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FR3072715B1 - Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures - Google Patents

Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures Download PDF

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Publication number
FR3072715B1
FR3072715B1 FR1759880A FR1759880A FR3072715B1 FR 3072715 B1 FR3072715 B1 FR 3072715B1 FR 1759880 A FR1759880 A FR 1759880A FR 1759880 A FR1759880 A FR 1759880A FR 3072715 B1 FR3072715 B1 FR 3072715B1
Authority
FR
France
Prior art keywords
thermal protection
turbomachine
casing
crankcase
protection cover
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
FR1759880A
Other languages
English (en)
Other versions
FR3072715A1 (fr
Inventor
Olivier BAZOT
Jeremy Philippe Pierre Edynak
Farhana Hussain
Fanny Marie LIBES
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1759880A priority Critical patent/FR3072715B1/fr
Priority to US16/163,814 priority patent/US10858954B2/en
Publication of FR3072715A1 publication Critical patent/FR3072715A1/fr
Application granted granted Critical
Publication of FR3072715B1 publication Critical patent/FR3072715B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F01D25/145—Thermally insulated casings
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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
    • F05D2220/3219—Application in turbines in gas turbines for a special turbine stage for a special compressor stage for the last stage of a compressor or a high pressure compressor
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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
    • F05D2240/15—Heat shield
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/231—Preventing heat transfer
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • 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)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un module (6) pour turbomachine. Le module (6) comprend un carter (20) pour turbomachine, et une enveloppe de protection thermique du carter. L'enveloppe de protection thermique est configurée pour recouvrir au moins partiellement le carter (20) pour le protéger thermiquement. Selon l'invention, le module (6) comprend une bande de protection contre l'usure (50) qui est située entre le carter (20) et l'enveloppe de protection thermique, dans une région de jonction du carter (20) et de l'enveloppe de protection thermique.
FR1759880A 2017-10-20 2017-10-20 Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures Active FR3072715B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1759880A FR3072715B1 (fr) 2017-10-20 2017-10-20 Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures
US16/163,814 US10858954B2 (en) 2017-10-20 2018-10-18 Turbo-engine housing, equipped with a thermal protection shell and an anti-wear strip

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1759880 2017-10-20
FR1759880A FR3072715B1 (fr) 2017-10-20 2017-10-20 Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures

Publications (2)

Publication Number Publication Date
FR3072715A1 FR3072715A1 (fr) 2019-04-26
FR3072715B1 true FR3072715B1 (fr) 2020-04-17

Family

ID=60450912

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1759880A Active FR3072715B1 (fr) 2017-10-20 2017-10-20 Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures

Country Status (2)

Country Link
US (1) US10858954B2 (fr)
FR (1) FR3072715B1 (fr)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4921401A (en) * 1989-02-23 1990-05-01 United Technologies Corporation Casting for a rotary machine
US5273397A (en) * 1993-01-13 1993-12-28 General Electric Company Turbine casing and radiation shield
FR2882573B1 (fr) * 2005-02-25 2007-04-13 Snecma Moteurs Sa Carter interne de turbomachine equipe d'un bouclier thermique
FR2925108B1 (fr) * 2007-12-14 2013-05-03 Snecma Module de turbomachine muni d'un dispositif d'amelioration des jeux radiaux
US10100670B2 (en) * 2013-06-14 2018-10-16 United Technologies Corporation Heatshield assembly with double lap joint for a gas turbine engine
FR3051826B1 (fr) 2016-05-25 2018-06-01 Safran Aircraft Engines Dispositif de commande d'elements a calage variable dans une turbomachine
US10371005B2 (en) * 2016-07-20 2019-08-06 United Technologies Corporation Multi-ply heat shield assembly with integral band clamp for a gas turbine engine
US10815804B2 (en) * 2017-04-04 2020-10-27 General Electric Company Turbine engine containment assembly and method for manufacturing the same
US10494116B2 (en) * 2017-07-27 2019-12-03 Rolls-Royce North American Technologies Inc. Heat shield for signature suppression system

Also Published As

Publication number Publication date
US10858954B2 (en) 2020-12-08
US20190120083A1 (en) 2019-04-25
FR3072715A1 (fr) 2019-04-26

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