IN2014DN05637A - - Google Patents
Info
- Publication number
- IN2014DN05637A IN2014DN05637A IN5637DEN2014A IN2014DN05637A IN 2014DN05637 A IN2014DN05637 A IN 2014DN05637A IN 5637DEN2014 A IN5637DEN2014 A IN 5637DEN2014A IN 2014DN05637 A IN2014DN05637 A IN 2014DN05637A
- Authority
- IN
- India
- Prior art keywords
- threads
- preform
- fibrous
- group
- rough form
- Prior art date
Links
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
-
- 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
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- B29C70/06—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
- B29C70/22—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 two directions forming a two dimensional structure
- B29C70/222—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 two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- 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
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D1/00—Woven fabrics designed to make specified articles
-
- 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
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D3/00—Woven fabrics characterised by their shape
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
-
- 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
-
- 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
- F05D2300/6034—Orientation of fibres, weaving, ply angle
Abstract
THE INVENTION RELATES TO A METHOD FOR PRODUCING A FIBROUS PREFORM FOR THE MANUFACTURE OF A TURBOMACHINE BLADE MADE OF COMPOSITE MATERIAL THE METHOD INVOLVING USING THREE DIMENSIONAL WEAVING TO CREATE A FIBROUS ROUGH FORM (100) IN A SINGLE PIECE WITH LAYERS OF LONGITUDINAL THREADS (C TO C) JOINED TOGETHER BY THREADS OF LAYERS OF TRANSVERSE THREADS (T TO T) AND SHAPING THE FIBROUS ROUGH FORM TO OBTAIN A FIBROUS PREFORM IN A SINGLE PIECE HAVING A PART THAT FORMS THE AEROFOIL PREFORM AND AT LEAST A PART THAT FORMS A PLATFORM PREFORM. DURING THE COURSE OF THE WEAVING PROCESS THE THREADS (C TO C) OF A FIRST GROUP OF LONGITUDINAL THREADS ARE LED OUT FROM THE FIBROUS ROUGH FORM ON THE SIDE OF ONE OF THE LATERAL FACES (110A) OF THE ROUGH FORM TO FORM A PART (120) THAT CORRESPONDS TO A PREFORM OF A BLADE PLATFORM AND THREADS (C AND C) OF A SECOND GROUP OF LONGITUDINAL THREADS ARE INJECTED INTO THE FIBROUS ROUGH FORM WITH MUTUAL CRISS CROSSING BETWEEN THE THREADS OF THE FIRST GROUP AND THE THREADS OF THE SECOND GROUP. THE INVENTION ALSO RELATES TO A PREFORM OBTAINED USING THIS METHOD.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261584406P | 2012-01-09 | 2012-01-09 | |
PCT/FR2013/050026 WO2013104852A2 (en) | 2012-01-09 | 2013-01-07 | Fibrous preform of a turbomachine blade made of composite material with in-built platform, and method of producing same |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014DN05637A true IN2014DN05637A (en) | 2015-04-03 |
Family
ID=47628361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN5637DEN2014 IN2014DN05637A (en) | 2012-01-09 | 2013-01-07 |
Country Status (9)
Country | Link |
---|---|
US (1) | US9771810B2 (en) |
EP (1) | EP2802701B1 (en) |
JP (1) | JP6038178B2 (en) |
CN (1) | CN104040056B (en) |
BR (1) | BR112014016859B1 (en) |
CA (1) | CA2862685C (en) |
IN (1) | IN2014DN05637A (en) |
RU (1) | RU2612628C2 (en) |
WO (1) | WO2013104852A2 (en) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105026123B (en) * | 2012-11-13 | 2018-02-09 | 斯内克马公司 | Monolithic prefabricated component and blade for turbine |
FR3011253B1 (en) * | 2013-10-01 | 2016-06-10 | Snecma | FIBROUS STRUCTURE WITH FLEET COMBINATION |
FR3018473B1 (en) | 2014-03-17 | 2016-04-08 | Snecma | METHOD FOR MANUFACTURING A CAMERA PLATFORM IN COMPOSITE MATERIAL WITH INTEGRATED JOINTS FOR TURBOMACHINE BLOWER |
FR3021349B1 (en) | 2014-05-22 | 2021-07-02 | Herakles | METHOD OF MANUFACTURING A TURBOMACHINE VANE FROM COMPOSITE MATERIAL, THUS OBTAINED VANE AND TURBOMACHINE INCORPORATING IT |
FR3037097B1 (en) * | 2015-06-03 | 2017-06-23 | Snecma | COMPOSITE AUBE COMPRISING A PLATFORM WITH A STIFFENER |
FR3032462B1 (en) | 2015-02-10 | 2017-03-10 | Aircelle Sa | METHOD FOR MANUFACTURING A WOVEN REINFORCED FIBER PREFORM COMPRISING AN EVOLUTIVE SECTION |
FR3035676B1 (en) * | 2015-04-29 | 2017-05-12 | Snecma | DAWN WITH PLATFORMS POSSESSING A STIFFENER |
FR3035678B1 (en) * | 2015-04-29 | 2017-05-12 | Snecma | DAWN WITH PLATFORMS HAVING A RESTRAINT LEG |
FR3035677B1 (en) * | 2015-04-29 | 2017-05-12 | Snecma | DAWN HAVING PLATFORMS HAVING HOISTING PORTIONS |
FR3035675B1 (en) * | 2015-04-29 | 2017-05-12 | Snecma | DAWN WITH PLATFORMS COMPRISING INSERTS |
CN105544060A (en) * | 2016-01-29 | 2016-05-04 | 上海仪耐新材料科技有限公司 | Embedded type stitched three-dimensional bullet-proof fabric |
US10436036B2 (en) * | 2016-07-05 | 2019-10-08 | Safran Aircraft Engines | Fitted platform for a turbine engine fan, and a method of fabricating it |
US20180171806A1 (en) * | 2016-12-21 | 2018-06-21 | Rolls-Royce North American Technologies, Inc. | Three-dimensionally woven ceramic matrix composite turbine blade |
FR3063448B1 (en) * | 2017-03-01 | 2019-04-05 | Safran Aircraft Engines | PREFORME AND AUBE MONOBLOC FOR TURBOMACHINE |
JP6700615B2 (en) * | 2017-03-31 | 2020-05-27 | 株式会社豊田自動織機 | Fiber structure and fiber reinforced composite material |
JP6790967B2 (en) * | 2017-03-31 | 2020-11-25 | 株式会社豊田自動織機 | Fiber structure and fiber reinforced composite |
FR3066531B1 (en) | 2017-05-19 | 2019-05-03 | Safran Aircraft Engines | DAWN IN COMPOSITE MATERIAL AND INTEGRATED PLATFORM FOR AN AIRCRAFT TURBOMACHINE |
FR3082854B1 (en) * | 2018-06-25 | 2020-09-11 | Safran Ceram | FIBROUS STRUCTURE AND PART IN COMPOSITE MATERIAL INCORPORATING SUCH STRUCTURE |
WO2019097147A1 (en) | 2017-11-14 | 2019-05-23 | Safran Ceramics | Fibrous structure and component made of composite material incorporating such a structure |
FR3076814B1 (en) * | 2018-01-12 | 2020-01-31 | Safran Aircraft Engines | BLADE OR COMPOSITE PROPELLER BLADE WITH INTEGRATED LONGER FOR AIRCRAFT |
US20190390555A1 (en) * | 2018-06-22 | 2019-12-26 | United Technologies Corporation | Composite airfoil with cleft in platform |
FR3091723B1 (en) * | 2019-01-15 | 2021-04-02 | Safran Aircraft Engines | Composite blade or propeller blade for aircraft incorporating a shaping part |
FR3092034B1 (en) * | 2019-01-30 | 2022-12-02 | Safran Aircraft Engines | Casing in composite material with local thickness variation |
FR3093297B1 (en) * | 2019-02-28 | 2022-08-12 | Safran Aircraft Engines | METHOD FOR MAKING A WOVEN PIECE TAKING ACCOUNT OF OFF-FRAME |
CN109972271B (en) * | 2019-03-27 | 2023-03-14 | 南京玻璃纤维研究设计院有限公司 | Variable thickness preform, composite component and yarn reducing method of variable thickness preform |
US11434177B2 (en) | 2019-05-13 | 2022-09-06 | Rolls-Royce Plc | Ceramic matrix composite vane with hybrid construction |
US20210086471A1 (en) * | 2019-09-20 | 2021-03-25 | United Technologies Corporation | Composite material marking and identification |
FR3102392B1 (en) * | 2019-10-29 | 2021-10-08 | Safran | Woven fiber preform to make a blower blade in composite material |
CN111365079A (en) * | 2020-04-01 | 2020-07-03 | 南京航空航天大学 | Ceramic matrix composite turbine rotor blade disk tenon connecting structure and turbine disk |
FR3113647B1 (en) | 2020-08-27 | 2023-04-14 | Safran Aircraft Engines | NON-FLOWED PROPELLER WITH VARIABLE PITCH BLADE COMPRISING PLATFORMS WITH REDUCED DISTURBANCE |
CN115949471B (en) * | 2023-01-04 | 2023-12-22 | 北京航空航天大学 | Orthogonal three-dimensional woven composite material outlet guide vane and manufacturing method thereof |
US11846192B1 (en) | 2023-04-21 | 2023-12-19 | General Electric Company | Airfoil assembly with a trunnion and spar |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
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JPH0772482B2 (en) * | 1991-12-26 | 1995-08-02 | 工業技術院長 | Radial rotor and manufacturing method thereof |
US6446675B1 (en) * | 2001-07-05 | 2002-09-10 | Albany International Techniweave, Inc. | Minimum distortion 3D woven preforms |
CA2449746C (en) * | 2001-09-12 | 2010-03-09 | Lockheed Martin Corporation | Woven preform for structural joints |
FR2861143B1 (en) | 2003-10-20 | 2006-01-20 | Snecma Moteurs | TURBOMACHINE BLADE, IN PARTICULAR BLADE OF BLOWER AND METHOD OF MANUFACTURING THE SAME |
DE10350917B3 (en) | 2003-10-31 | 2005-05-25 | Rle International Produktentwicklungsgesellschaft Mbh | Transmission interruption-free manual transmission |
FR2887601B1 (en) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | MECHANICAL PIECE AND METHOD FOR MANUFACTURING SUCH A PART |
US7655581B2 (en) * | 2005-11-17 | 2010-02-02 | Albany Engineered Composites, Inc. | Hybrid three-dimensional woven/laminated struts for composite structural applications |
US8079387B2 (en) * | 2008-10-29 | 2011-12-20 | Albany Engineered Composites, Inc. | Pi-shaped preform |
FR2939153B1 (en) * | 2008-11-28 | 2011-12-09 | Snecma Propulsion Solide | REALIZING A FIBROUS STRUCTURE WITH AN EVOLVING THICKNESS THROUGH 3D WEAVING |
FR2939129B1 (en) * | 2008-11-28 | 2014-08-22 | Snecma Propulsion Solide | TURBOMACHINE TURBINE IN COMPOSITE MATERIAL AND PROCESS FOR MANUFACTURING THE SAME. |
FR2943942B1 (en) * | 2009-04-06 | 2016-01-29 | Snecma | PROCESS FOR MANUFACTURING A TURBOMACHINE BLADE OF COMPOSITE MATERIAL |
FR2946999B1 (en) * | 2009-06-18 | 2019-08-09 | Safran Aircraft Engines | CMC TURBINE DISPENSER ELEMENT, PROCESS FOR MANUFACTURING SAME, AND DISPENSER AND GAS TURBINE INCORPORATING SAME. |
FR2953885B1 (en) | 2009-12-14 | 2012-02-10 | Snecma | TURBOMACHINE DRAFT IN COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING THE SAME |
FR2961846B1 (en) * | 2010-06-28 | 2012-08-03 | Snecma Propulsion Solide | TURBOMACHINE TURBOMACHINE WITH COMPLEMENTARY ASYMMETRIC GEOMETRY |
FR2961845B1 (en) * | 2010-06-28 | 2013-06-28 | Snecma Propulsion Solide | TURBOMACHINE DAWN WITH COMPLEMENTARY PAIRE / IMPAIRE GEOMETRY AND METHOD OF MANUFACTURING THE SAME |
RU2612927C2 (en) * | 2011-12-14 | 2017-03-13 | Снекма | Fibrous structure woven as single part by 3d braiding and its application for making part from composite material |
-
2013
- 2013-01-07 EP EP13701834.7A patent/EP2802701B1/en active Active
- 2013-01-07 WO PCT/FR2013/050026 patent/WO2013104852A2/en active Application Filing
- 2013-01-07 IN IN5637DEN2014 patent/IN2014DN05637A/en unknown
- 2013-01-07 CA CA2862685A patent/CA2862685C/en active Active
- 2013-01-07 JP JP2014550750A patent/JP6038178B2/en active Active
- 2013-01-07 RU RU2014132876A patent/RU2612628C2/en active
- 2013-01-07 BR BR112014016859-8A patent/BR112014016859B1/en active IP Right Grant
- 2013-01-07 US US14/371,220 patent/US9771810B2/en active Active
- 2013-01-07 CN CN201380004969.XA patent/CN104040056B/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2802701A2 (en) | 2014-11-19 |
BR112014016859A8 (en) | 2017-07-04 |
RU2612628C2 (en) | 2017-03-09 |
JP2015509159A (en) | 2015-03-26 |
EP2802701B1 (en) | 2016-11-16 |
CA2862685A1 (en) | 2013-07-18 |
CN104040056A (en) | 2014-09-10 |
US20140369848A1 (en) | 2014-12-18 |
CN104040056B (en) | 2016-05-04 |
JP6038178B2 (en) | 2016-12-07 |
CA2862685C (en) | 2020-03-10 |
WO2013104852A2 (en) | 2013-07-18 |
BR112014016859B1 (en) | 2021-02-09 |
US9771810B2 (en) | 2017-09-26 |
WO2013104852A3 (en) | 2014-02-20 |
BR112014016859A2 (en) | 2017-06-13 |
RU2014132876A (en) | 2016-02-27 |
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