FR3082233B1 - Ensemble de turbine - Google Patents
Ensemble de turbine Download PDFInfo
- Publication number
- FR3082233B1 FR3082233B1 FR1855112A FR1855112A FR3082233B1 FR 3082233 B1 FR3082233 B1 FR 3082233B1 FR 1855112 A FR1855112 A FR 1855112A FR 1855112 A FR1855112 A FR 1855112A FR 3082233 B1 FR3082233 B1 FR 3082233B1
- Authority
- FR
- France
- Prior art keywords
- platform
- stator
- cavities
- rotor
- bladed
- 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.)
- Active
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000007789 sealing Methods 0.000 abstract 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and 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
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F05D2230/50—Building or constructing in particular ways
- F05D2230/54—Building or constructing in particular ways by sheet metal manufacturing
-
- 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
- F05D2240/55—Seals
- F05D2240/57—Leaf seals
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Ensemble (10) de turbine de turbomachine (1) d'aéronef, comprenant au moins un rotor (12) aubagé et un stator (13) aubagé comprenant une première plateforme (131) sur laquelle sont fixées des pales et une deuxième plateforme (133) séparée de la première plateforme (131) par un pied (135), de sorte qu'entre les deux plateformes (131, 133) le stator (13) présente deux cavités annulaires (136, 137). Au moins une tôle annulaire (17) monobloc formant un anneau complet est fixée de manière amovible dans l'une des cavités (136, 137) pour assurer une étanchéité dynamique entre le rotor (12) et le stator (13).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1855112A FR3082233B1 (fr) | 2018-06-12 | 2018-06-12 | Ensemble de turbine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1855112 | 2018-06-12 | ||
FR1855112A FR3082233B1 (fr) | 2018-06-12 | 2018-06-12 | Ensemble de turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3082233A1 FR3082233A1 (fr) | 2019-12-13 |
FR3082233B1 true FR3082233B1 (fr) | 2020-07-17 |
Family
ID=62875038
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1855112A Active FR3082233B1 (fr) | 2018-06-12 | 2018-06-12 | Ensemble de turbine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3082233B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3117160B1 (fr) | 2020-12-07 | 2022-11-18 | Safran Aircraft Engines | Redresseur de turbomachine d’aeronef |
FR3119194B1 (fr) * | 2021-01-27 | 2023-07-07 | Safran Aircraft Engines | Distributeur de turbine pour turbomachine |
FR3120649A1 (fr) | 2021-03-12 | 2022-09-16 | Safran Aircraft Engines | Ensemble statorique de turbine |
FR3126024A1 (fr) | 2021-08-04 | 2023-02-10 | Safran Aircraft Engines | Secteur de distributeur de turbine équipé avec une structure en nid d’abeille |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2974841B1 (fr) * | 2011-05-04 | 2013-06-07 | Snecma | Dispositif d'etancheite pour distributeur de turbine de turbomachine |
US9080449B2 (en) * | 2011-08-16 | 2015-07-14 | United Technologies Corporation | Gas turbine engine seal assembly having flow-through tube |
FR3001252B1 (fr) * | 2013-01-23 | 2015-02-13 | Snecma | Aubage fixe de distribution de flux comprenant une plate-forme interne a renforts integres |
FR3001760B1 (fr) * | 2013-02-05 | 2015-01-30 | Snecma | Aubage de distribution de flux comportant une platine d'etancheite amelioree |
FR3003599B1 (fr) * | 2013-03-25 | 2017-11-17 | Snecma | Aubage fixe de distribution de flux ameliore |
FR3039589B1 (fr) * | 2015-07-28 | 2020-01-10 | Safran Aircraft Engines | Etage de turbomachine, en particulier de turbine basse-pression |
DE102017209420A1 (de) * | 2017-06-02 | 2018-12-06 | MTU Aero Engines AG | Dichtungsanordnung mit angeschweißtem Dichtungsblech, Strömungsmaschine und Herstellungsverfahren |
-
2018
- 2018-06-12 FR FR1855112A patent/FR3082233B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3082233A1 (fr) | 2019-12-13 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20191213 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |