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FR2997725B1 - Carter de turbomachine - Google Patents

Carter de turbomachine Download PDF

Info

Publication number
FR2997725B1
FR2997725B1 FR1260493A FR1260493A FR2997725B1 FR 2997725 B1 FR2997725 B1 FR 2997725B1 FR 1260493 A FR1260493 A FR 1260493A FR 1260493 A FR1260493 A FR 1260493A FR 2997725 B1 FR2997725 B1 FR 2997725B1
Authority
FR
France
Prior art keywords
turbomachine housing
turbomachine
housing
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
FR1260493A
Other languages
English (en)
Other versions
FR2997725A1 (fr
Inventor
Romain Plante
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 FR1260493A priority Critical patent/FR2997725B1/fr
Publication of FR2997725A1 publication Critical patent/FR2997725A1/fr
Application granted granted Critical
Publication of FR2997725B1 publication Critical patent/FR2997725B1/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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1260493A 2012-11-05 2012-11-05 Carter de turbomachine Active FR2997725B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1260493A FR2997725B1 (fr) 2012-11-05 2012-11-05 Carter de turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1260493A FR2997725B1 (fr) 2012-11-05 2012-11-05 Carter de turbomachine
FR1260493 2012-11-05

Publications (2)

Publication Number Publication Date
FR2997725A1 FR2997725A1 (fr) 2014-05-09
FR2997725B1 true FR2997725B1 (fr) 2018-03-02

Family

ID=47666300

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1260493A Active FR2997725B1 (fr) 2012-11-05 2012-11-05 Carter de turbomachine

Country Status (1)

Country Link
FR (1) FR2997725B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3005100B1 (fr) * 2013-04-26 2015-05-01 Snecma Carter de turbomachine
FR3092136B1 (fr) 2019-01-29 2021-10-22 Safran Aircraft Engines Carter de soufflante pour une turbomachine d’aeronef
FR3098543B1 (fr) 2019-07-10 2021-07-02 Safran Aircraft Engines Procede de fabrication d’un carter pour une turbomachine d’aeronef
US11788434B2 (en) 2019-07-15 2023-10-17 Safran Aircraft Engines Method for producing a casing for an aircraft turbine engine
FR3100834B1 (fr) 2019-09-12 2023-07-07 Safran Aircraft Engines Virole annulaire acoustique de turbomachine et procede de fabrication associe
FR3106610B1 (fr) 2020-01-29 2023-04-14 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication
FR3106612B1 (fr) 2020-01-29 2022-07-22 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication
FR3106611B1 (fr) 2020-01-29 2023-02-24 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication
FR3127014A1 (fr) 2021-09-15 2023-03-17 Safran Aircraft Engines Procede de fabrication d’un carter pour une turbomachine d’aeronef
US11753967B2 (en) * 2021-12-21 2023-09-12 Rolls-Royce Deutschland Ltd & Co Kg Fan case assembly for a gas turbine engine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
US6206631B1 (en) * 1999-09-07 2001-03-27 General Electric Company Turbomachine fan casing with dual-wall blade containment structure
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
FR2926791B1 (fr) * 2008-01-29 2010-05-28 Aircelle Sa Entree d'air pour nacelle d'aeronef, et ensemble propulsif comprenant une telle entree d'air
FR2974225B1 (fr) * 2011-04-15 2014-09-19 Snecma Structure insonorisante de type panneau acoustique notamment pour paroi interne de nacelle de turbomachine.

Also Published As

Publication number Publication date
FR2997725A1 (fr) 2014-05-09

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