining ring 17, configured to axially block the blades 3 on the disc 2.
  • the picture 3 represents a portion of a bladed wheel 1 and a holding system 19 for removing the bladed wheel 1.
  • the holding system 19 comprises a plurality of inserts 21.
  • the inserts 21 are here inserted aligned in a circumferential direction in each of the inter-blade spaces 15 so as to maintain the relative position of the blades 3 and to allow the dismantling of the disc 1.
  • the insert 21 comprises a first part 23 and a second part 25.
  • the first part 23 is configured to maintain the relative position of the blades 3.
  • the first part 23 comprises a first contact surface 27, configured to come into contact with a blade 5a of a first blade 3a and match the shape of the convex face of the blade 5a.
  • the first contact surface 27 therefore has a concave shape.
  • the first contact surface 27 and the convex face of the blade 5a have complementary shapes.
  • the first part 23 further comprises a second contact surface 29, configured to come into contact with a blade 5b of a second blade 3b and match the shape of the concave face of the blade 5b.
  • the second contact surface 29 therefore has a convex shape.
  • the second contact surface 29 and the concave face of the blade 5b have complementary shapes.
  • the first and second vanes 3a, 3b are adjacent in the circumferential direction of the vane wheel.
  • the convex face of the blade 5a and the concave face of the blade 5b face each other in the circumferential direction.
  • the surfaces of the blades 5a, 5b of the first and second blades 3a, 3b define the inter-blade space 15.
  • the first part 23 of the insert 21 has a shape corresponding to a portion of the inter-blade space 15, when the blades 3 are in the nominal position.
  • the inserts 21 are mounted in the inter-blade spaces 15 at a holding position, the blades of the blade wheel are held together via the inserts, which releases the stresses applied by the blade roots. 7 at the level of the cells of the disk in which the blade roots are mounted and thus allows easy assembly or disassembly of the disk.
  • At least the portions of the first part 23 of the insert 21 in contact with the blades 5a, 5b of the blades 3a, 3b, and preferably at least the first part 23 of the insert 21, comprise/comprises a aluminum-based alloy, and/or a polymer having a Shore A hardness of between 75 and 100.
  • the polymer is a resin.
  • the dimension of the section of the first part 23 of the insert 21 according to a plane normal to the radial direction DR is greater than the dimension according to this plane of the inter-blade space 15 near the blade roots 7.
  • the insert 21, in the position for maintaining the relative position of the blades 3, is positioned in the inter-blade space 15 at the level of a portion having substantially the same dimension as the dimension of the section of the insert 21 along a plane normal to the radial direction DR.
  • the inserts 21 are arranged at the level of a first end portion of the inter-blade spaces 15, defined, for each inter-blade space, between the blade root 7 and the center of the inter-blade space. 15 in the radial direction DR.
  • the inserts 21, and more particularly their first part 23, have a thickness e in the radial direction DR greater than or equal to 10% of the height h of the blade in the radial direction DR.
  • the holding position of each insert is at a determined height of the inter-blade space 15, or of the adjacent blades 5.
  • the center of the insert in the radial direction that is to say, a height of the insert corresponding to half of its thickness e
  • the height according to the radial direction, corresponding to the holding position is significantly different at the height determined for certain inserts.
  • the difference between the actual height of the position in which the inserts 21 are held and the determined height is less than or equal to 5% of the total height of the blade 5, or of the inter-blade space 15.
  • the thickness e is approximately 10 mm, for a blade height of approximately 100 mm.
  • the greatest length in an axial direction DA of the first part 23 is 15 mm, that is to say between 70 and 100% of the length in the axial direction DA of the blade 5 of the blade 3.
  • the second part 25 of the insert 21 is connected to the first part of the insert 23.
  • the first and second parts 23, 25 are formed together.
  • the second part 25 extends, here, in the extension of the first part 23 in the axial direction DA.
  • the second part 25 provides a gripping means making it possible to engage or disengage the insert 21 from the inter-blade space 15.
  • the second part 25 can also serve as a support for mounting the insert 21 on other elements.
  • the holding system 19 may further comprise a gripping portion 31 of the inserts 21.
  • the gripping portion 31 can be mounted on the second part 25.
  • the gripping portion 31 makes it possible to form a handle, long enough to allow a user to grasp it easily.
  • the gripping portion 31 facilitates the manipulation of the inserts 21 and their insertion into the inter-blade spaces 15.
  • the gripping portion 31 is removably mounted on the second part 25. In this way, the user can use the same gripping portion 31 for mounting all the inserts 21.
  • the holding system 19 may comprise a positioning device 33.
  • the positioning device 33 may comprise a positioning ring 35 configured to be positioned against the blades 3, in a circumferential direction.
  • the positioning ring 35 includes oblong slots 37 opening towards the inter-blade space 15.
  • the oblong slots 37 extend in a radial direction DR so as to allow a slightly different positioning of the inserts 21 with respect to each other in the radial direction DR, so as to take into account dimensional tolerances/dispersions.
  • the second part 25 comprises a bored blind hole 38 extending along the axial direction DA.
  • the blind hole 38 is intended to come opposite the oblong slot 37, when the insert 21 is in the holding position.
  • a fixing member 39 makes it possible to fix the insert 21 on the positioning ring 35.
  • the fixing member 39 is a screw, configured to be inserted into the blind hole 38 bored.
  • the insert 21 could be fixed on the positioning ring 35 by any other means. In this way, the inserts 21 are substantially aligned along the circumferential direction.
  • an internal radial abutment disc could be provided at a predetermined height, corresponding to the holding position of the inserts 21.
  • the second part 25 of the inserts could then come into abutment against the internal disk.
  • the inserts 21 are inserted, one by one, aligned in a circumferential direction in each of the inter-blade spaces 15, in their holding position.
  • the inserts 21 are first inserted at an outer portion of the inter-blade space 15, as shown in figure 9 , then the inserts 21 are moved, for example thanks to the gripping portion 31, in the radial direction DR, according to the arrow F, that is to say inwards, until reaching the holding position.
  • outer portion of the inter-blade space 15 is meant a portion defined between the center of the blade 5 in the radial direction DR and the outer end of the blade 5.
  • the inserts 21 are placed directly at their holding position by a movement which follows the shape of the first and second contact surfaces 27, 29, thanks to the gripping portion 31 which forms, in this variant, a lever arm and which thus makes it possible to exert sufficient force on the insert 21 to insert it directly into the holding position.
  • the positioning ring 35 can be arranged so that the oblong slots 37 are at the level of the holding position of the inserts 21.
  • the inserts are mounted, and face the oblong slots, they are fixed to the positioning ring 35, here thanks to the fixing members 39 which can be inserted into the blind holes 37 of the inserts 21.
  • the disc 2 can be removed. After removing the disc 2, it is possible, for example, to replace the the retaining ring 17. Then, the disc 2 can be reengaged with all of the blade roots 7 of the blades 3, since their relative position has been maintained by the inserts. Finally, once the blades 3 have been reassembled on the disc 2, the retaining system 19 can be removed.
  • a second embodiment of the holding system is shown in figure 8 .
  • the elements common to the different embodiments are identified by the same reference numerals.
  • the second embodiment differs from the first embodiment in that the inserts 21 each comprise a first member 41 and a second member 43.
  • the first and second members 41, 43 are configured to be arranged, in an inter-blade space 15
  • the first member 41 is placed against the blade 5a of the first blade 3a and the second member 43 is placed against the blade 5b of the second blade 3b, adjacent circumferentially to the first blade 3a.
  • the first and second members 41, 43 face each other in the circumferential direction of the paddle wheel.
  • the inserts 21 further each comprise a clamping part 45, configured to be inserted, in the axial direction DA, between the first and second members 41, 43, so as to hold the first and second members 41, 43 against the blades 5a , 5b.
  • the clamping piece 45 has a wedge or bevel shape.
  • At least one of the first and second members 41, 43 comprises a guide surface.
  • each of the first and second members 41, 43 comprises a guide surface.
  • the guide surfaces are here formed by grooves 47, 49, made in each of the first and second members 41, 43.
  • the edges of the grooves 47, 49 allow the radial blocking of the clamping part 45 and a guiding in axial translation of clamping piece 45.
  • the clamping part 41 comprises an axial stop configured to come into contact with the first and second members 41, 43 when the clamping part 45 is mounted between the first and second members 41, 43.
  • an internal disc 34 of radial abutment could be provided at a predetermined height, corresponding to the holding position of the inserts 21.
  • the first and second members could be positioned in abutment against the internal disc 34, before the insertion of the clamping piece.
  • the inserts 21 are inserted, one by one, into each of the inter-blade spaces 15, in their holding position.
  • the first member 41 of an insert 21 is placed against the blade 5a of the first blade 3a, at the level of the holding position.
  • the second member 43 of the insert 21 is placed against the blade 5b of the second blade 3b, circumferentially adjacent to the first blade 3a, also at the level of the holding position, so that the second member 43 is placed in face of first member 41 in the circumferential direction of the paddle wheel.
  • the clamping piece 45 is inserted between the first and second members 41, 43.
  • Inserts 21 are thus inserted into each of the inter-blade spaces 15.
  • the disc 2 can be removed. After removing the disc 2, it is possible, for example, to replace the retaining ring 17. Then, the disk 2 can be easily reengaged with all of the blade roots 7 of the blades 3, since their relative position has been maintained by inserts. Finally, once the blades 3 have been reassembled on the disc 2, the retaining system 19 can be removed.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Crushing And Grinding (AREA)

Description

DOMAINE TECHNIQUETECHNICAL AREA

Le présent exposé concerne un système de maintien pour le démontage d'une roue à aubes et un procédé de démontage d'une roue à aubes.This presentation relates to a holding system for removing a paddle wheel and a method for removing a paddle wheel.

ARRIERE-PLAN TECHNOLOGIQUETECHNOLOGICAL BACKGROUND

Il est connu de l'art antérieur, notamment du document FR 3 008 448 , un rotor de turbine comprenant une roue à aubes 1 mobile, c'est-à-dire configurée pour être entrainée en rotation autour de l'axe du rotor, représentée en figure 1, formant une couronne, et qui comprend un disque 2 autour duquel sont montées circonférentiellement un ensemble d'aubes 3. Il est également connu de maintenir axialement les aubes 3 grâce à un anneau de retenue 17. En fonctionnement, l'anneau de retenue 17 est sujet à une usure plus rapide que le disque 2. Il est donc à remplacer plus régulièrement. Or, pour atteindre l'anneau de retenue 17, et pouvoir le remplacer, il convient de retirer les roues à aubes disposées en aval de la roue à aubes qui comprend l'anneau de retenue usagé. Or, pour retirer les aubes des différentes roues à aubes mobiles disposées en aval, il convient de retirer une à une les aubes des disques, puis, une fois l'anneau de retenue remplacé, remonter une à une les aubes sur les disques des roues à aubes mobiles. Une telle opération est chronophage et représente un coût important. FR 2604936 et US 5026032 divulguent deux dispositifs de serrage de pièce.It is known from the prior art, in particular from the document FR 3 008 448 , a turbine rotor comprising a movable blade wheel 1, that is to say configured to be driven in rotation around the axis of the rotor, shown in figure 1 , forming a crown, and which comprises a disc 2 around which are circumferentially mounted a set of blades 3. It is also known to hold the blades 3 axially by means of a retaining ring 17. In operation, the retaining ring 17 is subject to faster wear than disk 2. It must therefore be replaced more regularly. However, to reach the retaining ring 17, and to be able to replace it, it is necessary to remove the impellers arranged downstream of the impeller which includes the used retaining ring. However, to remove the blades from the various impellers with movable blades arranged downstream, it is necessary to remove the blades from the discs one by one, then, once the retaining ring has been replaced, reassemble the blades on the discs of the wheels one by one. with moving paddles. Such an operation is time-consuming and represents a significant cost. EN 2604936 and US 5026032 disclose two workpiece clamping devices.

PRESENTATIONPRESENTATION

Le présent exposé vise à résoudre tout ou partie des inconvénients mentionnés ci-dessus.This presentation aims to resolve all or part of the drawbacks mentioned above.

A cet effet, le présent exposé concerne un système de maintien pour le démontage d'une roue à aubes, la roue à aubes comprenant :

  • un disque,
  • une pluralité d'aubes configurée pour être montée circonférentiellement autour du disque, la pluralité d'aubes définissant une pluralité d'espaces inter-aubes, les espaces inter-aubes étant chacun défini circonférentiellement entre deux aubes adjacentes de la pluralité d'aubes,
le système de maintien comprenant une pluralité d'inserts, chacun des inserts étant configuré pour être inséré aligné selon une direction circonférentielle dans chacun des espaces inter-aubes dans une position de maintien de façon à maintenir la position relative des aubes lorsque la pluralité d'aubes est démontée du disque.To this end, the present presentation relates to a holding system for dismantling a bladed wheel, the bladed wheel comprising:
  • a disk,
  • a plurality of vanes configured to be mounted circumferentially around the disk, the plurality of vanes defining a plurality of inter-vane spaces, the spaces inter-blades each being defined circumferentially between two adjacent blades of the plurality of blades,
the holding system comprising a plurality of inserts, each of the inserts being configured to be inserted aligned in a circumferential direction in each of the inter-blade spaces in a holding position so as to maintain the relative position of the blades when the plurality of vanes is removed from the disc.

On appelle axe de la roue à aubes, l'axe de symétrie (ou quasi-symétrie) de celui-ci. Cet axe correspond à l'axe de rotation de la roue à aubes. La direction axiale correspond à la direction de l'axe de la roue à aubes et une direction radiale est une direction perpendiculaire à l'axe de la roue à aubes et coupant cet axe. De même, un plan axial est un plan contenant l'axe de la roue à aubes et un plan radial est un plan perpendiculaire à cet axe.The axis of the paddle wheel is called the axis of symmetry (or quasi-symmetry) thereof. This axis corresponds to the axis of rotation of the paddle wheel. The axial direction corresponds to the direction of the axis of the blade wheel and a radial direction is a direction perpendicular to the axis of the blade wheel and intersecting this axis. Similarly, an axial plane is a plane containing the axis of the impeller and a radial plane is a plane perpendicular to this axis.

Une circonférence s'entend comme un cercle appartenant à un plan radial et dont le centre appartient à l'axe de la roue à aubes. Une direction circonférentielle est une direction suivant une circonférence.A circumference is understood as a circle belonging to a radial plane and whose center belongs to the axis of the paddle wheel. A circumferential direction is a direction following a circumference.

Sauf précision contraire, les adjectifs intérieur/interne et extérieur/externe sont utilisés en référence à une direction radiale de sorte que la partie intérieure d'un élément est, suivant une direction radiale, plus proche de l'axe de la roue à aubes que la partie extérieure du même élément.Unless otherwise specified, the adjectives interior/internal and exterior/external are used with reference to a radial direction so that the interior part of an element is, in a radial direction, closer to the axis of the impeller than the outer part of the same element.

Grâce à ces dispositions, il est possible d'accéder à l'anneau de retenue en démontant le disque d'une roue à aubes mobile donnée, sans avoir à démonter les roues à aubes mobiles disposées en aval. Ainsi, un gain de temps est obtenu pour accéder à un anneau de retenue endommagé porté par cette roue à aubes mobile donnée. En effet, la position relative des aubes étant maintenue, il est possible de démonter et remonter l'ensemble des aubes sur le disque en une seule fois, sans avoir à les démonter ou remonter une par une. Ainsi, le démontage et remontage de la roue à aubes est plus rapide et plus efficace. En outre, les inserts reprenant les efforts s'exerçant sur le disque, le disque est plus facilement démontable.Thanks to these arrangements, it is possible to access the retaining ring by dismantling the disk of a given impeller, without having to disassemble the impellers with impellers arranged downstream. Thus, a saving of time is obtained in accessing a damaged retaining ring carried by this given movable impeller. Indeed, the relative position of the blades being maintained, it is possible to disassemble and reassemble all of the blades on the disk at one time, without having to disassemble or reassemble them one by one. Thus, the disassembly and reassembly of the paddle wheel is faster and more efficient. In addition, the inserts taking up the forces exerted on the disc, the disc is more easily removable.

La position de maintien se trouve à une hauteur déterminée de l'espace inter-aubes selon la direction radiale.The holding position is at a determined height of the inter-blade space in the radial direction.

Lorsqu'un insert se trouve dans la position de maintien, le centre de l'insert selon la direction radiale se trouve au niveau de la hauteur déterminée.When an insert is in the holding position, the center of the insert in the radial direction is at the determined height.

Par exemple, la position de maintien des inserts est préférablement au plus proche du disque, afin de maintenir au mieux les aubes.For example, the position for holding the inserts is preferably as close as possible to the disk, in order to hold the blades as well as possible.

Dans certains modes de réalisation, la roue à aubes comprend en outre un anneau de retenue configuré pour maintenir axialement les aubes sur le disque.In some embodiments, the blade wheel further includes a retainer ring configured to axially retain the blades to the disk.

Dans certains modes de réalisation, chaque aube de la pluralité d'aubes comprend un pied, une pale et une tête, disposés dans cet ordre selon une direction longitudinale de l'aube. Lorsque l'aube est montée sur le disque, la direction longitudinale de l'aube correspond à la direction radiale.In certain embodiments, each vane of the plurality of vanes comprises a root, a blade and a head, arranged in this order along a longitudinal direction of the vane. When the blade is mounted on the disc, the longitudinal direction of the blade corresponds to the radial direction.

Dans certains modes de réalisation, la position de maintien des inserts se trouve au niveau d'une portion interne de l'espace inter-aubes, défini entre le pied d'aube et le centre de l'espace inter-aubes selon une direction radiale.In certain embodiments, the position for holding the inserts is at an internal portion of the inter-blade space, defined between the blade root and the center of the inter-blade space in a radial direction. .

On comprend qu'au moins une partie de chaque insert a une forme correspondant à l'espace inter-aubes, défini entre deux aubes adjacentes. De plus, au moins une portion des inserts épouse la forme d'une portion des pales de deux aubes adjacentes.It is understood that at least a part of each insert has a shape corresponding to the inter-blade space, defined between two adjacent blades. In addition, at least a portion of the inserts matches the shape of a portion of the blades of two adjacent blades.

On comprend que, dans la position de maintien, chaque insert est disposé contre, et de préférence directement contre, chacune des aubes adjacentes définissant l'espace inter-aubes.It will be understood that, in the holding position, each insert is placed against, and preferably directly against, each of the adjacent blades defining the inter-blade space.

Dans certains modes de réalisation, chacun des inserts comprend au moins une portion en alliage à base d'aluminium, et/ou un polymère ayant une dureté shore A comprise entre 75 et 100.In certain embodiments, each of the inserts comprises at least one portion made of an aluminum-based alloy, and/or a polymer having a shore A hardness of between 75 and 100.

Par « à base de », on entend un alliage comprenant au moins 50% en masse d'aluminium.By “based on”, is meant an alloy comprising at least 50% by weight of aluminium.

Par exemple, les inserts pourraient comprendre une portion comprenant un alliage à base d'aluminium recouvert d'un polymère.For example, the inserts could comprise a portion comprising an aluminum-based alloy covered with a polymer.

Par exemple, le polymère est une résine.For example, the polymer is a resin.

On comprend que l'au moins une portion comprenant de l'aluminium, ou un polymère ayant une dureté shore A comprise entre 75 et 100 est une portion en contact avec une aube.It is understood that the at least one portion comprising aluminum, or a polymer having a Shore A hardness of between 75 and 100 is a portion in contact with a blade.

Par exemple, l'au moins une portion est constituée d'un alliage à base d'aluminium, et/ou d'un polymère ayant une dureté shore A comprise entre 75 et 100.For example, the at least one portion consists of an alloy based on aluminium, and/or a polymer having a shore A hardness of between 75 and 100.

On comprend que le matériau formant l'aube est moins tendre que l'alliage à base d'aluminium et/ou le polymère ayant une dureté shore A comprise entre 75 et 100.It is understood that the material forming the blade is less soft than the aluminum-based alloy and/or the polymer having a Shore A hardness of between 75 and 100.

Ainsi, lorsque les inserts sont installés dans leur position de maintien, le risque d'abîmer les aubes, qui sont formées dans un matériau plus dur que le matériau des portions des inserts en contact avec les aubes, est plus limité.Thus, when the inserts are installed in their holding position, the risk of damaging the blades, which are formed from a harder material than the material of the portions of the inserts in contact with the blades, is more limited.

Dans certains modes de réalisation, les inserts ont une épaisseur selon une direction radiale supérieure ou égale à 10% de la hauteur d'une pale d'une aube selon la direction radiale.In some embodiments, the inserts have a thickness in a radial direction greater than or equal to 10% of the height of a blade of a vane in the radial direction.

On entend par hauteur d'une pale d'une aube la distance la plus grande entre une plateforme du pied d'aube et une plateforme de la tête d'aube.By height of a blade of a blade is meant the greatest distance between a platform of the blade root and a platform of the blade tip.

Ainsi, des surfaces de contact suffisantes avec les aubes sont garanties et le maintien de la position des aubes les unes par rapport aux autres est plus efficace.Thus, sufficient contact surfaces with the blades are guaranteed and maintaining the position of the blades relative to each other is more effective.

Par exemple, l'épaisseur est d'environ 10 mm, pour une hauteur de pale d'environ 100 mm.For example, the thickness is about 10 mm, for a blade height of about 100 mm.

Selon un exemple ne faisant pas partie de l'invention revendiquée, l'insert comprend une première partie et une deuxième partie. La première partie est la partie de l'insert destinée à être insérée dans l'espace inter-aubes. La deuxième partie sert, par exemple, au montage de l'insert. La plus grande longueur selon une direction axiale de la première partie est comprise entre 10 mm et 20 mm, c'est-à-dire représente entre 70% et 100% de la longueur de la pale de l'aube selon la direction axiale.According to an example not forming part of the claimed invention, the insert comprises a first part and a second part. The first part is the part of the insert intended to be inserted into the inter-blade space. The second part is used, for example, for mounting the insert. The greatest length in an axial direction of the first part is between 10 mm and 20 mm, that is to say represents between 70% and 100% of the length of the blade of the blade in the axial direction.

Dans certains modes de réalisation, le système de maintien comprend une portion de préhension configurée pour être montée sur un insert de la pluralité d'inserts, la portion de préhension étant configurée pour permettre la préhension de l'insert et faciliter le montage de l'insert dans un espace inter-aubes.In some embodiments, the holding system includes a gripping portion configured to be mounted on an insert of the plurality of inserts, the gripping portion being configured to allow the gripping of the insert and to facilitate the mounting of the insert in an inter-blade space.

Ainsi, la manipulation des inserts lors de leur insertion dans les espaces inter-aubes est facilitée.Thus, the handling of the inserts during their insertion into the inter-blade spaces is facilitated.

Par exemple, la portion de préhension peut permettre de monter directement les inserts au niveau de leur position de maintien, par un mouvement qui suit la forme de l'insert. En effet, la portion de préhension peut former un bras de levier qui permet ainsi de pouvoir exercer une force suffisante sur l'insert pour l'insérer directement dans la position de maintien.For example, the gripping portion can make it possible to mount the inserts directly at their holding position, by a movement which follows the shape of the insert. Indeed, the gripping portion can form a lever arm which thus makes it possible to be able to exert sufficient force on the insert to insert it directly into the holding position.

Dans certains modes de réalisation, le système de maintien comprend un dispositif de positionnement de la pluralité d'inserts, chaque insert de la pluralité d'inserts étant configuré pour être rapporté sur le dispositif de positionnement de façon à maintenir en position les inserts, c'est-à-dire de façon à ce que les inserts soient disposés dans la position de maintien.In certain embodiments, the holding system comprises a device for positioning the plurality of inserts, each insert of the plurality of inserts being configured to be attached to the positioning device so as to hold the inserts in position, c 'that is to say so that the inserts are arranged in the holding position.

Ainsi, les inserts sont sensiblement alignés selon une direction circonférentielle, ce qui permet d'équilibrer les efforts exercés sur les aubes, et ainsi de maintenir plus efficacement la position des aubes les unes par rapport aux autres, et facilitera le démontage du disque.Thus, the inserts are substantially aligned in a circumferential direction, which makes it possible to balance the forces exerted on the blades, and thus to more effectively maintain the position of the blades with respect to each other, and will facilitate the dismantling of the disc.

Par exemple, le dispositif de positionnement permet des positions de maintien des inserts légèrement différentes selon la direction radiale, de façon à compenser les tolérances/dispersions dimensionnelles des aubes.For example, the positioning device allows slightly different insert holding positions in the radial direction, so as to compensate for the dimensional tolerances/dispersions of the blades.

Par « sensiblement » ou « légèrement », on entend que la hauteur réelle selon la direction radiale des inserts dans leur position de maintien diffère d'au plus 5% par rapport à la hauteur déterminée.By "substantially" or "slightly" is meant that the actual height in the radial direction of the inserts in their holding position differs by at most 5% relative to the determined height.

Le dispositif de positionnement permet le blocage radial des inserts ce qui permet de garantir l'intégrité de l'ensemble comprenant les aubes et les inserts, notamment lorsque le disque est démonté.The positioning device allows radial blocking of the inserts which makes it possible to guarantee the integrity of the assembly comprising the blades and the inserts, in particular when the disc is disassembled.

Dans certains modes de réalisation, le dispositif de positionnement comprend un anneau de positionnement, l'anneau de positionnement comprenant des éléments de fixation pour permettre la fixation des inserts sur l'anneau de positionnement.In some embodiments, the positioning device includes a positioning ring, the positioning ring including fasteners to allow attachment of the inserts to the positioning ring.

Ainsi, les inserts sont maintenus dans leur position de maintien, ce qui permet de maintenir plus efficacement la position relative des aubes.Thus, the inserts are held in their holding position, which makes it possible to more effectively maintain the relative position of the blades.

On comprend que le dispositif de positionnement est annulaire.It is understood that the positioning device is annular.

Dans certains modes de réalisation, les éléments de fixation permettent la fixation des inserts sur l'anneau de positionnement.In some embodiments, the fasteners allow attachment of the inserts to the positioning ring.

Dans certains modes de réalisation, les éléments de fixation du dispositif de positionnement sont destinés à être disposés en face des inserts lorsque les inserts sont en position de maintien, pour permettre la fixation des inserts sur le dispositif de positionnement.In certain embodiments, the fixing elements of the positioning device are intended to be arranged opposite the inserts when the inserts are in the holding position, to allow the fixing of the inserts on the positioning device.

Par exemple, les éléments de fixation comprennent des lumières oblongues débouchant chacune face à un espace inter-aubes. Par exemple, les lumières oblongues s'étendent selon la direction radiale de façon à permettre un positionnement légèrement différent des inserts les uns par rapport aux autres selon la direction radiale.For example, the fixing elements comprise oblong openings each emerging facing an inter-blade space. For example, the oblong slots extend in the radial direction so as to allow a slightly different positioning of the inserts relative to each other in the radial direction.

Par exemple, les inserts comprennent chacun un trou borgne s'étendant selon la direction axiale. Le trou borgne est destiné à venir en regard de la lumière oblongue lorsque l'insert est dans la position de maintien.For example, the inserts each comprise a blind hole extending in the axial direction. The blind hole is intended to come opposite the oblong slot when the insert is in the holding position.

Par exemple, un organe de fixation permet de fixer l'insert sur l'anneau de positionnement, en coopérant avec le trou borgne.For example, a fixing member makes it possible to fix the insert on the positioning ring, cooperating with the blind hole.

Par exemple, le trou borgne est alésé et l'organe de fixation est fileté.For example, the blind hole is reamed and the fastener is threaded.

Par exemple, les organes de fixation sont filetés et sont configurés pour coopérer avec les trous borgnes alésés présents dans chacun des inserts. En outre, les organes de fixation sont configurés pour maintenir les inserts contre l'anneau de positionnement, par exemple grâce à un élément de butée, tel qu'une tête de vis.For example, the fasteners are threaded and are configured to cooperate with the reamed blind holes present in each of the inserts. Furthermore, the fixing members are configured to hold the inserts against the positioning ring, for example thanks to a stop element, such as a screw head.

Dans certains modes de réalisation, les inserts comprennent chacun un premier organe et un deuxième organe, les premier et deuxième organes étant configurés pour être disposés dans un espace inter-aubes, le premier organe étant disposé contre une première aube, et le deuxième organe étant disposé contre une deuxième aube circonférentiellement adjacente à la première aube ; et une pièce de serrage, configurée pour être insérée entre les premier et deuxième organes de façon à maintenir l'insert entre les première et deuxième aubes.In certain embodiments, the inserts each comprise a first member and a second member, the first and second members being configured to be placed in an inter-blade space, the first member being placed against a first blade, and the second member being disposed against a second vane circumferentially adjacent to the first vane; and a clamp, configured to be inserted between the first and second bodies so as to maintain the insert between the first and second blades.

Par exemple, la pièce de serrage est configurée pour être insérée entre les premier et deuxième organes selon la direction axiale.For example, the clamping piece is configured to be inserted between the first and second members in the axial direction.

Ainsi, le montage des inserts peut être réalisé axialement notamment lorsque le montage radial est difficile à réaliser dans certaines circonstances. Ce mode de réalisation des inserts permet également d'adapter le serrage à chaque espace inter-aubes, en fonction de l'insertion de la pièce de serrage.Thus, the mounting of the inserts can be carried out axially in particular when the radial mounting is difficult to achieve in certain circumstances. This embodiment of the inserts also makes it possible to adapt the clamping to each inter-blade space, depending on the insertion of the clamping part.

Par exemple, le système de maintien comprend un disque de butée, permettant le positionnement des inserts.For example, the holding system includes a stop disk, allowing the positioning of the inserts.

Selon un exemple ne faisant pas partie de l'invention revendiquée, au moins un des premier et deuxième organes comprend une surface de guidage, configurée pour guider la pièce de serrage lors de son insertion entre les premier et deuxième organes et éviter le déplacement radial de la pièce de serrage.According to an example not forming part of the claimed invention, at least one of the first and second members comprises a guide surface, configured to guide the clamping part during its insertion between the first and second members and to avoid the radial displacement of the clamping piece.

Selon un exemple ne faisant pas partie de l'invention revendiquée, la pièce de serrage comprend une butée configurée pour venir au contact des premier et deuxième organes lorsque la pièce de serrage est montée entre les premier et deuxième organes.According to an example not forming part of the claimed invention, the clamping part comprises an abutment configured to come into contact with the first and second members when the clamping part is mounted between the first and second members.

Selon un exemple ne faisant pas partie de l'invention revendiquée, la pièce de serrage a une forme de coin, en biseau, conique ou rectangulaire.According to an example not forming part of the claimed invention, the clamping piece has a wedge, bevel, conical or rectangular shape.

Le présent exposé se rapporte en outre à un procédé de démontage d'une roue à aubes comprenant un disque et une pluralité d'aubes montée circonférentiellement autour du disque, la pluralité d'aubes définissant une pluralité d'espaces inter-aubes, les espaces inter-aubes étant chacun défini circonférentiellement entre deux aubes adjacentes de la pluralité d'aubes, le procédé de démontage comprenant les étapes suivantes :

  1. A. insérer une pluralité d'inserts d'un système de maintien alignés selon une direction circonférentielle dans les espaces inter-aubes dans une position de maintien de sorte que la position relative des aubes soit maintenue ;
  2. B. retirer le disque.
This presentation also relates to a method for disassembling a blade wheel comprising a disc and a plurality of blades mounted circumferentially around the disc, the plurality of blades defining a plurality of inter-blade spaces, the spaces inter-blades each being defined circumferentially between two adjacent blades of the plurality of blades, the dismantling method comprising the following steps:
  1. A. inserting a plurality of inserts of a retaining system aligned in a circumferential direction into the inter-blade spaces in a retaining position so that the relative position of the blades is maintained;
  2. B. remove the disc.

Grâce à ces dispositions, il est possible d'accéder à l'anneau de retenue en démontant le disque d'une roue à aubes mobile donnée, sans avoir à démonter les roues à aubes mobiles disposées en aval. Ainsi, un gain de temps est obtenu pour accéder à un anneau de retenue endommagé porté par cette roue à aubes mobile donnée. En effet, la position relative des aubes étant maintenue, il est possible de démonter et remonter l'ensemble des aubes sur le disque en une seule fois, sans avoir à les démonter ou remonter une par une. Ainsi, le démontage et remontage de la roue à aubes est plus rapide et plus efficace. En outre, les inserts reprenant les efforts s'exerçant sur le disque, le disque est plus facilement démontable.Thanks to these provisions, it is possible to access the retaining ring by dismantling the disk of a moving blade wheel given, without having to disassemble the impellers arranged downstream. Thus, a saving of time is obtained in accessing a damaged retaining ring carried by this given movable impeller. Indeed, the relative position of the blades being maintained, it is possible to disassemble and reassemble all of the blades on the disk at one time, without having to disassemble or reassemble them one by one. Thus, the disassembly and reassembly of the paddle wheel is faster and more efficient. In addition, the inserts taking up the forces exerted on the disc, the disc is more easily removable.

Selon un exemple ne faisant pas partie de l'invention revendiquée, le procédé comprend en outre les étapes suivantes :

  • remplacer un anneau de retenue configuré pour maintenir la position des aubes selon une direction axiale,
  • réengager les aubes sur le disque,
  • retirer le système de maintien de la roue à aubes.
According to an example not forming part of the claimed invention, the method further comprises the following steps:
  • replacing a retaining ring configured to maintain the position of the blades in an axial direction,
  • re-engage the blades on the disc,
  • remove the impeller retainer.

Dans certains modes de réalisation, lors de l'étape A:

  • on insère les inserts au niveau d'une portion radialement externe des espaces inter-aubes, et
  • on déplace les inserts selon une direction radiale, radialement vers l'intérieur, jusqu'à atteindre la position de maintien.
In some embodiments, during step A:
  • the inserts are inserted at a radially outer portion of the inter-blade spaces, and
  • the inserts are moved in a radial direction, radially inwards, until the holding position is reached.

Ainsi, il est possible de régler la position des inserts en fonction de l'effort que l'on souhaite appliquer sur les aubes et en fonction des tolérances/dispersions dimensionnelles des aubes.Thus, it is possible to adjust the position of the inserts according to the force which it is desired to apply to the blades and according to the dimensional tolerances/dispersions of the blades.

Selon une variante ne faisant pas partie de l'invention revendiquée, on insère les inserts directement au niveau de leur position de maintien, grâce à une portion de préhension, par un mouvement qui suit la forme de l'insert. En effet, la portion de préhension peut former un bras de levier qui permet ainsi de pouvoir exercer une force suffisante sur l'insert pour l'insérer directement dans la position de maintien.According to a variant not forming part of the claimed invention, the inserts are inserted directly at their holding position, thanks to a gripping portion, by a movement which follows the shape of the insert. Indeed, the gripping portion can form a lever arm which thus makes it possible to be able to exert sufficient force on the insert to insert it directly into the holding position.

Dans certains modes de réalisation, les inserts comprennent chacun un premier organe, un deuxième organe et une pièce de serrage, lors de l'étape A :

  • on dispose le premier organe d'un insert, dans un espace inter-aubes, contre une première aube au niveau de la position de maintien,
  • on dispose le deuxième organe de l'insert, dans l'espace inter-aubes, contre une deuxième aube, adjacente à la première aube, de façon à ce que le deuxième organe soit disposé circonférentiellement en regard du premier organe,
  • on insère la pièce de serrage entre les premier et deuxième organes de façon à maintenir l'insert dans la position de maintien.
In certain embodiments, the inserts each comprise a first member, a second member and a clamping piece, during step A:
  • the first member of an insert is placed, in an inter-blade space, against a first blade at the holding position,
  • the second member of the insert is placed, in the inter-blade space, against a second blade, adjacent to the first blade, so that the second member is arranged circumferentially opposite the first member,
  • the clamping piece is inserted between the first and second members so as to hold the insert in the holding position.

Ainsi, le montage des inserts peut être réalisé axialement si le montage radial est difficile à réaliser dans certaines circonstances.Thus, the mounting of the inserts can be carried out axially if the radial mounting is difficult to carry out in certain circumstances.

Par exemple, pour positionner et maintenir les inserts dans la position de maintien, on peut disposer un dispositif de positionnement au niveau de la position de maintien des inserts.For example, to position and hold the inserts in the holding position, it is possible to arrange a positioning device at the level of the holding position of the inserts.

BREVE DESCRIPTION DES DESSINSBRIEF DESCRIPTION OF THE DRAWINGS

L'invention et ses avantages seront mieux compris à la lecture de la description détaillée faite ci-après de différents modes de réalisation de l'invention donnés à titre d'exemples non limitatifs. Cette description fait référence aux pages de figures annexées, sur lesquelles :

  • la figure 1 représente une roue à aubes ;
  • la figure 2 représente une vue en coupe de la roue à aubes selon le plan II-II de la figure 1 ;
  • la figure 3 représente une vue schématique portion d'une roue à aubes dans laquelle des inserts sont insérés dans les espaces inter-aubes ;
  • la figure 4 représente un insert selon un exemple ne faisant pas partie de l'invention revendiquée;
  • la figure 5 représente un insert monté sur la roue à aubes et fixé à un dispositif de positionnement ;
  • la figure 6 représente un insert selon une mode de réalisation sur lequel est montée une portion de préhension ;
  • la figure 7 représente une portion de la roue à aubes, sur laquelle est monté un système de maintien selon une mode de réalisation ;
  • la figure 8 représente une portion de la roue à aubes, sur laquelle est montée un insert selon le deuxième mode de réalisation ;
  • la figure 9 représente une étape du montage d'un insert selon une mode de réalisation dans un espace inter-aubes.
The invention and its advantages will be better understood on reading the detailed description given below of various embodiments of the invention given by way of non-limiting examples. This description refers to the pages of appended figures, on which:
  • the figure 1 represents a waterwheel;
  • the picture 2 represents a sectional view of the paddle wheel according to the plane II-II of the figure 1 ;
  • the picture 3 shows a schematic view portion of a paddle wheel in which inserts are inserted into the inter-blade spaces;
  • the figure 4 represents an insert according to an example not forming part of the claimed invention;
  • the figure 5 shows an insert mounted on the impeller and attached to a positioning device;
  • the figure 6 represents an insert according to one embodiment on which a gripping portion is mounted;
  • the figure 7 represents a portion of the paddle wheel, on which is mounted a holding system according to one embodiment;
  • the figure 8 represents a portion of the paddle wheel, on which is mounted an insert according to the second embodiment;
  • the figure 9 represents a step in the assembly of an insert according to one embodiment in an inter-blade space.

DESCRIPTION DETAILLEEDETAILED DESCRIPTION

La figure 1 représente une roue à aubes 1. Par exemple, la roue à aubes 1 est installée au niveau de la turbine basse pression d'une turbomachine.The figure 1 represents a blade wheel 1. For example, the blade wheel 1 is installed at the level of the low pressure turbine of a turbomachine.

La roue à aubes 1 comprend un disque 2 et une pluralité d'aubes 3. La pluralité d'aubes 3 est montée sur le disque 2 autour de sa circonférence.The paddle wheel 1 comprises a disc 2 and a plurality of vanes 3. The plurality of vanes 3 are mounted on the disc 2 around its circumference.

La figure 2 est une coupe de la roue à aubes 1 selon le plan II-II représenté en figure 1. L'aube 3 représentée sur la figure 2 comprend une pale 5, un pied d'aube 7 et une tête d'aube 9. Le pied d'aube 7 comprend une plateforme radialement interne 11. La tête d'aube 9 comprend une plateforme 13 radialement externe. La pale 5 s'étend radialement entre les plateformes 11, 13. Toutes les aubes 3 de la pluralité d'aubes sont analogues à l'aube représentée en figure 1. Les pales 5 des aubes 3 ont chacune une face concave et une face convexe.The picture 2 is a section of the bladed wheel 1 according to the plane II-II shown in figure 1 . Dawn 3 represented on the figure 2 comprises a blade 5, a blade root 7 and a blade tip 9. The blade root 7 comprises a radially inner platform 11. The blade tip 9 comprises a radially outer platform 13. The blade 5 extends radially between the platforms 11, 13. All the blades 3 of the plurality of blades are similar to the blade shown in figure 1 . The blades 5 of the blades 3 each have a concave face and a convex face.

Lorsqu'elles sont montées sur le disque 2, les aubes 3 s'étendent selon une direction radiale DR et sont espacées les unes des autres de manière à définir des espaces inter-aubes 15, visibles sur la figure 1 par exemple. On comprend qu'un espace inter-aubes 15 est défini entre deux aubes 3 adjacentes. La distance entre deux pales 5 d'aubes 3 adjacentes est plus importante à proximité des têtes d'aube 9 qu'à proximité des pieds d'aube 7. Ainsi, la distance entre deux pales d'aubes décroît entre les têtes d'aube 9 et les pieds d'aube 7.When they are mounted on the disc 2, the vanes 3 extend in a radial direction DR and are spaced apart from each other so as to define inter-vane spaces 15, visible on the figure 1 for example. It is understood that an inter-blade space 15 is defined between two adjacent blades 3. The distance between two blades 5 of adjacent blades 3 is greater near the blade tips 9 than at proximity of the blade roots 7. Thus, the distance between two blade blades decreases between the blade tips 9 and the blade roots 7.

Les aubes 3 sont montées sur le disque 2 dans une position nominale de fonctionnement.The vanes 3 are mounted on the disc 2 in a nominal operating position.

Les figures 1 et 2 représentent également un anneau de retenue 17, configuré pour bloquer axialement les aubes 3 sur le disque 2.The figure 1 and 2 also represent a retaining ring 17, configured to axially block the blades 3 on the disc 2.

La figure 3 représente une portion d'une roue à aubes 1 et un système de maintien 19 pour le démontage de la roue à aubes 1. Le système de maintien 19 comprend une pluralité d'inserts 21. Les inserts 21 sont ici insérés aligné selon une direction circonférentielle dans chacun des espaces inter-aubes 15 de façon à maintenir la position relative des aubes 3 et à permettre le démontage du disque 1.The picture 3 represents a portion of a bladed wheel 1 and a holding system 19 for removing the bladed wheel 1. The holding system 19 comprises a plurality of inserts 21. The inserts 21 are here inserted aligned in a circumferential direction in each of the inter-blade spaces 15 so as to maintain the relative position of the blades 3 and to allow the dismantling of the disc 1.

Un insert selon un exemple ne faisant pas partie de l'invention revendiquée est représenté en figures 4 et 5.An insert according to an example not forming part of the claimed invention is shown in figures 4 and 5 .

L'insert 21 comprend une première partie 23 et une deuxième partie 25. La première partie 23 est configurée pour maintenir la position relative des aubes 3. La première partie 23 comprend une première surface de contact 27, configurée pour venir au contact d'une pale 5a d'une première aube 3a et épouser la forme de la face convexe de la pale 5a. Ici, la première surface de contact 27 a donc une forme concave. Autrement dit, la première surface de contact 27 et la face convexe de la pale 5a ont des formes complémentaires.The insert 21 comprises a first part 23 and a second part 25. The first part 23 is configured to maintain the relative position of the blades 3. The first part 23 comprises a first contact surface 27, configured to come into contact with a blade 5a of a first blade 3a and match the shape of the convex face of the blade 5a. Here, the first contact surface 27 therefore has a concave shape. In other words, the first contact surface 27 and the convex face of the blade 5a have complementary shapes.

La première partie 23 comprend en outre une deuxième surface de contact 29, configurée pour venir au contact d'une pale 5b d'une deuxième aube 3b et épouser la forme de la face concave de la pale 5b. Ici, la deuxième surface de contact 29 a donc une forme convexe. Autrement dit, la deuxième surface de contact 29 et la face concave de la pale 5b ont des formes complémentaires. Les première et deuxième aubes 3a, 3b sont adjacentes dans la direction circonférentielle de la roue à aubes.The first part 23 further comprises a second contact surface 29, configured to come into contact with a blade 5b of a second blade 3b and match the shape of the concave face of the blade 5b. Here, the second contact surface 29 therefore has a convex shape. In other words, the second contact surface 29 and the concave face of the blade 5b have complementary shapes. The first and second vanes 3a, 3b are adjacent in the circumferential direction of the vane wheel.

La face convexe de la pale 5a et la face concave de la pale 5b se font face dans la direction circonférentielle. Les surfaces des pales 5a, 5b des première et deuxième aubes 3a, 3b définissent l'espace inter-aubes 15.The convex face of the blade 5a and the concave face of the blade 5b face each other in the circumferential direction. The surfaces of the blades 5a, 5b of the first and second blades 3a, 3b define the inter-blade space 15.

On comprend que la première partie 23 de l'insert 21 a une forme correspondant à une portion de l'espace inter-aubes 15, lorsque les aubes 3 sont en position nominale. Ainsi, lorsque les inserts 21 sont montés dans les espaces inter-aubes 15 au niveau d'une position de maintien, les aubes de la roue à aubes sont maintenues ensemble via les inserts, ce qui libère les contraintes appliquées par les pieds d'aubes 7 au niveau des alvéoles du disque dans lequel sont montés les pieds d'aube et permet ainsi un montage ou un démontage aisé du disque.It will be understood that the first part 23 of the insert 21 has a shape corresponding to a portion of the inter-blade space 15, when the blades 3 are in the nominal position. Thus, when the inserts 21 are mounted in the inter-blade spaces 15 at a holding position, the blades of the blade wheel are held together via the inserts, which releases the stresses applied by the blade roots. 7 at the level of the cells of the disk in which the blade roots are mounted and thus allows easy assembly or disassembly of the disk.

Par exemple, au moins les portions de la première partie 23 de l'insert 21 en contact avec les pales 5a, 5b des aubes 3a, 3b, et de préférence au moins la première partie 23 de l'insert 21, comprennent/comprend un alliage à base d'aluminium, et/ou un polymère ayant une dureté shore A comprise entre 75 et 100. Par exemple, le polymère est une résine.For example, at least the portions of the first part 23 of the insert 21 in contact with the blades 5a, 5b of the blades 3a, 3b, and preferably at least the first part 23 of the insert 21, comprise/comprises a aluminum-based alloy, and/or a polymer having a Shore A hardness of between 75 and 100. For example, the polymer is a resin.

La dimension de la section de la première partie 23 de l'insert 21 selon un plan normal à la direction radiale DR est plus importante que la dimension selon ce plan de l'espace inter-aubes 15 à proximité des pieds d'aube 7. Ainsi, l'insert 21, dans la position de maintien de la position relative des aubes 3, est positionné dans l'espace inter-aubes 15 au niveau d'une portion ayant sensiblement la même dimension que la dimension de la section de l'insert 21 selon un plan normal à la direction radiale DR.The dimension of the section of the first part 23 of the insert 21 according to a plane normal to the radial direction DR is greater than the dimension according to this plane of the inter-blade space 15 near the blade roots 7. Thus, the insert 21, in the position for maintaining the relative position of the blades 3, is positioned in the inter-blade space 15 at the level of a portion having substantially the same dimension as the dimension of the section of the insert 21 along a plane normal to the radial direction DR.

Généralement, les inserts 21 sont disposés au niveau d'une première portion d'extrémité des espaces inter-aubes 15, définie, pour chaque espace inter-aubes, entre le pied d'aube 7 et le centre de l'espace inter-aubes 15 selon la direction radiale DR.Generally, the inserts 21 are arranged at the level of a first end portion of the inter-blade spaces 15, defined, for each inter-blade space, between the blade root 7 and the center of the inter-blade space. 15 in the radial direction DR.

Les inserts 21, et plus particulièrement leur première partie 23, ont une épaisseur e selon la direction radiale DR supérieure ou égale à 10% de la hauteur h de la pale selon la direction radiale DR.The inserts 21, and more particularly their first part 23, have a thickness e in the radial direction DR greater than or equal to 10% of the height h of the blade in the radial direction DR.

La position de maintien de chaque insert se trouve à une hauteur déterminée de l'espace inter-aubes 15, ou des pales adjacentes 5. Lorsque l'insert 21 est dans la position maintien, le centre de l'insert selon la direction radiale, c'est-à-dire une hauteur de l'insert correspondant à la moitié de son épaisseur e, se trouve au niveau de la hauteur déterminée. Parfois, à cause des tolérances ou dispersions dimensionnelles des aubes, la hauteur selon la direction radiale, correspondant à la position de maintien, est sensiblement différente à la hauteur déterminée pour certains inserts. Toutefois, la différence entre la hauteur réelle de la position de maintien des inserts 21 et la hauteur déterminée est inférieure ou égale à 5% de la hauteur totale de la pale 5, ou de l'espace inter-aubes 15.The holding position of each insert is at a determined height of the inter-blade space 15, or of the adjacent blades 5. When the insert 21 is in the holding position, the center of the insert in the radial direction, that is to say, a height of the insert corresponding to half of its thickness e, is at the level of the determined height. Sometimes, because of the dimensional tolerances or dispersions of the blades, the height according to the radial direction, corresponding to the holding position, is significantly different at the height determined for certain inserts. However, the difference between the actual height of the position in which the inserts 21 are held and the determined height is less than or equal to 5% of the total height of the blade 5, or of the inter-blade space 15.

Par exemple, l'épaisseur e est d'environ 10 mm, pour une hauteur de pale d'environ 100 mm. Par exemple, la plus grande longueur selon une direction axiale DA de la première partie 23 est de 15 mm, c'est-à-dire entre 70 et 100% de la longueur selon la direction axiale DA de la pale 5 de l'aube 3.For example, the thickness e is approximately 10 mm, for a blade height of approximately 100 mm. For example, the greatest length in an axial direction DA of the first part 23 is 15 mm, that is to say between 70 and 100% of the length in the axial direction DA of the blade 5 of the blade 3.

La deuxième partie 25 de l'insert 21 est reliée à la première partie de l'insert 23. Par exemple les première et deuxième parties 23, 25 sont formées ensemble.The second part 25 of the insert 21 is connected to the first part of the insert 23. For example the first and second parts 23, 25 are formed together.

La deuxième partie 25 s'étend, ici, dans le prolongement de la première partie 23 selon la direction axiale DA. La deuxième partie 25 fournit un moyen de préhension permettant d'engager ou de désengager l'insert 21 de l'espace inter-aubes 15. La deuxième partie 25 peut également servir de support pour le montage de l'insert 21 sur d'autres éléments.The second part 25 extends, here, in the extension of the first part 23 in the axial direction DA. The second part 25 provides a gripping means making it possible to engage or disengage the insert 21 from the inter-blade space 15. The second part 25 can also serve as a support for mounting the insert 21 on other elements.

Par exemple, comme représenté en figure 6, le système de maintien 19 peut comprendre en outre une portion de préhension 31 des inserts 21. La portion de préhension 31 peut être montée sur la deuxième partie 25. La portion de préhension 31 permet de former un manche, suffisamment long pour permettre à un utilisateur de l'empoigner facilement. Ainsi, la portion de préhension 31 permet de faciliter la manipulation des inserts 21 et leur insertion dans les espaces inter-aubes 15. Par exemple, la portion de préhension 31 est montée de façon amovible sur la deuxième partie 25. De cette manière, l'utilisateur peut utiliser la même portion de préhension 31 pour le montage de l'ensemble des inserts 21.For example, as shown in figure 6 , the holding system 19 may further comprise a gripping portion 31 of the inserts 21. The gripping portion 31 can be mounted on the second part 25. The gripping portion 31 makes it possible to form a handle, long enough to allow a user to grasp it easily. Thus, the gripping portion 31 facilitates the manipulation of the inserts 21 and their insertion into the inter-blade spaces 15. For example, the gripping portion 31 is removably mounted on the second part 25. In this way, the user can use the same gripping portion 31 for mounting all the inserts 21.

En outre, comme représenté sur la figure 7, le système de maintien 19 peut comprendre un dispositif de positionnement 33. Le dispositif de positionnement 33 peut comprendre un anneau de positionnement 35 configuré pour être positionné contre les aubes 3, selon une direction circonférentielle. L'anneau de positionnement 35 comprend des lumières oblongues 37 débouchant vers l'espace inter-aubes 15. Les lumières oblongues 37 s'étendent selon une direction radiale DR de façon à permettre un positionnement légèrement différent des inserts 21 les uns par rapport aux autres selon la direction radiale DR, de manière à tenir compte des tolérances/dispersions dimensionnelles.Furthermore, as shown in the figure 7 , the holding system 19 may comprise a positioning device 33. The positioning device 33 may comprise a positioning ring 35 configured to be positioned against the blades 3, in a circumferential direction. The positioning ring 35 includes oblong slots 37 opening towards the inter-blade space 15. The oblong slots 37 extend in a radial direction DR so as to allow a slightly different positioning of the inserts 21 with respect to each other in the radial direction DR, so as to take into account dimensional tolerances/dispersions.

Par exemple, la deuxième partie 25 comprend un trou borgne 38 alésé s'étendant selon la direction axiale DA. Le trou borgne 38 est destiné à venir en regard de la lumière oblongue 37, lorsque l'insert 21 est dans la position de maintien. Un organe de fixation 39 permet de fixer l'insert 21 sur l'anneau de positionnement 35. Par exemple, comme représenté, l'organe de fixation 39 est une vis, configurée pour s'insérer dans le trou borgne 38 alésé. Toutefois, l'insert 21 pourrait être fixé sur l'anneau de positionnement 35 par tout autre moyen. De cette manière, les inserts 21 sont sensiblement alignés le long de la direction circonférentielle.For example, the second part 25 comprises a bored blind hole 38 extending along the axial direction DA. The blind hole 38 is intended to come opposite the oblong slot 37, when the insert 21 is in the holding position. A fixing member 39 makes it possible to fix the insert 21 on the positioning ring 35. For example, as shown, the fixing member 39 is a screw, configured to be inserted into the blind hole 38 bored. However, the insert 21 could be fixed on the positioning ring 35 by any other means. In this way, the inserts 21 are substantially aligned along the circumferential direction.

Dans le but de positionner les inserts 21 à une même hauteur radiale dans les espaces inter-aubes selon un autre mode de réalisation (non représenté), un disque interne de butée radiale pourrait être prévu au niveau d'une hauteur prédéterminée, correspondant à la position de maintien des inserts 21. La deuxième partie 25 des inserts pourraient alors venir en butée contre le disque interne. Une fois la pluralité d'inserts montée, on positionne un disque externe de blocage radial permettant de maintenir la position des inserts 21.In order to position the inserts 21 at the same radial height in the inter-blade spaces according to another embodiment (not shown), an internal radial abutment disc could be provided at a predetermined height, corresponding to the holding position of the inserts 21. The second part 25 of the inserts could then come into abutment against the internal disk. Once the plurality of inserts has been mounted, an external radial locking disc is positioned to maintain the position of the inserts 21.

Le procédé de démontage de la roue à aubes 2 selon le premier mode de réalisation est décrit ci-après.The method for dismantling the bladed wheel 2 according to the first embodiment is described below.

Dans un premier temps, on insère les inserts 21, un par un, aligné selon une direction circonférentielle dans chacun des espaces inter-aubes 15, dans leur position de maintien.Initially, the inserts 21 are inserted, one by one, aligned in a circumferential direction in each of the inter-blade spaces 15, in their holding position.

Pour cela, on insère d'abord les inserts 21 au niveau d'une portion externe de l'espace inter-aubes 15, comme représenté en figure 9, puis on déplace les inserts 21, par exemple grâce à la portion de préhension 31, dans la direction radiale DR, selon la flèche F, c'est-à-dire vers l'intérieur, jusqu'à atteindre la position de maintien. On entend par portion externe de l'espace inter-aubes 15, une portion définie entre le centre de la pale 5 selon la direction radiale DR et l'extrémité externe de la pale 5.For this, the inserts 21 are first inserted at an outer portion of the inter-blade space 15, as shown in figure 9 , then the inserts 21 are moved, for example thanks to the gripping portion 31, in the radial direction DR, according to the arrow F, that is to say inwards, until reaching the holding position. By outer portion of the inter-blade space 15 is meant a portion defined between the center of the blade 5 in the radial direction DR and the outer end of the blade 5.

Selon une variante, on dispose directement les inserts 21 au niveau de leur position de maintien par un mouvement qui suit la forme des première et deuxième surfaces de contact 27, 29, grâce à la portion de préhension 31 qui forme, dans cette variante, un bras de levier et qui permet ainsi d'exercer une force suffisante sur l'insert 21 pour l'insérer directement dans la position de maintien.According to a variant, the inserts 21 are placed directly at their holding position by a movement which follows the shape of the first and second contact surfaces 27, 29, thanks to the gripping portion 31 which forms, in this variant, a lever arm and which thus makes it possible to exert sufficient force on the insert 21 to insert it directly into the holding position.

Selon un exemple ne faisant pas partie de l'invention revendiquée, pour positionner et maintenir les inserts 21 dans la position de maintien, on peut disposer l'anneau de positionnement 35 de façon à ce que les lumières oblongues 37 se trouvent au niveau de la position de maintien des inserts 21. Ainsi, lorsque les inserts sont montés, et font face aux lumières oblongues, on les fixe à l'anneau de positionnement 35, ici grâce aux organes de fixation 39 pouvant s'insérer dans les trous borgnes 37 des inserts 21.According to an example not forming part of the claimed invention, to position and hold the inserts 21 in the holding position, the positioning ring 35 can be arranged so that the oblong slots 37 are at the level of the holding position of the inserts 21. Thus, when the inserts are mounted, and face the oblong slots, they are fixed to the positioning ring 35, here thanks to the fixing members 39 which can be inserted into the blind holes 37 of the inserts 21.

Une fois que l'ensemble des espaces inter-aubes 15 de la roue à aubes 1 est pourvu d'un insert 21, on peut retirer le disque 2. Après avoir retiré le disque 2, on peut, par exemple, procéder au remplacement de l'anneau de retenue 17. Ensuite, on peut réengager le disque 2 avec l'ensemble des pieds d'aube 7 des aubes 3, puisque leur position relative a été maintenue par les inserts. Enfin, une fois les aubes 3 remontées sur le disque 2, on peut retirer le système de maintien 19.Once all of the inter-blade spaces 15 of the bladed wheel 1 are provided with an insert 21, the disc 2 can be removed. After removing the disc 2, it is possible, for example, to replace the the retaining ring 17. Then, the disc 2 can be reengaged with all of the blade roots 7 of the blades 3, since their relative position has been maintained by the inserts. Finally, once the blades 3 have been reassembled on the disc 2, the retaining system 19 can be removed.

Un deuxième mode de réalisation du système de maintien est représenté en figure 8. Dans ce qui suit, les éléments communs aux différents modes de réalisation sont identifiés par les mêmes références numériques. Le deuxième mode de réalisation diffère du premier mode de réalisation en ce que les inserts 21 comprennent chacun un premier organe 41 et un deuxième organe 43. Les premier et deuxième organes 41, 43 sont configurés pour être disposés, dans un espace inter-aubes 15. Le premier organe 41 est disposé contre la pale 5a de la première aube 3a et le deuxième organe 43 est disposé contre la pale 5b de la deuxième aube 3b, adjacente circonférentiellement à la première aube 3a. Les premier et deuxième organes 41, 43 se font face dans la direction circonférentielle de la roue à aubes.A second embodiment of the holding system is shown in figure 8 . In what follows, the elements common to the different embodiments are identified by the same reference numerals. The second embodiment differs from the first embodiment in that the inserts 21 each comprise a first member 41 and a second member 43. The first and second members 41, 43 are configured to be arranged, in an inter-blade space 15 The first member 41 is placed against the blade 5a of the first blade 3a and the second member 43 is placed against the blade 5b of the second blade 3b, adjacent circumferentially to the first blade 3a. The first and second members 41, 43 face each other in the circumferential direction of the paddle wheel.

Les inserts 21 comprennent en outre chacun une pièce de serrage 45, configurée pour être insérée, selon la direction axiale DA, entre les premier et deuxième organes 41, 43, de façon à maintenir les premier et deuxième organes 41, 43 contre les pales 5a, 5b. Dans l'exemple de réalisation représenté, la pièce de serrage 45 a une forme de coin ou de biseau.The inserts 21 further each comprise a clamping part 45, configured to be inserted, in the axial direction DA, between the first and second members 41, 43, so as to hold the first and second members 41, 43 against the blades 5a , 5b. In the embodiment shown, the clamping piece 45 has a wedge or bevel shape.

De façon à guider la pièce de serrage 45 entre les premier et deuxième organes 41, 43 lors de son insertion selon la direction axiale et donc éviter son déplacement radial, au moins un des premier et deuxième organes 41, 43 comprend une surface de guidage. Dans l'exemple représenté, chacun des premier et deuxième organes 41, 43 comprend une surface de guidage.In order to guide the clamping piece 45 between the first and second members 41, 43 during its insertion in the axial direction and therefore prevent its radial displacement, at least one of the first and second members 41, 43 comprises a guide surface. In the example shown, each of the first and second members 41, 43 comprises a guide surface.

Les surfaces de guidage sont ici formées par des gorges 47, 49, ménagées dans chacun des premier et deuxième organes 41, 43. Les bords des gorges 47, 49 permettent le blocage radial de la pièce de serrage 45 et un guidage en translation axiale de la pièce de serrage 45.The guide surfaces are here formed by grooves 47, 49, made in each of the first and second members 41, 43. The edges of the grooves 47, 49 allow the radial blocking of the clamping part 45 and a guiding in axial translation of clamping piece 45.

Dans un mode de réalisation, non représenté, la pièce de serrage 41 comprend une butée axiale configurée pour venir au contact des premier et deuxième organes 41, 43 lorsque la pièce de serrage 45 est montée entre les premier et deuxième organes 41, 43.In one embodiment, not shown, the clamping part 41 comprises an axial stop configured to come into contact with the first and second members 41, 43 when the clamping part 45 is mounted between the first and second members 41, 43.

Par exemple, afin de positionner les inserts 21 à une même hauteur radiale dans les espaces inter-aubes selon le mode de réalisation représenté en figure 8, un disque interne 34 de butée radiale pourrait être prévu au niveau d'une hauteur prédéterminée, correspondant à la position de maintien des inserts 21. Les premier et deuxième organes pourraient être positionnés en butée contre le disque interne 34, avant l'insertion de la pièce de serrage.For example, in order to position the inserts 21 at the same radial height in the inter-blade spaces according to the embodiment shown in figure 8 , an internal disc 34 of radial abutment could be provided at a predetermined height, corresponding to the holding position of the inserts 21. The first and second members could be positioned in abutment against the internal disc 34, before the insertion of the clamping piece.

Le procédé de démontage de la roue à aubes 1 grâce à un système de maintien selon le deuxième mode de réalisation est décrit ci-après.The method for removing the bladed wheel 1 using a holding system according to the second embodiment is described below.

Dans un premier temps, on insère les inserts 21, un par un, dans chacun des espaces inter-aubes 15, dans leur position de maintien.First, the inserts 21 are inserted, one by one, into each of the inter-blade spaces 15, in their holding position.

Pour cela, on dispose le premier organe 41 d'un insert 21 contre la pale 5a de la première aube 3a, au niveau de la position de maintien. Ensuite, on dispose le deuxième organe 43 de l'insert 21 contre la pale 5b de la deuxième aube 3b, circonférentiellement adjacente à la première aube 3a, également au niveau de la position de maintien, de sorte que le deuxième organe 43 soit disposé en face du premier organe 41 dans la direction circonférentielle de la roue à aubes. Ensuite, on insère la pièce de serrage 45 entre les premier et deuxième organes 41, 43.For this, the first member 41 of an insert 21 is placed against the blade 5a of the first blade 3a, at the level of the holding position. Then, the second member 43 of the insert 21 is placed against the blade 5b of the second blade 3b, circumferentially adjacent to the first blade 3a, also at the level of the holding position, so that the second member 43 is placed in face of first member 41 in the circumferential direction of the paddle wheel. Then, the clamping piece 45 is inserted between the first and second members 41, 43.

On insère ainsi des inserts 21 dans chacun des espaces inter-aubes 15.Inserts 21 are thus inserted into each of the inter-blade spaces 15.

Une fois que l'ensemble des espaces inter-aubes 15 de la roue à aubes 1 est pourvu d'un insert 21, de la même manière que dans le premier mode de réalisation, on peut retirer le disque 2. Après avoir retiré le disque 2, on peut, par exemple, procéder au remplacement de l'anneau de retenue 17. Ensuite, on peut réengager facilement le disque 2 avec l'ensemble des pieds d'aube 7 des aubes 3, puisque leur position relative a été maintenue par les inserts. Enfin, une fois les aubes 3 remontées sur le disque 2, on peut retirer le système de maintien 19.Once all of the inter-blade spaces 15 of the bladed wheel 1 are provided with an insert 21, in the same way as in the first embodiment, the disc 2 can be removed. After removing the disc 2, it is possible, for example, to replace the retaining ring 17. Then, the disk 2 can be easily reengaged with all of the blade roots 7 of the blades 3, since their relative position has been maintained by inserts. Finally, once the blades 3 have been reassembled on the disc 2, the retaining system 19 can be removed.

Bien que la présente invention ait été décrite en se référant à des modes de réalisation spécifiques, il est évident que des modifications et des changements peuvent être effectués sur ces exemples sans sortir de la portée générale de l'invention telle que définie par les revendications. Par conséquent, la description et les dessins doivent être considérés dans un sens illustratif plutôt que restrictif.Although the present invention has been described with reference to specific embodiments, it is obvious that modifications and changes can be made to these examples without departing from the general scope of the invention as defined by the claims. Accordingly, the description and the drawings should be considered in an illustrative rather than restrictive sense.

Il est également évident que toutes les caractéristiques décrites en référence à un procédé sont transposables, seules ou en combinaison, à un dispositif, et inversement, toutes les caractéristiques décrites en référence à un dispositif sont transposables, seules ou en combinaison, à un procédé.It is also obvious that all the characteristics described with reference to a method can be transposed, alone or in combination, to a device, and conversely, all the characteristics described with reference to a device can be transposed, alone or in combination, to a method.

Claims (10)

  1. A holding system (19) for the dismantling of a blade wheel (1), the blade wheel (1) comprising:
    - a disc (2),
    - a plurality of blades (3) configured to be mounted circumferentially around the disc (2), the plurality of blades (3) defining a plurality of inter-blade spaces (15), each of the inter-blade spaces (15) being defined circumferentially between two adjacent blades (3a, 3b) of the plurality of blades (3),
    the holding system (19) comprising a plurality of inserts (21), characterized in that each of the inserts (21) are configured to be inserted into each of the inter-blade spaces (15) in a holding position so as to hold the relative position of the blades (3) when the plurality of blades (3) is dismantled from the disc (2).
  2. The holding system (19) according to claim 1, wherein each of the inserts (21) comprises at least one portion made of an aluminum-based alloy, and/or a polymer having a Shore A hardness comprised between 75 and 100.
  3. The holding system (19) according to one of claims 1 or 2, wherein the inserts have a thickness (e) in a radial direction (DR) greater than or equal to 10% of the height (h) of an airfoil of a blade in the radial direction (DR).
  4. The holding system (19) according to one of the preceding claims, comprising a grip portion (31) configured to be mounted on an insert (21) of the plurality of inserts, the grip portion (31) being configured to allow the gripping of the insert (21) and facilitate the mounting of the insert (21) in an inter-blade space (15).
  5. The holding system (19) according to one of the preceding claims, comprising a device (33, 34) for positioning the plurality of inserts, each insert (21) of the plurality of inserts being configured to be applied to the positioning device (33, 34) so as to hold the inserts (21) in position.
  6. The holding system according to claim 5, wherein the positioning device (33) comprises a positioning ring (35), the positioning ring (35) comprising fastening elements (37) to allow the fastening of the inserts (21) on the positioning ring (35).
  7. The holding system (19) according to one of claims 1 to 3, wherein each of the inserts (21) comprises:
    - a first member (41) and a second member (43), the first and second members (41, 43) being configured to be disposed in an inter-blade space (15), the first member (41) being disposed against a first blade (3a), and the second member (43) being disposed against a second blade (3b) circumferentially adjacent to the first blade (3a); and
    - a clamping part (45), configured to be inserted between the first and second members (41, 43) so as to hold the insert (21) between the first and second blades (3a, 3b).
  8. A method for dismantling a blade wheel (1) comprising a disc (2) and a plurality of blades (3) mounted circumferentially around the disc (2), the plurality of blades (3) defining a plurality of inter-blade spaces (15), each of the inter-blade spaces (15) being defined circumferentially between two adjacent blades of the plurality of blades (3), characterized in that the dismantling method comprises the following steps:
    A. inserting a plurality of inserts (21) of a holding system (19) into the inter-blade spaces (15) in a holding position so that the relative position of the blades (3) is held;
    B. withdrawing the disc (2).
  9. The method according to claim 8, wherein, during step A:
    - the inserts are inserted at a radially outer portion of the inter-blade spaces (15);
    - the inserts (21) are moved in a radial direction (DR), radially inward, until they reach the holding position.
  10. The method according to claim 8, wherein each of the inserts (21) comprises a first member (41), a second member (43) and a clamping part (45), during step A:
    - the first member (41) of an insert (21) is disposed, in an inter-blade space (15), against a first blade (3a) at the holding position;
    - the second member (43) of the insert (21) is disposed, in the inter-blade space (15), against a second blade (3b), adjacent to the first blade (3a), so that the second member (43) is disposed circumferentially facing the first member (41);
    - the clamping part (45) is inserted between the first and second members (41, 43) so as to hold the insert (21) in the holding position.
EP19735372.5A 2018-06-12 2019-06-06 Holding system for the dismantling of a blade wheel Active EP3807500B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1855124A FR3082232B1 (en) 2018-06-12 2018-06-12 HOLDING SYSTEM FOR DISMANTLING A BLADE WHEEL
PCT/FR2019/051351 WO2019239036A1 (en) 2018-06-12 2019-06-06 Holding system for the dismantling of a blade wheel

Publications (2)

Publication Number Publication Date
EP3807500A1 EP3807500A1 (en) 2021-04-21
EP3807500B1 true EP3807500B1 (en) 2022-07-27

Family

ID=63036184

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19735372.5A Active EP3807500B1 (en) 2018-06-12 2019-06-06 Holding system for the dismantling of a blade wheel

Country Status (8)

Country Link
US (1) US11441431B2 (en)
EP (1) EP3807500B1 (en)
JP (1) JP7485618B2 (en)
CN (1) CN112313396B (en)
CA (1) CA3102895A1 (en)
FR (1) FR3082232B1 (en)
RU (1) RU2765596C1 (en)
WO (1) WO2019239036A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113942657B (en) * 2021-10-09 2023-09-08 中国直升机设计研究所 Repair method for rear edge and tip rear edge of composite blade

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DE3634268A1 (en) * 1986-10-08 1988-04-21 Hauni Werke Koerber & Co Kg WORKPIECE CLAMPING DEVICE
JPS6445903A (en) * 1987-08-17 1989-02-20 Sumitomo Heavy Industries Jig for inserting turbine blade
US5026032A (en) * 1990-02-22 1991-06-25 Southern California Edison Blade assembly tool
JP2000008806A (en) * 1998-06-25 2000-01-11 Honda Motor Co Ltd Blade demounting device for turbine rotor
US6736706B1 (en) * 2002-12-03 2004-05-18 General Electric Company Device for defining a designated flow path through a dovetail slot in a gas turbine engine disk
US7080434B2 (en) * 2003-06-06 2006-07-25 General Electric Company Fixture having integrated datum locators
FR2857708B1 (en) * 2003-07-15 2005-09-23 Snecma Moteurs IMPROVED DEVICE FOR FASTENING A MOTOR SHAFT ON A BEARING BRACKET
FR2913735B1 (en) * 2007-03-16 2013-04-19 Snecma ROTOR DISC OF A TURBOMACHINE
FR2918106B1 (en) * 2007-06-27 2011-05-06 Snecma AXIS RETAINING DEVICE OF AUBES MOUNTED ON A TURBOMACHINE ROTOR DISC.
CN103370499B (en) * 2011-02-09 2015-11-25 西门子公司 For the axle extending portion of method that supporting mass is dismantled from the rotor of gas turbine and tubulose
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FR2990238B1 (en) * 2012-05-02 2015-10-30 Snecma METHOD FOR REAR CUTTING OF A CONNECTION NUT IN A DOUBLE-BODY TURBOJURY, TOOLING DEVICE
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US11092039B2 (en) * 2016-10-27 2021-08-17 General Electric Company Apparatus for circumferential separation of turbine blades

Also Published As

Publication number Publication date
BR112020025238A2 (en) 2021-03-09
WO2019239036A1 (en) 2019-12-19
FR3082232B1 (en) 2020-08-28
JP7485618B2 (en) 2024-05-16
RU2765596C1 (en) 2022-02-01
CA3102895A1 (en) 2019-12-19
CN112313396A (en) 2021-02-02
EP3807500A1 (en) 2021-04-21
FR3082232A1 (en) 2019-12-13
CN112313396B (en) 2023-10-27
US20210254481A1 (en) 2021-08-19
JP2021527180A (en) 2021-10-11
US11441431B2 (en) 2022-09-13

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