GB2484350B - Advanced fibre placement lay-up - Google Patents
Advanced fibre placement lay-upInfo
- Publication number
- GB2484350B GB2484350B GB1017058.7A GB201017058A GB2484350B GB 2484350 B GB2484350 B GB 2484350B GB 201017058 A GB201017058 A GB 201017058A GB 2484350 B GB2484350 B GB 2484350B
- Authority
- GB
- United Kingdom
- Prior art keywords
- fibre placement
- advanced fibre
- lay
- placement lay
- advanced
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
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
- B29C70/30—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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- 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
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
-
- 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
-
- 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
- B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
-
- 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
- B29C70/32—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 on a rotating mould, former or core
- B29C70/323—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 on a rotating mould, former or core on the inner surface of a rotating mould
-
- 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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
-
- 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
- B29D22/00—Producing hollow articles
-
- 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
- F01D25/243—Flange connections; Bolting arrangements
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1017058.7A GB2484350B (en) | 2010-10-08 | 2010-10-08 | Advanced fibre placement lay-up |
PCT/GB2011/051789 WO2012046021A1 (en) | 2010-10-08 | 2011-09-22 | Advance fibre placement lay-up |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1017058.7A GB2484350B (en) | 2010-10-08 | 2010-10-08 | Advanced fibre placement lay-up |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201017058D0 GB201017058D0 (en) | 2010-11-24 |
GB2484350A GB2484350A (en) | 2012-04-11 |
GB2484350B true GB2484350B (en) | 2013-06-05 |
Family
ID=43304327
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1017058.7A Active GB2484350B (en) | 2010-10-08 | 2010-10-08 | Advanced fibre placement lay-up |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2484350B (en) |
WO (1) | WO2012046021A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111655452A (en) * | 2017-12-06 | 2020-09-11 | 赛峰航空器发动机 | Method for making an ordered network of acoustic channels from a wear-resistant material |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9149997B2 (en) | 2012-09-14 | 2015-10-06 | United Technologies | Composite flange from braided preform |
US20140119904A1 (en) | 2012-11-01 | 2014-05-01 | United Technologies Corporation | In-situ pressure enhanced processing of composite articles |
US9481158B2 (en) * | 2013-07-11 | 2016-11-01 | The Boeing Company | Short course fiber placement head |
DE102015210959A1 (en) * | 2015-06-15 | 2016-12-15 | Schunk Kohlenstofftechnik Gmbh | Paddle wheel and method of making a paddle wheel |
US10399276B2 (en) | 2015-08-12 | 2019-09-03 | General Electric Company | System and method for controlling at least one variable during layup of a composite part using automated fiber placement |
FR3074445A1 (en) * | 2017-12-06 | 2019-06-07 | Safran Aircraft Engines | METHOD FOR INTEGRATED ADDITIVE MANUFACTURE OF A COATING ON A TURBOMACHINE CARTER |
BR112020011357B1 (en) * | 2017-12-06 | 2023-12-19 | Safran Aircraft Engines | METHOD FOR IN SITU DEPOSITION OF A COATING BY ADDITIVE MANUFACTURING, SYSTEM FOR DEPOSITION OF FILAMENTARY MATERIAL, AND COATING OF TURBOM MACHINE WALLS SUSCEPTIBLE TO ABRASION |
US11724467B2 (en) * | 2020-12-18 | 2023-08-15 | The Boeing Company | System and method for laying up composite barrel shaped structures |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050023414A1 (en) * | 2003-07-28 | 2005-02-03 | The Boeing Company | Composite fuselage machine |
US20050039844A1 (en) * | 2003-08-22 | 2005-02-24 | The Boeing Company | Automated composite lay-up to an internal fuselage mandrel |
US20080196825A1 (en) * | 2007-02-21 | 2008-08-21 | Alexander Hamlyn | Method and apparatus for making structures of composite material, in particular airplane fuselage sections |
GB2452298A (en) * | 2007-08-30 | 2009-03-04 | Gkn Aerospace Services Ltd | Composite structure with a hollow body and a rim |
EP2433783A2 (en) * | 2010-09-27 | 2012-03-28 | CLAAS Fertigungstechnik GmbH | Lay-up apparatus and method for producing a workpiece made of composite material |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT311668B (en) * | 1969-11-04 | 1973-11-26 | Herd Und Ofenfabrik Koloseus E | Device for the production of hollow bodies |
DE2031959A1 (en) * | 1970-06-27 | 1972-01-13 | Maschf Augsburg Nuernberg Ag | Two layer plastic pipe - with longitudinally reinforced inner layer and circumferentially reinforced outer layer |
DE10251580B4 (en) * | 2002-03-08 | 2013-01-10 | Airbus Operations Gmbh | Method for producing a component made of fiber-reinforced plastic |
US7138167B2 (en) * | 2002-08-12 | 2006-11-21 | Shikibo Ltd. | Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform |
US8475895B2 (en) * | 2006-11-21 | 2013-07-02 | General Electric Company | Articles comprising composite structures having mounting flanges |
DE102008042574B4 (en) * | 2008-10-02 | 2010-06-10 | Airbus Deutschland Gmbh | Apparatus for depositing and draping sections of a reinforcing fiber structure to produce a profile preform and method |
-
2010
- 2010-10-08 GB GB1017058.7A patent/GB2484350B/en active Active
-
2011
- 2011-09-22 WO PCT/GB2011/051789 patent/WO2012046021A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050023414A1 (en) * | 2003-07-28 | 2005-02-03 | The Boeing Company | Composite fuselage machine |
US20050039844A1 (en) * | 2003-08-22 | 2005-02-24 | The Boeing Company | Automated composite lay-up to an internal fuselage mandrel |
US20080196825A1 (en) * | 2007-02-21 | 2008-08-21 | Alexander Hamlyn | Method and apparatus for making structures of composite material, in particular airplane fuselage sections |
GB2452298A (en) * | 2007-08-30 | 2009-03-04 | Gkn Aerospace Services Ltd | Composite structure with a hollow body and a rim |
EP2433783A2 (en) * | 2010-09-27 | 2012-03-28 | CLAAS Fertigungstechnik GmbH | Lay-up apparatus and method for producing a workpiece made of composite material |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111655452A (en) * | 2017-12-06 | 2020-09-11 | 赛峰航空器发动机 | Method for making an ordered network of acoustic channels from a wear-resistant material |
CN111655452B (en) * | 2017-12-06 | 2023-01-17 | 赛峰航空器发动机 | Method for making an ordered network of acoustic channels from a wear-resistant material |
Also Published As
Publication number | Publication date |
---|---|
GB201017058D0 (en) | 2010-11-24 |
GB2484350A (en) | 2012-04-11 |
WO2012046021A1 (en) | 2012-04-12 |
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