FR3093298B1 - Réparation ou reprise de fabrication d’une pièce en matériau composite - Google Patents
Réparation ou reprise de fabrication d’une pièce en matériau composite Download PDFInfo
- Publication number
- FR3093298B1 FR3093298B1 FR1902143A FR1902143A FR3093298B1 FR 3093298 B1 FR3093298 B1 FR 3093298B1 FR 1902143 A FR1902143 A FR 1902143A FR 1902143 A FR1902143 A FR 1902143A FR 3093298 B1 FR3093298 B1 FR 3093298B1
- Authority
- FR
- France
- Prior art keywords
- composite material
- densified
- fibrous reinforcement
- fibrous
- matrix
- 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
Links
- 239000002131 composite material Substances 0.000 title abstract 4
- 238000004519 manufacturing process Methods 0.000 title 1
- 230000002787 reinforcement Effects 0.000 abstract 5
- 239000011159 matrix material Substances 0.000 abstract 3
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
Classifications
-
- 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
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
- B29C73/14—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using elements composed of two parts joined together after having been placed one on each side of the article
-
- 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
- F01D25/005—Selecting particular materials
-
- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
-
- 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
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
- B29C73/10—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using patches sealing on the surface of the article
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/008—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of an organic adhesive, e.g. phenol resin or pitch
-
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- 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
- 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
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/48—Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/48—Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
- C04B2235/483—Si-containing organic compounds, e.g. silicone resins, (poly)silanes, (poly)siloxanes or (poly)silazanes
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5252—Fibers having a specific pre-form
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
- C04B2235/616—Liquid infiltration of green bodies or pre-forms
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/94—Products characterised by their shape
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2230/80—Repairing, retrofitting or upgrading 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
- F05D2300/00—Materials; Properties thereof
-
- 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)
- Mechanical Engineering (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Textile Engineering (AREA)
- Woven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Réparation ou reprise de fabrication d’une pièce en matériau composite Une pièce (10) de turbine à gaz en matériau composite comprend un renfort fibreux présentant un tissage tridimensionnel entre une pluralité de fils de chaîne et une pluralité de fils de trame, ledit renfort fibreux étant densifié par une matrice. Le renfort fibreux densifié s’étend en largeur entre une extrémité aval et une extrémité amont suivant une direction axiale et en épaisseur entre une surface interne (11) et une surface externe (12) suivant une direction radiale. Le renfort fibreux densifié par la matrice comporte une portion évidée s’étendant sur toute l’épaisseur du renfort fibreux. Une pièce de comblement en matériau composite (50) est présente dans le volume libre de la pièce délimité par la portion évidée, la pièce de comblement (50) comprenant une préforme fibreuse présentant un tissage tridimensionnel, ladite préforme fibreuse étant densifiée par une matrice. Figure pour l’abrégé : Fig. 7.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1902143A FR3093298B1 (fr) | 2019-03-01 | 2019-03-01 | Réparation ou reprise de fabrication d’une pièce en matériau composite |
PCT/FR2020/050341 WO2020178500A1 (fr) | 2019-03-01 | 2020-02-24 | Reparation ou reprise de fabrication d' une piece en materiau composite |
EP20713712.6A EP3930991A1 (fr) | 2019-03-01 | 2020-02-24 | Reparation ou reprise de fabrication d' une piece en materiau composite |
CN202311164404.XA CN117183413A (zh) | 2019-03-01 | 2020-02-24 | 修复或恢复由复合材料制成的部件的生产 |
CN202080024415.6A CN113631359B (zh) | 2019-03-01 | 2020-02-24 | 修复或恢复由复合材料制成的部件的生产 |
US17/435,234 US20220145775A1 (en) | 2019-03-01 | 2020-02-24 | Repairing or resuming production of a component made of composite material |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1902143A FR3093298B1 (fr) | 2019-03-01 | 2019-03-01 | Réparation ou reprise de fabrication d’une pièce en matériau composite |
FR1902143 | 2019-03-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3093298A1 FR3093298A1 (fr) | 2020-09-04 |
FR3093298B1 true FR3093298B1 (fr) | 2021-03-12 |
Family
ID=67185367
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1902143A Active FR3093298B1 (fr) | 2019-03-01 | 2019-03-01 | Réparation ou reprise de fabrication d’une pièce en matériau composite |
Country Status (5)
Country | Link |
---|---|
US (1) | US20220145775A1 (fr) |
EP (1) | EP3930991A1 (fr) |
CN (2) | CN113631359B (fr) |
FR (1) | FR3093298B1 (fr) |
WO (1) | WO2020178500A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3121382B1 (fr) | 2021-03-30 | 2023-11-17 | Safran Aircraft Engines | Réparation d’une pièce en matériau composite |
CN113085230A (zh) * | 2021-05-10 | 2021-07-09 | 北京航空航天大学 | 一种复合材料维修结构及维修方法 |
FR3139497B1 (fr) * | 2022-09-14 | 2024-09-06 | Safran Aircraft Engines | Procédé de réparation d’un carter de soufflante |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4961799A (en) * | 1984-10-29 | 1990-10-09 | The Boeing Company | Blind-side panel repair method |
US4916880A (en) * | 1986-07-21 | 1990-04-17 | The Boeing Company | Apparatus for repairing a hole in a structural wall of composite material |
US5190611A (en) * | 1991-02-13 | 1993-03-02 | The Boeing Company | Bearing load restoration method for composite structures |
US6820334B2 (en) * | 2002-04-19 | 2004-11-23 | General Electric Company | Method for repairing articles of ceramic composites |
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 |
US7419556B2 (en) * | 2005-10-11 | 2008-09-02 | United Technologies Corporation | Method of repair for inlet caps of turbine engines |
US20070095457A1 (en) | 2005-11-02 | 2007-05-03 | The Boeing Company | Fast line maintenance repair method and system for composite structures |
US8043453B2 (en) * | 2005-12-23 | 2011-10-25 | The Boeing Company | System and method for reworking composites |
FR2913053B1 (fr) * | 2007-02-23 | 2009-05-22 | Snecma Sa | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
GB0721546D0 (en) * | 2007-11-01 | 2007-12-12 | Rolls Royce Plc | Composite material repair |
DE102008021788A1 (de) * | 2008-04-30 | 2009-11-12 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zum Reparieren einer Flugzeugkomponente |
FR2946999B1 (fr) * | 2009-06-18 | 2019-08-09 | Safran Aircraft Engines | Element de distributeur de turbine en cmc, procede pour sa fabrication, et distributeur et turbine a gaz l'incorporant. |
FR2983428B1 (fr) * | 2011-12-01 | 2014-01-17 | Snecma Propulsion Solide | Procede de fabrication d'une aube de turbomachine en materiau composite a plates-formes integrees |
DE102011056088B4 (de) * | 2011-12-06 | 2013-07-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Reparaturverfahren |
JP6321429B2 (ja) * | 2014-03-31 | 2018-05-09 | 学校法人大同学園 | 繊維強化樹脂部材の修理方法および研削方法 |
US9545782B2 (en) * | 2014-05-13 | 2017-01-17 | The Boeing Company | Method and apparatus for repairing composite materials |
FR3031469B1 (fr) * | 2015-01-14 | 2017-09-22 | Snecma | Carter en materiau composite a matrice organique auto-raidi |
GB2531600A (en) * | 2014-10-24 | 2016-04-27 | Short Brothers Plc | Apparatus and methods for manufacturing and repairing fibre-reinforced composite materials |
US10213964B2 (en) * | 2015-05-08 | 2019-02-26 | The Boeing Company | Methods and apparatus for repairing composite materials |
FR3037854B1 (fr) * | 2015-06-29 | 2018-03-23 | Safran Aircraft Engines | Procede de fabrication d'un carter de soufflante en materiau composite a panneau abradable integre pour moteur a turbine a gaz et carter ainsi obtenu |
US11181011B2 (en) * | 2015-12-22 | 2021-11-23 | Safran Aircraft Engines | Lighter-weight casing made of composite material and method of manufacturing same |
FR3059934B1 (fr) * | 2016-12-14 | 2018-11-30 | Safran Aircraft Engines | Moule d'impregnation a aiguilles pour la realisation d'une piece a partir d'une preforme tissee |
DE102017117383A1 (de) * | 2017-08-01 | 2019-02-07 | Airbus Operations Gmbh | Verfahren und Vorrichtung zum Reparieren eines aus einem Schichtverbundwerkstoff in mehreren Schichten aufgebauten Bauteils |
WO2019112662A1 (fr) * | 2017-12-05 | 2019-06-13 | Siemens Aktiengesellschaft | Structure de paroi à interface tridimensionnelle entre une partie métallique et une partie composite à matrice céramique |
-
2019
- 2019-03-01 FR FR1902143A patent/FR3093298B1/fr active Active
-
2020
- 2020-02-24 EP EP20713712.6A patent/EP3930991A1/fr active Pending
- 2020-02-24 CN CN202080024415.6A patent/CN113631359B/zh active Active
- 2020-02-24 WO PCT/FR2020/050341 patent/WO2020178500A1/fr active Application Filing
- 2020-02-24 US US17/435,234 patent/US20220145775A1/en active Pending
- 2020-02-24 CN CN202311164404.XA patent/CN117183413A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
EP3930991A1 (fr) | 2022-01-05 |
US20220145775A1 (en) | 2022-05-12 |
CN117183413A (zh) | 2023-12-08 |
CN113631359B (zh) | 2023-09-29 |
CN113631359A (zh) | 2021-11-09 |
FR3093298A1 (fr) | 2020-09-04 |
WO2020178500A1 (fr) | 2020-09-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3093298B1 (fr) | Réparation ou reprise de fabrication d’une pièce en matériau composite | |
CA2702316C (fr) | Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion | |
CA2979474C (fr) | Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique | |
EP0855496B1 (fr) | Flexible de découplage monté dans une ligne d'échappement d'un moteur de véhicule automobile | |
FR2950416A1 (fr) | Dispositif accroche-flammes comprenant un support de bras et un ecran de protection thermique monoblocs | |
FR3036433B1 (fr) | Ensemble d'anneau de turbine avec maintien par crabotage | |
FR2825785A1 (fr) | Liaison de chambre de combustion cmc de turbomachine en deux parties | |
FR2825780A1 (fr) | Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique | |
EP2886804B1 (fr) | Dispositif d'étanchéité pour un compresseur de turbomachine | |
EP1265036A1 (fr) | Montage élastique de chambre de combustion CMC de turbomachine dans un carter métallique | |
KR20030061679A (ko) | 가스 터빈용 내측 압축기 방출 케이스 | |
FR3002750A1 (fr) | 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 | |
FR2935464A1 (fr) | Dispositif de fixation d'un bras accroche flammes sur un carter de post-combustion. | |
FR2865502A1 (fr) | Bras monobloc accroche-flammes pour un dispositif de post combustion d'un turboreacteur a double flux | |
FR2911666A1 (fr) | Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif | |
FR3084694A1 (fr) | Fixation d'un distributeur a un carter d'une turbomachine | |
FR3070425B1 (fr) | Element aubage profile d'un ensemble propulsif en composite stratifie | |
FR2825782A1 (fr) | Montage flottant radial de chambre de combustion cmc de turbomachine dans un carter metallique | |
FR3090462B1 (fr) | Pièce en composite à renfort fibreux avec une résistance aux vibrations augmentée | |
FR2992019A1 (fr) | Carter en materiau composite pour chambre de combustion de moteur a turbine a gaz | |
FR3076851A1 (fr) | Aube a insert composite revetu d'une couche metallique | |
FR2875266A1 (fr) | Collecteur d'echappement pour moteur a combustion interne | |
FR2708086A1 (fr) | Structure tubulaire sectorisée travaillant à l'implosion. | |
FR3090465A1 (fr) | Procede de fabrication d'une piece de turbomachine en materiau composite et piece de turbomachine correspondante | |
FR3121951A1 (fr) | Systeme de renforcement pour un carter de soufflante en materiau composite, carter de soufflante et turbomachine correspondants |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20200904 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |