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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 ROTOR

Info

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
Application number
FR1261773A
Other languages
French (fr)
Other versions
FR2999249A1 (en
Inventor
Christophe Scholtes
Antoine Robert Alain Brunet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR1261773A priority Critical patent/FR2999249B1/en
Publication of FR2999249A1 publication Critical patent/FR2999249A1/en
Application granted granted Critical
Publication of FR2999249B1 publication Critical patent/FR2999249B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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

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)

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.

FR1261773A 2012-12-07 2012-12-07 COMPRESSOR FOR TURBOMACHINE WITH COOLING MEANS FOR A ROTATING SEAL ENSURING SEALING BETWEEN A RECTIFIER AND A ROTOR Active FR2999249B1 (en)

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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106930982A (en) * 2015-11-16 2017-07-07 通用电气公司 Gas turbine engine with guide vanes with cooling inlets

Families Citing this family (5)

* Cited by examiner, † Cited by third party
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
FR3117532B1 (en) 2020-12-10 2024-05-24 Safran Aircraft Engines Turbine blade for an aircraft turbomachine, provided with a primary flow ejection channel towards an inter-lip cavity
FR3133063B1 (en) * 2022-02-25 2024-08-02 Safran Aircraft Engines Turbomachine blading, comprising a blade and a platform which has an internal flow suction and ejection channel.
FR3145585B1 (en) 2023-02-06 2025-01-10 Safran Aircraft Engines RECTIFIER BLADE FOR TURBOMACHINE COMPRESSOR, ASSOCIATED COMPRESSOR AND TURBOMACHINE
CN117905537B (en) * 2024-02-06 2025-05-06 中国航发湖南动力机械研究所 Injection cooling structure and engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6471216B1 (en) * 1999-05-24 2002-10-29 General Electric Company Rotating seal
JP2005513329A (en) * 2001-12-13 2005-05-12 アルストム テクノロジー リミテッド Sealed structure for turbine engine components
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106930982A (en) * 2015-11-16 2017-07-07 通用电气公司 Gas turbine engine with guide vanes with cooling inlets
CN106930982B (en) * 2015-11-16 2019-04-16 通用电气公司 Gas turbine engine with vanes with cooling inlet

Also Published As

Publication number Publication date
FR2999249A1 (en) 2014-06-13

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