IN2014DN03149A - - Google Patents
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- Publication number
- IN2014DN03149A IN2014DN03149A IN3149DEN2014A IN2014DN03149A IN 2014DN03149 A IN2014DN03149 A IN 2014DN03149A IN 3149DEN2014 A IN3149DEN2014 A IN 3149DEN2014A IN 2014DN03149 A IN2014DN03149 A IN 2014DN03149A
- Authority
- IN
- India
- Prior art keywords
- mandrel
- intended
- central wall
- side plates
- vacuum bag
- Prior art date
Links
- 230000003014 reinforcing effect Effects 0.000 abstract 2
- 238000005056 compaction Methods 0.000 abstract 1
- 239000002131 composite material Substances 0.000 abstract 1
- 238000005470 impregnation Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 230000002787 reinforcement Effects 0.000 abstract 1
- 239000011347 resin Substances 0.000 abstract 1
- 229920005989 resin Polymers 0.000 abstract 1
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
- 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
- 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
- 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
The invention relates to an impregnation mandrel for the production of a gas turbine casing made from composite material comprising: a mandrel (100) having a central wall (102) and two side plates (104a 104b); compaction bars (106a 106b) each including (i) a wedge (108a 108b) intended to bear against the fibrous reinforcing part covering the angles formed between the central wall and the side plates of the mandrel and (ii) an attachment flange (110a 110b) intended to be attached to the corresponding side plate of the mandrel; a flexible casing (118) forming the vacuum bag and intended to be applied at least against the fibrous reinforcing part covering the central wall of the mandrel; and means (120 124) for injecting resin into a space (122) defined between the vacuum bag and the mandrel at one of the longitudinal ends of the fibrous reinforcement and for extracting same at the opposite end.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201161551544P | 2011-10-26 | 2011-10-26 | |
| PCT/FR2012/052367 WO2013060966A1 (en) | 2011-10-26 | 2012-10-17 | Impregnation mandrel comprising a vacuum bag for the production of a gas turbine casing from composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2014DN03149A true IN2014DN03149A (en) | 2015-05-22 |
Family
ID=47227962
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN3149DEN2014 IN2014DN03149A (en) | 2011-10-26 | 2012-10-17 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9415549B2 (en) |
| EP (1) | EP2771174B1 (en) |
| JP (1) | JP6092232B2 (en) |
| CN (1) | CN103889693B (en) |
| BR (1) | BR112014009733B1 (en) |
| CA (1) | CA2852379C (en) |
| IN (1) | IN2014DN03149A (en) |
| RU (1) | RU2618006C2 (en) |
| WO (1) | WO2013060966A1 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3005159B1 (en) * | 2013-04-26 | 2015-05-15 | Snecma | PROCEDURE FOR MEASURING THE THICKNESS OF A FIBROUS TEXTURE WRAPPED ON AN IMPREGNATION CHUCK AND WINDING MACHINE USING SUCH A METHOD |
| CN103801676B (en) * | 2013-12-20 | 2015-10-28 | 西北工业大学 | C fthe liquid-solid pressure former of/Mg composite material thin wall profiled piece and method |
| US10226899B2 (en) * | 2015-01-02 | 2019-03-12 | The Boeing Company | System and method of forming a component using a mandrel assembly |
| CN104890259B (en) * | 2015-06-01 | 2017-07-28 | 陶友瑞 | A kind of Processes and apparatus of fiber reinforcement MC nylon |
| EP3115184B1 (en) * | 2015-07-08 | 2018-09-12 | Airbus Operations GmbH | Improved method for vacuum bagging |
| FR3048435B1 (en) * | 2016-03-02 | 2018-04-06 | Safran Aircraft Engines | INSTALLATION AND METHOD FOR MANUFACTURING FIBROUS BAND-SHAPED TEXTURE HAVING IN THE CROSS-SECTIONAL SECTION AN EVOLVING PROFILE |
| FR3068640B1 (en) * | 2017-07-07 | 2019-08-02 | Safran Aircraft Engines | METHOD AND TOOLS FOR MANUFACTURING A PIECE BY RESIN INJECTION IN A WOVEN FIBER PREFORM |
| ES2955978T3 (en) * | 2017-12-18 | 2023-12-11 | Xtek Ltd | Isostatic Lateral Pressure Armored Composite Consolidation |
| US11479002B2 (en) * | 2020-04-23 | 2022-10-25 | Raytheon Technologies Corporation | Compression tool and method of forming gas turbine engine components |
| FR3114043B1 (en) * | 2020-09-16 | 2022-09-09 | Safran Aircraft Engines | Mold for the manufacture of a turbomachine fan casing in composite material with differential expansion |
| FR3126916B1 (en) * | 2021-09-16 | 2024-05-10 | Safran Aircraft Engines | Compaction block of a fan casing mold |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1020798B (en) | 1955-05-17 | 1957-12-12 | Rene Droz | Measuring device for length measurements |
| 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 (en) * | 1995-06-19 | 1997-09-12 | Europ Propulsion | METHODS AND APPARATUS FOR MANUFACTURING COMPOSITE MATERIAL ANNULAR PARTS AND PREFORMS THEREFOR |
| RU2213661C1 (en) * | 2002-06-21 | 2003-10-10 | Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики | Built-up mandrel for manufacture of cylinder-shaped parts |
| FR2879498B1 (en) * | 2004-12-16 | 2009-01-30 | Snecma Propulsion Solide Sa | DENSIFICATION OF FIBROUS STRUCTURES BY RTM FOR THE PRODUCTION OF PARTS IN COMPOSITE MATERIAL |
| 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 (en) * | 2007-02-23 | 2009-05-22 | Snecma Sa | PROCESS FOR MANUFACTURING A GAS TURBINE CASE OF COMPOSITE MATERIAL AND CARTER THUS OBTAINED |
| US8440276B2 (en) * | 2008-02-11 | 2013-05-14 | Albany Engineered Composites, Inc. | Multidirectionally reinforced shape woven preforms for composite structures |
| JP5151668B2 (en) * | 2008-05-13 | 2013-02-27 | 東レ株式会社 | Manufacturing method of FRP |
| JP5476916B2 (en) * | 2009-10-16 | 2014-04-23 | 東レ株式会社 | Manufacturing method of fiber reinforced plastic |
| FR2958875B1 (en) | 2010-04-20 | 2017-07-07 | Snecma | DEVICE FOR MANUFACTURING A CASE OF COMPOSITE MATERIAL AND MANUFACTURING METHOD USING SUCH A DEVICE |
| CA2852376C (en) * | 2011-10-26 | 2020-04-07 | Snecma | Impregnation mandrel comprising a clamping system for the production of gas turbine casings from composite material |
-
2012
- 2012-10-17 EP EP12791518.9A patent/EP2771174B1/en active Active
- 2012-10-17 CA CA2852379A patent/CA2852379C/en active Active
- 2012-10-17 CN CN201280052933.4A patent/CN103889693B/en active Active
- 2012-10-17 BR BR112014009733A patent/BR112014009733B1/en active IP Right Grant
- 2012-10-17 US US14/352,159 patent/US9415549B2/en active Active
- 2012-10-17 WO PCT/FR2012/052367 patent/WO2013060966A1/en active Application Filing
- 2012-10-17 JP JP2014537689A patent/JP6092232B2/en active Active
- 2012-10-17 RU RU2014121009A patent/RU2618006C2/en active
- 2012-10-17 IN IN3149DEN2014 patent/IN2014DN03149A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| EP2771174B1 (en) | 2015-12-16 |
| RU2014121009A (en) | 2015-12-10 |
| WO2013060966A1 (en) | 2013-05-02 |
| CN103889693A (en) | 2014-06-25 |
| BR112014009733A2 (en) | 2017-04-18 |
| EP2771174A1 (en) | 2014-09-03 |
| BR112014009733B1 (en) | 2020-04-07 |
| US20140262046A1 (en) | 2014-09-18 |
| CA2852379A1 (en) | 2013-05-02 |
| US9415549B2 (en) | 2016-08-16 |
| JP2015501241A (en) | 2015-01-15 |
| RU2618006C2 (en) | 2017-05-02 |
| CN103889693B (en) | 2016-03-16 |
| JP6092232B2 (en) | 2017-03-08 |
| CA2852379C (en) | 2019-04-30 |
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