FR3005991B1 - Dispositif d'interface entre deux elements de turbomachine - Google Patents
Dispositif d'interface entre deux elements de turbomachineInfo
- Publication number
- FR3005991B1 FR3005991B1 FR1354648A FR1354648A FR3005991B1 FR 3005991 B1 FR3005991 B1 FR 3005991B1 FR 1354648 A FR1354648 A FR 1354648A FR 1354648 A FR1354648 A FR 1354648A FR 3005991 B1 FR3005991 B1 FR 3005991B1
- Authority
- FR
- France
- Prior art keywords
- interface device
- turbomachine elements
- turbomachine
- elements
- interface
- 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
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
- F01D11/08—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
-
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F05D2240/60—Shafts
- F05D2240/62—Flexible
-
- 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
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1354648A FR3005991B1 (fr) | 2013-05-23 | 2013-05-23 | Dispositif d'interface entre deux elements de turbomachine |
US14/280,801 US9677413B2 (en) | 2013-05-23 | 2014-05-19 | Interface device between two turbomachine elements |
GB1409255.5A GB2517028B (en) | 2013-05-23 | 2014-05-23 | Interface device between two turbomachine elements |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1354648A FR3005991B1 (fr) | 2013-05-23 | 2013-05-23 | Dispositif d'interface entre deux elements de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3005991A1 FR3005991A1 (fr) | 2014-11-28 |
FR3005991B1 true FR3005991B1 (fr) | 2015-06-26 |
Family
ID=48906357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1354648A Active FR3005991B1 (fr) | 2013-05-23 | 2013-05-23 | Dispositif d'interface entre deux elements de turbomachine |
Country Status (3)
Country | Link |
---|---|
US (1) | US9677413B2 (fr) |
FR (1) | FR3005991B1 (fr) |
GB (1) | GB2517028B (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10519873B2 (en) * | 2016-04-06 | 2019-12-31 | General Electric Company | Air bypass system for rotor shaft cooling |
DE102016225875A1 (de) * | 2016-12-21 | 2018-06-21 | MTU Aero Engines AG | Turbomaschinen-Dichtungsanordnung |
FR3067387B1 (fr) * | 2017-06-07 | 2019-06-28 | Safran Aircraft Engines | Ecope d'alimentation en air pour l'alimentation d'un systeme de refroidissement et de controle des jeux d'une turbine |
FR3095232B1 (fr) * | 2019-04-16 | 2022-06-03 | Safran Aircraft Engines | Ensemble pour une turbine de turbomachine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2746996C3 (de) * | 1977-10-19 | 1980-09-04 | Karl Ing.(Grad.) 4040 Neuss Weinhold | Rohrkupplung zum lösbaren Verbinden zweier Rohrenden |
GB9118158D0 (en) * | 1991-08-22 | 1991-10-09 | Birch Fred P | Improved hollow pivotable coupling |
US5603531A (en) * | 1994-12-06 | 1997-02-18 | United Technologies Corporation | Blind assembly-swivel crossover tube |
US5947412A (en) * | 1997-01-10 | 1999-09-07 | Titan Corporation | Jet engine noise suppressor assembly |
WO1998058158A1 (fr) * | 1997-06-19 | 1998-12-23 | Mitsubishi Heavy Industries, Ltd. | Dispositif d'etancheite pour aubes de stator de turbine a gaz |
US5996936A (en) * | 1997-09-29 | 1999-12-07 | General Electric Company | Fluidic throat exhaust nozzle |
US5993150A (en) * | 1998-01-16 | 1999-11-30 | General Electric Company | Dual cooled shroud |
US6126389A (en) * | 1998-09-02 | 2000-10-03 | General Electric Co. | Impingement cooling for the shroud of a gas turbine |
FR2883599B1 (fr) * | 2005-03-23 | 2010-04-23 | Snecma Moteurs | Dispositif de liaison entre une enceinte de passage d'air de refroidissement et un aubage de distributeur dans une turbomachine |
FR2904663B1 (fr) * | 2006-08-01 | 2012-02-03 | Snecma | Turbomachine a double flux a variation artificielle de sa section de col |
US7578424B2 (en) * | 2006-09-05 | 2009-08-25 | United Technologies Corporation | Method of joining a microwave transparent component to a host component |
US7823389B2 (en) * | 2006-11-15 | 2010-11-02 | General Electric Company | Compound clearance control engine |
-
2013
- 2013-05-23 FR FR1354648A patent/FR3005991B1/fr active Active
-
2014
- 2014-05-19 US US14/280,801 patent/US9677413B2/en active Active
- 2014-05-23 GB GB1409255.5A patent/GB2517028B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB201409255D0 (en) | 2014-07-09 |
FR3005991A1 (fr) | 2014-11-28 |
GB2517028B (en) | 2019-07-03 |
US20140348637A1 (en) | 2014-11-27 |
GB2517028A (en) | 2015-02-11 |
US9677413B2 (en) | 2017-06-13 |
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Legal Events
Date | Code | Title | Description |
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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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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |