FR3014945B1 - Carter d'echappement logeant un etage de turbine pour turbomachine - Google Patents

Carter d'echappement logeant un etage de turbine pour turbomachine Download PDF

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Publication number
FR3014945B1
FR3014945B1 FR1362675A FR1362675A FR3014945B1 FR 3014945 B1 FR3014945 B1 FR 3014945B1 FR 1362675 A FR1362675 A FR 1362675A FR 1362675 A FR1362675 A FR 1362675A FR 3014945 B1 FR3014945 B1 FR 3014945B1
Authority
FR
France
Prior art keywords
turbomachine
turbine
downstream
exhaust case
turbine floor
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
FR1362675A
Other languages
English (en)
Other versions
FR3014945A1 (fr
Inventor
Guy Vieillefond
Pascal Bontaz
Devradj Gustave
Jerome Lebegue
Didier Mattard
Helene Namer
Miguel Palazuelos
Sebastien PRESTEL
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1362675A priority Critical patent/FR3014945B1/fr
Publication of FR3014945A1 publication Critical patent/FR3014945A1/fr
Application granted granted Critical
Publication of FR3014945B1 publication Critical patent/FR3014945B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F05D2220/3215—Application in turbines in gas turbines for a special turbine stage the last stage of the turbine
    • 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
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Abstract

L'invention concerne un ensemble pour turbomachine comprenant une partie aval de turbine (10) et un carter d'échappement (40) situé en aval de la partie aval de turbine (10), la partie aval de turbine (10) comprenant un carter de turbine (30). Le carter d'échappement (40) comprend une virole externe (400) et au moins une chape de fixation (48) du carter d'échappement (40) à un mât d'accrochage de turbomachine. Selon l'invention, une portion amont (410) de la virole externe (400) loge au moins une partie d'un dernier étage de turbine (10) de la partie aval de turbine (10).
FR1362675A 2013-12-16 2013-12-16 Carter d'echappement logeant un etage de turbine pour turbomachine Active FR3014945B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1362675A FR3014945B1 (fr) 2013-12-16 2013-12-16 Carter d'echappement logeant un etage de turbine pour turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1362675 2013-12-16
FR1362675A FR3014945B1 (fr) 2013-12-16 2013-12-16 Carter d'echappement logeant un etage de turbine pour turbomachine

Publications (2)

Publication Number Publication Date
FR3014945A1 FR3014945A1 (fr) 2015-06-19
FR3014945B1 true FR3014945B1 (fr) 2019-03-15

Family

ID=50137876

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1362675A Active FR3014945B1 (fr) 2013-12-16 2013-12-16 Carter d'echappement logeant un etage de turbine pour turbomachine

Country Status (1)

Country Link
FR (1) FR3014945B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3134410B1 (fr) * 2022-04-11 2024-07-19 Safran Aircraft Engines Ensemble pour turbine et turbomachine associée

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6684626B1 (en) * 2002-07-30 2004-02-03 General Electric Company Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
US7195447B2 (en) * 2004-10-29 2007-03-27 General Electric Company Gas turbine engine and method of assembling same
EP2330274A1 (fr) * 2009-12-03 2011-06-08 Siemens Aktiengesellschaft Turbine et son procédé de fonctionnement

Also Published As

Publication number Publication date
FR3014945A1 (fr) 2015-06-19

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