FR2942844A1 - Ensemble d'anneau de turbine avec arret axial - Google Patents
Ensemble d'anneau de turbine avec arret axial Download PDFInfo
- Publication number
- FR2942844A1 FR2942844A1 FR0951445A FR0951445A FR2942844A1 FR 2942844 A1 FR2942844 A1 FR 2942844A1 FR 0951445 A FR0951445 A FR 0951445A FR 0951445 A FR0951445 A FR 0951445A FR 2942844 A1 FR2942844 A1 FR 2942844A1
- Authority
- FR
- France
- Prior art keywords
- ring
- support structure
- turbine
- leg
- assembly 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.)
- Granted
Links
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- 238000000280 densification Methods 0.000 description 10
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 9
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- 238000000576 coating method Methods 0.000 description 4
- 238000007596 consolidation process Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 238000009941 weaving Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
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- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
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- 230000008595 infiltration Effects 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000005055 methyl trichlorosilane Substances 0.000 description 2
- JLUFWMXJHAVVNN-UHFFFAOYSA-N methyltrichlorosilane Chemical compound C[Si](Cl)(Cl)Cl JLUFWMXJHAVVNN-UHFFFAOYSA-N 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- 239000007833 carbon precursor Substances 0.000 description 1
- 239000011153 ceramic matrix composite Substances 0.000 description 1
- 239000012700 ceramic precursor Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
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- 238000009966 trimming Methods 0.000 description 1
- 210000003462 vein Anatomy 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- 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
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims (8)
- REVENDICATIONS1. Ensemble d'anneau de turbine comprenant un anneau de turbine formé d'un ensemble de secteurs d'anneau (10) et une structure de support de l'anneau de turbine, chaque secteur d'anneau ayant une section sensiblement en forme de it avec une base annulaire (12) ayant une face interne du côté d'une veine d'écoulement de flux gazeux dans la turbine et une face externe à partir de laquelle font saillie deux pattes d'accrochage amont (14) et aval (16) ayant des extrémités maintenues en appui radial contre des surfaces de la structure de support, caractérisé en ce que chaque secteur d'anneau (10) est maintenu axialement par engagement mutuel de reliefs complémentaires (17, 37) sur des surfaces d'appui en regard d'une patte d'accrochage (16) et d'une partie (36) de la structure de support.
- 2. Ensemble d'anneau de turbine selon la revendication 1, caractérisé en ce qu' une première patte (14) a une partie d'extrémité qui est engagée sensiblement axialement dans un logement à section sensiblement en U formé par un crochet (34) de la structure de support d'anneau et qui est maintenue sensiblement sans jeu radial dans le logement lorsque le secteur d'anneau est en place, et la seconde patte (16) est maintenue en appui radial contre une surface d'appui (36a) de la structure de support d'anneau, et le relief de maintien axial (17) formé sur une surface d'une patte d'accrochage est formé sur la seconde patte (16) .
- 3. Ensemble d'anneau de turbine selon la revendication 2, caractérisé en ce que le logement à section en U est délimité par des branches interne et externe opposées, et la branche interne (34a) a une longueur inférieure à celle de la branche externe (3412).
- 4. Ensemble d'anneau de turbine selon l'une quelconque des revendications 2 et 3, caractérisé en ce que le logement à section en U est délimité par des branches interne et externe opposées et la face intérieure (35b) de la branche externe présente un décrochement (35ç) à partir duquel, en direction du fond du logement, la distance radiale entre les faces intérieures des branches interne et externe est augmentée.
- 5. Ensemble d'anneau de turbine selon l'une quelconque des revendications 2 à 4, caractérisé en ce que la première patte (14) est la patte amont et la seconde patte (16) est la patte aval. 5 10
- 6. Ensemble d'anneau de turbine selon la revendication 5, caractérisé en ce qu'un joint d'étanchéité (20) est interposé entre la seconde patte (16) et la surface d'appui (36a) de la structure de support d'anneau.
- 7. Ensemble d'anneau de turbine selon l'une quelconque des revendications 1 à 6, caractérisé en ce que le relief de maintien axial sur la surface d'appui d'une patte d'accrochage (16) est sous forme d'une rainure (17) coopérant avec une nervure (37) formée sur la surface d'appui de la structure de support d'anneau.
- 8. Ensemble d'anneau de turbine selon la revendication 7, caractérisé en ce que la rainure (17) est à profil sensiblement en forme de V.
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0951445A FR2942844B1 (fr) | 2009-03-09 | 2009-03-09 | Ensemble d'anneau de turbine avec arret axial |
EP10715282A EP2406466B1 (fr) | 2009-03-09 | 2010-03-01 | Ensemble d'anneau de turbine |
RU2011140942/06A RU2522264C2 (ru) | 2009-03-09 | 2010-03-01 | Сборка обоймы турбины |
CA2750938A CA2750938A1 (fr) | 2009-03-09 | 2010-03-01 | Ensemble d'anneau de turbine |
US13/255,436 US9080463B2 (en) | 2009-03-09 | 2010-03-01 | Turbine ring assembly |
JP2011553489A JP5646517B2 (ja) | 2009-03-09 | 2010-03-01 | タービンリング組立体 |
PCT/FR2010/050342 WO2010103213A1 (fr) | 2009-03-09 | 2010-03-01 | Ensemble d'anneau de turbine |
ES10715282T ES2398727T3 (es) | 2009-03-09 | 2010-03-01 | Conjunto de anillo de turbina |
BRPI1013342A BRPI1013342A8 (pt) | 2009-03-09 | 2010-03-01 | Conjunto de anel de turbina |
CN201080004094XA CN102272419A (zh) | 2009-03-09 | 2010-03-01 | 涡轮环组件 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0951445A FR2942844B1 (fr) | 2009-03-09 | 2009-03-09 | Ensemble d'anneau de turbine avec arret axial |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2942844A1 true FR2942844A1 (fr) | 2010-09-10 |
FR2942844B1 FR2942844B1 (fr) | 2014-06-27 |
Family
ID=41130259
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0951445A Active FR2942844B1 (fr) | 2009-03-09 | 2009-03-09 | Ensemble d'anneau de turbine avec arret axial |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2942844B1 (fr) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2465466C1 (ru) * | 2011-05-05 | 2012-10-27 | Открытое акционерное общество "Авиадвигатель" | Высокотемпературная турбина газотурбинного двигателя |
WO2015088869A1 (fr) * | 2013-12-12 | 2015-06-18 | General Electric Company | Système de support de carénage cmc |
FR3041994A1 (fr) * | 2015-10-06 | 2017-04-07 | Herakles | Ensemble d'anneau de turbine |
US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
US10378387B2 (en) | 2013-05-17 | 2019-08-13 | General Electric Company | CMC shroud support system of a gas turbine |
US10400619B2 (en) | 2014-06-12 | 2019-09-03 | General Electric Company | Shroud hanger assembly |
US10465558B2 (en) | 2014-06-12 | 2019-11-05 | General Electric Company | Multi-piece shroud hanger assembly |
CN111188655A (zh) * | 2015-05-22 | 2020-05-22 | 赛峰飞机发动机公司 | 涡轮环组件 |
WO2021191538A1 (fr) | 2020-03-24 | 2021-09-30 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
US11668207B2 (en) | 2014-06-12 | 2023-06-06 | General Electric Company | Shroud hanger assembly |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1099826A1 (fr) * | 1999-11-10 | 2001-05-16 | Snecma Moteurs | Dispositif de fixation pour une virole de turbine |
US20040062639A1 (en) * | 2002-09-30 | 2004-04-01 | Glynn Christopher Charles | Turbine engine shroud assembly including axially floating shroud segment |
US20050152777A1 (en) * | 2004-01-08 | 2005-07-14 | Thompson Jeff B. | Resilent seal on leading edge of turbine inner shroud |
GB2445075A (en) * | 2006-12-21 | 2008-06-25 | Gen Electric | Turbine shroud supporting arrangement |
FR2919345A1 (fr) * | 2007-07-26 | 2009-01-30 | Snecma Sa | Anneau pour une roue de turbine de turbomachine. |
-
2009
- 2009-03-09 FR FR0951445A patent/FR2942844B1/fr active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1099826A1 (fr) * | 1999-11-10 | 2001-05-16 | Snecma Moteurs | Dispositif de fixation pour une virole de turbine |
US20040062639A1 (en) * | 2002-09-30 | 2004-04-01 | Glynn Christopher Charles | Turbine engine shroud assembly including axially floating shroud segment |
US20050152777A1 (en) * | 2004-01-08 | 2005-07-14 | Thompson Jeff B. | Resilent seal on leading edge of turbine inner shroud |
GB2445075A (en) * | 2006-12-21 | 2008-06-25 | Gen Electric | Turbine shroud supporting arrangement |
FR2919345A1 (fr) * | 2007-07-26 | 2009-01-30 | Snecma Sa | Anneau pour une roue de turbine de turbomachine. |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2465466C1 (ru) * | 2011-05-05 | 2012-10-27 | Открытое акционерное общество "Авиадвигатель" | Высокотемпературная турбина газотурбинного двигателя |
US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
US10378387B2 (en) | 2013-05-17 | 2019-08-13 | General Electric Company | CMC shroud support system of a gas turbine |
US10309244B2 (en) | 2013-12-12 | 2019-06-04 | General Electric Company | CMC shroud support system |
WO2015088869A1 (fr) * | 2013-12-12 | 2015-06-18 | General Electric Company | Système de support de carénage cmc |
US10400619B2 (en) | 2014-06-12 | 2019-09-03 | General Electric Company | Shroud hanger assembly |
US10465558B2 (en) | 2014-06-12 | 2019-11-05 | General Electric Company | Multi-piece shroud hanger assembly |
US11092029B2 (en) | 2014-06-12 | 2021-08-17 | General Electric Company | Shroud hanger assembly |
US11668207B2 (en) | 2014-06-12 | 2023-06-06 | General Electric Company | Shroud hanger assembly |
US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
CN111188655A (zh) * | 2015-05-22 | 2020-05-22 | 赛峰飞机发动机公司 | 涡轮环组件 |
FR3041994A1 (fr) * | 2015-10-06 | 2017-04-07 | Herakles | Ensemble d'anneau de turbine |
WO2021191538A1 (fr) | 2020-03-24 | 2021-09-30 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
FR3108672A1 (fr) | 2020-03-24 | 2021-10-01 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
Also Published As
Publication number | Publication date |
---|---|
FR2942844B1 (fr) | 2014-06-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TQ | Partial transmission of property |
Owner name: HERAKLES, FR Effective date: 20131121 Owner name: SNECMA, FR Effective date: 20131121 Owner name: SNECMA PROPULSION SOLIDE, FR Effective date: 20131121 |
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PLFP | Fee payment |
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Year of fee payment: 12 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20200409 Owner name: SNECMA PROPULSION SOLIDE, FR Effective date: 20200409 Owner name: SAFRAN CERAMICS, FR Effective date: 20200409 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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