FR3116545B1 - Texture fibreuse de renfort d'une aube de turbomachine - Google Patents
Texture fibreuse de renfort d'une aube de turbomachine Download PDFInfo
- Publication number
- FR3116545B1 FR3116545B1 FR2012107A FR2012107A FR3116545B1 FR 3116545 B1 FR3116545 B1 FR 3116545B1 FR 2012107 A FR2012107 A FR 2012107A FR 2012107 A FR2012107 A FR 2012107A FR 3116545 B1 FR3116545 B1 FR 3116545B1
- Authority
- FR
- France
- Prior art keywords
- fibrous reinforcement
- turbomachine blade
- reinforcement texture
- texture
- blade
- 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
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
-
- 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
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/02—Reinforcing materials; Prepregs
-
- 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
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
-
- 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
- F05D2300/601—Fabrics
- F05D2300/6012—Woven fabrics
-
- 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
- F05D2300/6033—Ceramic matrix composites [CMC]
-
- 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)
- Textile Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Woven Fabrics (AREA)
Abstract
Texture fibreuse de renfort d’une aube de turbomachine L’invention concerne une texture fibreuse (11) de renfort d’une aube de turbomachine réalisée en une seule pièce et formant au moins préforme du profil aérodynamique (10) de l’aube et de l’élément de plateforme (24 ; 28). Figure pour l’abrégé : Fig. 2.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2012107A FR3116545B1 (fr) | 2020-11-25 | 2020-11-25 | Texture fibreuse de renfort d'une aube de turbomachine |
PCT/FR2021/052012 WO2022112683A1 (fr) | 2020-11-25 | 2021-11-15 | Texture fibreuse de renfort d'une aube de turbomachine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2012107 | 2020-11-25 | ||
FR2012107A FR3116545B1 (fr) | 2020-11-25 | 2020-11-25 | Texture fibreuse de renfort d'une aube de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3116545A1 FR3116545A1 (fr) | 2022-05-27 |
FR3116545B1 true FR3116545B1 (fr) | 2022-11-25 |
Family
ID=75108420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2012107A Active FR3116545B1 (fr) | 2020-11-25 | 2020-11-25 | Texture fibreuse de renfort d'une aube de turbomachine |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3116545B1 (fr) |
WO (1) | WO2022112683A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3137014A1 (fr) * | 2022-06-22 | 2023-12-29 | Safran Landing Systems | Renfort fibreux pour la fabrication d’une pièce composite destinée à être articulée avec d’autres pièces |
FR3137012A1 (fr) * | 2022-06-22 | 2023-12-29 | Safran Landing Systems | Renfort fibreux pour la fabrication d’une pièce composite destinée à être articulée avec d’autres pièces |
FR3142931A1 (fr) * | 2022-12-09 | 2024-06-14 | Safran Ceramics | Préforme d’aube en une seule pièce intégrant des portions de tissu unidirectionnel traversantes |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3021349B1 (fr) * | 2014-05-22 | 2021-07-02 | Herakles | Procede de fabrication d'une aube de turbomachine en materiau composite, aube ainsi obtenue et turbomachine l'incorporant |
US10577939B2 (en) * | 2016-11-01 | 2020-03-03 | Rolls-Royce Corporation | Turbine blade with three-dimensional CMC construction elements |
-
2020
- 2020-11-25 FR FR2012107A patent/FR3116545B1/fr active Active
-
2021
- 2021-11-15 WO PCT/FR2021/052012 patent/WO2022112683A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2022112683A1 (fr) | 2022-06-02 |
FR3116545A1 (fr) | 2022-05-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3116545B1 (fr) | Texture fibreuse de renfort d'une aube de turbomachine | |
US9914282B2 (en) | Composite material with controlled fracture regions | |
FR3021349B1 (fr) | Procede de fabrication d'une aube de turbomachine en materiau composite, aube ainsi obtenue et turbomachine l'incorporant | |
EP1557532A3 (fr) | Aube creuse de soufflante pour moteur à turbine à gaz, moteur à turbine à gaz ainsi que procédé pour faire une telle aube creuse de soufflante | |
EP2031185A3 (fr) | Élément de moteur à turbine à parties multiples ayant un canal de refroidissement et procédé de fabrication dudit élément | |
FR3111658B1 (fr) | Aube en matériau composite à renfort fibreux tissé tridimensionnel et peau tissée bidimensionnel et son procédé de fabrication | |
FR3086881B1 (fr) | Texture fibreuse pour realiser une aube de soufflante en materiau composite | |
US10458261B2 (en) | Intermediate casing guide vane wheel | |
FR3105292B1 (fr) | Aube en matériau composite avec bord d’attaque rapporté à densité variable | |
FR3096400B1 (fr) | Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir | |
FR3049002B1 (fr) | Pale de turbomachine aeronautique comprenant un element rapporte en materiau composite formant bord de fuite et procede de fabrication d'une telle pale | |
US20060104816A1 (en) | Running wheel | |
WO2008031413A3 (fr) | Procédé de planification d'entretien | |
FR3116753B1 (fr) | Procédé de fabrication d'une aube en matériau composite avec plateformes et pattes de fixation intégrées | |
RU2434141C2 (ru) | Сектор направляющих лопаток газотурбинного двигателя, ступень сжатия, компрессор и газотурбинный двигатель | |
EP3428394B1 (fr) | Aube de soufflante de moteur à turbine à gaz et procédé de conception d'une aube de soufflante | |
MA43857A (fr) | Élément d'intégration pour une pale de turbine éolienne | |
FR3096399B1 (fr) | Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir | |
US11530614B2 (en) | Vane arc segment formed of fiber-reinforced composite | |
FR3076851B1 (fr) | Aube a insert composite revetu d'une couche metallique | |
US10260350B2 (en) | Gas turbine engine airfoil structure | |
US11725522B2 (en) | Airfoil with wishbone fiber structure | |
FR3011269A1 (fr) | Aube de redresseur pour moteur a turbine a gaz a structure hybride | |
JP2016526129A (ja) | タービンエンジンブレードプリフォーム | |
US20110250072A1 (en) | Replacement part for a gas turbine blade of a gas turbine, gas turbine blade and method for repairing a gas turbine blade |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20220527 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |