EP1205637A1 - Cooling device for stator ring - Google Patents
Cooling device for stator ring Download PDFInfo
- Publication number
- EP1205637A1 EP1205637A1 EP01402865A EP01402865A EP1205637A1 EP 1205637 A1 EP1205637 A1 EP 1205637A1 EP 01402865 A EP01402865 A EP 01402865A EP 01402865 A EP01402865 A EP 01402865A EP 1205637 A1 EP1205637 A1 EP 1205637A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- stator ring
- ramps
- ring
- ventilation assembly
- shells
- 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.)
- Granted
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
- F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
- F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
Definitions
- This talk deals with a set of ventilation of a stator ring, intended to convey a gas at a determined temperature up to a ring turbomachine stator to adjust its diameter and the game he will do with blade tips of rotor rotating in it.
- Such ventilation assemblies are commonly used in turbojets and consist of multi-branched conduits taken up and the ends of which are provided with holes to blow gas and especially air to a large number of points, judiciously distributed, of the ring.
- Terminal conduits are very often ramps running around the rings, in the shape of an arc of a circle and embracing part of their perimeter. Often too, the gas is blown in the axial direction, on outer ribs of the ring rather than on the ring itself, so that the diameter is controlled by these ribs which are more rigid and govern therefore the deformations of the ring proper.
- the assembly which will be described here is characterized in that it is easy to manufacture, despite the large number of conduits that are generally required use, and assemble to the ring despite the complications which can arise from dilations differential thermal at different times of machine operation.
- the invention thus relates to a ventilation assembly of a ring stator composed of branched conduits comprising supply lines, distributors and ramps adjacent to the ring and provided with holes blowing of gases directed towards the ring, characterized in what the ramps are made up of pairs of half shells including a flange and a border surrounding the flange, the pairs of half-shells being joined by the edges, the distributors include spool coils between the ramps and fitted with end edges shaped to fit on side cheek openings of the flanges.
- a stator ring 1 is associated with a group of ventilation units 2 conforming to the invention, each of which occupies a portion of the circumference of ring 1 and includes a group of ramps 3 parallel and in an arc, distributor 4 for distributing air from ventilation between all ramps 3 and a duct supply 5 (visible in Figure 2) connected to the distributor 4.
- supply lines 5 join after one or more others distributors, which are not shown because they are not the subject of this invention; this one relates more specifically to the end of the assemblies ventilation 2, i.e. their parts which are close to ring 1 to be ventilated.
- each of the ramps 3 is composed of a half-shell left 7 and a right half shell 8 of which each of these is assembled to one of these. More precisely, the half-shells 7 and 8 of the two genera each include a flange 9 substantially flat and a border 10 established around the flange 9, the borders 10 of pairs of half-shells 7 and 8 additional being extended and joined to form a single ramp.
- Half-shells 7 and 8 can be made by simple operation stamping and the connections between the borders 10 can be performed by welding. This mode of manufacturing is extremely simple and avoids having to machine tubes to bring them to shapes and desired dimensions, which would probably be a lot more tedious.
- half-shells of left 7 can generally be built at from the same tool as the right half-shells 8 which are symmetrical to the previous ones by the plane of seal.
- This overall similarity does not exclude some dissimilarities of details.
- half-shells 7 and 8 could be constructed with borders 10 of different widths, so for example favor ventilation by the 3 most wide.
- An example of application of this process appears in Figure 2, where three ramps 3 ventilate two ribs 11, the central ramp being placed between the two ribs 11 and ventilating them both, which justifies that its width is double.
- the distributor 4 also includes coils 15 in the form of a short cylinder serving spacers between the ramps 3 and with the conduit 5. It is often beneficial that they are similar, but they can also be different in particular in length. They understand generally edges 16 to be engaged in the openings 13 ramps 3 to hold them in place, and flanges 17 pressing on the ramps 3 to define the spacing of these. Distributor 4 is formed when the coils 15 have been soldered to ramps 3. However, the distribution duct 5 remains generally separate from dispenser 4 and can slide in the input coil 15, a seal sealing 18 being added between them, however.
- one of the coils 15 comprises planar faces and opposite 19 enclosing the end 20 (here enlarged) of the rib 11 which the corresponding coil 15 overcomes.
- the reduction in the axial clearance between the coil 15 and the enlarged portion of the rib 11 contributes to ensuring the axial positioning of the distributors 4 on the ring 1.
- the second coil overlaps its ring with axial play, this to allow the relative dilations between the housings 4 and casing 1 without generating a connection hyperstatic and unwanted constraints.
- FIG. 3 shows that the end 20 of this rib 11 has a v-notch 21 in which the central, cylindrical portion of the coil 15 rests in self-centering, which guarantees the distributor 4 against radial movements and tangents to ring 1: perfect positioning radial, tangential and in orientation along the axis of the engine is performed.
- Brackets 22 are linked to one end of the stator ring 1 by fixing bolts 23 and include a wing 24 under one end of the ruler 6; the other end of it is placed on a boss 25 of the stator ring 1.
- Bolts 26 and 27 are screwed to wing 24 and boss 25. They maintain the ends of rule 6 on them by compressing springs 28 based on rule 6 by washers 29.
- Such an assembly has the property of allow better control of the support effort of rules 6 on equettes 24 and 25. If this effect is excessive, the assembly is rigid and does not allow thermal respiration.
- rule 6 to which ramps 3 are welded, is provided with 30 wide openings around bolts 26 and 27, so that it can be move by sliding axially and tangentially by compared to the stator ring. This flexible mounting avoids therefore to produce excessive internal stresses in ventilation assembly 2, since the ramps 3 have the ability to move above the ring 1 without exerting too much effort. These relative displacements are generally due to thermal expansions differential.
- the support of one of the coils 15 against the end 20 of the corresponding rib 11 offers also some flexibility by allowing all of ventilation 2 to move to the ends, while being recalled towards the stator ring 1 and the bottom of the vé 21 by springs 28. This flexibility is valuable by absorbing expansions inevitable differential thermal with such equipment.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Motor Or Generator Cooling System (AREA)
- Motor Or Generator Frames (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
Abstract
Description
Cet exposé traite d'un ensemble de ventilation d'un anneau de stator, destiné à acheminer un gaz à une température déterminée jusqu'à un anneau de stator de turbomachine afin de régler son diamètre et le jeu qu'il fera avec des extrémités d'aubes de rotor tournant en lui.This talk deals with a set of ventilation of a stator ring, intended to convey a gas at a determined temperature up to a ring turbomachine stator to adjust its diameter and the game he will do with blade tips of rotor rotating in it.
De tels ensembles de ventilation sont couramment utilisés dans les turboréacteurs et consistent en des conduits se ramifiant à plusieurs reprises et dont les extrémités sont munies de perçages pour souffler du gaz et notamment de l'air à un grand nombre de points, répartis judicieusement, de l'anneau. Les conduits terminaux sont très souvent des rampes courant autour des anneaux, en forme d'arc de cercle et embrassant une partie de leur périmètre. Souvent aussi, le gaz est soufflé en direction axiale, sur des nervures extérieures de l'anneau plutôt que sur l'anneau lui-même, afin que le diamètre soit contrôlé par ces nervures qui sont plus rigides et régissent donc les déformations de l'anneau proprement dit.Such ventilation assemblies are commonly used in turbojets and consist of multi-branched conduits taken up and the ends of which are provided with holes to blow gas and especially air to a large number of points, judiciously distributed, of the ring. Terminal conduits are very often ramps running around the rings, in the shape of an arc of a circle and embracing part of their perimeter. Often too, the gas is blown in the axial direction, on outer ribs of the ring rather than on the ring itself, so that the diameter is controlled by these ribs which are more rigid and govern therefore the deformations of the ring proper.
L'ensemble qui sera décrit ici se caractérise en ce qu'il est facile à fabriquer, malgré le grand nombre de conduits qu'il faut généralement employer, et à assembler à l'anneau malgré les complications qui peuvent naítre de dilatations thermiques différentielles à différents moments de fonctionnement de la machine. The assembly which will be described here is characterized in that it is easy to manufacture, despite the large number of conduits that are generally required use, and assemble to the ring despite the complications which can arise from dilations differential thermal at different times of machine operation.
Sous sa forme la plus générale, l'invention concerne ainsi un ensemble de ventilation d'un anneau de stator composé de conduits ramifiés comprenant des conduits d'alimentation, des distributeurs et des rampes adjacentes à l'anneau et munies de perçages de soufflage de gaz dirigés vers l'anneau, caractérisé en ce que les rampes sont composées de paires de demi-coquilles comprenant un flasque et une bordure entourant le flasque, les paires de demi-coquilles étant jointes par les bordures, les distributeurs comprennent des bobines en entretoises entre les rampes et munies de bords d'extrémité façonnés pour s'ajuster sur des ouvertures de joues latérales des flasques.In its most general form, the invention thus relates to a ventilation assembly of a ring stator composed of branched conduits comprising supply lines, distributors and ramps adjacent to the ring and provided with holes blowing of gases directed towards the ring, characterized in what the ramps are made up of pairs of half shells including a flange and a border surrounding the flange, the pairs of half-shells being joined by the edges, the distributors include spool coils between the ramps and fitted with end edges shaped to fit on side cheek openings of the flanges.
D'autres aspects caractéristiques et avantages de l'invention apparaítront plus nettement à la description des figures suivantes :
- la figure 1 est une vue générale de l'ensemble,
- la figure 2 est une vue d'un distributeur à la ramification d'un conduit,
- la figure 3 expose un mode de support de l'ensemble sur l'anneau,
- et la figure 4 représente un groupe de rampes en coupe près de leur extrémité, ainsi qu'un moyen de maintien sur l'anneau.
- FIG. 1 is a general view of the assembly,
- FIG. 2 is a view of a distributor at the branching of a conduit,
- FIG. 3 shows a method of supporting the assembly on the ring,
- and FIG. 4 represents a group of ramps in section near their end, as well as a means of holding on the ring.
Un anneau de stator 1 est associé à un
groupe d'ensembles 2 de ventilation conformes à
l'invention, dont chacun occupe une portion de la
circonférence de l'anneau 1 et comprend un groupe de
rampes 3 parallèles et en arc de cercle, un
distributeur 4 permettant de répartir de l'air de
ventilation entre toutes les rampes 3 et un conduit
d'alimentation 5 (visible à la figure 2) abouché au
distributeur 4. En général, les conduits d'alimentation
5 se rejoignent après un ou plusieurs autres
distributeurs, qui ne sont cependant pas montrés car
ils ne font pas l'objet de cette invention ; celle-ci
concerne plus spécifiquement l'extrémité des ensembles
de ventilation 2, c'est-à-dire leurs parties qui sont
proches de l'anneau 1 à ventiler. On remarquera encore
des moyens de maintien des rampes 3 sur l'anneau 1,
comprenant des règles 6 dont les extrémités sont
assujetties à l'anneau 1 et qui couvrent chacun une des
extrémités d'un des groupes de rampes 3 en les
croisant.A stator ring 1 is associated with a
group of
Comme on le voit aussi à la figure 2,
chacune des rampes 3 est composée d'une demi-coquille
de gauche 7 et d'une demi-coquille de droite 8 dont
chacune de celles-ci est assemblée à une de celles-là.
Plus précisément, les demi-coquilles 7 et 8 des deux
genres comprennent chacune un flasque 9 sensiblement
plat et une bordure 10 établie autour du flasque 9, les
bordures 10 de paires de demi-coquilles 7 et 8
complémentaires étant mises en prolongement et jointes
pour former une rampe unique. Les demi-coquilles 7 et 8
peuvent être fabriquées par une simple opération
d'estampage et les liaisons entre les bordures 10
peuvent être exécutées par soudage. Ce mode de
fabrication est extrêmement simple et évite d'avoir à
usiner des tubes pour les amener aux formes et aux
dimensions voulues, ce qui serait probablement beaucoup
plus fastidieux. De plus, toutes les demi-coquilles de
gauche 7 pourront généralement être construites à
partir du même outil que les demi-coquilles de droite 8
qui sont symétriques aux précédentes par le plan de
joint. Cette similitude d'ensemble n'exclurait pas
certaines dissemblances de détails. Par exemple, les
demi-coquilles 7 et 8 pourraient être construites avec
des bordures 10 de largeur différente, afin par exemple
de privilégier la ventilation par les rampes 3 les plus
larges. Un exemple d'application de ce procédé apparaít
à la figure 2, où trois rampes 3 ventilent deux
nervures 11, la rampe centrale étant placée entre les
deux nervures 11 et les ventilant toutes deux, ce qui
justifie que sa largeur soit double. Les orifices de
soufflage 12 par lesquels l'air s'échappe des rampes 3
sont exécutés à volonté avant ou après l'estampage des
demi-coquilles 7 et 8, en n'omettant par exemple que
les demi-coquilles d'extrémité, qui ne sont situées
devant aucune des nervures 11.As we also see in Figure 2,
each of the
D'autres ouvertures, plus larges, portent
la référence 13 et sont exécutées à travers des joues
14 des flasques 9, hormis à une demi-coquilles extrême
10, pour former le distributeur 4. Les joues 14
s'étendent latéralement à partir des centres des
flasques 9 dans ce mode de réalisation et leur sont
coplanaires. Les extrémités des rampes 3 sont closes
par des tôles continues qui leur sont soudées.Other, larger openings carry
the
Le distributeur 4 comprend encore des
bobines 15 en forme de cylindre court servant
d'entretoises entre les rampes 3 et avec le conduit
d'alimentation 5. Il est souvent avantageux qu'elles
soient semblables, mais elles peuvent aussi être
différentes notamment en longueur. Elles comprennent
généralement des bords 16 à engager dans les ouvertures
13 des rampes 3 pour les maintenir en place, et des
collerettes 17 en appui sur les rampes 3 pour définir
l'écartement de celles-ci. Le distributeur 4 est
constitué quand les bobines 15 ont été soudées aux
rampes 3. Toutefois, le conduit de distribution 5 reste
généralement distinct du distributeur 4 et peut
coulisser dans la bobine 15 d'entrée, un joint
d'étanchéité 18 étant cependant ajouté entre eux.The distributor 4 also includes
Pour conclure avec la figure 2, on notera
qu'une des bobines 15 comprend des faces planes et
opposées 19 enserrant l'extrémité 20 (ici élargie) de
la nervure 11 que la bobine 15 correspondante surmonte.
La réduction du jeu axial entre la bobine 15 et la
portion élargie de la nervure 11 contribue à assurer le
positionnement axial des distributeurs 4 sur l'anneau
1. Ceci permet d'assurer le positionnement axial du
distributeur 4, de régler au plus précis les entrefers
entre les rampes 3 et les anneaux de contrôle 11 et de
maítriser au mieux les échanges convectifs créés par le
douchage en air des anneaux 11. On notera que la
seconde bobine chevauche son anneau avec un jeu axial,
ceci pour permettre les dilations relatives entre les
boítiers 4 et le carter 1 sans générer de liaison
hyperstatique et de contraintes indésirées.To conclude with Figure 2, we will note
that one of the
La constitution de l'ensemble de
ventilation en éléments standardisés et soudés entre
eux est particulièrement simple et avantageuse. On va
maintenant, dans la suite de cet exposé, décrire la
façon dont l'ensemble de ventilation 2 est assujetti à
l'anneau 1. La figure 3 montre encore que l'extrémité
20 de cette nervure 11 possède une entaille en vé 21
dans laquelle la portion centrale, cylindrique, de la
bobine 15 repose en s'auto-centrant, ce qui garantit le
distributeur 4 contre les mouvements radiaux et
tangents à l'anneau 1 : une mise en position parfaite
radiale, tangentielle et en orientation selon l'axe du
moteur est réalisée.The constitution of the whole of
ventilation in standardized and welded elements between
them is particularly simple and advantageous. We go
now, in the rest of this talk, describe the
how the
Les moyens aux règles 6 vont maintenant
être décrits complètement, en liaison à la figure 4
pour montrer comment ils parachèvent le maintien des
rampes 3. Des équerres 22 sont liées à une extrémité de
l'anneau de stator 1 par des boulons de fixation 23 et
comprennent une aile 24 sous une extrémité de la règle
6 ; l'autre extrémité de celle-ci est posée sur un
bossage 25 de l'anneau de stator 1. Des boulons 26 et
27 sont vissés à l'aile 24 et au bossage 25. Ils
maintiennent les extrémités de la règle 6 sur ceux-ci
en comprimant des ressorts 28 s'appuyant sur la règle 6
par des rondelles 29. Un tel montage a la propriété de
permettre de mieux maítriser l'effort d'appui des
règles 6 sur les équettes 24 et 25. Si cet effet est
excessif, l'assemblage est rigide et ne permet pas la
respiration thermique. La meilleure maítrise vient du
fait qu'il est plus facile de calibrer un effort de
compression d'un ressort 28 par la hauteur sous
collerette de la coupelle 31, que de régler un effort
de traction dans un boulon 26 en le serrant au couple.
De plus, la règle 6, à laquelle les rampes 3 sont
soudées, est ménagée avec des ouvertures 30 larges
autour des boulons 26 et 27, de manière à pouvoir se
déplacer en glissant axialement et tangentiellement par
rapport à l'anneau de stator. Ce montage souple évite
donc de produire des contraintes internes excessives
dans l'ensemble de ventilation 2, puisque les rampes 3
ont la faculté de se déplacer au-dessus de l'anneau 1
sans exercer trop d'efforts. Ces déplacements relatifs
sont dus généralement à des dilatations thermiques
différentielles. L'appui d'une des bobines 15 contre
l'extrémité 20 de la nervure 11 correspondante offre
aussi quelque souplesse en autorisant l'ensemble de
ventilation 2 à se déplacer aux extrémités, tout en
étant rappelé vers l'anneau 1 de stator et le fond du
vé 21 par les ressorts 28. Cette souplesse est
précieuse en permettant d'absorber les dilatations
thermiques différentielles inévitables avec un tel
appareillage.The means to
Claims (7)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0014373A FR2816352B1 (en) | 2000-11-09 | 2000-11-09 | VENTILATION ASSEMBLY OF A STATOR RING |
FR0014373 | 2000-11-09 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1205637A1 true EP1205637A1 (en) | 2002-05-15 |
EP1205637B1 EP1205637B1 (en) | 2003-07-09 |
Family
ID=8856230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01402865A Expired - Lifetime EP1205637B1 (en) | 2000-11-09 | 2001-11-08 | Ventilating device for stator ring |
Country Status (9)
Country | Link |
---|---|
US (1) | US6896038B2 (en) |
EP (1) | EP1205637B1 (en) |
JP (1) | JP3913032B2 (en) |
CA (1) | CA2361103C (en) |
DE (1) | DE60100448T2 (en) |
ES (1) | ES2199921T3 (en) |
FR (1) | FR2816352B1 (en) |
RU (1) | RU2276733C2 (en) |
UA (1) | UA73938C2 (en) |
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FR2865237B1 (en) * | 2004-01-16 | 2006-03-10 | Snecma Moteurs | IMPROVEMENTS IN GAME CONTROL DEVICES IN A GAS TURBINE |
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FR3089560B1 (en) * | 2018-12-06 | 2021-01-22 | Safran Aircraft Engines | Device for maintaining a cooling tube for a turbomachine casing |
FR3089545B1 (en) * | 2018-12-07 | 2021-01-29 | Safran Aircraft Engines | Device for cooling a turbine housing for a turbomachine |
US11788425B2 (en) * | 2021-11-05 | 2023-10-17 | General Electric Company | Gas turbine engine with clearance control system |
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EP1577502A1 (en) * | 2004-03-18 | 2005-09-21 | Snecma | Spraybar configuration to control the tip clearance in a gas turbine |
FR2867805A1 (en) * | 2004-03-18 | 2005-09-23 | Snecma Moteurs | TURBOMACHINE HIGH-PRESSURE TURBINE STATOR AND METHOD OF ASSEMBLY |
FR2867806A1 (en) * | 2004-03-18 | 2005-09-23 | Snecma Moteurs | DEVICE FOR CONTROLLING GAS TURBINE SET WITH AIR FLOW BALANCING |
US7309209B2 (en) | 2004-03-18 | 2007-12-18 | Snecma Moteurs | Device for tuning clearance in a gas turbine, while balancing air flows |
US7360987B2 (en) | 2004-03-18 | 2008-04-22 | Snecma | Stator of a high-pressure turbine of a turbomachine, and a method of assembling it |
EP1577501A1 (en) * | 2004-03-18 | 2005-09-21 | Snecma | High pressure turbine stator of a turbo-engine and his assembling process |
US8668438B2 (en) | 2009-04-16 | 2014-03-11 | Rolls-Royce Plc | Turbine casing cooling |
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WO2013186757A2 (en) | 2012-06-14 | 2013-12-19 | Avio S.P.A. | Gas turbine for aeronautic engines |
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ITTO20120519A1 (en) * | 2012-06-14 | 2013-12-15 | Avio Spa | GAS TURBINE FOR AERONAUTICAL MOTORS |
US9790810B2 (en) | 2012-06-14 | 2017-10-17 | Ge Avio S.R.L. | Stator casing cooling system |
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CN107923259A (en) * | 2015-08-27 | 2018-04-17 | 赛峰飞机发动机公司 | The device of the manifold of the shell for the turbine for passing through air jet cooling turbine engines for attachment |
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CN106382136B (en) * | 2016-11-18 | 2017-07-25 | 中国科学院工程热物理研究所 | A kind of transonic speed tip active control device |
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EP3415724A1 (en) * | 2017-06-12 | 2018-12-19 | United Technologies Corporation | Resilient mounting assembly for a turbine engine |
FR3089544A1 (en) * | 2018-12-10 | 2020-06-12 | Safran Aircraft Engines | COOLING DEVICE FOR A TURBOMACHINE HOUSING |
FR3099798A1 (en) * | 2019-08-09 | 2021-02-12 | Safran Aircraft Engines | Set for a turbomachine turbine |
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WO2021028634A1 (en) * | 2019-08-09 | 2021-02-18 | Safran Aircraft Engines | Assembly intended for holding a manifold housing of a device for cooling a turbomachine turbine casing |
WO2021209713A1 (en) | 2020-04-17 | 2021-10-21 | Safran Aircraft Engines | Turbine housing cooling device |
FR3109406A1 (en) * | 2020-04-17 | 2021-10-22 | Safran Aircraft Engines | TURBINE CASE COOLING DEVICE |
US11879347B2 (en) | 2020-04-17 | 2024-01-23 | Safran Aircraft Engines | Turbine housing cooling device |
Also Published As
Publication number | Publication date |
---|---|
DE60100448T2 (en) | 2004-04-15 |
JP2002195007A (en) | 2002-07-10 |
JP3913032B2 (en) | 2007-05-09 |
RU2276733C2 (en) | 2006-05-20 |
UA73938C2 (en) | 2005-10-17 |
FR2816352B1 (en) | 2003-01-31 |
US6896038B2 (en) | 2005-05-24 |
US20020053837A1 (en) | 2002-05-09 |
CA2361103A1 (en) | 2002-05-09 |
ES2199921T3 (en) | 2004-03-01 |
FR2816352A1 (en) | 2002-05-10 |
CA2361103C (en) | 2009-12-29 |
EP1205637B1 (en) | 2003-07-09 |
DE60100448D1 (en) | 2003-08-14 |
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