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FR3015569B1 - Carter pour un ensemble propulsif - Google Patents

Carter pour un ensemble propulsif Download PDF

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Publication number
FR3015569B1
FR3015569B1 FR1362957A FR1362957A FR3015569B1 FR 3015569 B1 FR3015569 B1 FR 3015569B1 FR 1362957 A FR1362957 A FR 1362957A FR 1362957 A FR1362957 A FR 1362957A FR 3015569 B1 FR3015569 B1 FR 3015569B1
Authority
FR
France
Prior art keywords
carter
propulsive assembly
panels
casing
propulsive
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
FR1362957A
Other languages
English (en)
Other versions
FR3015569A1 (fr
Inventor
Edmond Fert Jeremy
Julien Pavillet
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 FR1362957A priority Critical patent/FR3015569B1/fr
Priority to CA2875044A priority patent/CA2875044C/fr
Priority to US14/576,694 priority patent/US9981751B2/en
Publication of FR3015569A1 publication Critical patent/FR3015569A1/fr
Application granted granted Critical
Publication of FR3015569B1 publication Critical patent/FR3015569B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • 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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • 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
    • F05D2230/72—Maintenance
    • 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
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

Ensemble propulsif d'aéronef, comportant un moteur et une nacelle comprenant un carter(16) de révolution délimitant une veine d'écoulement d'un flux d'air, caractérisé en ce que ce carter comporte au moins deux ouvertures obturées par des panneaux (18) amovibles et interchangeables, au moins l'un de ces panneaux portant un équipement (24) de l'ensemble propulsif.
FR1362957A 2013-12-19 2013-12-19 Carter pour un ensemble propulsif Active FR3015569B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1362957A FR3015569B1 (fr) 2013-12-19 2013-12-19 Carter pour un ensemble propulsif
CA2875044A CA2875044C (fr) 2013-12-19 2014-12-11 Carter pour un ensemble propulsif
US14/576,694 US9981751B2 (en) 2013-12-19 2014-12-19 Casing for a propulsion unit

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1362957A FR3015569B1 (fr) 2013-12-19 2013-12-19 Carter pour un ensemble propulsif
FR1362957 2013-12-19

Publications (2)

Publication Number Publication Date
FR3015569A1 FR3015569A1 (fr) 2015-06-26
FR3015569B1 true FR3015569B1 (fr) 2019-01-25

Family

ID=50231378

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1362957A Active FR3015569B1 (fr) 2013-12-19 2013-12-19 Carter pour un ensemble propulsif

Country Status (3)

Country Link
US (1) US9981751B2 (fr)
CA (1) CA2875044C (fr)
FR (1) FR3015569B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10072584B2 (en) * 2013-12-03 2018-09-11 United Technologies Corporation Multi-bypass stream gas turbine engine with enlarged bypass flow area
US10125684B2 (en) 2015-12-29 2018-11-13 Pratt & Whitney Canada Corp. Surface cooler for aero engine
US11090600B2 (en) * 2017-01-04 2021-08-17 General Electric Company Particle separator assembly for a turbine engine
FR3078947B1 (fr) * 2018-03-13 2020-03-13 Airbus Operations Systeme de propulsion d'un aeronef comportant un turboreacteur double flux et un systeme de prelevement d'air a encombrement reduit
FR3081926B1 (fr) 2018-05-30 2021-01-15 Safran Aircraft Engines Embouchure d'un conduit de gaz chaud de moteur d'aeronef a travers une paroi du moteur
FR3085438B1 (fr) 2018-08-30 2021-01-22 Safran Aircraft Engines Embouchure d'ejection d'un gaz chaud a travers une paroi de moteur d'aeronef
FR3087840B1 (fr) 2018-10-29 2021-01-08 Safran Aircraft Engines Capot de nacelle pour ensemble propulsif d'aeronef
FR3097898B1 (fr) * 2019-06-26 2021-06-25 Safran Aircraft Engines Dechargement d’une veine d’un ensemble propulsif pour reduire le battement des aubes d’une soufflante
US20250043695A1 (en) * 2023-07-31 2025-02-06 Rolls-Royce North American Technologies Inc. Thermally compliant flange joint for use with gas turbine engine components

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2865001B1 (fr) * 2004-01-12 2008-05-09 Snecma Moteurs Turboreacteur comprenant un bras de raccord de servitudes, et le bras de raccord de servitudes.
FR2866070B1 (fr) * 2004-02-05 2008-12-05 Snecma Moteurs Turboreacteur a fort taux de dilution
FR2880920B1 (fr) 2005-01-20 2007-07-06 Snecma Moteurs Sa Turbomoteur a double corps avec des moyens d'entrainement du boitier d'accessoires
FR2891313A1 (fr) * 2005-09-26 2007-03-30 Airbus France Sas Turbomoteur a double flux pourvu d'un prerefroidisseur
US7607308B2 (en) 2005-12-08 2009-10-27 General Electric Company Shrouded turbofan bleed duct
FR2902830B1 (fr) * 2006-06-27 2008-08-08 Airbus France Sas Turboreacteur pour aeronef
US7861512B2 (en) * 2006-08-29 2011-01-04 Pratt & Whitney Canada Corp. Turbofan bypass duct air cooled fluid cooler installation
FR2905975B1 (fr) * 2006-09-20 2008-12-05 Snecma Sa Conduite de soufflante pour une turbomachine.
US8714923B2 (en) * 2007-03-23 2014-05-06 Ogin, Inc. Fluid turbine
EP2128023B1 (fr) * 2008-05-29 2012-05-23 Pratt & Whitney Canada Corp. Un moteur à turbine à gaz comprenant un ensemble refroidisseur
DE102009011635A1 (de) * 2009-03-04 2010-09-09 Rolls-Royce Deutschland Ltd & Co Kg Luftleitelement eines Laufspalteinstellungssystems einer Fluggasturbine
FR2948636B1 (fr) * 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
US8529195B2 (en) * 2010-10-12 2013-09-10 General Electric Company Inducer for gas turbine system
US9267390B2 (en) * 2012-03-22 2016-02-23 Honeywell International Inc. Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine
EP3084183B1 (fr) * 2013-12-18 2019-07-10 United Technologies Corporation Ensemble de commande d'écoulement d'échangeur de chaleur et procédé correspondant

Also Published As

Publication number Publication date
CA2875044A1 (fr) 2015-06-19
CA2875044C (fr) 2022-07-19
US20150175269A1 (en) 2015-06-25
US9981751B2 (en) 2018-05-29
FR3015569A1 (fr) 2015-06-26

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