FR3003295B1 - Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblage - Google Patents
Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblageInfo
- Publication number
- FR3003295B1 FR3003295B1 FR1352256A FR1352256A FR3003295B1 FR 3003295 B1 FR3003295 B1 FR 3003295B1 FR 1352256 A FR1352256 A FR 1352256A FR 1352256 A FR1352256 A FR 1352256A FR 3003295 B1 FR3003295 B1 FR 3003295B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- collection device
- assembly method
- seal collection
- seal
- 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
- 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
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
-
- 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
- F01D25/14—Casings modified therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1352256A FR3003295B1 (fr) | 2013-03-14 | 2013-03-14 | Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1352256A FR3003295B1 (fr) | 2013-03-14 | 2013-03-14 | Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblage |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3003295A1 FR3003295A1 (fr) | 2014-09-19 |
| FR3003295B1 true FR3003295B1 (fr) | 2017-12-22 |
Family
ID=48901086
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1352256A Active FR3003295B1 (fr) | 2013-03-14 | 2013-03-14 | Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblage |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR3003295B1 (fr) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5316437A (en) * | 1993-02-19 | 1994-05-31 | General Electric Company | Gas turbine engine structural frame assembly having a thermally actuated valve for modulating a flow of hot gases through the frame hub |
| US6227798B1 (en) * | 1999-11-30 | 2001-05-08 | General Electric Company | Turbine nozzle segment band cooling |
| US6511284B2 (en) * | 2001-06-01 | 2003-01-28 | General Electric Company | Methods and apparatus for minimizing gas turbine engine thermal stress |
| US7743613B2 (en) * | 2006-11-10 | 2010-06-29 | General Electric Company | Compound turbine cooled engine |
-
2013
- 2013-03-14 FR FR1352256A patent/FR3003295B1/fr active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3003295A1 (fr) | 2014-09-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20170717 |
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| PLFP | Fee payment |
Year of fee payment: 6 |
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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 |
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| PLFP | Fee payment |
Year of fee payment: 13 |
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| PLFP | Fee payment |
Year of fee payment: 14 |