FR2926612B1 - ROTOR DRUM FOR A TURBOMACHINE - Google Patents
ROTOR DRUM FOR A TURBOMACHINEInfo
- Publication number
- FR2926612B1 FR2926612B1 FR0800337A FR0800337A FR2926612B1 FR 2926612 B1 FR2926612 B1 FR 2926612B1 FR 0800337 A FR0800337 A FR 0800337A FR 0800337 A FR0800337 A FR 0800337A FR 2926612 B1 FR2926612 B1 FR 2926612B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- rotor drum
- drum
- rotor
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/10—Shaft sealings
- F04D29/102—Shaft sealings especially adapted for elastic fluid pumps
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
- F01D11/127—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 with a deformable or crushable structure, e.g. honeycomb
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine
-
- 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)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0800337A FR2926612B1 (en) | 2008-01-23 | 2008-01-23 | ROTOR DRUM FOR A TURBOMACHINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0800337A FR2926612B1 (en) | 2008-01-23 | 2008-01-23 | ROTOR DRUM FOR A TURBOMACHINE |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2926612A1 FR2926612A1 (en) | 2009-07-24 |
| FR2926612B1 true FR2926612B1 (en) | 2012-12-28 |
Family
ID=39708176
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR0800337A Active FR2926612B1 (en) | 2008-01-23 | 2008-01-23 | ROTOR DRUM FOR A TURBOMACHINE |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2926612B1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109611160A (en) * | 2018-12-26 | 2019-04-12 | 北京航空航天大学 | The rotating parts are fluid-tight "horseshoe" grate teeth |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8328507B2 (en) * | 2009-05-15 | 2012-12-11 | United Technologies Corporation | Knife edge seal assembly |
| FR2999249B1 (en) * | 2012-12-07 | 2015-01-09 | Snecma | COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR |
| CN103422913A (en) * | 2013-08-29 | 2013-12-04 | 哈尔滨工程大学 | Turbine with honeycomb inner-wall casing |
| RU2712560C2 (en) * | 2014-10-15 | 2020-01-29 | Сафран Серамикс | Rotary assembly for turbine engine comprising self-supporting rotor casing |
| US10794208B2 (en) | 2015-07-08 | 2020-10-06 | Raytheon Technologies Corporation | Non-contact seal assembly for rotational equipment with linkage between adjacent rotors |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2973938A (en) * | 1958-08-18 | 1961-03-07 | Gen Electric | Cooling means for a multi-stage turbine |
| US3056579A (en) * | 1959-04-13 | 1962-10-02 | Gen Electric | Rotor construction |
| FR2600377B1 (en) * | 1986-06-18 | 1988-09-02 | Snecma | DEVICE FOR MONITORING THE COOLING AIR FLOWS OF AN ENGINE TURBINE |
| US5232339A (en) * | 1992-01-28 | 1993-08-03 | General Electric Company | Finned structural disk spacer arm |
| FR2825748B1 (en) * | 2001-06-07 | 2003-11-07 | Snecma Moteurs | TURBOMACHINE ROTOR ARRANGEMENT WITH TWO BLADE DISCS SEPARATED BY A SPACER |
-
2008
- 2008-01-23 FR FR0800337A patent/FR2926612B1/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109611160A (en) * | 2018-12-26 | 2019-04-12 | 北京航空航天大学 | The rotating parts are fluid-tight "horseshoe" grate teeth |
| CN109611160B (en) * | 2018-12-26 | 2020-08-11 | 北京航空航天大学 | Fluid-tight 'horseshoe' comb tooth of rotating part |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2926612A1 (en) | 2009-07-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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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| CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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| PLFP | Fee payment |
Year of fee payment: 13 |
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| PLFP | Fee payment |
Year of fee payment: 14 |
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| PLFP | Fee payment |
Year of fee payment: 15 |
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| PLFP | Fee payment |
Year of fee payment: 16 |
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| PLFP | Fee payment |
Year of fee payment: 17 |
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| PLFP | Fee payment |
Year of fee payment: 18 |