BR112012018456A2 - método de fabricação de uma pá de material compósito tendo canais internos, e uma pá de turbomáquina de material compósito - Google Patents
método de fabricação de uma pá de material compósito tendo canais internos, e uma pá de turbomáquina de material compósitoInfo
- Publication number
- BR112012018456A2 BR112012018456A2 BR112012018456A BR112012018456A BR112012018456A2 BR 112012018456 A2 BR112012018456 A2 BR 112012018456A2 BR 112012018456 A BR112012018456 A BR 112012018456A BR 112012018456 A BR112012018456 A BR 112012018456A BR 112012018456 A2 BR112012018456 A2 BR 112012018456A2
- Authority
- BR
- Brazil
- Prior art keywords
- composite material
- shovel
- internal channels
- manufacturing
- yarns
- Prior art date
Links
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
- 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
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/52—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles soluble or fusible
-
- 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
- B29C70/40—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
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
-
- 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
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/224—Carbon, e.g. graphite
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Textile Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Woven Fabrics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
método de fabricação de uma pá de material compósito tendo canais internos, e uma pá de turbomáquina de material compósito. pá (10) de turbomáquina de material compósito compreendendo um reforço fibroso obtido por tecelagem de uma primeira pluralidade de fios e uma segunda pluralidade de fios, os fios da referida primeira pluralidade de fios sendo dispostos em camadas sucessivas e estendendo-se na direção longitudinal do esboço fibroso correspondendo à direção longitudinal da pá (10), o referido reforço sendo densificado por uma matriz. a pá compreende um ou vários canais internos (21, 22, 23) estendendo-se na direção longitudinal de referida pá.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1050503A FR2955609B1 (fr) | 2010-01-26 | 2010-01-26 | Aube composite a canaux internes |
PCT/FR2011/050107 WO2011092416A1 (fr) | 2010-01-26 | 2011-01-20 | Methode de fabrication d'une aube a canaux internes en composite et aube de turbomachine en composite |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112012018456A2 true BR112012018456A2 (pt) | 2017-06-20 |
Family
ID=43017146
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012018456A BR112012018456A2 (pt) | 2010-01-26 | 2011-01-20 | método de fabricação de uma pá de material compósito tendo canais internos, e uma pá de turbomáquina de material compósito |
Country Status (8)
Country | Link |
---|---|
US (1) | US10180069B2 (pt) |
EP (1) | EP2528727B1 (pt) |
CN (1) | CN102741043B (pt) |
BR (1) | BR112012018456A2 (pt) |
CA (1) | CA2787358C (pt) |
FR (1) | FR2955609B1 (pt) |
RU (1) | RU2559451C2 (pt) |
WO (1) | WO2011092416A1 (pt) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
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US8662855B2 (en) * | 2010-08-31 | 2014-03-04 | United Technologies Corporation | Integrally woven composite fan blade using progressively larger weft yarns |
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 |
US20120260590A1 (en) * | 2011-04-12 | 2012-10-18 | Lambert Walter L | Parallel Wire Cable |
US9328623B2 (en) * | 2011-10-05 | 2016-05-03 | General Electric Company | Turbine system |
CN104105581B (zh) | 2012-01-25 | 2016-08-17 | 斯奈克玛 | 由复合材料制造螺旋桨叶片的方法 |
FR2985940B1 (fr) * | 2012-01-25 | 2014-10-24 | Snecma | Procede de fabrication d'une pale d'helice en materiau composite |
FR2989977B1 (fr) * | 2012-04-26 | 2014-05-23 | Snecma | Ebauche fibreuse tissee en une seule piece par tissage tridimensionnel pour la realisation d'une plate-forme a caisson ferme pour soufflante de turbomachine en materiau composite |
US10011043B2 (en) | 2012-04-27 | 2018-07-03 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite |
US10450235B2 (en) | 2012-04-27 | 2019-10-22 | General Electric Company | Method of producing an internal cavity in a ceramic matrix composite and mandrel therefor |
FR2999173B1 (fr) * | 2012-12-10 | 2015-12-18 | Snecma | Procede de realisation d'une aube de turbomachine en materiau composite oxyde/oxyde munie de canaux internes |
ITCO20120059A1 (it) * | 2012-12-13 | 2014-06-14 | Nuovo Pignone Srl | Metodi per produrre pale cave sagomate in 3d di turbomacchine mediante produzione additiva, pale cave di turbomacchina e turbomacchine |
EP3004559B1 (en) | 2013-05-29 | 2020-01-15 | General Electric Company | Method of forming a ceramic matrix composite component with cooling features |
US10054048B2 (en) * | 2013-07-26 | 2018-08-21 | Lockheed Martin Corporation | Suprression of shock-induced airflow separation |
EP2921647A1 (en) * | 2014-03-20 | 2015-09-23 | Alstom Technology Ltd | Gas turbine blade comprising bended leading and trailing edges |
FR3032145B1 (fr) | 2015-01-29 | 2017-02-10 | Snecma | Procede de fabrication d'une pale d'helice |
FR3032173B1 (fr) | 2015-01-29 | 2018-07-27 | Safran Aircraft Engines | Pale d'helice de turbopropulseur a soufflage |
FR3053328B1 (fr) * | 2016-06-29 | 2022-01-21 | Herakles | Procede de fabrication d'une piece en materiau composite a matrice ceramique |
JP6790967B2 (ja) * | 2017-03-31 | 2020-11-25 | 株式会社豊田自動織機 | 繊維構造体及び繊維強化複合材 |
EP3406778B1 (en) | 2017-05-22 | 2022-04-13 | Ratier-Figeac SAS | Method of manufacturing a composite aircraft blade |
US11066335B2 (en) * | 2017-09-06 | 2021-07-20 | General Electric Company | Articles for creating hollow structures in ceramic matrix composites |
EP3539758B1 (en) | 2018-03-14 | 2022-07-27 | Ratier-Figeac SAS | Method of manufacturing a composite article |
FR3084695A1 (fr) * | 2018-07-31 | 2020-02-07 | Safran Aircraft Engines | Aube composite a armature metallique et son procede de fabrication |
CN109278318A (zh) * | 2018-08-31 | 2019-01-29 | 武汉纺织大学 | 一种碳纤维织物增强尼龙复合材料的制备方法 |
US11040915B2 (en) * | 2018-09-11 | 2021-06-22 | General Electric Company | Method of forming CMC component cooling cavities |
FR3087701B1 (fr) * | 2018-10-30 | 2021-11-26 | Safran Aircraft Engines | Hybridation des fibres du renfort fibreux d'une aube de soufflante |
FR3087699B1 (fr) * | 2018-10-30 | 2021-11-26 | Safran Aircraft Engines | Hybridation des fibres du renfort fibreux d'une aube |
CN110076524B (zh) * | 2019-04-30 | 2020-07-31 | 沈阳透平机械股份有限公司 | 一种轴流型压缩机静叶流道板的加工方法 |
FR3100270B1 (fr) * | 2019-08-28 | 2021-07-30 | Safran Aircraft Engines | Hybridation des fibres du renfort fibreux d’une aube de soufflante |
US11180999B2 (en) * | 2019-12-20 | 2021-11-23 | General Electric Company | Ceramic matrix composite component and method of producing a ceramic matrix composite component |
US11326470B2 (en) * | 2019-12-20 | 2022-05-10 | General Electric Company | Ceramic matrix composite component including counterflow channels and method of producing |
US11441778B2 (en) * | 2019-12-20 | 2022-09-13 | Raytheon Technologies Corporation | Article with cooling holes and method of forming the same |
FR3106519B1 (fr) * | 2020-01-28 | 2022-01-28 | Safran | Préforme fibreuse tissée pour réaliser une pièce en matériau composite, notamment une aube de turbomachine |
FR3107719B1 (fr) * | 2020-03-02 | 2023-02-10 | Safran Aircraft Engines | Texture fibreuse pour aube de turbomachine en matériau composite |
FR3107918B1 (fr) | 2020-03-03 | 2022-09-16 | Safran Aircraft Engines | Aube de soufflante comprenant un insert de fibres raides |
CN113182783A (zh) * | 2021-05-11 | 2021-07-30 | 四川简阳瑞特机械设备有限公司 | 喷嘴转动叶片加工工艺 |
FR3124107B1 (fr) * | 2021-06-17 | 2024-01-12 | Safran Aircraft Engines | Préforme fibreuse avec raidisseurs formés par des couches unidirectionnelles de fils |
CN114427481B (zh) * | 2022-01-06 | 2024-01-09 | 西北工业大学 | 具有内部冷却槽道的陶瓷基复合材料涡轮转子叶片、模具及制备方法 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
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SU954573A1 (ru) * | 1979-12-21 | 1982-08-30 | Предприятие П/Я А-1125 | Рабоча лопатка осевой турбины |
US5013216A (en) * | 1988-09-09 | 1991-05-07 | Airfoil Textron Inc. | Composite blade perform with divergent root |
US4885973A (en) * | 1988-12-14 | 1989-12-12 | Airfoil Textron Inc. | Method of making composite articles |
RU2078948C1 (ru) * | 1993-12-30 | 1997-05-10 | Яков Петрович Гохштейн | Теплоизолированная турбинная лопатка |
JPH08207078A (ja) * | 1995-02-03 | 1996-08-13 | Kawamoto Seisakusho:Kk | プラスチック製品とその成形方法およびプラスチック製遠心羽根車とその成形方法 |
US6627019B2 (en) | 2000-12-18 | 2003-09-30 | David C. Jarmon | Process for making ceramic matrix composite parts with cooling channels |
US6746755B2 (en) * | 2001-09-24 | 2004-06-08 | Siemens Westinghouse Power Corporation | Ceramic matrix composite structure having integral cooling passages and method of manufacture |
FR2861143B1 (fr) * | 2003-10-20 | 2006-01-20 | Snecma Moteurs | Aube de turbomachine, notamment aube de soufflante et son procede de fabrication |
GB0428201D0 (en) * | 2004-12-22 | 2005-01-26 | Rolls Royce Plc | A composite blade |
BRPI0607568A2 (pt) * | 2005-05-03 | 2010-04-06 | Stork Sp Aerospace B V | método para fabricar um membro estrutural oco reforçado com fibra, e, membro estrutural oco reforçado com fibra |
FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
US7674093B2 (en) * | 2006-12-19 | 2010-03-09 | General Electric Company | Cluster bridged casting core |
FR2912469B1 (fr) * | 2007-02-12 | 2009-05-08 | Snecma Propulsion Solide Sa | Procede de fabrication d'une structure a lobes de melangeur de flux en cmc pour moteur aeronautique a turbine de gaz. |
FR2929149B1 (fr) * | 2008-03-25 | 2010-04-16 | Snecma | Procede de fabrication d'une aube creuse |
FR2939130B1 (fr) * | 2008-11-28 | 2011-09-16 | Snecma Propulsion Solide | Procede de fabrication de piece de forme de forme complexe en materiau composite. |
-
2010
- 2010-01-26 FR FR1050503A patent/FR2955609B1/fr active Active
-
2011
- 2011-01-20 BR BR112012018456A patent/BR112012018456A2/pt not_active IP Right Cessation
- 2011-01-20 CA CA2787358A patent/CA2787358C/fr active Active
- 2011-01-20 US US13/575,170 patent/US10180069B2/en active Active
- 2011-01-20 EP EP11704664.9A patent/EP2528727B1/fr active Active
- 2011-01-20 WO PCT/FR2011/050107 patent/WO2011092416A1/fr active Application Filing
- 2011-01-20 CN CN201180007349.2A patent/CN102741043B/zh active Active
- 2011-01-20 RU RU2012136437/05A patent/RU2559451C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2787358C (fr) | 2018-02-27 |
CN102741043A (zh) | 2012-10-17 |
FR2955609A1 (fr) | 2011-07-29 |
RU2559451C2 (ru) | 2015-08-10 |
RU2012136437A (ru) | 2014-03-10 |
EP2528727A1 (fr) | 2012-12-05 |
CA2787358A1 (fr) | 2011-08-04 |
FR2955609B1 (fr) | 2012-04-27 |
CN102741043B (zh) | 2016-03-30 |
EP2528727B1 (fr) | 2019-03-06 |
US10180069B2 (en) | 2019-01-15 |
WO2011092416A1 (fr) | 2011-08-04 |
US20130017094A1 (en) | 2013-01-17 |
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Legal Events
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B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 8A ANUIDADE. |
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B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO ARQUIVAMENTO PUBLICADO NA RPI 2497 DE 13/11/2018. |