EP1114916B1 - Device for the axial retention of blades in a rim - Google Patents
Device for the axial retention of blades in a rim Download PDFInfo
- Publication number
- EP1114916B1 EP1114916B1 EP01400007A EP01400007A EP1114916B1 EP 1114916 B1 EP1114916 B1 EP 1114916B1 EP 01400007 A EP01400007 A EP 01400007A EP 01400007 A EP01400007 A EP 01400007A EP 1114916 B1 EP1114916 B1 EP 1114916B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade
- disc
- wedging
- retaining
- arrangement according
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
Definitions
- the subject of this invention is a axial blade retainer arrangement in a turbomachine disk, which we can especially use in blowers to the entrance of these.
- US-A-3556 675 shows an example of padlocking of blade roots in a disc by means of chocks and rings fixed on the disc.
- the wedging pieces form a set relatively flexible which is exploited here possibilities of deformation by allowing the dawn of move in the groove up to a limit determined.
- a relatively large energy is absorbed without excessive force being exerted on the dawn struck.
- the deformation is reversible, that is to say that the parts of the rigging set come back to their original state after the shock, dawn is pushed back to its original position, other shocks may still be absorbed, and in particular others shocks after the initial shock can be absorbed in the same event.
- This assembly elastic in the axial direction, sliding blade in an axial groove or slightly oblique differs from known arrangements, where dawn is is rigidly connected to the disk and deprived of any possibility of axial displacement, or restraint axially by a part likely to break or flambé in case of excessive axial force. Dawn undergoing shock will be likely to break easily in the first case, and the piece broken or having flamed will not be able to support other charges elevated during the same event in the second case.
- Another aspect of the invention is that however, limits the deformation that the pieces of stalling are likely to suffer, so they do not keep of permanent deformations: a stop is added for that, between dawn and the disc. When the dawn shifting was enough to reach the stop position, the mechanical system becomes much more rigid, that is to say that much larger stress increases are necessary to produce displacements additional. The energy of the axial impact as well as the efforts are then shared between the two levels of the restraining arrangement of the stop system, and avoiding breaking one or the other of the systems.
- the restraint of the first level is of a flexibility as it lets dawn slide in the alveolus of the disc without great axial effort before the second level does not intervene after a game imposed and, at that moment, retain dawn by including stiffness and ability of the arrangement.
- the utility of the invention is not limited the absorption of shock forces consecutive to a next dawn break, but to all the causes axial forces on the blades, such as the impacts solid bodies, birds or others.
- a general definition thereof is a dual-flexible retaining arrangement of a blade in a disk according to axial displacements of the blade, comprising a first level of deformation at significant flexibility and a second level of distortion marked by a disappearance of games enters at minus a chain of elements of the arrangement and by a decreased flexibility coupled with increasing burden elements of the chain, without breaking or buckling none of the elements of the chain.
- the arrangement of holding a dawn in a disk where dawn can slide substantially axially in the disk includes wedges of the blade, and is characterized in that the wedging pieces are joined by pairs of thrust surfaces directed axially and ending either on a portion of the record or on a parts, which is connected to the disc, the pieces of wedging or the portion of the disc being at least partially flexible, and in that a determined game exists in the axial direction between either a portion of the disk be a portion of an attachment to the disk, and either a portion of the dawn, or a portion of a attachment at dawn, said game being consumed when a determined axial force was exerted on the dawn.
- the arrangement can be on one side dawn, or both sides, the game being then advantageously on one side and the wedging parts of the other side.
- Figure 1 shows some parts essential features of a turbomachine blower, one of which cone 1, a disc 2 covered by cone 1 and vanes 3 whose blades 4 come out of cone 1 and which include still feet 5 housed in grooves of the disk 2.
- the dawn feet have a section bulbous, dovetailed, or swollen analogous in a groove of complementary shape, to interlock with it and to prohibit centrifugal movements of extraction of the blades 3 when the cone 1 rotates with the rotor of the turbomachine.
- Figure 2 represents the front of the arrangement.
- the dawn foot 5 is placed on a hold 7 which keeps it in place against the top of the groove by overflowing towards the front, where the hold 7 comes up against a ring of circumferential retention 8 which itself stumbles towards the front against a flange 9 of the disc 2.
- the ring of circumferential retention has notches 25 of limited angular extension which receive the wedge ends 7 and prevent them from moving axially in the grooves 26, as is known.
- a flange 10 covers the ring 8, the flange 9 and the shim 7 and is in the form of an envelope 11 pretty thin bolted to an outer portion 12 of the disc 2 via screws 13.
- An important aspect of the invention lies in the pairs of abutment surfaces 27, 28 and 29 in look, surfaces respectively arranged on the foot 5 and the hold 7, on the hold 7 and the ring 8, and on the ring 8 and the flange 9; these surfaces are directed in the axial direction.
- Disk 2 is bolted to a drum 14 which includes a flange 15 ending in a hood which covers the dawn foot 5 and the hold 7.
- the drum 14 is provided with a flange 18 provided with notches 17 each of which comes to cap a tenon 19 of a rear portion 20 of the blade root 5, and a heel 21 of this rear portion 20 extends behind the flange 18, from which he is separated by a determined game in normal circumstances, where dawn does not undergo any effort axial axis. When this eventuality appears and as dawn moves forward, the game 22 gradually diminishes but remains parts 7, 8 and 9 begin to undergo deformation.
- This conception of montage from dawn to two successive levels of rigidity can be set implemented by technical arrangements presenting a different appearance, as shown in Figure 4.
- the foot dawn 5 is still lying on a wedge 7 climb into the same groove of the disc 2, and its position on the circumference can be provided by a similar piece to ring 8 but that is not represented here and does not participates more in the assembly of the invention.
- a flask 30 covers at the front the hold 7 and the dawn foot 5; it is united to the disc 2 by bolts 31 and extends radially outward before curved hook-shaped 32 of angular extension limited which is located opposite the foot of blade 5; he includes, not far from the bolts 31, a thinned portion 33 which gives it extra flexibility.
- the disc 2 comprises a flange 34 extending towards outside, with angular extension notches limited and finishing behind the hook 32 also notched between him and the flask itself.
- the notches of the hook 32 and the flange 34 are extended by so that the solid parts of these two pieces are facing and separated in normal time from a game 35.
Description
Le sujet de cette invention est un agencement de retenue d'aubes en direction axiale dans un disque de turbomachine, qu'on pourra particulièrement employer dans les soufflantes à l'entrée de celles-ci.The subject of this invention is a axial blade retainer arrangement in a turbomachine disk, which we can especially use in blowers to the entrance of these.
On se préoccupe ici des situations d'avarie qui peuvent survenir quand une aube se rompt par un choc provoqué par l'entrée d'un corps étranger dans la machine ou lors d'une défaillance. L'aube se détachant heurte sa voisine et exerce des efforts axiaux et radiaux importants sur elle, qui peuvent la rompre à son tour. Le dispositif proposé ici permet d'absorber la composante axiale d'une force de choc s'exerçant sur l'aube. Il s'agit d'un agencement particulier faisant intervenir les pièces de calage de l'aube, situées entre le disque et un pied de l'aube coulissant dans une rainure et qui arrêtent son mouvement axial dans la rainure.We are concerned here about the damage situations that can occur when a dawn breaks by a shock caused by the entry of a foreign body into the machine or during a failure. Dawn standing out hitting her neighbor and exerting axial and important radials on it, which can break it at his turn. The device proposed here makes it possible to absorb the axial component of a shock force acting on dawn. This is a special arrangement intervene the wedges of the dawn, located between the disc and a dawn foot sliding in a groove and stop its axial movement in the groove.
US-A- 3556 675 montre un exemple de blocage de pieds d'aubes dans un disque au moyen de pièces de calage et d'anneaux fixés sur le disque.US-A-3556 675 shows an example of padlocking of blade roots in a disc by means of chocks and rings fixed on the disc.
Selon l'invention, les pièces de calage forment un ensemble relativement flexible dont on exploite ici les possibilités de déformation en permettant à l'aube de se déplacer dans la rainure jusqu'à une limite déterminée. Une énergie relativement importante est absorbée sans qu'une force excessive s'exerce sur l'aube heurtée. La déformation est réversible, c'est-à-dire que les pièces de l'ensemble de calage reviennent à leur état original après le choc, l'aube est repoussée à sa position initiale, d'autres chocs pourront encore être absorbés, et notamment d'autres chocs ultérieurs au choc initial peuvent être absorbés dans le même événement.According to the invention, the wedging pieces form a set relatively flexible which is exploited here possibilities of deformation by allowing the dawn of move in the groove up to a limit determined. A relatively large energy is absorbed without excessive force being exerted on the dawn struck. The deformation is reversible, that is to say that the parts of the rigging set come back to their original state after the shock, dawn is pushed back to its original position, other shocks may still be absorbed, and in particular others shocks after the initial shock can be absorbed in the same event.
Ce montage, élastique en direction axiale, d'aube coulissant dans une rainure axiale ou légèrement oblique diffère des agencements connus, où l'aube est soit reliée de façon rigide au disque et privée de toute possibilité de débattement axial, ou retenue axialement par une pièce susceptible de se rompre ou de flamber en cas de force axiale excessive. L'aube subissant le choc sera susceptible de se rompre facilement dans le premier cas, et la pièce rompue ou ayant flambé ne pourra pas supporter d'autres charges élevées au cours du même événement dans le second cas.This assembly, elastic in the axial direction, sliding blade in an axial groove or slightly oblique differs from known arrangements, where dawn is is rigidly connected to the disk and deprived of any possibility of axial displacement, or restraint axially by a part likely to break or flambé in case of excessive axial force. Dawn undergoing shock will be likely to break easily in the first case, and the piece broken or having flamed will not be able to support other charges elevated during the same event in the second case.
Un autre aspect de l'invention est qu'on limite toutefois la déformation que les pièces de calage risquent de subir, afin qu'elles ne gardent pas de déformations permanentes : une butée est ajoutée pour cela entre l'aube et le disque. Quand le déplacement de l'aube a été suffisant pour atteindre la position de butée, le système mécanique devient beaucoup plus rigide, c'est-à-dire que des accroissements d'effort beaucoup plus importants sont nécessaires pour produire des déplacements supplémentaires. L'énergie du choc axial ainsi que les efforts sont alors partagés entre les deux niveaux de l'agencement de retenue du système d'arrêt, et on évite la rupture de l'un ou l'autre des systèmes.Another aspect of the invention is that however, limits the deformation that the pieces of stalling are likely to suffer, so they do not keep of permanent deformations: a stop is added for that, between dawn and the disc. When the dawn shifting was enough to reach the stop position, the mechanical system becomes much more rigid, that is to say that much larger stress increases are necessary to produce displacements additional. The energy of the axial impact as well as the efforts are then shared between the two levels of the restraining arrangement of the stop system, and avoiding breaking one or the other of the systems.
La retenue du premier niveau est d'une souplesse telle qu'elle laisse l'aube coulisser dans l'alvéole du disque sans grand effort axial avant que le deuxième niveau n'intervienne au bout d'un jeu imposé et, à ce moment, retienne l'aube en incluant les raideurs et capacités de l'agencement.The restraint of the first level is of a flexibility as it lets dawn slide in the alveolus of the disc without great axial effort before the second level does not intervene after a game imposed and, at that moment, retain dawn by including stiffness and ability of the arrangement.
L'utilité de l'invention n'est pas limitée à l'absorption des forces de chocs consécutives à une rupture d'aube voisine, mais à toutes les causes d'efforts axiaux sur les aubes, telles que les impacts de corps solides, oiseaux ou autres.The utility of the invention is not limited the absorption of shock forces consecutive to a next dawn break, but to all the causes axial forces on the blades, such as the impacts solid bodies, birds or others.
On verra que de nombreuses variantes de réalisation, extérieurement différentes les unes des autres, sont possibles pour l'invention, mais une définition générale de celle-ci est un agencement de retenue à double souplesse d'une aube dans un disque selon des déplacements axiaux de l'aube, comprenant un premier niveau de déformation à souplesse importante et un deuxième niveau de déformation marqué par une disparition de jeux entre au moins une chaíne d'éléments de l'agencement et par une diminution de souplesse jointe à une charge croissante des éléments de la chaíne, sans rupture ni flambage d'aucun des éléments de la chaíne. Avantageusement, l'agencement de retenue d'une aube dans un disque où l'aube peut coulisser substantiellement axialement dans le disque, comprend des pièces de calage de l'aube, et est caractérisé en ce que les pièces de calage sont jointes par des paires de surfaces de butée dirigées axialement et finissant soit sur une portion du disque, soit sur une des pièces de calage, qui est unie au disque, les pièces de calage ou la portion du disque étant au moins partiellement flexibles, et en ce qu'un jeu déterminé existe en direction axiale entre soit une portion du disque soit une portion d'une pièce jointe au disque, et soit une portion de l'aube, soit une portion d'une pièce jointe à l'aube, ledit jeu étant consommé quand un effort axial déterminé a été exercé sur l'aube. We will see that many variants of realization, externally different from each other others, are possible for the invention, but a general definition thereof is a dual-flexible retaining arrangement of a blade in a disk according to axial displacements of the blade, comprising a first level of deformation at significant flexibility and a second level of distortion marked by a disappearance of games enters at minus a chain of elements of the arrangement and by a decreased flexibility coupled with increasing burden elements of the chain, without breaking or buckling none of the elements of the chain. Advantageously, the arrangement of holding a dawn in a disk where dawn can slide substantially axially in the disk, includes wedges of the blade, and is characterized in that the wedging pieces are joined by pairs of thrust surfaces directed axially and ending either on a portion of the record or on a parts, which is connected to the disc, the pieces of wedging or the portion of the disc being at least partially flexible, and in that a determined game exists in the axial direction between either a portion of the disk be a portion of an attachment to the disk, and either a portion of the dawn, or a portion of a attachment at dawn, said game being consumed when a determined axial force was exerted on the dawn.
L'agencement peut se trouver d'un seul côté de l'aube, ou des deux côtés, le jeu étant alors avantageusement d'un côté et les pièces de calage de l'autre côté.The arrangement can be on one side dawn, or both sides, the game being then advantageously on one side and the wedging parts of the other side.
Tout cela, ainsi que des aspects plus particuliers, apparaítra mieux à la description qui suit, en liaison aux dessins annexés et dont la liste est donnée ci-dessous :
- La figure 1 est une vue générale d'une soufflante et montre un assemblage de fixation des aubes ;
- Les figures 2 et 3 représentent pour un mode de réalisation de l'invention les deux extrémités de l'agencement de retenue des aubes ;
- La figure 3A est une vue axiale d'un élément essentiel de la figure 3 ;
- Et la figure 4 illustre un autre mode de réalisation de l'invention.
- Figure 1 is a general view of a blower and shows a blade attachment assembly;
- Figures 2 and 3 show for an embodiment of the invention the two ends of the blade retainer arrangement;
- Figure 3A is an axial view of an essential element of Figure 3;
- And Figure 4 illustrates another embodiment of the invention.
La figure 1 représente certaines parties
essentielles d'une soufflante de turbomachine, dont un
cône 1, un disque 2 couvert par le cône 1 et des aubes
3 dont les pales 4 sortent du cône 1 et qui comprennent
encore des pieds 5 logés dans des rainures du disque 2.
Ainsi qu'il est connu, les pieds d'aube ont une section
en bulbe, en queue d'aronde ou renflée de façon
analogue dans une rainure de forme complémentaire, de
façon à s'imbriquer en elle et à interdire les
mouvements centrifuges d'extraction des aubes 3 quand
le cône 1 tourne avec le rotor de la turbomachine.Figure 1 shows some parts
essential features of a turbomachine blower, one of which
cone 1, a
On se reporte maintenant plus précisément à
la figure 2 qui représente l'avant de l'agencement. Le
pied d'aube 5 est posé sur une cale 7 qui le maintient
en place contre le haut de la rainure en débordant vers
l'avant, où la cale 7 bute contre un anneau de
rétention circonférencielle 8 qui lui-même bute vers
l'avant contre une bride 9 du disque 2. L'anneau de
rétention circonférentielle présente des crans 25
d'extension angulaire limitée qui reçoivent les
extrémités des cales 7 et les empêchent de se déplacer
axialement dans les rainures 26, ainsi qu'il est connu.
De plus, un flasque 10 couvre l'anneau 8, la bride 9 et
la cale 7 et se présente sous forme d'une enveloppe 11
assez mince boulonnée à une portion externe 12 du
disque 2 par l'intermédiaire de vis 13.We are now referring more specifically to
Figure 2 which represents the front of the arrangement. The
Un aspect important de l'invention réside
dans les couples de surfaces de butée 27, 28 et 29 en
regard, surfaces disposées respectivement sur le pied 5
et la cale 7, sur la cale 7 et l'anneau 8, et sur
l'anneau 8 et la bride 9 ; ces surfaces sont dirigées
en direction axiale.An important aspect of the invention lies
in the pairs of
Quand le pied d'aube 5 est déplacé vers
l'avant, il repousse la cale 7, puis l'anneau 8,
jusqu'à ce que la bride 9 soit touchée, par un contact
successif des surfaces des paires 27, 28 et 29. Mais
cet empilement en direction axiale est assez souple à
cause du nombre des pièces impliquées et de leurs
possibilités de se déformer, surtout par la flexion et
la torsion de l'anneau 8 dues à sa minceur et à un
décalage radial des paires de surfaces de butée 28 et
29 entre lesquelles il est situé : un déplacement
supplémentaire d'une valeur déterminée du pied d'aube 5
nécessitera donc d'exercer une certaine force, mais
relativement faible dans un premier stade de la
déformation. Un col 6 du disque 2, menant à la bride 9,
fléchit aussi sous la charge et offre une souplesse
supplémentaire.When the
On passe maintenant à la figure 3, où est
représenté l'autre côté du disque 2 et de l'aube 1.We now go to Figure 3, where is
represented the other side of the
Le disque 2 y est boulonné à un tambour 14
qui comprend une bride 15 finissant en un capot qui
couvre le pied d'aube 5 et la cale 7. De plus, le
tambour 14 est muni d'une bride 18 munie d'encoches 17
dont chacune d'elles vient coiffer un tenon 19 d'une
portion arrière 20 du pied d'aube 5, et un talon 21 de
cette portion arrière 20 s'étend derrière la bride 18,
dont il est séparé par un jeu 22 déterminé dans des
circonstances normales, où l'aube ne subit pas d'effort
axial important. Quand cette éventualité apparaít et
que l'aube se déplace vers l'avant, le jeu 22
s'amenuise progressivement mais subsiste alors que les
pièces 7, 8 et 9 commencent à subir une déformation.
Quand celle-ci atteint une certaine valeur, le jeu 22
est consommé et un contact direct s'instaure entre le
talon 21 et la nervure 18 ; comme ces deux pièces sont
beaucoup plus rigides que celles de l'avant de
l'assemblage, des forces beaucoup plus importantes sont
nécessaires pour déplacer encore l'aube vers l'avant,
ce qui fait qu'on obtient un montage de l'aube
faiblement rigide pour de petits déplacements mais
fortement rigide pour des déplacements plus importants.
Cette propriété permet d'absorber des énergies de choc
assez importantes reçues par l'aube lors de cas de
charges exceptionnelles comme l'ingestion d'oiseaux ou
surtout la perte d'aube, sans risquer d'endommager les
différentes pièces de l'agencement de retenue.
Cette conception du montage de l'aube à
deux niveaux successifs de rigidité peut être mise en
oeuvre par des agencements techniques présentant un
aspect différent, comme le montre la figure 4. Le pied
d'aube 5 est encore posé sur une cale 7 montée dans la
même rainure du disque 2, et sa position sur la
circonférence peut être assurée par une pièce analogue
à l'anneau 8, mais qui n'est pas représentée ici et ne
participe plus au montage de l'invention. Ici un
flasque 30 couvre à l'avant la cale 7 et le pied d'aube
5 ; il est uni au disque 2 par des boulons 31 et
s'étend radialement vers l'extérieur avant de se
recourber en forme de crochet 32 d'extension angulaire
limitée qui se situe en regard du pied d'aube 5 ; il
comprend, non loin des boulons 31, une portion amincie
33 qui lui confère un surcroít de souplesse. De plus,
le disque 2 comprend une bride 34 s'étendant vers
l'extérieur, munie de crans d'extension angulaire
limitée et finissant derrière le crochet 32 également
cranté, entre lui et le flasque 30 proprement dit. Les
crans du crochet 32 et de la bride 34 se prolongent de
sorte que les parties pleines de ces deux pièces sont
en regard et séparées en temps normal d'un jeu 35. This conception of montage from dawn to
two successive levels of rigidity can be set
implemented by technical arrangements presenting a
different appearance, as shown in Figure 4. The
Dans cette conception, tous les éléments du
montage à deux niveaux de rigidité se trouvent donc à
l'avant des aubes, le jeu 35 ayant le rôle du jeu 22
précédent. Quand une aube subit une force vers l'avant,
le pied d'aube 5 repousse la cale 7 en faisant fléchir
le flasque 30 par la partie amincie 33, jusqu'à ce que
le jeu 35 ait disparu et que le crochet 32 bute contre
la bride 34 beaucoup plus rigide que le flasque 30, ce
qui accroít fortement la résistance du montage aux
déplacements supplémentaires de l'aube. La déformation
des pièces de calage s'accomplit par la butée entre
deux paires de surfaces 27 et 36, situées
respectivement sur le pied 5 et la cale 7 (comme
précédemment), et entre la cale 7 et le flasque 30.In this design, all elements of the
mounting at two levels of rigidity are therefore at
the front of the blades, the
Claims (10)
- Double-flexibility arrangement for retaining a blade in a disc (2) where the blade can slide substantially axially in the disc, comprising blade-wedging parts (7, 8), characterized in that the wedging parts are joined by pairs of abutment surfaces (27, 28, 29) directed axially and ending on a portion (9) of the disc, the wedging parts (7, 8) and the portion (9) of the disc being at least partially flexible and constituting a first level of deformation with significant flexibility, and in that there is a determined clearance (22) in the axial direction between a portion (18) of a piece (14, 15) joined to the disc (2) and a portion (21) of the blade, the said clearance being used up when a determined axial force has been exerted on the blade, the using-up of the said clearance constituting a second level of deformation.
- Retaining arrangement according to Claim 1, characterized in that the wedging pieces (7, 8) and the clearance (22) are situated on two opposite sides of the blade.
- Arrangement for retaining a blade in a disc (2) according to Claim 1, where the blade can slide substantially axially in the disc, comprising blade wedging pieces (7, 30), characterized in that the wedging pieces are joined by pairs of abutment surfaces (36) directed axially and finishing in one of the wedging pieces (30) which is connected to the disc (2), the wedging pieces being at least partially flexible, and in that there is a determined clearance (35) in the axial direction between a portion of the disc (34) and a portion (32) of a wedging piece (30), the said clearance being used up when a determined axial force has been exerted on the blade.
- Retaining arrangement according to Claim 3, characterized in that it lies entirely on one side of the blade.
- Retaining arrangement according to any one of Claims 1 to 4, characterized in that the wedging pieces comprise a wedge (7) slipped under a root (5) of the blade.
- Retaining arrangement according to Claim 5, characterized in that the wedging pieces comprise a retaining ring (8) for circumferentially retaining the wedge (7).
- Retaining arrangement according to Claim 6, characterized in that the ring (8) is arranged between two of the said pairs (28, 29) of abutment surfaces offset radially so as to be able to flex.
- Retaining arrangement according to Claim 3, characterized in that the wedging pieces comprise an endplate (30) which is connected to the disc (2).
- Retaining arrangement according to Claim 8, characterized in that the endplate (30) is provided with a thinner and flexible part (33).
- Retaining arrangement according to Claim 9, characterized in that the endplate (30) has an end bent into a hook shape (32) which acts as a rigid abutment when the clearance (35) is used up.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0000110A FR2803623B1 (en) | 2000-01-06 | 2000-01-06 | ARRANGEMENT FOR AXIAL RETENTION OF BLADES IN A DISC |
FR0000110 | 2000-01-06 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1114916A1 EP1114916A1 (en) | 2001-07-11 |
EP1114916B1 true EP1114916B1 (en) | 2005-08-24 |
EP1114916B8 EP1114916B8 (en) | 2005-10-26 |
Family
ID=8845652
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01400007A Expired - Lifetime EP1114916B8 (en) | 2000-01-06 | 2001-01-04 | Device for the axial retention of blades in a rim |
Country Status (5)
Country | Link |
---|---|
US (1) | US6595755B2 (en) |
EP (1) | EP1114916B8 (en) |
JP (1) | JP4153666B2 (en) |
DE (1) | DE60112820T2 (en) |
FR (1) | FR2803623B1 (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6951448B2 (en) * | 2002-04-16 | 2005-10-04 | United Technologies Corporation | Axial retention system and components thereof for a bladed rotor |
JP3836050B2 (en) * | 2002-06-07 | 2006-10-18 | 三菱重工業株式会社 | Turbine blade |
FR2844562B1 (en) * | 2002-09-18 | 2004-10-29 | Snecma Moteurs | CONTROL OF THE AXIAL POSITION OF A BLOWER ROTOR BLADE |
FR2881174B1 (en) * | 2005-01-27 | 2010-08-20 | Snecma Moteurs | DEVICE FOR POSITIONING A DASHBOARD AND AUBAGE DISK COMPRISING SUCH A DEVICE |
FR2888897B1 (en) | 2005-07-21 | 2007-10-19 | Snecma | DEVICE FOR DAMPING THE VIBRATION OF AN AXIAL RETAINING RING OF BLOWER BLADES OF A TURBOMACHINE |
JP2007247406A (en) * | 2006-03-13 | 2007-09-27 | Ihi Corp | Holding structure of fan blade |
US20090053064A1 (en) * | 2006-09-01 | 2009-02-26 | Ress Jr Robert A | Fan blade retention system |
FR2911632B1 (en) * | 2007-01-18 | 2009-08-21 | Snecma Sa | ROTOR DISC OF TURBOMACHINE BLOWER |
FR2931871B1 (en) * | 2008-05-29 | 2011-08-19 | Snecma | BLOWER ROTOR FOR A TURBOMACHINE. |
US8087874B2 (en) * | 2009-02-27 | 2012-01-03 | Honeywell International Inc. | Retention structures and exit guide vane assemblies |
FR2961847B1 (en) * | 2010-06-25 | 2012-08-17 | Snecma | AUBES MOBILE WHEEL IN COMPOSITE MATERIAL FOR A TURBINE GAS TURBINE ENGINE WITH A WAVEBASE / TIGHTENING DISC |
FR2968363B1 (en) * | 2010-12-03 | 2014-12-05 | Snecma | TURBOMACHINE ROTOR WITH ANTI-WEAR BOND BETWEEN A DISC AND A RING |
FR2971822B1 (en) * | 2011-02-21 | 2015-04-24 | Snecma | BLOWER ROTOR, ESPECIALLY FOR A TURBOMACHINE |
FR2974864B1 (en) * | 2011-05-04 | 2016-05-27 | Snecma | ROTOR OF TURBOMACHINE WITH MEANS OF AXIAL RETENTION OF AUBES |
FR2974863B1 (en) * | 2011-05-06 | 2015-10-23 | Snecma | TURBOMACHINE BLOWER DISK |
US9376926B2 (en) * | 2012-11-15 | 2016-06-28 | United Technologies Corporation | Gas turbine engine fan blade lock assembly |
EP2933436A1 (en) * | 2014-04-15 | 2015-10-21 | Siemens Aktiengesellschaft | Wheel disc with at least one sealing sheet metal panel |
FR3075284B1 (en) * | 2017-12-18 | 2020-09-04 | Safran Aircraft Engines | SHOCK ABSORBER |
WO2021012341A1 (en) * | 2019-07-23 | 2021-01-28 | 广东美的制冷设备有限公司 | Axial flow fan, air conditioning outdoor unit and air conditioner |
FR3121171B1 (en) * | 2021-03-25 | 2023-04-14 | Safran Aircraft Engines | Fan rotor for a turbomachine |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3556675A (en) * | 1969-01-29 | 1971-01-19 | Gen Electric | Turbomachinery rotor with integral shroud |
US3656865A (en) * | 1970-07-21 | 1972-04-18 | Gen Motors Corp | Rotor blade retainer |
FR2419389A1 (en) * | 1978-03-08 | 1979-10-05 | Snecma | IMPROVEMENTS TO TURBOMACHINE ROTOR FLANGES |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4304523A (en) * | 1980-06-23 | 1981-12-08 | General Electric Company | Means and method for securing a member to a structure |
US4453890A (en) * | 1981-06-18 | 1984-06-12 | General Electric Company | Blading system for a gas turbine engine |
FR2535794A1 (en) * | 1982-11-08 | 1984-05-11 | Snecma | AXIAL AND RADIAL BLADE SUPPORT DEVICE |
FR2585069B1 (en) * | 1985-07-16 | 1989-06-09 | Snecma | DEVICE FOR LIMITING THE ANGULAR DEFLECTION OF BLADES MOUNTED ON A TURBOMACHINE ROTOR DISC |
US5151013A (en) * | 1990-12-27 | 1992-09-29 | United Technologies Corporation | Blade lock for a rotor disk and rotor blade assembly |
US5259728A (en) * | 1992-05-08 | 1993-11-09 | General Electric Company | Bladed disk assembly |
US5302086A (en) * | 1992-08-18 | 1994-04-12 | General Electric Company | Apparatus for retaining rotor blades |
FR2695433B1 (en) * | 1992-09-09 | 1994-10-21 | Snecma | Annular seal placed at an axial end of a rotor and covering blade pinouts. |
FR2715975B1 (en) * | 1994-02-10 | 1996-03-29 | Snecma | Turbomachine rotor with axial or inclined through blade grooves. |
GB9412963D0 (en) * | 1994-06-28 | 1994-09-28 | Rolls Royce Plc | Gas turbine engine fan blade assembly |
FR2728299B1 (en) * | 1994-12-14 | 1997-01-24 | Snecma | DEVICE FOR AXIAL FIXING OF TURBO-SPINDLE ROTOR BLADES |
FR2746456B1 (en) * | 1996-03-21 | 1998-04-30 | Snecma | DEVICE FOR RETAINING THE FOOT OF THE BLADES OF A BLOWER |
-
2000
- 2000-01-06 FR FR0000110A patent/FR2803623B1/en not_active Expired - Fee Related
-
2001
- 2001-01-02 US US09/750,758 patent/US6595755B2/en not_active Expired - Lifetime
- 2001-01-04 EP EP01400007A patent/EP1114916B8/en not_active Expired - Lifetime
- 2001-01-04 DE DE60112820T patent/DE60112820T2/en not_active Expired - Lifetime
- 2001-01-05 JP JP2001000861A patent/JP4153666B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US20010007633A1 (en) | 2001-07-12 |
DE60112820T2 (en) | 2006-06-01 |
DE60112820D1 (en) | 2005-09-29 |
JP2001234890A (en) | 2001-08-31 |
US6595755B2 (en) | 2003-07-22 |
EP1114916A1 (en) | 2001-07-11 |
EP1114916B8 (en) | 2005-10-26 |
FR2803623B1 (en) | 2002-03-01 |
FR2803623A1 (en) | 2001-07-13 |
JP4153666B2 (en) | 2008-09-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1114916B1 (en) | Device for the axial retention of blades in a rim | |
CA2607245C (en) | Bearing arrangement of a rotating shaft and turbojet equipped with such an arrangement | |
CA2644335C (en) | Turbine or compressor stage, in particular of a turbine engine | |
EP1659266B1 (en) | Common decoupling device for the first and the second bearings of the drive shaft of a turbomachine, and turbomachine and compressor with such a device | |
EP1498624B1 (en) | Device for fixing a motor shaft onto a bearing support | |
FR2930595A1 (en) | BLOWER ROTOR OF A TURBOMACHINE OR A TEST ENGINE | |
FR2585069A1 (en) | DEVICE FOR LIMITING THE ANGULAR DEBATMENT OF AUBES MOUNTED ON A TURBOMACHINE ROTOR DISK | |
FR2783579A1 (en) | RETAINING ARRANGEMENT FOR A BEARING, IN PARTICULAR FOR A HIGH PRESSURE COMPRESSOR SHAFT | |
FR2888621A1 (en) | Bearing support retaining device for turbomachine e.g. twin-spool turbine, has cables disposed parallel to fusible screw, fixed to bearing supports, and each comprising downstream and upstream ends housed in corresponding troughs | |
EP2300685B1 (en) | Turbomachine fan rotor | |
EP1489268A1 (en) | Roll bearing supports arrangement for an aircraft engine rotary shaft and aircraft engine provided with such an arrangement | |
FR2890105A1 (en) | Retention ring immobilization device for e.g. engine of aircraft, has stops positioned such that stops are stopped respectively against immobilization hooks, and slot covered by other hook when retention ring is placed in groove | |
FR2716502A1 (en) | Sealing between vanes and intermediate platforms. | |
EP1818507B1 (en) | Rotor wheel of a turbomachine | |
EP1515002B1 (en) | Anti-rotation means for turbine stator vanes in the split plane of the casing | |
EP0764766B1 (en) | Device for suppressing vibrations mounted between rotor blades | |
FR2622653A1 (en) | ARTICULATED TRANSMISSION SEAL, WITH A LARGE TELESCOPIC RACE, IN PARTICULAR FOR THE AUTOMOBILE | |
FR2946400A1 (en) | Blowing rotor disk for e.g. turbojet engine of aircraft, has swiveling shoes comprising external surfaces mounted on vane bases, where shoes are applied and guided on complementary cylindrical journals of lateral surfaces of cavities | |
FR2841933A1 (en) | Self-locking wedge for turbojet blower disc blades comprises heel supported on blade root upstream face and wedge shaped runner located with play behind locking ring | |
WO2023099856A1 (en) | Assembly comprising a shim mounted on a disk of a moving gear of a turbomachine, and moving gear | |
FR3106615A1 (en) | Turbomachine assembly | |
WO2020239803A1 (en) | Assembly for turbomachine | |
FR3121706A1 (en) | FLASHING TABS FOR TURBOMACHINE ROTOR BLADE FOOT | |
FR3096729A1 (en) | Turbomachine assembly | |
EP3976926A1 (en) | Turbomachine assembly having a damper |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20010119 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FR GB |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
AKX | Designation fees paid |
Free format text: DE FR GB |
|
17Q | First examination report despatched |
Effective date: 20040323 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20050824 |
|
RAP2 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: SNECMA |
|
REF | Corresponds to: |
Ref document number: 60112820 Country of ref document: DE Date of ref document: 20050929 Kind code of ref document: P |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20060526 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 17 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 18 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: CD Owner name: SAFRAN AIRCRAFT ENGINES Effective date: 20170719 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20191219 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20191218 Year of fee payment: 20 Ref country code: GB Payment date: 20191223 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R071 Ref document number: 60112820 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20210103 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20210103 |