BR112015001033A2 - método para fabricar um revestimento de turbomáquina, e, revestimento de turbomáquina - Google Patents
método para fabricar um revestimento de turbomáquina, e, revestimento de turbomáquinaInfo
- Publication number
- BR112015001033A2 BR112015001033A2 BR112015001033A BR112015001033A BR112015001033A2 BR 112015001033 A2 BR112015001033 A2 BR 112015001033A2 BR 112015001033 A BR112015001033 A BR 112015001033A BR 112015001033 A BR112015001033 A BR 112015001033A BR 112015001033 A2 BR112015001033 A2 BR 112015001033A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbomachine
- coating
- protective layer
- manufacturing
- mandrel
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
- B29K2309/08—Glass
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
-
- 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
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2260/95—Preventing corrosion
-
- 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
-
- 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
- F05D2300/6032—Metal matrix composites [MMC]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
1 / 1 resumo âmãtodo para fabricar um revestimento de turbomãquina, e, revestimento de turbomãquinaâ a invenã§ã£o refere-se a um mã©todo para fabricar um revestimento de turbomã¡quina a partir de material compã³sito compreendendo as seguintes etapas sucessivas: - criar uma camada protetora semirrãgida a partir de fibras de vidro secas que protege contra corrosã£o galvã¢nica, - arranjar a camada protetora em um mandril perfilado aplicando a camada protetora contra o seu flange radial anular, - formar e densificar o reforã§o fibroso no mandril ainda cobrindo a camada protetora.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1256850A FR2993317B1 (fr) | 2012-07-16 | 2012-07-16 | Carter de turbomachine dans un materiau composite et procede de fabrication associe |
FR1256850 | 2012-07-16 | ||
PCT/FR2013/051626 WO2014013161A1 (fr) | 2012-07-16 | 2013-07-08 | Procédé de fabrication d'un carter de turbomachine dans un matériau composite et carter associé |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112015001033A2 true BR112015001033A2 (pt) | 2017-06-27 |
BR112015001033B1 BR112015001033B1 (pt) | 2021-11-30 |
Family
ID=47553188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015001033-4A BR112015001033B1 (pt) | 2012-07-16 | 2013-07-08 | Método para fabricar um revestimento de turbomáquina, e, revestimento de turbomáquina |
Country Status (9)
Country | Link |
---|---|
US (1) | US9909447B2 (pt) |
EP (1) | EP2872746B1 (pt) |
JP (1) | JP2015524757A (pt) |
CN (1) | CN104471195B (pt) |
BR (1) | BR112015001033B1 (pt) |
CA (1) | CA2879052C (pt) |
FR (1) | FR2993317B1 (pt) |
RU (1) | RU2637282C2 (pt) |
WO (1) | WO2014013161A1 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10392950B2 (en) | 2015-05-07 | 2019-08-27 | General Electric Company | Turbine band anti-chording flanges |
AU2016278867B2 (en) * | 2015-06-18 | 2020-04-23 | Nuovo Pignone Tecnologie Srl | Casing for a turbomachine |
AU2017248807A1 (en) | 2016-04-15 | 2018-10-25 | Felicitex Therapeutics, Inc. | Combinations for the treatment of neoplasms using quiescent cell targeting and inhibitors of mitosis |
CN107399091B (zh) * | 2017-07-11 | 2019-09-06 | 北京汽车集团有限公司 | 异形复合材料轴、其制备方法以及与金属法兰的连接方法 |
FR3074088B1 (fr) * | 2017-11-30 | 2021-02-12 | Safran Aircraft Engines | Carter en materiau composite renforce et son procede de fabrication |
FR3100561B1 (fr) * | 2019-09-10 | 2023-01-20 | Safran Aircraft Engines | Fixation d’une virole acoustique a une enveloppe de carter pour une turbomachine d’aeronef |
FR3105076B1 (fr) * | 2019-12-23 | 2023-04-14 | Safran Aircraft Engines | Procede de fabrication d’un carter pour une turbomachine d’aeronef |
CN117445243A (zh) * | 2023-12-21 | 2024-01-26 | 浙江航引新材料科技有限公司 | 一种法兰纤维预制体及其制备方法 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR200181300Y1 (ko) * | 1999-12-13 | 2000-05-15 | 포항종합제철주식회사 | 플랜지 이음에 있어서 갈바닉 부식 방지 장치 |
FR2869074B1 (fr) * | 2004-04-14 | 2006-07-21 | Snecma Moteurs Sa | Systeme de protection d'arbre principal de moteur a palier fusible |
US7431978B2 (en) * | 2004-12-22 | 2008-10-07 | General Electric Company | Reinforced matrix composite containment duct |
US7246990B2 (en) * | 2004-12-23 | 2007-07-24 | General Electric Company | Composite fan containment case for turbine engines |
US7429165B2 (en) * | 2006-06-14 | 2008-09-30 | General Electric Company | Hybrid blade for a steam turbine |
DE102006041321A1 (de) * | 2006-09-01 | 2008-03-06 | Rolls-Royce Deutschland Ltd & Co Kg | Gehäuseabschnitt, insbesondere Fangehäuse, für ein Gasturbinentriebwerk |
US7713021B2 (en) * | 2006-12-13 | 2010-05-11 | General Electric Company | Fan containment casings and methods of manufacture |
US20080157418A1 (en) * | 2006-12-27 | 2008-07-03 | Lee Alan Blanton | Methods for fabricating composite structures with flanges having tethered corners |
FR2913053B1 (fr) | 2007-02-23 | 2009-05-22 | Snecma Sa | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
US9032706B2 (en) * | 2008-09-26 | 2015-05-19 | Pratt & Whitney Canada Corp. | Composite fan case with integral containment zone |
US9140135B2 (en) * | 2010-09-28 | 2015-09-22 | United Technologies Corporation | Metallic radius block for composite flange |
US8672609B2 (en) * | 2009-08-31 | 2014-03-18 | United Technologies Corporation | Composite fan containment case assembly |
FR2966508B1 (fr) * | 2010-10-22 | 2015-04-03 | Snecma | Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication |
-
2012
- 2012-07-16 FR FR1256850A patent/FR2993317B1/fr active Active
-
2013
- 2013-07-08 EP EP13744717.3A patent/EP2872746B1/fr active Active
- 2013-07-08 US US14/415,183 patent/US9909447B2/en active Active
- 2013-07-08 CN CN201380037741.0A patent/CN104471195B/zh active Active
- 2013-07-08 JP JP2015522142A patent/JP2015524757A/ja active Pending
- 2013-07-08 WO PCT/FR2013/051626 patent/WO2014013161A1/fr active Application Filing
- 2013-07-08 CA CA2879052A patent/CA2879052C/fr active Active
- 2013-07-08 RU RU2015104986A patent/RU2637282C2/ru active
- 2013-07-08 BR BR112015001033-4A patent/BR112015001033B1/pt active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
BR112015001033B1 (pt) | 2021-11-30 |
CN104471195B (zh) | 2016-08-17 |
RU2015104986A (ru) | 2016-09-10 |
CN104471195A (zh) | 2015-03-25 |
US9909447B2 (en) | 2018-03-06 |
CA2879052A1 (fr) | 2014-01-23 |
EP2872746A1 (fr) | 2015-05-20 |
FR2993317B1 (fr) | 2014-08-15 |
FR2993317A1 (fr) | 2014-01-17 |
CA2879052C (fr) | 2020-04-14 |
WO2014013161A1 (fr) | 2014-01-23 |
EP2872746B1 (fr) | 2018-12-26 |
JP2015524757A (ja) | 2015-08-27 |
RU2637282C2 (ru) | 2017-12-01 |
US20150192032A1 (en) | 2015-07-09 |
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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] | ||
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 08/07/2013, OBSERVADAS AS CONDICOES LEGAIS. |