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FR3011584B1 - EXTENSION OF INTERMEDIATE CASING - Google Patents

EXTENSION OF INTERMEDIATE CASING Download PDF

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Publication number
FR3011584B1
FR3011584B1 FR1359653A FR1359653A FR3011584B1 FR 3011584 B1 FR3011584 B1 FR 3011584B1 FR 1359653 A FR1359653 A FR 1359653A FR 1359653 A FR1359653 A FR 1359653A FR 3011584 B1 FR3011584 B1 FR 3011584B1
Authority
FR
France
Prior art keywords
extension
intermediate casing
casing
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
FR1359653A
Other languages
French (fr)
Other versions
FR3011584A1 (en
Inventor
Christophe Perdrigeon
Justine Emma Dubois Margaux
Eugene Henri Servant Regis
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 FR1359653A priority Critical patent/FR3011584B1/en
Publication of FR3011584A1 publication Critical patent/FR3011584A1/en
Application granted granted Critical
Publication of FR3011584B1 publication Critical patent/FR3011584B1/en
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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • 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
    • F02C7/28—Arrangement of seals

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1359653A 2013-10-04 2013-10-04 EXTENSION OF INTERMEDIATE CASING Active FR3011584B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1359653A FR3011584B1 (en) 2013-10-04 2013-10-04 EXTENSION OF INTERMEDIATE CASING

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1359653 2013-10-04
FR1359653A FR3011584B1 (en) 2013-10-04 2013-10-04 EXTENSION OF INTERMEDIATE CASING

Publications (2)

Publication Number Publication Date
FR3011584A1 FR3011584A1 (en) 2015-04-10
FR3011584B1 true FR3011584B1 (en) 2018-02-23

Family

ID=49667451

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1359653A Active FR3011584B1 (en) 2013-10-04 2013-10-04 EXTENSION OF INTERMEDIATE CASING

Country Status (1)

Country Link
FR (1) FR3011584B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3064980B1 (en) * 2017-04-05 2022-05-13 Airbus Operations Sas PROPULSION SYSTEM OF AN AIRCRAFT COMPRISING A NACELLE WITH AN IMPROVED OPENING SYSTEM
FR3067004B1 (en) * 2017-05-30 2021-04-16 Airbus Operations Sas PROPULSION SYSTEM OF AN AIRCRAFT CONTAINING A NACELLE WITH AN IMPROVED OPENING SYSTEM
FR3078109B1 (en) * 2018-02-16 2020-03-20 Safran Aircraft Engines FIRE RESISTANCE DEVICE FOR INTERPOSING BETWEEN AN UPSTREAM END OF AN AIRCRAFT TURBOMACHINE MOUNTING MAT, AND A TURBOMACHINE COVER DELIMITING AN INTER-VEIN COMPARTMENT

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2861364B1 (en) * 2003-10-22 2006-02-03 Airbus France DEVICE FOR MOUNTING A FITTING BETWEEN AN AIR INLET OF AN AIRCRAFT ENGINE AND A MAT.
FR2865002B1 (en) * 2004-01-12 2006-05-05 Snecma Moteurs DOUBLE FLOW TURBOREACTOR COMPRISING A SERVITUDE DISTRIBUTION SUPPORT AND THE SERVITUDE DISTRIBUTION SUPPORT.
FR2905991B1 (en) * 2006-09-20 2012-01-13 Snecma INTEGRATED PROPULSIVE SYSTEM COMPRISING A DOUBLE FLOW TURBOREACTOR ENGINE.
FR2920140B1 (en) * 2007-08-20 2009-10-30 Aircelle Sa NACELLE DE TURBOREACTEUR, INTENDED TO EQUIP AN AIRCRAFT
FR2925120B1 (en) * 2007-12-18 2010-02-19 Snecma INTERMEDIATE CARTER EXTENSION FOR AIRCRAFT TURBOJET ENGINE COMPRISING A SECULATED ANNULAR GROOVE OF RECEPTION OF NACELLE HOODS

Also Published As

Publication number Publication date
FR3011584A1 (en) 2015-04-10

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