EP1540189B1 - Restraining device for fan blade root - Google Patents
Restraining device for fan blade root Download PDFInfo
- Publication number
- EP1540189B1 EP1540189B1 EP03761637A EP03761637A EP1540189B1 EP 1540189 B1 EP1540189 B1 EP 1540189B1 EP 03761637 A EP03761637 A EP 03761637A EP 03761637 A EP03761637 A EP 03761637A EP 1540189 B1 EP1540189 B1 EP 1540189B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade
- packing member
- zone
- metal structure
- end zones
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/322—Blade mountings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Definitions
- the invention relates to a device for retaining the foot of the fan blades.
- the wedge comprises between the two elastomeric side edges, on either side of the central metal zone, a metal lower part which rests on the bottom of the cell.
- the object of the invention is to improve the performance of the impacted blade by ensuring that the shim can absorb a portion of the impact energy beyond the rotation permitted by the shim according to the state of the technique.
- the wedge thus works according to the principle of a leaf spring in the event of violent impact on the dawn.
- the lower recess is advantageously connected to the upstream and downstream end zones by lunulae.
- the lower recess is filled by overmoulding with the semi-rigid elastomeric material.
- the central zone has a recessed profile relative to the profile of the cell.
- the wedge 5 shown on the Figures 3, 4 and 5 is in the form of a curvilinear plate of longitudinal axis XX '. It is constituted a metal structure having recessed portions filled by overmoulding with a semi-rigid elastomeric material.
- the lower recess 21 may optionally be filled by the elastomeric material, but this is not mandatory.
- the overmolding of the metal structure by the elastomeric material is performed at a slightly higher rib than that of the metal part. This arrangement makes it possible to mount the wedge 5 in compression under the foot 3 of the blade 4 in order to annihilate the residual clearance between the wedge 5 and the blade root in the cell 2 of the disk 1.
- the figure 6 shows the deformation undergone by the metal intermediate part of the wedge 5 in the event of violent impact of the blade 4.
- the depth of the recess 21 can be determined in such a way that the wedge 5 functions as a spring, while maintaining its elasticity. It can also be determined so that the wedge 5 plastically deforms and absorbs some of the impact energy.
- the lower surface of the intermediate portion can be connected to the upstream and downstream end zones 11 by lunulae 16 and 17, as is shown in FIG. figure 7 .
Abstract
Description
L'invention concerne un dispositif de retenue du pied des aubes de soufflante.The invention relates to a device for retaining the foot of the fan blades.
Elle concerne plus précisément une cale destinée à retenir le pied d'une aube de soufflante dans une alvéole curviligne ménagée à la périphérie d'un disque de rotor, ladite aube comportant deux flancs appelés respectivement intrados et extrados, ladite cale se présentant sous la forme d'une plaque curviligne constituée d'une structure métallique ayant des parties évidées comblées par surmoulage avec un matériau élastomère semi-rigide, notamment sur le bord latéral situé du côté de l'intrados de l'aube entre deux zones extrêmes amont et aval de structure entièrement métallique, sur le bord latéral situé du côté de l'extrados de l'aube entre une zone centrale de structure essentiellement métallique et lesdites zones extrêmes, et sur les deux parties supérieures de ladite cale qui s'étendent entre lesdits deux bords latéraux en élastomère, de part et d'autre de ladite zone centrale métallique.It relates more specifically to a wedge intended to retain the foot of a fan blade in a curvilinear cavity formed on the periphery of a rotor disc, said blade comprising two flanks respectively called intrados and extrados, said wedge being in the form a curvilinear plate consisting of a metal structure having recessed portions filled by overmoulding with a semi-rigid elastomeric material, in particular on the lateral edge situated on the underside side of the blade between two upstream and downstream end zones of all-metal structure, on the lateral edge located on the side of the upper surface of the blade between a central zone of essentially metallic structure and said end zones, and on the two upper parts of said wedge which extend between said two lateral edges elastomer, on both sides of said central metal zone.
Une telle cale est dévoilée par
Dans ce document, la cale comporte entre les deux bords latéraux en élastomère, de part et d'autre de la zone centrale métallique, une partie inférieure métallique qui repose sur le fond de l'alvéole.In this document, the wedge comprises between the two elastomeric side edges, on either side of the central metal zone, a metal lower part which rests on the bottom of the cell.
En cas de choc violent subit par l'aube, la plaque ne peut pivoter que d'un angle très faible par suite de la raideur élevée de la structure métallique.In the event of violent shock experienced by the blade, the plate can rotate only a very small angle due to the high stiffness of the metal structure.
Le but de l'invention est d'améliorer la tenue de l'aube percutée en faisant en sorte que la cale puisse absorber une partie de l'énergie d'impact au-delà de la rotation permise par la cale selon l'état de la technique.The object of the invention is to improve the performance of the impacted blade by ensuring that the shim can absorb a portion of the impact energy beyond the rotation permitted by the shim according to the state of the technique.
Le but est atteint selon l'invention par le fait que la structure métallique comporte en outre un évidement inférieur qui s'étend entre les deux zones extrêmes amont et aval sur toute sa surface.The object is achieved according to the invention in that the metal structure further comprises a lower recess which extends between the two upstream and downstream end zones over its entire surface.
La cale travaille ainsi selon le principe d'un ressort à lame en cas de choc violent sur l'aube.The wedge thus works according to the principle of a leaf spring in the event of violent impact on the dawn.
Afin d'améliorer encore la souplesse de la cale, l'évidement inférieur se raccorde avantageusement aux zones extrêmes amont et aval par des lunules.To further improve the flexibility of the wedge, the lower recess is advantageously connected to the upstream and downstream end zones by lunulae.
De préférence, l'évidement inférieur est comblé par surmoulage avec le matériau élastomère semi-rigide.Preferably, the lower recess is filled by overmoulding with the semi-rigid elastomeric material.
Si nécessaire, la zone centrale comporte un profil en retrait par rapport au profil de l'alvéole.If necessary, the central zone has a recessed profile relative to the profile of the cell.
D'autres avantages et caractéristiques de l'invention ressortiront à la lecture de la description suivante faite à titre d'exemple et en référence aux dessins annexés dans lesquels :
- la
figure 1 est une coupe radiale d'un dispositif de retenue d'un pied d'aube d'une soufflante, - la
figure 2 est une coupe transversale d'un pied d'aube logé dans une alvéole et maintenu au moyen d'une cale selon l'invention, - la
figure 3 est une vue en coupe longitudinale d'une cale de retenue d'un pied d'aube selon l'invention, - la
figure 4 est une vue de dessus de la cale de lafigure 3 , - la
figure 5 est une coupe selon la ligne V-V de lafigure 4 , - la
figure 6 est une vue en coupe longitudinale de la cale de retenue selon l'invention soumise à un effort de compression suite à la rotation de l'aube, et - la
figure 7 est une coupe longitudinale d'une variante de la cale de retenue selon l'invention.
- the
figure 1 is a radial section of a device for retaining a blade root of a fan, - the
figure 2 is a cross section of a blade root housed in a cell and held by means of a wedge according to the invention, - the
figure 3 is a longitudinal sectional view of a wedge for retaining a blade root according to the invention, - the
figure 4 is a top view of the hold of thefigure 3 , - the
figure 5 is a section along line VV of thefigure 4 , - the
figure 6 is a longitudinal sectional view of the holding wedge according to the invention subjected to a compressive force following the rotation of the blade, and - the
figure 7 is a longitudinal section of a variant of the holding wedge according to the invention.
Les
La cale 5 représentée sur les
La cale 5 comporte deux zones extrêmes amont 10 et aval 11 de structure entièrement métallique reliées entre elles par une partie intermédiaire métallique de section variable qui présente :
- sur sa face située du côté de l'intrados de l'aube 4, un évidement 13 comblé par un matériau élastomère formant un bord latéral qui s'étend entre les zones
extrêmes amont 10 etaval 13, - sur sa face située du côté de l'extrados de l'aube 4, deux
14, 15 disposés de part et d'autre d'une zone centrale métallique 12 de structure métallique, et également comblés par le matériau élastomère,évidements - sur sa face supérieure de part et d'autre de la zone centrale métallique 12, entre l'évidement 13 et les
évidements 14 et 15, deuxévidements 18 et 19 comblés par le matériau élastomère, et - sur sa face inférieure 20, entre les zones
extrêmes amont 10 etaval 11, unévidement 21 qui s'étend sur toute cette surface et notamment sous la zone centrale métallique 12.
- on its face located on the underside side of the blade 4, a
recess 13 filled with an elastomeric material forming a lateral edge which extends between the upstream and 10 and 13,downstream end zones - on its face located on the extrados side of the blade 4, two
14, 15 disposed on either side of a metalrecesses central zone 12 of metal structure, and also filled by the elastomeric material, - on its upper face on either side of the
central metal zone 12, between therecess 13 and the 14 and 15, tworecesses 18 and 19 filled by the elastomeric material, andrecesses - on its
underside 20, between the upstream anddownstream end zones 10, arecess 21 which extends over the entire surface and in particular under thecentral metal zone 12.
La face inférieure 20 de la partie intermédiaire métallique reliant les zones extrêmes amont 10 et aval 11 entièrement métalliques se trouve donc dans un plan sensiblement parallèle au plan contenant les faces inférieures des zones extrêmes amont 10 et aval 11. La partie intermédiaire métallique se comporte ainsi comme une lame ressort dans le cas où elle est soumise à des efforts de compression appliqués notamment au-dessus de la zone centrale métallique 12.The
L'évidement inférieur 21 peut éventuellement être comblé par le matériau élastomère, mais ceci n'est pas obligatoire.The
Le surmoulage de la structure métallique par le matériau élastomère est effectué à une côte légèrement supérieure à celle de la partie métallique. Cette disposition permet de monter la cale 5 en compression sous le pied 3 de l'aube 4 afin d'annihiler le jeu résiduel entre la cale 5 et le pied d'aube dans l'alvéole 2 du disque 1.The overmolding of the metal structure by the elastomeric material is performed at a slightly higher rib than that of the metal part. This arrangement makes it possible to mount the
Lorsque l'évidement inférieur 21 est comblé par du matériau élastomère, la section transversale de la cale 5 est sensiblement homogène d'une extrémité à l'autre de cette cale 5.When the
Toutefois, la zone centrale métallique 12 peut présenter, si besoin est, un profil usiné 22 en retrait par rapport au profil 23 de l'alvéole 2 pour permettre une rotation du pied 3 de l'aube 4 autour de l'axe BB' en cas de choc violent sur l'intrados de l'aube 4.However, the metal
Cet axe BB' coupe le plan transversal médian de la cale 5 au point référencé Q sur les
La
La profondeur de l'évidement 21 peut être déterminée de telle manière que la cale 5 fonctionne comme un ressort, tout en conservant son élasticité. On peut également la déterminer pour que la cale 5 se déforme plastiquement et absorbe une partie de l'énergie d'impact.The depth of the
Pour accroître encore la souplesse de la cale 5, la surface inférieure de la partie intermédiaire peut être raccordée aux zones extrêmes amont 10 et aval 11 par des lunules 16 et 17, ainsi que cela est montré sur la
Claims (4)
- A packing member (5) for retaining the root of a blade (4) in a fan in a curved socket (2) arranged on the periphery of a rotor disk (1), said blade (4) having a convex flank and a concave flank, said packing member (5) being in the form of a curvilinear plate constituted by a metal structure having hollowed out portions that are filled in by overmolding with a semi-rigid elastomer material, in particular on the lateral edge situated on the concave side of the blade (4) between an upstream end zone (10) and a downstream end zone (11), which end zones are of entirely metal structure, on the lateral edge situated on the convex side of the blade between said end zones and a central zone, that is essentially of metal structure, and on the two top portions of said packing member which extend between said two elastomer lateral edges on either side of said metal central zone, said packing member being characterized by the fact that the metal structure further comprises a bottom recess (21) extending over its entire surface (20) between the upstream end zone (10) and the downstream end zone (11).
- A packing member according to claim 1, characterized by the fact that the bottom recess (21) is connected to the upstream end zone (10) and downstream end zone (11) by crescent-shaped portions (16, 17).
- A packing member according to claim 1 or claim 2, characterized by the fact that the bottom recess (21) is filled in by being overmolded with the semi-rigid elastomer material.
- A packing member according to any one of claims 1 to 3, characterized by the fact that the central zone (12) has a profile (22) that is set back relative to the profile (23) of the socket (2).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0207977A FR2841609B1 (en) | 2002-06-27 | 2002-06-27 | BLOWER RETAINER LEVEL RETAINER |
FR0207977 | 2002-06-27 | ||
PCT/FR2003/001955 WO2004003390A1 (en) | 2002-06-27 | 2003-06-25 | Restraining device for fan blade root |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1540189A1 EP1540189A1 (en) | 2005-06-15 |
EP1540189B1 true EP1540189B1 (en) | 2010-06-16 |
Family
ID=29724920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03761637A Expired - Lifetime EP1540189B1 (en) | 2002-06-27 | 2003-06-25 | Restraining device for fan blade root |
Country Status (9)
Country | Link |
---|---|
US (1) | US7108484B2 (en) |
EP (1) | EP1540189B1 (en) |
JP (1) | JP4188320B2 (en) |
AU (1) | AU2003263256A1 (en) |
CA (1) | CA2489787C (en) |
DE (1) | DE60333021D1 (en) |
FR (1) | FR2841609B1 (en) |
RU (1) | RU2309301C2 (en) |
WO (1) | WO2004003390A1 (en) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2881174B1 (en) | 2005-01-27 | 2010-08-20 | Snecma Moteurs | DEVICE FOR POSITIONING A DASHBOARD AND AUBAGE DISK COMPRISING SUCH A DEVICE |
FR2918129B1 (en) * | 2007-06-26 | 2009-10-30 | Snecma Sa | IMPROVEMENT TO AN INTERCALE BETWEEN A FOOT OF DAWN AND THE BACKGROUND OF THE ALVEOLE OF THE DISK IN WHICH IT IS MOUNTED |
FR2927998A1 (en) * | 2008-02-25 | 2009-08-28 | Snecma Sa | TESTING MACHINE FOR A WAVE FOOT COATING. |
FR2927997A1 (en) * | 2008-02-25 | 2009-08-28 | Snecma Sa | METHOD FOR TESTING A WAVE FOOT COATING |
US8186961B2 (en) * | 2009-01-23 | 2012-05-29 | Pratt & Whitney Canada Corp. | Blade preloading system |
FR2945074B1 (en) | 2009-04-29 | 2011-06-03 | Snecma | REINFORCED BLOW OF BREATHING BLADE |
US8616850B2 (en) * | 2010-06-11 | 2013-12-31 | United Technologies Corporation | Gas turbine engine blade mounting arrangement |
FR2974864B1 (en) * | 2011-05-04 | 2016-05-27 | Snecma | ROTOR OF TURBOMACHINE WITH MEANS OF AXIAL RETENTION OF AUBES |
FR2975428B1 (en) * | 2011-05-17 | 2015-11-20 | Snecma | TURBOMACHINE AUBES WHEEL |
FR2978796B1 (en) * | 2011-08-03 | 2013-08-09 | Snecma | TURBOMACHINE AUBES WHEEL |
US8716673B2 (en) * | 2011-11-29 | 2014-05-06 | Fei Company | Inductively coupled plasma source as an electron beam source for spectroscopic analysis |
US8851854B2 (en) | 2011-12-16 | 2014-10-07 | United Technologies Corporation | Energy absorbent fan blade spacer |
GB201212750D0 (en) * | 2012-07-18 | 2012-08-29 | Rolls Royce Plc | A rotor assembly |
FR2996584A1 (en) * | 2012-10-10 | 2014-04-11 | Snecma | FOOTBED FOR LEVELED BLADE FOOT |
US9359906B2 (en) * | 2012-12-18 | 2016-06-07 | United Technologies Corporation | Rotor blade root spacer with a fracture feature |
US9422819B2 (en) * | 2012-12-18 | 2016-08-23 | United Technologies Corporation | Rotor blade root spacer for arranging between a rotor disk and a root of a rotor blade |
EP2946080B1 (en) | 2013-01-17 | 2018-05-30 | United Technologies Corporation | Rotor blade root spacer with grip element |
WO2015053922A1 (en) | 2013-10-11 | 2015-04-16 | United Technologies Corporation | Compressible fan blade with root spacer |
GB201417417D0 (en) * | 2014-10-02 | 2014-11-19 | Rolls Royce Plc | Slider |
US10465537B2 (en) * | 2016-05-27 | 2019-11-05 | General Electric Company | Margin bucket dovetail radial support feature for axial entry buckets |
US10738626B2 (en) * | 2017-10-24 | 2020-08-11 | General Electric Company | Connection assemblies between turbine rotor blades and rotor wheels |
CN109630465A (en) * | 2018-12-16 | 2019-04-16 | 中国航发沈阳发动机研究所 | A kind of fan gasket |
US11555407B2 (en) | 2020-05-19 | 2023-01-17 | General Electric Company | Turbomachine rotor assembly |
KR102454379B1 (en) * | 2020-09-08 | 2022-10-14 | 두산에너빌리티 주식회사 | rotor and turbo-machine comprising the same |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3216699A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Airfoil member assembly |
US5123813A (en) * | 1991-03-01 | 1992-06-23 | General Electric Company | Apparatus for preloading an airfoil blade in a gas turbine engine |
FR2746456B1 (en) * | 1996-03-21 | 1998-04-30 | Snecma | DEVICE FOR RETAINING THE FOOT OF THE BLADES OF A BLOWER |
FR2807096B1 (en) * | 2000-03-30 | 2002-05-31 | Abb Alstom Power Nv | ROTOR DISC OF TURBINE EQUIPPED WITH FINS ON FOOT AND TREE OF MOUNTING A FIN ON A DISC |
US6481971B1 (en) * | 2000-11-27 | 2002-11-19 | General Electric Company | Blade spacer |
-
2002
- 2002-06-27 FR FR0207977A patent/FR2841609B1/en not_active Expired - Fee Related
-
2003
- 2003-06-25 CA CA2489787A patent/CA2489787C/en not_active Expired - Lifetime
- 2003-06-25 US US10/517,611 patent/US7108484B2/en not_active Expired - Lifetime
- 2003-06-25 WO PCT/FR2003/001955 patent/WO2004003390A1/en active Application Filing
- 2003-06-25 JP JP2004516862A patent/JP4188320B2/en not_active Expired - Lifetime
- 2003-06-25 RU RU2005101881/06A patent/RU2309301C2/en active
- 2003-06-25 EP EP03761637A patent/EP1540189B1/en not_active Expired - Lifetime
- 2003-06-25 DE DE60333021T patent/DE60333021D1/en not_active Expired - Lifetime
- 2003-06-25 AU AU2003263256A patent/AU2003263256A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
JP2005530955A (en) | 2005-10-13 |
RU2309301C2 (en) | 2007-10-27 |
US7108484B2 (en) | 2006-09-19 |
JP4188320B2 (en) | 2008-11-26 |
WO2004003390A1 (en) | 2004-01-08 |
FR2841609B1 (en) | 2004-09-10 |
EP1540189A1 (en) | 2005-06-15 |
US20050254951A1 (en) | 2005-11-17 |
FR2841609A1 (en) | 2004-01-02 |
RU2005101881A (en) | 2005-10-27 |
CA2489787C (en) | 2011-08-09 |
AU2003263256A1 (en) | 2004-01-19 |
DE60333021D1 (en) | 2010-07-29 |
CA2489787A1 (en) | 2004-01-08 |
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