FR2999249B1 - COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR - Google Patents
COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTORInfo
- Publication number
- FR2999249B1 FR2999249B1 FR1261773A FR1261773A FR2999249B1 FR 2999249 B1 FR2999249 B1 FR 2999249B1 FR 1261773 A FR1261773 A FR 1261773A FR 1261773 A FR1261773 A FR 1261773A FR 2999249 B1 FR2999249 B1 FR 2999249B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- rectifier
- compressor
- rotor
- cooling means
- 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
- 238000007789 sealing Methods 0.000 title abstract 4
- 238000001816 cooling Methods 0.000 abstract 3
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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/545—Ducts
-
- 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
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/321—Application in turbines in gas turbines for a special turbine stage
- F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
-
- 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
Abstract
L'invention concerne le refroidissement d'une nervure d'étanchéité (36a, 36b) d'un joint tournant (30) assurant l'étanchéité entre un arbre de rotor (18) et un redresseur (24) dans un compresseur axial (10) de turbomachine. L'invention propose à cet effet des moyens de canalisation d'air (48) aptes à prélever de l'air de refroidissement en aval du redresseur (24) et capables d'injecter cet air de refroidissement de sorte que ce dernier baigne un flanc de la nervure d'étanchéité.The invention relates to cooling a sealing rib (36a, 36b) of a rotary joint (30) sealing between a rotor shaft (18) and a stator (24) in an axial compressor (10). ) turbomachine. The invention provides for this purpose air ducting means (48) capable of taking cooling air downstream of the rectifier (24) and capable of injecting this cooling air so that the latter bathes a sidewall. of the sealing rib.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1261773A FR2999249B1 (en) | 2012-12-07 | 2012-12-07 | COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1261773A FR2999249B1 (en) | 2012-12-07 | 2012-12-07 | COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2999249A1 FR2999249A1 (en) | 2014-06-13 |
FR2999249B1 true FR2999249B1 (en) | 2015-01-09 |
Family
ID=47714358
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1261773A Active FR2999249B1 (en) | 2012-12-07 | 2012-12-07 | COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2999249B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106930982A (en) * | 2015-11-16 | 2017-07-07 | 通用电气公司 | Band has the gas-turbine unit of the stator of cooling entrance |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3085405B1 (en) * | 2018-08-28 | 2020-12-04 | Safran Aircraft Engines | PRESSURIZATION OF THE INTER-LECHETTES CAVITY BY DERIVATION OF THE BYPASS FLOW |
FR3117532A1 (en) * | 2020-12-10 | 2022-06-17 | Safran Aircraft Engines | Turbine blade for an aircraft turbomachine, provided with a primary flow ejection channel towards an inter-sealer cavity |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6471216B1 (en) * | 1999-05-24 | 2002-10-29 | General Electric Company | Rotating seal |
EP1456507B1 (en) * | 2001-12-13 | 2013-05-01 | Alstom Technology Ltd | Sealing assembly for components of a turbo-engine |
FR2926612B1 (en) * | 2008-01-23 | 2012-12-28 | Snecma | ROTOR DRUM FOR A TURBOMACHINE |
DE102008011746A1 (en) * | 2008-02-28 | 2009-09-03 | Mtu Aero Engines Gmbh | Device and method for diverting a leakage current |
-
2012
- 2012-12-07 FR FR1261773A patent/FR2999249B1/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106930982A (en) * | 2015-11-16 | 2017-07-07 | 通用电气公司 | Band has the gas-turbine unit of the stator of cooling entrance |
CN106930982B (en) * | 2015-11-16 | 2019-04-16 | 通用电气公司 | Band has the gas-turbine unit of the guide vane of cooling entrance |
Also Published As
Publication number | Publication date |
---|---|
FR2999249A1 (en) | 2014-06-13 |
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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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Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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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: 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 |