BR112017003641A2 - palheta difusora, motor de turbina, e, método para fabricar uma palheta difusora. - Google Patents
palheta difusora, motor de turbina, e, método para fabricar uma palheta difusora.Info
- Publication number
- BR112017003641A2 BR112017003641A2 BR112017003641A BR112017003641A BR112017003641A2 BR 112017003641 A2 BR112017003641 A2 BR 112017003641A2 BR 112017003641 A BR112017003641 A BR 112017003641A BR 112017003641 A BR112017003641 A BR 112017003641A BR 112017003641 A2 BR112017003641 A2 BR 112017003641A2
- Authority
- BR
- Brazil
- Prior art keywords
- diffuser vane
- fiber reinforcement
- turbine engine
- fibers
- manufacturing
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/0005—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor using fibre reinforcements
-
- 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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
-
- 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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/17—Component parts, details or accessories; Auxiliary operations
- B29C45/40—Removing or ejecting moulded articles
-
- 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
-
- 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
- B29C70/78—Moulding material on one side only of the preformed part
-
- 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
-
- 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
-
- 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
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
-
- 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)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
a invenção se refere a uma palheta difusora (2) para um motor de turbina a gás, compreendendo um conjunto de palhetas (4) feito de um material compósito tendo um reforço de fibra densificado por uma matriz, o reforço de fibra sendo obtido de fibras longas pré-impregnadas, aglomeradas na forma de uma esteira, o conjunto de palhetas sendo provido pelo menos em uma borda dianteira com uma tira de reforço (10 1), a dita tira de reforço sendo feita de uma única tira de tecido unidirecional ou de artigo têxtil, ou por empilhamento de uma pluralidade de dobras pré-impregnadas de tecido unidirecional ou de artigo têxtil feito de fibras de carbono ou de fibras de vidro, e pelo menos uma plataforma (6, 8) posicionada em uma extremidade radial do conjunto de palhetas, a plataforma sendo feita de um material compósito tendo um reforço de fibra densificado por uma matriz, o reforço de fibra sendo obtido de fibras longas pré-impregnadas. a invenção se refere também a um método para fabricar tal palheta.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1458020A FR3025248B1 (fr) | 2014-08-27 | 2014-08-27 | Aube de redresseur en materiau composite pour moteur a turbine a gaz et son procede de fabrication |
FR1458020 | 2014-08-27 | ||
PCT/FR2015/052237 WO2016030613A1 (fr) | 2014-08-27 | 2015-08-20 | Aube de redresseur en matériau composite pour moteur a turbine a gaz et son procédé de fabrication. |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112017003641A2 true BR112017003641A2 (pt) | 2017-12-05 |
BR112017003641B1 BR112017003641B1 (pt) | 2022-03-22 |
Family
ID=51688328
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017003641-0A BR112017003641B1 (pt) | 2014-08-27 | 2015-08-20 | Palheta difusora, motor de turbina, e, método para fabricar uma palheta difusora |
Country Status (9)
Country | Link |
---|---|
US (1) | US20170254212A1 (pt) |
EP (1) | EP3194151A1 (pt) |
JP (1) | JP2017528641A (pt) |
CN (1) | CN106794641A (pt) |
BR (1) | BR112017003641B1 (pt) |
CA (1) | CA2957834C (pt) |
FR (1) | FR3025248B1 (pt) |
RU (1) | RU2703225C2 (pt) |
WO (1) | WO2016030613A1 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWI675052B (zh) * | 2018-03-15 | 2019-10-21 | 日商福美化學工業股份有限公司 | 擬等向性補強薄片、frp成形體、以及frp成形體之製造方法 |
GB201811019D0 (en) * | 2018-07-04 | 2018-08-15 | Rolls Royce Plc | Methos and Tool Set For Manufacturing A Composite Component |
FR3090462B1 (fr) * | 2018-12-21 | 2021-01-15 | Safran | Pièce en composite à renfort fibreux avec une résistance aux vibrations augmentée |
CN110039798A (zh) * | 2019-05-31 | 2019-07-23 | 洛阳北玻台信风机技术有限责任公司 | 一种碳纤维材质的三元流离心风机叶轮及其成型方法 |
FR3100741B1 (fr) * | 2019-09-13 | 2021-09-10 | Safran | Dispositif de fabrication d’une piece creuse |
CN113665039B (zh) * | 2020-05-15 | 2023-08-04 | 中国航发商用航空发动机有限责任公司 | 一种风扇叶片平台及其制备方法 |
US11352891B2 (en) | 2020-10-19 | 2022-06-07 | Pratt & Whitney Canada Corp. | Method for manufacturing a composite guide vane having a metallic leading edge |
US11946391B2 (en) * | 2021-03-11 | 2024-04-02 | General Electric Company | Turbine engine with composite airfoil having a non-metallic leading edge protective wrap |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB788517A (en) * | 1955-04-16 | 1958-01-02 | Elmer Pershing Warnken | Improvements relating to blades of air-foil configuration and method of making same |
FR1357485A (fr) | 1963-05-27 | 1964-04-03 | Voith Getriebe Kg | Raccord pour solidariser (de facon libérable et étanche aux fluides) deux sections de conduit tubulaire |
US4941937A (en) * | 1988-04-28 | 1990-07-17 | The Budd Company | Method for bonding reinforcement members to FRP panels |
US5141400A (en) * | 1991-01-25 | 1992-08-25 | General Electric Company | Wide chord fan blade |
DE4237031C1 (de) * | 1992-11-03 | 1994-02-10 | Mtu Muenchen Gmbh | Verstellbare Leitschaufel |
FR2699499B1 (fr) * | 1992-12-23 | 1995-03-10 | Eurocopter France | Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection. |
US6821087B2 (en) * | 2002-01-21 | 2004-11-23 | Honda Giken Kogyo Kabushiki Kaisha | Flow-rectifying member and its unit and method for producing flow-rectifying member |
US6648597B1 (en) * | 2002-05-31 | 2003-11-18 | Siemens Westinghouse Power Corporation | Ceramic matrix composite turbine vane |
US7645120B2 (en) * | 2005-04-27 | 2010-01-12 | Honda Motor Co., Ltd. | Flow-guiding member unit and its production method |
FR2892339B1 (fr) * | 2005-10-21 | 2009-08-21 | Snecma Sa | Procede de fabrication d'une aube de turbomachine composite, et aube obtenue par ce procede |
FR2907707B1 (fr) * | 2006-10-26 | 2009-01-30 | Snecma Sa | Procede de fabrication d'une aube temoin en materiau composite |
US7988094B2 (en) * | 2007-01-12 | 2011-08-02 | Scott Ernest Ostrem | Aircraft window erosion shield |
US7895745B2 (en) * | 2007-03-09 | 2011-03-01 | General Electric Company | Method for fabricating elongated airfoils for wind turbines |
FR2933634B1 (fr) * | 2008-07-10 | 2010-08-27 | Snecma | Aube redresseur de soufflante en composite 3d |
US8961142B2 (en) * | 2009-04-10 | 2015-02-24 | Xemc Darwind B.V. | Protected wind turbine blade, a method of manufacturing it and a wind turbine |
US20110194941A1 (en) * | 2010-02-05 | 2011-08-11 | United Technologies Corporation | Co-cured sheath for composite blade |
US20120003098A1 (en) * | 2010-07-01 | 2012-01-05 | Spx Cooling Technologies, Inc. | Flared tip fan blade and method of manufacturing same |
FR2965202B1 (fr) * | 2010-09-28 | 2012-10-12 | Snecma | Procede de fabrication d'une piece et piece massive composite obtenue par ce procede |
FR2975037B1 (fr) * | 2011-05-13 | 2014-05-09 | Snecma Propulsion Solide | Aube de turbomachine composite avec pied integre |
US8734925B2 (en) * | 2011-10-19 | 2014-05-27 | Hexcel Corporation | High pressure molding of composite parts |
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 |
JP2013181437A (ja) * | 2012-02-29 | 2013-09-12 | Mitsubishi Heavy Ind Ltd | 風車回転翼 |
FR2992887B1 (fr) * | 2012-07-09 | 2015-05-01 | Snecma | Procede de fixation d'un renfort metallique structurel sur une partie d'une aube de turbine a gaz en materiau composite et moule d'injection pour la mise en oeuvre d'un tel procede |
-
2014
- 2014-08-27 FR FR1458020A patent/FR3025248B1/fr active Active
-
2015
- 2015-08-20 JP JP2017511286A patent/JP2017528641A/ja active Pending
- 2015-08-20 WO PCT/FR2015/052237 patent/WO2016030613A1/fr active Application Filing
- 2015-08-20 US US15/506,343 patent/US20170254212A1/en not_active Abandoned
- 2015-08-20 RU RU2017109815A patent/RU2703225C2/ru active
- 2015-08-20 CN CN201580045790.8A patent/CN106794641A/zh active Pending
- 2015-08-20 BR BR112017003641-0A patent/BR112017003641B1/pt active IP Right Grant
- 2015-08-20 EP EP15763962.6A patent/EP3194151A1/fr not_active Withdrawn
- 2015-08-20 CA CA2957834A patent/CA2957834C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3025248B1 (fr) | 2019-08-23 |
RU2017109815A3 (pt) | 2019-02-13 |
WO2016030613A1 (fr) | 2016-03-03 |
BR112017003641B1 (pt) | 2022-03-22 |
CN106794641A (zh) | 2017-05-31 |
FR3025248A1 (fr) | 2016-03-04 |
CA2957834C (fr) | 2023-03-28 |
JP2017528641A (ja) | 2017-09-28 |
US20170254212A1 (en) | 2017-09-07 |
RU2703225C2 (ru) | 2019-10-15 |
RU2017109815A (ru) | 2018-09-27 |
EP3194151A1 (fr) | 2017-07-26 |
CA2957834A1 (fr) | 2016-03-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 20/08/2015, OBSERVADAS AS CONDICOES LEGAIS. |