BR112014009733A2 - mandril de impregnação com reservatório a vácuo para a fabricação de um cárter de turbina a gás em material compósito - Google Patents
mandril de impregnação com reservatório a vácuo para a fabricação de um cárter de turbina a gás em material compósitoInfo
- Publication number
- BR112014009733A2 BR112014009733A2 BR112014009733A BR112014009733A BR112014009733A2 BR 112014009733 A2 BR112014009733 A2 BR 112014009733A2 BR 112014009733 A BR112014009733 A BR 112014009733A BR 112014009733 A BR112014009733 A BR 112014009733A BR 112014009733 A2 BR112014009733 A2 BR 112014009733A2
- Authority
- BR
- Brazil
- Prior art keywords
- mandrel
- vacuum reservoir
- manufacture
- composite material
- gas turbine
- 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
- B29C70/28—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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- 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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- 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
- B29C33/30—Mounting, exchanging or centering
-
- 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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- 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
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C2043/3205—Particular pressure exerting means for making definite 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
-
- 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
- B29L2031/748—Machines or parts thereof not otherwise provided for
- B29L2031/7504—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
- 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)
- Combustion & Propulsion (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1/1 resumo “mandril de impregnação com reservatório a vácuo para a fabricação de um cárter de turbina a gás em material compósito” trata-se de mandril de impregnação para a fabricação de um cárter de turbina a gás em material compósito que compreende um mandril (100) que tem uma parede central (102) e dois flanges laterais (104a, 104b), barras de compactação (106a, 106b) que compreendem, cada uma, uma cunha (108a, 108b) destinada a ser colocada em apoio contra a parte do reforço fibroso que cobre os ângulos formados entre a parede central e os flanges do mandril, e um rebordo de fixação (110a, 110b) destinado a ser fixado no flange correspondente do mandril, um envoltório flexível (118) que forma reservatório a vácuo destinado a ser aplicado pelo menos na parte do reforço fibroso que cobre a parede central do mandril e meios (120, 124) para injetar a resina em um espaço (122) delimitado entre o reservatório a vácuo e o mandril no nível de uma extremidade longitudinal do reforço fibroso e para extrair a mesma no nível de uma extremidade oposta.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161551544P | 2011-10-26 | 2011-10-26 | |
PCT/FR2012/052367 WO2013060966A1 (fr) | 2011-10-26 | 2012-10-17 | Mandrin d'impregnation a bache vide pour la fabrication d'un carter de turbine a gaz en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112014009733A2 true BR112014009733A2 (pt) | 2017-04-18 |
BR112014009733B1 BR112014009733B1 (pt) | 2020-04-07 |
Family
ID=47227962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014009733A BR112014009733B1 (pt) | 2011-10-26 | 2012-10-17 | mandril de impregnação para a fabricação de um cárter de turbina a gás em material compósito e máquina de enrolamento de uma textura fibrosa em um mandril de impregnação |
Country Status (9)
Country | Link |
---|---|
US (1) | US9415549B2 (pt) |
EP (1) | EP2771174B1 (pt) |
JP (1) | JP6092232B2 (pt) |
CN (1) | CN103889693B (pt) |
BR (1) | BR112014009733B1 (pt) |
CA (1) | CA2852379C (pt) |
IN (1) | IN2014DN03149A (pt) |
RU (1) | RU2618006C2 (pt) |
WO (1) | WO2013060966A1 (pt) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3005159B1 (fr) * | 2013-04-26 | 2015-05-15 | Snecma | Procedure de mesure de l'epaisseur d'une texture fibreuse enroulee sur un mandrin d'impregnation et machine d'enroulement mettant en œuvre un tel procede |
CN103801676B (zh) * | 2013-12-20 | 2015-10-28 | 西北工业大学 | Cf/Mg复合材料薄壁异型件液-固压力成形装置及方法 |
CN104890259B (zh) * | 2015-06-01 | 2017-07-28 | 陶友瑞 | 一种纤维增强mc尼龙的工艺及设备 |
EP3115184B1 (en) * | 2015-07-08 | 2018-09-12 | Airbus Operations GmbH | Improved method for vacuum bagging |
FR3048435B1 (fr) * | 2016-03-02 | 2018-04-06 | Safran Aircraft Engines | Installation et procede pour la fabrication d'une texture fibreuse en forme de bande presentant en section transversale un profil evolutif |
DK3727785T3 (da) * | 2017-12-18 | 2023-09-18 | Xtek Ltd | Isostatisk sidetryksafskærmet kompositkonsolidering |
US11479002B2 (en) | 2020-04-23 | 2022-10-25 | Raytheon Technologies Corporation | Compression tool and method of forming gas turbine engine components |
FR3114043B1 (fr) * | 2020-09-16 | 2022-09-09 | Safran Aircraft Engines | Moule pour la fabrication d’un carter de soufflante de turbomachine en matériau composite à dilatation différentielle |
FR3126916B1 (fr) * | 2021-09-16 | 2024-05-10 | Safran Aircraft Engines | Cale de compactage d’un moule de carter de soufflante |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1020798B (de) | 1955-05-17 | 1957-12-12 | Rene Droz | Messgeraet fuer Laengemessungen |
US4718959A (en) * | 1985-12-02 | 1988-01-12 | The B. F. Goodrich Company | Method of making a bearing assembly |
US5145621A (en) * | 1990-04-20 | 1992-09-08 | General Electric Company | Crossover mold tool for consolidating composite material |
US5597435A (en) * | 1992-12-24 | 1997-01-28 | General Electric Company | Method using restrained cauls for composite molding |
FR2735456B1 (fr) * | 1995-06-19 | 1997-09-12 | Europ Propulsion | Procedes et appareil pour la fabrication de pieces annulaires en materiau composite et de preformes pour ces pieces |
RU2213661C1 (ru) * | 2002-06-21 | 2003-10-10 | Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики | Разборная оправка для изготовления деталей цилиндрической формы |
FR2879498B1 (fr) * | 2004-12-16 | 2009-01-30 | Snecma Propulsion Solide Sa | Densification de structures fibreuses par rtm pour la realisation de pieces en materiau composite |
US7335012B2 (en) * | 2004-12-22 | 2008-02-26 | General Electric Company | Apparatus for fabricating reinforced composite materials |
US20070272346A1 (en) * | 2006-05-23 | 2007-11-29 | Gkn Westland Aerospace, Inc. | System and method for consolidating dry fabric around a mandrel |
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 |
US8440276B2 (en) * | 2008-02-11 | 2013-05-14 | Albany Engineered Composites, Inc. | Multidirectionally reinforced shape woven preforms for composite structures |
JP5151668B2 (ja) * | 2008-05-13 | 2013-02-27 | 東レ株式会社 | Frpの製造方法 |
JP5476916B2 (ja) * | 2009-10-16 | 2014-04-23 | 東レ株式会社 | 繊維強化プラスチックの製造方法 |
FR2958875B1 (fr) * | 2010-04-20 | 2017-07-07 | Snecma | Dispositif de fabrication d'un carter en materiau composite et procede de fabrication mettant en oeuvre un tel dispositif |
US9452562B2 (en) * | 2011-10-26 | 2016-09-27 | Snecma | Impregnation clamping mandrel for making gas turbine casings made of composite material |
-
2012
- 2012-10-17 JP JP2014537689A patent/JP6092232B2/ja active Active
- 2012-10-17 RU RU2014121009A patent/RU2618006C2/ru active
- 2012-10-17 CA CA2852379A patent/CA2852379C/fr active Active
- 2012-10-17 EP EP12791518.9A patent/EP2771174B1/fr active Active
- 2012-10-17 IN IN3149DEN2014 patent/IN2014DN03149A/en unknown
- 2012-10-17 BR BR112014009733A patent/BR112014009733B1/pt active IP Right Grant
- 2012-10-17 WO PCT/FR2012/052367 patent/WO2013060966A1/fr active Application Filing
- 2012-10-17 CN CN201280052933.4A patent/CN103889693B/zh active Active
- 2012-10-17 US US14/352,159 patent/US9415549B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN103889693A (zh) | 2014-06-25 |
US20140262046A1 (en) | 2014-09-18 |
CN103889693B (zh) | 2016-03-16 |
JP6092232B2 (ja) | 2017-03-08 |
US9415549B2 (en) | 2016-08-16 |
CA2852379A1 (fr) | 2013-05-02 |
WO2013060966A1 (fr) | 2013-05-02 |
IN2014DN03149A (pt) | 2015-05-22 |
BR112014009733B1 (pt) | 2020-04-07 |
CA2852379C (fr) | 2019-04-30 |
EP2771174A1 (fr) | 2014-09-03 |
RU2014121009A (ru) | 2015-12-10 |
JP2015501241A (ja) | 2015-01-15 |
RU2618006C2 (ru) | 2017-05-02 |
EP2771174B1 (fr) | 2015-12-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according art. 34 industrial property law | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure | ||
B09A | Decision: intention to grant | ||
B16A | Patent or certificate of addition of invention granted |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 17/10/2012, OBSERVADAS AS CONDICOES LEGAIS. |