FR3003303B1 - Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion - Google Patents

Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion

Info

Publication number
FR3003303B1
FR3003303B1 FR1352353A FR1352353A FR3003303B1 FR 3003303 B1 FR3003303 B1 FR 3003303B1 FR 1352353 A FR1352353 A FR 1352353A FR 1352353 A FR1352353 A FR 1352353A FR 3003303 B1 FR3003303 B1 FR 3003303B1
Authority
FR
France
Prior art keywords
turbopropulser
turbojet
turbomachine
aircraft
aircraft turbopropulser
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
FR1352353A
Other languages
English (en)
Other versions
FR3003303A1 (fr
Inventor
Romain Plante
Jeremy Galiano
Florent Rognin
Gerome Sonois
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
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
Priority to FR1352353A priority Critical patent/FR3003303B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to RU2015138543A priority patent/RU2015138543A/ru
Priority to CA2905793A priority patent/CA2905793A1/fr
Priority to US14/775,141 priority patent/US20160032834A1/en
Priority to EP14715361.3A priority patent/EP2971738A1/fr
Priority to JP2015562284A priority patent/JP2016513773A/ja
Priority to PCT/FR2014/050566 priority patent/WO2014140483A1/fr
Priority to CN201611151155.0A priority patent/CN106979040A/zh
Priority to BR112015023057A priority patent/BR112015023057A8/pt
Priority to CN201480015664.3A priority patent/CN105051360A/zh
Publication of FR3003303A1 publication Critical patent/FR3003303A1/fr
Application granted granted Critical
Publication of FR3003303B1 publication Critical patent/FR3003303B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • 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
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • 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)
FR1352353A 2013-03-15 2013-03-15 Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion Active FR3003303B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
FR1352353A FR3003303B1 (fr) 2013-03-15 2013-03-15 Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
BR112015023057A BR112015023057A8 (pt) 2013-03-15 2014-03-12 turbomáquina
US14/775,141 US20160032834A1 (en) 2013-03-15 2014-03-12 Turbine engine, such as an airplane turbofan or turboprop engine
EP14715361.3A EP2971738A1 (fr) 2013-03-15 2014-03-12 Turbomachine, telle qu'un turboréacteur ou un turbopropulseur d'avion
JP2015562284A JP2016513773A (ja) 2013-03-15 2014-03-12 航空機のターボファンまたはターボプロップエンジンなどのタービンエンジン
PCT/FR2014/050566 WO2014140483A1 (fr) 2013-03-15 2014-03-12 Turbomachine, telle qu'un turboréacteur ou un turbopropulseur d'avion
RU2015138543A RU2015138543A (ru) 2013-03-15 2014-03-12 Газотурбинный двигатель, такой как турбореактивный или турбовинтовой двигатель самолета
CA2905793A CA2905793A1 (fr) 2013-03-15 2014-03-12 Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
CN201480015664.3A CN105051360A (zh) 2013-03-15 2014-03-12 涡轮发动机，诸如航空涡扇发动机或涡轮螺旋桨发动机
CN201611151155.0A CN106979040A (zh) 2013-03-15 2014-03-12 涡轮发动机

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1352353A FR3003303B1 (fr) 2013-03-15 2013-03-15 Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion

Publications (2)

Publication Number Publication Date
FR3003303A1 FR3003303A1 (fr) 2014-09-19
FR3003303B1 true FR3003303B1 (fr) 2017-06-30

Family

ID=48225059

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1352353A Active FR3003303B1 (fr) 2013-03-15 2013-03-15 Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion

Country Status (9)

Country Link
US (1) US20160032834A1 (fr)
EP (1) EP2971738A1 (fr)
JP (1) JP2016513773A (fr)
CN (2) CN106979040A (fr)
BR (1) BR112015023057A8 (fr)
CA (1) CA2905793A1 (fr)
FR (1) FR3003303B1 (fr)
RU (1) RU2015138543A (fr)
WO (1) WO2014140483A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3059362B1 (fr) 2016-11-30 2021-01-01 Safran Aircraft Engines Carter de turbomachine comportant une structure acoustique et un element abradable
US10662813B2 (en) 2017-04-13 2020-05-26 General Electric Company Turbine engine and containment assembly for use in a turbine engine
US10458281B2 (en) 2017-06-12 2019-10-29 United Technologies Corporation Resilient mounting assembly for a turbine engine
FR3068007B1 (fr) * 2017-06-23 2021-07-16 Safran Nacelles Dispositif de traitement acoustique pour nacelle de turboreacteur d'aeronef
CN107795557B (zh) * 2017-11-10 2020-02-14 中国航发航空科技股份有限公司 一种用于发动机转子叶片榫头的粘胶成型装置及粘胶方法
FR3085447B1 (fr) * 2018-09-04 2020-09-11 Safran Aircraft Engines Carter de soufflante pour une turbomachine d'aeronef integrant directement des portions abradable et ayant des proprietes acoustiques
FR3086785B1 (fr) * 2018-09-28 2022-01-21 Airbus Operations Sas Ensemble comportant deux panneaux acoustiques juxtaposes dans lequel les panneaux comportent une face resistive qui s'etend jusqu'a une paroi d'extremite
FR3095025B1 (fr) * 2019-04-12 2021-03-05 Safran Aircraft Engines Joint d’étanchéité à labyrinthe comportant un élément abradable à densité variable de cellules
JP7445822B2 (ja) 2021-03-31 2024-03-07 川崎重工業株式会社 ターボファンエンジンのファンケースアッセンブリ

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1260493A (fr) 1959-07-17
FR1260495A (fr) 1960-06-23 1961-05-05 Thomson Houston Comp Francaise Perfectionnements aux machines électriques
US5482429A (en) * 1994-04-29 1996-01-09 United Technologies Corporation Fan blade containment assembly
US5662757A (en) * 1994-10-17 1997-09-02 General Electric Company Method of removing an abradable shroud assembly for turbomachinery
US5776579A (en) * 1996-03-28 1998-07-07 The Boeing Company Structural bonding with encapsulated foaming adhesive
US6364603B1 (en) * 1999-11-01 2002-04-02 Robert P. Czachor Fan case for turbofan engine having a fan decoupler
GB0119608D0 (en) * 2001-08-11 2001-10-03 Rolls Royce Plc A guide vane assembly
US6619913B2 (en) * 2002-02-15 2003-09-16 General Electric Company Fan casing acoustic treatment
US6652222B1 (en) * 2002-09-03 2003-11-25 Pratt & Whitney Canada Corp. Fan case design with metal foam between Kevlar
GB2407343B (en) * 2003-10-22 2006-04-19 Rolls Royce Plc An acoustic liner for a gas turbine engine casing
FR2866074B1 (fr) * 2004-02-11 2006-04-28 Snecma Moteurs Architecture d'un turboreacteur ayant une double soufflante a l'avant
FR2866387B1 (fr) * 2004-02-12 2008-03-14 Snecma Moteurs Adaptation aerodynamique de la soufflante arriere d'un turboreacteur double soufflante
FR2931205B1 (fr) * 2008-05-16 2010-05-14 Aircelle Sa Ensemble propulsif pour aeronef, et structure d'entree d'air pour un tel ensemble
GB2478144A (en) * 2010-02-26 2011-08-31 Rolls Royce Plc Panelled assembly, eg for a gas turbine engine ducted fan casing
FR2975943B1 (fr) * 2011-06-01 2013-05-17 Aircelle Sa Procede de fabrication d'un panneau d'attenuation acoustique
FR2979385A1 (fr) * 2011-08-22 2013-03-01 Snecma Panneau d'isolation acoustique pour turbomachine et turbomachine comportant un tel panneau
US9194299B2 (en) * 2012-12-21 2015-11-24 United Technologies Corporation Anti-torsion assembly

Also Published As

Publication number Publication date
US20160032834A1 (en) 2016-02-04
BR112015023057A2 (pt) 2017-07-18
CA2905793A1 (fr) 2014-09-18
CN106979040A (zh) 2017-07-25
BR112015023057A8 (pt) 2019-12-03
CN105051360A (zh) 2015-11-11
WO2014140483A1 (fr) 2014-09-18
RU2015138543A (ru) 2017-04-19
EP2971738A1 (fr) 2016-01-20
JP2016513773A (ja) 2016-05-16
FR3003303A1 (fr) 2014-09-19

Similar Documents

Publication Publication Date Title
FR2989426B1 (fr) Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
FR3003303B1 (fr) Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
EP3548709A4 (fr) Système de lavage de moteur de turbine à gaz
EP3004597A4 (fr) Composant de moteur à turbine à gaz possédant des bandes de déclenchement
FR3021358B1 (fr) Boite d'engrenages de turbomachine d'aeronef
EP3108106A4 (fr) Surface portante de moteur à turbine à gaz
EP3108113A4 (fr) Profil aérodynamique de turbine à gaz
GB201511454D0 (en) Aircraft engine nacelle
FR3005453B1 (fr) Nacelle de turboreacteur d'aeronef
EP3108123A4 (fr) Surface portante de moteur à turbine à gaz
EP2860402A4 (fr) Turbomachines
EP3108116A4 (fr) Profil aérodynamique de moteur à turbine à gaz
EP3022400A4 (fr) Aubes de turbine à congés de raccordement variables
EP3510254A4 (fr) Système de lavage pour moteur à turbine à gaz
EP3108114A4 (fr) Surface portante pour turbine à gaz
EP3108118A4 (fr) Surface portante de moteur à turbine à gaz
EP3108104A4 (fr) Surface portante de moteur à turbine à gaz
EP3108110A4 (fr) Surface portante pour turbine à gaz
GB2544869B (en) Turbojet engine with offset fans with a differential system
EP3114321A4 (fr) Profil aérodynamique de moteur à turbine à gaz
EP3509766A4 (fr) Système de lavage de moteur de turbine à gaz
EP3126638A4 (fr) Surface portante de moteur à turbine à gaz
EP3108109A4 (fr) Profil aérodynamique de moteur à turbine à gaz
GB2558071B (en) Turbine for turbine engine
FR3015594B1 (fr) Compresseur de turbomachine, en particulier de turbopropulseur ou de turboreacteur d'avion

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170717

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13