RU2450130C2 - Способ изготовления корпуса газовой турбины из композиционного материала и корпус, полученный таким способом - Google Patents
Способ изготовления корпуса газовой турбины из композиционного материала и корпус, полученный таким способом Download PDFInfo
- Publication number
- RU2450130C2 RU2450130C2 RU2008106944/02A RU2008106944A RU2450130C2 RU 2450130 C2 RU2450130 C2 RU 2450130C2 RU 2008106944/02 A RU2008106944/02 A RU 2008106944/02A RU 2008106944 A RU2008106944 A RU 2008106944A RU 2450130 C2 RU2450130 C2 RU 2450130C2
- Authority
- RU
- Russia
- Prior art keywords
- housing
- profile
- reinforcing fiber
- fibrous structure
- gas turbine
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 10
- 239000002131 composite material Substances 0.000 title claims description 13
- 239000012783 reinforcing fiber Substances 0.000 claims abstract description 15
- 239000011159 matrix material Substances 0.000 claims abstract description 10
- 238000009941 weaving Methods 0.000 claims description 32
- 238000004519 manufacturing process Methods 0.000 claims description 12
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 238000004804 winding Methods 0.000 description 20
- 239000000835 fiber Substances 0.000 description 14
- 239000004744 fabric Substances 0.000 description 8
- 229920005989 resin Polymers 0.000 description 6
- 239000011347 resin Substances 0.000 description 6
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 238000005336 cracking Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000000805 composite resin Substances 0.000 description 2
- 239000000356 contaminant Substances 0.000 description 2
- 230000032798 delamination Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005470 impregnation Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- XQUPVDVFXZDTLT-UHFFFAOYSA-N 1-[4-[[4-(2,5-dioxopyrrol-1-yl)phenyl]methyl]phenyl]pyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C(C=C1)=CC=C1CC1=CC=C(N2C(C=CC2=O)=O)C=C1 XQUPVDVFXZDTLT-UHFFFAOYSA-N 0.000 description 1
- 229910001094 6061 aluminium alloy Inorganic materials 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 239000004642 Polyimide Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000021715 photosynthesis, light harvesting Effects 0.000 description 1
- 229920003192 poly(bis maleimide) Polymers 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Images
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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/748—Machines or parts thereof not otherwise provided for
- B29L2031/7504—Turbines
-
- 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
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Woven Fabrics (AREA)
- Moulding By Coating Moulds (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0753449 | 2007-02-23 | ||
| FR0753449A FR2913053B1 (fr) | 2007-02-23 | 2007-02-23 | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2008106944A RU2008106944A (ru) | 2009-08-27 |
| RU2450130C2 true RU2450130C2 (ru) | 2012-05-10 |
Family
ID=38480544
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008106944/02A RU2450130C2 (ru) | 2007-02-23 | 2008-02-22 | Способ изготовления корпуса газовой турбины из композиционного материала и корпус, полученный таким способом |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8322971B2 (enExample) |
| EP (1) | EP1961923B1 (enExample) |
| JP (1) | JP5496461B2 (enExample) |
| CN (1) | CN101249725B (enExample) |
| CA (1) | CA2621729C (enExample) |
| ES (1) | ES2384898T3 (enExample) |
| FR (1) | FR2913053B1 (enExample) |
| RU (1) | RU2450130C2 (enExample) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2611914C2 (ru) * | 2014-04-10 | 2017-03-01 | Сафран Аэро Бустерс Са | Осевая турбомашина и корпус из композиционного материала для осевой турбомашины |
| RU2632352C2 (ru) * | 2012-08-03 | 2017-10-04 | Снекма | Способ неразрушающего контроля заготовки лопатки |
| RU2752691C2 (ru) * | 2017-04-13 | 2021-07-29 | Сафран | Способ изготовления детали из композиционного материала, содержащей корпус, продолженный усиленным крепежным концом |
Families Citing this family (115)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2939153B1 (fr) * | 2008-11-28 | 2011-12-09 | Snecma Propulsion Solide | Realisation d'une structure fibreuse a epaisseur evolutive par tissage 3d |
| GB2466793B (en) * | 2009-01-07 | 2011-11-09 | Ge Aviat Systems Ltd | Composite spars |
| FR2945573B1 (fr) * | 2009-05-12 | 2014-06-27 | Snecma | Mandrin pour la fabrication d'un carter en materiau composite pour une turbine a gaz. |
| FR2957093B1 (fr) * | 2010-03-02 | 2012-03-23 | Snecma | Preforme fibreuse pour un secteur d'anneau de turbine et son procede de fabrication. |
| FR2958875B1 (fr) | 2010-04-20 | 2017-07-07 | Snecma | Dispositif de fabrication d'un carter en materiau composite et procede de fabrication mettant en oeuvre un tel dispositif |
| FR2961740B1 (fr) * | 2010-06-25 | 2014-03-07 | Snecma | Procede de fabrication d'un article en materiau composite |
| WO2012007682A1 (fr) * | 2010-07-12 | 2012-01-19 | Snecma | Procede de realisation d'une piece massive |
| US8986797B2 (en) * | 2010-08-04 | 2015-03-24 | General Electric Company | Fan case containment system and method of fabrication |
| FR2965202B1 (fr) * | 2010-09-28 | 2012-10-12 | Snecma | Procede de fabrication d'une piece et piece massive composite obtenue par ce procede |
| US20120082541A1 (en) * | 2010-09-30 | 2012-04-05 | Enzo Macchia | Gas turbine engine casing |
| FR2966508B1 (fr) | 2010-10-22 | 2015-04-03 | Snecma | Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication |
| FR2970266B1 (fr) | 2011-01-10 | 2013-12-06 | Snecma | Procede de fabrication d'une piece metallique annulaire monobloc a insert de renfort en materiau composite, et piece obtenue |
| FR2970715B1 (fr) * | 2011-01-21 | 2014-10-17 | Snecma | Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant |
| FR2972129B1 (fr) * | 2011-03-03 | 2013-04-12 | Snecma | Piece en materiau composite comportant des elements de bossage |
| GB201103583D0 (en) * | 2011-03-03 | 2011-04-13 | Rolls Royce Plc | Fan casing for a turbofan engine |
| FR2972661B1 (fr) * | 2011-03-15 | 2013-04-12 | Snecma | Procede pour fabriquer une piece metallique de revolution monobloc a partir de structures fibreuses composites |
| FR2974026B1 (fr) | 2011-04-13 | 2014-09-19 | Snecma | Machine d'enroulement d'une texture fibreuse sur un mandrin d'impregnation |
| FR2974027B1 (fr) | 2011-04-13 | 2014-09-26 | Snecma | Dispositif de compactage pour machine d'enroulement d'une texture fibreuse sur un mandrin d'impregnation |
| FR2975735A1 (fr) * | 2011-05-27 | 2012-11-30 | Snecma | Carter de soufflante de turbomachine et procede pour sa fabrication |
| US9909505B2 (en) | 2011-07-05 | 2018-03-06 | United Technologies Corporation | Efficient, low pressure ratio propulsor for gas turbine engines |
| US9506422B2 (en) | 2011-07-05 | 2016-11-29 | United Technologies Corporation | Efficient, low pressure ratio propulsor for gas turbine engines |
| FR2977827B1 (fr) | 2011-07-13 | 2015-03-13 | Snecma | Procede de fabrication d'un carter de soufflante de turbomachine muni de revetements abradable et acoustique |
| FR2978692B1 (fr) | 2011-08-04 | 2013-09-06 | Snecma | Dispositif pour l'aide a la decoupe d'une couche de texture fibreuse enroulee sur un mandrin d'impregnation d'une machine d'enroulement |
| FR2979575B1 (fr) | 2011-09-05 | 2013-09-20 | Snecma | Procede et dispositif de fabrication d'une piece cylindrique en materiau composite |
| FR2981000B1 (fr) | 2011-10-06 | 2013-11-29 | Snecma | Dispositif pour la fabrication d'une piece en materiau composite |
| FR2981881B1 (fr) * | 2011-10-26 | 2013-12-13 | Snecma | Dispositif de maintien d'une texture fibreuse sur un mandrin d'impregnation d'une machine d'enroulement |
| BR112014010039B1 (pt) | 2011-10-26 | 2020-09-01 | Snecma | Mandril de impregnação para a realização de cárteres de turbina a gás em material compósito, máquina de enrolamento de uma textura fibrosa em um mandril de impregnação e método de impregnação de uma textura fibrosa para a realização de cárteres de turbina a gás em material compósito |
| BR112014009733B1 (pt) | 2011-10-26 | 2020-04-07 | Snecma | mandril de impregnação para a fabricação de um cárter de turbina a gás em material compósito e máquina de enrolamento de uma textura fibrosa em um mandril de impregnação |
| US9827639B2 (en) | 2012-02-03 | 2017-11-28 | Snecma | Method and system for attaching a piece of equipment to a structure made from composite material |
| FR2986582B1 (fr) | 2012-02-06 | 2014-03-14 | Snecma | Carter de soufflante pour moteur a turbine a gaz munie d'une bride pour la fixation d'equipements |
| US9050769B2 (en) | 2012-04-13 | 2015-06-09 | General Electric Company | Pre-form ceramic matrix composite cavity and method of forming and method of forming a ceramic matrix composite component |
| WO2013191070A1 (ja) * | 2012-06-21 | 2013-12-27 | 川崎重工業株式会社 | 航空機用エンジンのファンケース |
| US20140003923A1 (en) * | 2012-07-02 | 2014-01-02 | Peter Finnigan | Functionally graded composite fan containment case |
| FR2993317B1 (fr) | 2012-07-16 | 2014-08-15 | Snecma | Carter de turbomachine dans un materiau composite et procede de fabrication associe |
| FR2995038B1 (fr) * | 2012-08-30 | 2014-09-19 | Snecma | Carter de soufflante de turbine a gaz ayant une ceinture de fixation d'equipements |
| FR2995555B1 (fr) | 2012-09-17 | 2017-11-24 | Snecma | Machine d'enroulement d'une texture fibreuse permettant un controle d'alignement et de decadrage par analyse d'image |
| US9833930B2 (en) | 2012-10-23 | 2017-12-05 | Albany Engineered Composites, Inc. | Circumferential stiffeners for composite fancases |
| WO2014200571A2 (en) | 2013-02-19 | 2014-12-18 | United Technologies Corporation | Composite attachment structure with 3d weave |
| FR3002750B1 (fr) | 2013-03-01 | 2015-04-10 | Safran | Moule d'injection pour la fabrication d'une piece de revolution en materiau composite ayant des brides externes, et notamment d'un carter de turbine a gaz |
| FR3005159B1 (fr) | 2013-04-26 | 2015-05-15 | Snecma | Procedure de mesure de l'epaisseur d'une texture fibreuse enroulee sur un mandrin d'impregnation et machine d'enroulement mettant en œuvre un tel procede |
| FR3005042B1 (fr) | 2013-04-26 | 2016-01-01 | Snecma | Machine a tisser ou enrouler une texture fibreuse permettant un controle d'anomalies par analyse d'images |
| ITFI20130100A1 (it) * | 2013-05-03 | 2014-11-04 | Nuovo Pignone Srl | "composite material inlet plenum and gas turbine engine system comprising said plenum" |
| EP2821595B1 (fr) * | 2013-07-03 | 2025-05-21 | Safran Aero Boosters SA | Secteur d'aubes statorique à fixation mixte pour turbomachine axiale |
| FR3011253B1 (fr) * | 2013-10-01 | 2016-06-10 | Snecma | Structure fibreuse avec regroupement des flottes |
| FR3012516B1 (fr) * | 2013-10-30 | 2018-01-05 | Safran Aircraft Engines | Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant |
| EP2883688B1 (fr) * | 2013-12-13 | 2021-09-22 | Safran Aero Boosters SA | Carter annulaire composite de compresseur de turbomachine et procédé d'obtention de celui-ci |
| FR3015593B1 (fr) | 2013-12-20 | 2018-09-07 | Safran Aircraft Engines | Carter en materiau composite a matrice organique favorisant l'evacuation des fumees |
| FR3016187B1 (fr) * | 2014-01-09 | 2016-01-01 | Snecma | Protection contre le feu d'un carter de soufflante en materiau composite |
| FR3016188B1 (fr) | 2014-01-09 | 2016-01-01 | Snecma | Protection contre le feu d'une piece en materiau composite tisse tridimensionnel |
| FR3031469B1 (fr) * | 2015-01-14 | 2017-09-22 | Snecma | Carter en materiau composite a matrice organique auto-raidi |
| FR3025529B1 (fr) * | 2014-09-10 | 2017-07-14 | Aircelle Sa | Preforme pour raidisseur composite courbe pour piece axisymetrique telle qu’une virole |
| FR3026674B1 (fr) | 2014-10-07 | 2017-03-31 | Snecma | Procede de demoulage d'un materiau composite a matrice organique |
| FR3027959B1 (fr) * | 2014-10-31 | 2019-10-11 | Safran | Protection anti-feu d'une piece en materiau composite d'une turbine a gaz |
| DE102015204893B3 (de) * | 2015-03-18 | 2016-06-09 | MTU Aero Engines AG | Schutzeinrichtung für eine Strömungsmaschine |
| EP3951137A1 (en) * | 2015-04-24 | 2022-02-09 | Raytheon Technologies Corporation | Efficient, low pressure ratio propulsor for gas turbine engines |
| FR3041343B1 (fr) * | 2015-09-18 | 2021-04-02 | Snecma | Piece en materiau composite |
| CN108430746B (zh) * | 2015-12-22 | 2021-10-12 | 赛峰飞机发动机公司 | 由复合材料制成的轻质壳体以及其制造方法 |
| FR3045448B1 (fr) * | 2015-12-22 | 2018-01-26 | Safran Aircraft Engines | Carter allege en materiau composite et son procede de fabrication |
| FR3046613B1 (fr) | 2016-01-11 | 2018-02-09 | Safran | Procede de fabrication d'une structure textile a epaisseur variable |
| FR3046746B1 (fr) | 2016-01-15 | 2018-02-09 | Safran Aircraft Engines | Dispositif de guidage d'une texture fibreuse sur un mandrin d'impregnation, et mandrin d'impregnation et machine d'enroulement associes |
| US10519965B2 (en) | 2016-01-15 | 2019-12-31 | General Electric Company | Method and system for fiber reinforced composite panels |
| FR3048375B1 (fr) * | 2016-03-02 | 2018-04-06 | Safran Aircraft Engines | Installation et procede pour la formation d'une preforme fibreuse de revolution presentant en section radiale un profil evolutif |
| US10641287B2 (en) | 2016-09-06 | 2020-05-05 | Rolls-Royce Corporation | Fan containment case for a gas turbine engine |
| US10655500B2 (en) | 2016-09-06 | 2020-05-19 | Rolls-Royce Corporation | Reinforced fan containment case for a gas turbine engine |
| US10436061B2 (en) * | 2017-04-13 | 2019-10-08 | General Electric Company | Tapered composite backsheet for use in a turbine engine containment assembly |
| CA2969668A1 (fr) | 2017-06-02 | 2018-12-02 | Safran Aircraft Engines | Procede de demoulage d'un materiau composite a matrice organique |
| FR3070402B1 (fr) * | 2017-08-30 | 2020-08-28 | Safran Aircraft Engines | Texture fibreuse tissee pour la formation d'une preforme de carter |
| FR3070304B1 (fr) | 2017-08-30 | 2020-12-11 | Safran Aircraft Engines | Installation, procede de mise en forme et procede d'impregnation d'une preforme fibreuse |
| FR3070624B1 (fr) * | 2017-09-06 | 2019-09-13 | Safran Aircraft Engines | Carter en materiau composite a geometrie raidissante |
| US11040512B2 (en) * | 2017-11-08 | 2021-06-22 | Northrop Grumman Systems Corporation | Composite structures, forming apparatuses and related systems and methods |
| CN108004650B (zh) * | 2017-12-11 | 2020-03-17 | 南京玻璃纤维研究设计院有限公司 | 大尺寸变厚度回转体预制体及其制备方法 |
| FR3083567B1 (fr) * | 2018-07-04 | 2020-12-04 | Arianegroup Sas | Turbine a gaz renforcee pour moteur de vehicule |
| US11242866B2 (en) * | 2018-08-01 | 2022-02-08 | General Electric Company | Casing having a non-axisymmetric composite wall |
| FR3085299B1 (fr) | 2018-09-05 | 2021-04-16 | Safran Aircraft Engines | Carter en materiau composite avec raidisseur integre |
| FR3087827B1 (fr) | 2018-10-25 | 2020-10-09 | Safran Aircraft Engines | Carter de soufflante en materiau composite comprenant des brides metalliques |
| FR3092034B1 (fr) | 2019-01-30 | 2022-12-02 | Safran Aircraft Engines | Carter en matériau composite avec variation locale d’épaisseur |
| FR3092148B1 (fr) * | 2019-01-30 | 2021-01-08 | Safran Aircraft Engines | Carter de soufflante pour une turbomachine d’aeronef |
| FR3092787B1 (fr) | 2019-02-18 | 2021-02-26 | Safran Aircraft Engines | Réparation ou reprise de fabrication d’une pièce en matériau composite à renfort fibreux tissé tridimensionnel |
| FR3093298B1 (fr) * | 2019-03-01 | 2021-03-12 | Safran | Réparation ou reprise de fabrication d’une pièce en matériau composite |
| CN109866912A (zh) * | 2019-03-22 | 2019-06-11 | 宁波慈星股份有限公司 | 一种复合纤维飞机窗框及其成型方法 |
| FR3097799B1 (fr) | 2019-06-27 | 2021-06-18 | Safran Aircraft Engines | Pièce de révolution en matériau composite ayant une résistance au délaminage améliorée |
| FR3100158B1 (fr) | 2019-08-27 | 2021-07-30 | Safran | Texture fibreuse pour la fabrication d’une pièce en matériau composite et procédé de fabrication associé |
| FR3100737B1 (fr) | 2019-09-12 | 2021-08-20 | Safran Aircraft Engines | Procédé de fermeture d’un moule d’injection utilisant des plis sacrificiels anti-pincement |
| FR3100738B1 (fr) | 2019-09-12 | 2021-08-20 | Safran Aircraft Engines | Procédé de fermeture d’un moule d’injection utilisant des feuillards anti-pincement |
| CN112855616B (zh) * | 2019-11-26 | 2023-05-09 | 中国航发商用航空发动机有限责任公司 | 一种包容机匣及其制备方法 |
| EP3848488B1 (en) | 2020-01-08 | 2025-10-08 | Ratier-Figeac SAS | Propeller blade comprising a core and a braided cover of said core, bobbin and method for for braiding said braided cover |
| CN113357005A (zh) * | 2020-03-07 | 2021-09-07 | 通用电气公司 | 用于燃气涡轮发动机的风扇壳体 |
| FR3108555B1 (fr) | 2020-03-25 | 2022-04-01 | Safran Aircraft Engines | Procédé de fabrication d'une pièce de révolution en matériau composite et moule d’injection |
| FR3109180B1 (fr) | 2020-04-10 | 2022-03-11 | Safran Aircraft Engines | Procede de fabrication d’un carter pour une turbomachine d’aeronef |
| EP4161751A1 (fr) | 2020-06-04 | 2023-04-12 | Safran Aircraft Engines | Outillage d'injection pour piece de revolution en forme de tonneau |
| US20250144897A1 (en) | 2020-06-04 | 2025-05-08 | Safran Aircraft Engines | Rtm injection method and mould using symmetric anti-pinching sectors |
| US11648739B2 (en) | 2020-06-04 | 2023-05-16 | Safran Aircraft Engines | Rtm injection mold and method using asymmetric anti-pinching sectors |
| CN114055805B (zh) * | 2020-08-10 | 2023-09-08 | 中国航发商用航空发动机有限责任公司 | 航空发动机风扇易磨环的制造方法 |
| CN112696241B (zh) * | 2020-12-23 | 2022-05-24 | 南京航空航天大学 | 一种变编织角的三维编织复合材料机匣及设计方法 |
| FR3126917B1 (fr) | 2021-09-16 | 2023-09-29 | Safran Aircraft Engines | Système de fixation des deux moitiés de fût d’un moule d’injection d’un carter de soufflante |
| FR3126916B1 (fr) | 2021-09-16 | 2024-05-10 | Safran Aircraft Engines | Cale de compactage d’un moule de carter de soufflante |
| WO2023083841A1 (en) | 2021-11-09 | 2023-05-19 | Safran Aircraft Engines | Method for injecting resin and device for holding a fiber texture on an impregnation mandrel of a winding machine |
| FR3129868B1 (fr) | 2021-12-07 | 2024-06-21 | Safran Aircraft Engines | Pièce de révolution en matériau composite à haute tenue mécanique |
| US12209506B2 (en) | 2022-02-02 | 2025-01-28 | Rolls-Royce North American Technologies Inc. | Composite fan case containment hook and improved forward debris capture |
| FR3134337A1 (fr) | 2022-04-06 | 2023-10-13 | Safran | Pièce de révolution en matériau composite à capacité de rétention améliorée |
| GB202210346D0 (en) * | 2022-07-14 | 2022-08-31 | Rolls Royce Plc | Woven structure, method and apparatus for a flanged composite component |
| FR3138920B1 (fr) | 2022-08-22 | 2024-07-12 | Safran Aircraft Engines | Metier a tisser et procede de fabrication d’un tissu en forme |
| FR3146160B1 (fr) | 2023-02-24 | 2025-02-28 | Safran Aircraft Engines | Carter annulaire de turbomachine et son procédé de fabrication. |
| FR3146615B1 (fr) | 2023-03-15 | 2025-06-13 | Safran Aircraft Engines | Moule d’injection pour préforme fibreuse avec contre-moules ajustables |
| FR3146614B1 (fr) | 2023-03-15 | 2025-06-13 | Safran Aircraft Engines | Cale de compactage ajustable pour compenser l’usure des moules |
| FR3147730B1 (fr) | 2023-04-12 | 2025-04-18 | Safran | Pièce de révolution en matériau composite à résistance au délaminage améliorée |
| CN116604840A (zh) * | 2023-04-27 | 2023-08-18 | 中国航发北京航空材料研究院 | 一种双层结构复合材料包容机匣及其制备方法 |
| FR3152536A1 (fr) * | 2023-08-31 | 2025-03-07 | Safran | Aube à calage variable comportant une zone de centrage et de rétention |
| FR3154342A1 (fr) | 2023-10-20 | 2025-04-25 | Safran Aircraft Engines | Moule destiné à être utilisé pour la fabrication d'un carter de soufflante et procédé de fabrication d’un carter de soufflante |
| FR3155154A1 (fr) | 2023-11-09 | 2025-05-16 | Safran Aircraft Engines | Procédé de fabrication d’une virole de carter intermédiaire avec des propriétés localement optimisées |
| FR3155160A1 (fr) | 2023-11-09 | 2025-05-16 | Safran Aircraft Engines | Procédé de fabrication d’une pièce de révolution en matériau composite avec des propriétés localement optimisées |
| FR3160915A1 (fr) | 2024-04-08 | 2025-10-10 | Safran Aircraft Engines | Procédé de fabrication d’une préforme fibreuse de révolution utilisant une bande d’appel réutilisable |
| US12398656B1 (en) * | 2024-05-01 | 2025-08-26 | Pratt & Whitney Canada Corp. | Containment ring for gas turbine engine |
| FR3162017A1 (fr) | 2024-05-13 | 2025-11-14 | Safran Aircraft Engines | Procédé de fabrication d’une pièce de révolution en matériau composite avec portion à ténacité réduite inter-plis |
| FR3162016A1 (fr) | 2024-05-13 | 2025-11-14 | Safran Aircraft Engines | Procédé de fabrication d’une pièce de révolution en matériau composite avec l’insertion d’un antiadhésif inter-plis |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2270393C1 (ru) * | 2004-09-14 | 2006-02-20 | Закрытое акционерное общество "Центр перспективных разработок Открытого акционерного общества "Центральный научно-исследовательский институт специального машиностроения" (ЗАО "Центр перспективных разработок ОАО ЦНИИСМ") | Труба-оболочка из композиционного материала |
| US20060093847A1 (en) * | 2004-11-02 | 2006-05-04 | United Technologies Corporation | Composite sandwich with improved ballistic toughness |
| EP1674671A2 (en) * | 2004-12-23 | 2006-06-28 | General Electric Company | Composite fan containment case for turbine engines |
| EP1674244A1 (en) * | 2004-12-22 | 2006-06-28 | The General Electric Company | A fibre reinforced composite containment duct for gas turbine engines |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1485032A (en) * | 1974-08-23 | 1977-09-08 | Rolls Royce | Gas turbine engine casing |
| US4417848A (en) | 1982-02-01 | 1983-11-29 | United Technologies Corporation | Containment shell for a fan section of a gas turbine engine |
| GB2159886B (en) | 1984-06-07 | 1988-01-27 | Rolls Royce | Fan duct casing |
| FR2574476B1 (fr) * | 1984-12-06 | 1987-01-02 | Snecma | Carter de retention pour soufflante de turboreacteur |
| EP0294176A3 (en) | 1987-06-02 | 1989-12-27 | Corning Glass Works | Lightweight laminated or composite structures |
| JPH0755547B2 (ja) | 1987-10-13 | 1995-06-14 | 宇部興産株式会社 | エポキシ樹脂複合材製パイプ |
| DE3814954A1 (de) | 1988-05-03 | 1989-11-16 | Mtu Muenchen Gmbh | Berstschutzring fuer ein triebwerksgehaeuse |
| US5263516A (en) * | 1990-05-07 | 1993-11-23 | Schuylenburch Derck W P F Van | Three-dimensional woven structure |
| CA2042198A1 (en) * | 1990-06-18 | 1991-12-19 | Stephen C. Mitchell | Projectile shield |
| US5394906A (en) * | 1993-02-10 | 1995-03-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method and apparatus for weaving curved material preforms |
| US5447411A (en) * | 1993-06-10 | 1995-09-05 | Martin Marietta Corporation | Light weight fan blade containment system |
| US5516257A (en) * | 1994-04-28 | 1996-05-14 | United Technologies Corporation | Aircraft fan containment structure restraint |
| ATE194019T1 (de) * | 1995-04-06 | 2000-07-15 | Alexander Buesgen | Verfahren zum weben einer drei-dimensional geformten gewebezone |
| US6482497B1 (en) * | 1998-11-30 | 2002-11-19 | Rocky Mountain Composites Inc. | Pressure-cycled, packet-transfer infusion of resin-stitched preforms |
| US6280550B1 (en) * | 1998-12-15 | 2001-08-28 | General Electric Company | Fabrication of composite articles having an infiltrated matrix |
| EP1081388B1 (de) * | 1999-08-31 | 2005-06-01 | LTG Aktiengesellschaft | Ventilator |
| US20030186038A1 (en) * | 1999-11-18 | 2003-10-02 | Ashton Larry J. | Multi orientation composite material impregnated with non-liquid resin |
| US6290455B1 (en) | 1999-12-03 | 2001-09-18 | General Electric Company | Contoured hardwall containment |
| FR2861143B1 (fr) * | 2003-10-20 | 2006-01-20 | Snecma Moteurs | Aube de turbomachine, notamment aube de soufflante et son procede de fabrication |
| FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
| US7713021B2 (en) * | 2006-12-13 | 2010-05-11 | General Electric Company | Fan containment casings and methods of manufacture |
| US20080156419A1 (en) * | 2006-12-28 | 2008-07-03 | Lee Alan Blanton | Continuous debulking methods |
-
2007
- 2007-02-23 FR FR0753449A patent/FR2913053B1/fr not_active Expired - Fee Related
-
2008
- 2008-02-19 US US12/033,624 patent/US8322971B2/en active Active
- 2008-02-19 JP JP2008036946A patent/JP5496461B2/ja active Active
- 2008-02-21 EP EP08101816A patent/EP1961923B1/fr active Active
- 2008-02-21 CA CA2621729A patent/CA2621729C/fr active Active
- 2008-02-21 ES ES08101816T patent/ES2384898T3/es active Active
- 2008-02-22 RU RU2008106944/02A patent/RU2450130C2/ru active
- 2008-02-25 CN CN2008100816103A patent/CN101249725B/zh active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2270393C1 (ru) * | 2004-09-14 | 2006-02-20 | Закрытое акционерное общество "Центр перспективных разработок Открытого акционерного общества "Центральный научно-исследовательский институт специального машиностроения" (ЗАО "Центр перспективных разработок ОАО ЦНИИСМ") | Труба-оболочка из композиционного материала |
| US20060093847A1 (en) * | 2004-11-02 | 2006-05-04 | United Technologies Corporation | Composite sandwich with improved ballistic toughness |
| EP1674244A1 (en) * | 2004-12-22 | 2006-06-28 | The General Electric Company | A fibre reinforced composite containment duct for gas turbine engines |
| EP1674671A2 (en) * | 2004-12-23 | 2006-06-28 | General Electric Company | Composite fan containment case for turbine engines |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2632352C2 (ru) * | 2012-08-03 | 2017-10-04 | Снекма | Способ неразрушающего контроля заготовки лопатки |
| RU2611914C2 (ru) * | 2014-04-10 | 2017-03-01 | Сафран Аэро Бустерс Са | Осевая турбомашина и корпус из композиционного материала для осевой турбомашины |
| RU2752691C2 (ru) * | 2017-04-13 | 2021-07-29 | Сафран | Способ изготовления детали из композиционного материала, содержащей корпус, продолженный усиленным крепежным концом |
Also Published As
| Publication number | Publication date |
|---|---|
| US20080206048A1 (en) | 2008-08-28 |
| CA2621729C (fr) | 2015-02-03 |
| CN101249725A (zh) | 2008-08-27 |
| EP1961923B1 (fr) | 2012-04-11 |
| EP1961923A3 (fr) | 2010-11-17 |
| JP2008240724A (ja) | 2008-10-09 |
| CA2621729A1 (fr) | 2008-08-23 |
| FR2913053A1 (fr) | 2008-08-29 |
| US8322971B2 (en) | 2012-12-04 |
| JP5496461B2 (ja) | 2014-05-21 |
| CN101249725B (zh) | 2012-08-08 |
| ES2384898T3 (es) | 2012-07-13 |
| FR2913053B1 (fr) | 2009-05-22 |
| EP1961923A2 (fr) | 2008-08-27 |
| RU2008106944A (ru) | 2009-08-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2450130C2 (ru) | Способ изготовления корпуса газовой турбины из композиционного материала и корпус, полученный таким способом | |
| JP5588103B2 (ja) | ほぼ円筒形の複合材物品及びファンケーシング | |
| RU2703206C2 (ru) | Самоусиленный корпус, состоящий из композиционного материала с органической матрицей | |
| JP6049706B2 (ja) | タービンエンジンファンケーシング、およびこの種のケーシングおよび音響パネルによって形成されるアセンブリ | |
| CN112739530B (zh) | 具有一体化加强件的复合材料壳体 | |
| US11181011B2 (en) | Lighter-weight casing made of composite material and method of manufacturing same | |
| RU2598936C1 (ru) | Цилиндрический кожух и способ изготовления цилиндрического кожуха | |
| US20130216367A1 (en) | Case with ballistic liner | |
| FR2977827A1 (fr) | Procede de fabrication d'un carter de soufflante de turbomachine muni de revetements abradable et acoustique | |
| US7905972B2 (en) | Methods for making substantially cylindrical articles and fan casings | |
| JP2011527400A (ja) | 3d複合ブロワ用静翼 | |
| CN104975890A (zh) | 用于轴流式涡轮机的压缩机的复合壳体 | |
| US20220145775A1 (en) | Repairing or resuming production of a component made of composite material | |
| CN115246177B (zh) | 发动机机匣的制作方法 | |
| CN119136966A (zh) | 具有改进的保持能力的由复合材料制成的旋转对称部件 | |
| CN115111184A (zh) | 由混合材料形成的部件 | |
| CN120444096A (zh) | 用于制作用于涡轮发动机的壳体结构的预制件 | |
| CN121047650A (zh) | 制造用于复合部件的织造织物的方法 | |
| WO2025099386A1 (fr) | Procede de fabrication d'une piece de revolution en materiau composite avec des proprietes localement optimisees |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PD4A | Correction of name of patent owner |