BR112012030900A2 - método de fabricação de uma lâmina de turbomáquina - Google Patents
método de fabricação de uma lâmina de turbomáquinaInfo
- Publication number
- BR112012030900A2 BR112012030900A2 BR112012030900A BR112012030900A BR112012030900A2 BR 112012030900 A2 BR112012030900 A2 BR 112012030900A2 BR 112012030900 A BR112012030900 A BR 112012030900A BR 112012030900 A BR112012030900 A BR 112012030900A BR 112012030900 A2 BR112012030900 A2 BR 112012030900A2
- Authority
- BR
- Brazil
- Prior art keywords
- manufacturing
- turbocharger blade
- turbocharger
- blade
- Prior art date
Links
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
- 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
- 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
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- 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
- F05D2300/614—Fibres or filaments
-
- 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
- F05D2300/70—Treatment or modification of materials
- F05D2300/702—Reinforcement
-
- 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
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1055161A FR2961846B1 (fr) | 2010-06-28 | 2010-06-28 | Aube de turbomachine a geometrie asymetrique complementaire |
FR1055161 | 2010-06-28 | ||
PCT/FR2011/051431 WO2012001269A1 (fr) | 2010-06-28 | 2011-06-22 | Aube de turbomachine a geometrie asymetrique complementaire. |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112012030900A2 true BR112012030900A2 (pt) | 2016-11-08 |
BR112012030900B1 BR112012030900B1 (pt) | 2020-03-10 |
Family
ID=43532112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012030900-5A BR112012030900B1 (pt) | 2010-06-28 | 2011-06-22 | Método de fabricação de uma lâmina de turbomáquina |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP2585280B1 (pt) |
JP (1) | JP5866350B2 (pt) |
CN (1) | CN102971135B (pt) |
BR (1) | BR112012030900B1 (pt) |
CA (1) | CA2799706C (pt) |
FR (1) | FR2961846B1 (pt) |
RU (1) | RU2553872C2 (pt) |
WO (1) | WO2012001269A1 (pt) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2981602B1 (fr) * | 2011-10-25 | 2017-02-17 | Snecma Propulsion Solide | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs |
RU2612628C2 (ru) * | 2012-01-09 | 2017-03-09 | Снекма | Волокнистая предварительно отформованная заготовка лопатки газотурбинного двигателя, выполненная из композитного материала и имеющая встроенную платформу, и способ ее выполнения |
EP2802702B1 (fr) * | 2012-01-09 | 2018-12-26 | Safran Aircraft Engines | Piece de renfort a section en pi en materiau composite, notamment plate-forme de soufflante de turbomachine, et son procede de fabrication |
US9291061B2 (en) * | 2012-04-13 | 2016-03-22 | General Electric Company | Turbomachine blade tip shroud with parallel casing configuration |
FR2989608B1 (fr) * | 2012-04-24 | 2015-01-30 | Snecma | Procede d'usinage du bord de fuite d'une aube de turbomachine |
US9376916B2 (en) | 2012-06-05 | 2016-06-28 | United Technologies Corporation | Assembled blade platform |
GB201222975D0 (en) * | 2012-12-19 | 2013-01-30 | Composite Technology & Applic Ltd | An aerofoil structure |
CN104690982B (zh) * | 2013-12-10 | 2018-02-02 | 惠阳航空螺旋桨有限责任公司 | 一种发动机的复合材料静子叶片及其制备方法 |
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 |
FR3040147B1 (fr) | 2015-08-18 | 2018-04-20 | Safran Aircraft Engines | Aube composite avec element d'habillage aerodynamique integre et procede de fabrication de celle-ci |
FR3102392B1 (fr) * | 2019-10-29 | 2021-10-08 | Safran | Préforme fibreuse tissée pour réaliser une aube de soufflante en matériau composite |
CN111102017B (zh) * | 2019-12-13 | 2022-07-12 | 西安鑫垚陶瓷复合材料有限公司 | 航空发动机陶瓷基复合材料固定导向器叶片结构及其成型 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR958931A (pt) | 1950-03-21 | |||
FR2640258B1 (fr) | 1988-05-10 | 1991-06-07 | Europ Propulsion | Procede de fabrication de materiaux composites a renfort en fibres de carbure de silicium et a matrice ceramique |
US5827047A (en) * | 1996-06-27 | 1998-10-27 | United Technologies Corporation | Turbine blade damper and seal |
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 |
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 |
EP1916389A1 (en) * | 2006-10-26 | 2008-04-30 | Siemens Aktiengesellschaft | Turbine blade assembly |
RU2384749C1 (ru) * | 2008-11-11 | 2010-03-20 | РОССИЙСКАЯ ФЕДЕРАЦИЯ , от имени которой выступает МИНИСТЕРСТВО ПРОМЫШЛЕННОСТИ И ТОРГОВЛИ РОССИЙСКОЙ ФЕДЕРАЦИИ (МИНПРОМТОРГ РОССИИ) | Композитная лопатка вентилятора с многослойным армирующим материалом |
RU82009U1 (ru) * | 2008-11-18 | 2009-04-10 | Открытое акционерное общество Национальный институт авиационных технологий (ОАО НИАТ) | Композитная лопатка вентилятора |
FR2939129B1 (fr) * | 2008-11-28 | 2014-08-22 | Snecma Propulsion Solide | Aube de turbomachine en materiau composite et procede pour sa fabrication. |
-
2010
- 2010-06-28 FR FR1055161A patent/FR2961846B1/fr active Active
-
2011
- 2011-06-22 EP EP11738001.4A patent/EP2585280B1/fr active Active
- 2011-06-22 WO PCT/FR2011/051431 patent/WO2012001269A1/fr active Application Filing
- 2011-06-22 BR BR112012030900-5A patent/BR112012030900B1/pt active IP Right Grant
- 2011-06-22 RU RU2012153794/05A patent/RU2553872C2/ru active
- 2011-06-22 CA CA2799706A patent/CA2799706C/en active Active
- 2011-06-22 CN CN201180031842.8A patent/CN102971135B/zh active Active
- 2011-06-22 JP JP2013517439A patent/JP5866350B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
EP2585280B1 (fr) | 2018-06-13 |
FR2961846A1 (fr) | 2011-12-30 |
EP2585280A1 (fr) | 2013-05-01 |
CN102971135B (zh) | 2016-02-03 |
FR2961846B1 (fr) | 2012-08-03 |
RU2553872C2 (ru) | 2015-06-20 |
CN102971135A (zh) | 2013-03-13 |
CA2799706A1 (en) | 2012-01-05 |
RU2012153794A (ru) | 2014-08-10 |
JP5866350B2 (ja) | 2016-02-17 |
BR112012030900B1 (pt) | 2020-03-10 |
WO2012001269A1 (fr) | 2012-01-05 |
CA2799706C (en) | 2018-03-06 |
JP2013537595A (ja) | 2013-10-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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 22/06/2011, OBSERVADAS AS CONDICOES LEGAIS. |