JP2015514917A5 - - Google Patents
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- JP2015514917A5 JP2015514917A5 JP2015507575A JP2015507575A JP2015514917A5 JP 2015514917 A5 JP2015514917 A5 JP 2015514917A5 JP 2015507575 A JP2015507575 A JP 2015507575A JP 2015507575 A JP2015507575 A JP 2015507575A JP 2015514917 A5 JP2015514917 A5 JP 2015514917A5
- Authority
- JP
- Japan
- Prior art keywords
- fiber blank
- closed
- unconnected
- weft
- zone
- 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.)
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- 239000000835 fiber Substances 0.000 claims 68
- 238000011144 upstream manufacturing Methods 0.000 claims 8
- 239000002131 composite material Substances 0.000 claims 5
- 238000004519 manufacturing process Methods 0.000 claims 2
- 239000011159 matrix material Substances 0.000 claims 2
- 238000000034 method Methods 0.000 claims 2
- 238000009941 weaving Methods 0.000 claims 2
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1253881 | 2012-04-26 | ||
| FR1253881A FR2989977B1 (fr) | 2012-04-26 | 2012-04-26 | Ebauche fibreuse tissee en une seule piece par tissage tridimensionnel pour la realisation d'une plate-forme a caisson ferme pour soufflante de turbomachine en materiau composite |
| PCT/FR2013/050841 WO2013160584A1 (fr) | 2012-04-26 | 2013-04-17 | Ebauche fibreuse tissee en une seule piece par tissage tridimensionnel pour la realisation d'une plate-forme a caisson ferme pour soufflante de turbomachine en materiau composite. |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015514917A JP2015514917A (ja) | 2015-05-21 |
| JP2015514917A5 true JP2015514917A5 (enExample) | 2016-06-09 |
| JP6105051B2 JP6105051B2 (ja) | 2017-03-29 |
Family
ID=48430834
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015507575A Active JP6105051B2 (ja) | 2012-04-26 | 2013-04-17 | タービンエンジンファン用の複合材料から閉じたボックス構造プラットフォームを作るために3次元製織によって単一体として織られる繊維ブランク |
Country Status (9)
| Country | Link |
|---|---|
| US (2) | US10145039B2 (enExample) |
| EP (1) | EP2841631B1 (enExample) |
| JP (1) | JP6105051B2 (enExample) |
| CN (1) | CN104395515B (enExample) |
| BR (1) | BR112014026522B1 (enExample) |
| CA (1) | CA2871168C (enExample) |
| FR (1) | FR2989977B1 (enExample) |
| RU (1) | RU2623921C2 (enExample) |
| WO (1) | WO2013160584A1 (enExample) |
Families Citing this family (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2970715B1 (fr) * | 2011-01-21 | 2014-10-17 | Snecma | Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant |
| FR3018473B1 (fr) | 2014-03-17 | 2016-04-08 | Snecma | Procede de fabrication d'une plate-forme d'aube en materiau composite a joints integres pour soufflante de turbomachine |
| FR3037097B1 (fr) * | 2015-06-03 | 2017-06-23 | Snecma | Aube composite comprenant une plateforme munie d'un raidisseur |
| FR3029563B1 (fr) | 2014-12-08 | 2020-01-17 | Safran Aircraft Engines | Plateforme a faible rapport de moyeu |
| CN104723571B (zh) * | 2015-03-16 | 2016-10-05 | 天津工业大学 | 一种碳纤维盒型预制件的缝制方法及定型模具 |
| FR3035676B1 (fr) * | 2015-04-29 | 2017-05-12 | Snecma | Aube munie de plateformes possedant un raidisseur |
| JP6524880B2 (ja) * | 2015-10-15 | 2019-06-05 | 株式会社豊田自動織機 | 多層織物 |
| CN105442154B (zh) * | 2015-12-15 | 2017-05-10 | 机械科学研究总院先进制造技术研究中心 | 一种具有梯度结构的三维预制体织造方法 |
| US9725832B1 (en) * | 2016-02-09 | 2017-08-08 | Albany Engineered Composites, Inc. | Weaving multilayer products using multiple warp columns and heddle columns |
| US10436036B2 (en) | 2016-07-05 | 2019-10-08 | Safran Aircraft Engines | Fitted platform for a turbine engine fan, and a method of fabricating it |
| FR3060440B1 (fr) | 2016-12-21 | 2019-05-17 | Nimitech Innovation | Boitier auto-raidi en materiaux composites et procede de realisation |
| US10767502B2 (en) * | 2016-12-23 | 2020-09-08 | Rolls-Royce Corporation | Composite turbine vane with three-dimensional fiber reinforcements |
| US10557350B2 (en) | 2017-03-30 | 2020-02-11 | General Electric Company | I beam blade platform |
| FR3065182B1 (fr) * | 2017-04-13 | 2019-06-21 | Safran | Procede de fabrication d'une piece en materiau composite comportant un corps prolonge par une extremite de fixation renforcee |
| FR3082876B1 (fr) * | 2018-06-21 | 2021-01-22 | Safran Aircraft Engines | Soufflante comprenant une plateforme et un verrou de blocage |
| FR3084089B1 (fr) | 2018-07-23 | 2020-10-02 | Safran | Texture fibreuse pour carter en materiau composite a resistance au cisaillement amelioree |
| FR3093297B1 (fr) * | 2019-02-28 | 2022-08-12 | Safran Aircraft Engines | Procédé de réalisation d’une pièce en matériau tissé tenant compte du décadrage |
| CN109877993B (zh) * | 2019-03-05 | 2020-09-11 | 南京玻璃纤维研究设计院有限公司 | 一种预制体、一种复合部件以及一种复合部件的加工方法 |
| CN110318140B (zh) * | 2019-05-05 | 2020-08-18 | 宜兴市新立织造有限公司 | 一种实现四步法不等层织物一体化编织的编织方法 |
| KR102223117B1 (ko) * | 2019-05-29 | 2021-03-05 | 두산중공업 주식회사 | 트랜지션 피스과 이를 포함하는 연소기 및 가스 터빈 |
| FR3097904B1 (fr) | 2019-06-26 | 2021-06-11 | Safran Aircraft Engines | Plateforme inter-aube avec caisson sacrificiel |
| FR3105291B1 (fr) * | 2019-12-20 | 2023-03-10 | Safran Aircraft Engines | Aube de soufflante ou d’helice pour une turbomachine d’aeronef et son procede de fabrication |
| CN112626680B (zh) * | 2020-12-10 | 2022-04-22 | 南京玻璃纤维研究设计院有限公司 | 一种三维机织封闭式空腔结构的制备方法及其预制件 |
| FR3120374B1 (fr) * | 2021-03-03 | 2024-05-17 | Safran | Procédé de tissage tridimensionnel ou multicouche d’une structure fibreuse et structure fibreuse présentant un tissage tridimensionnel ou multicouche |
| FR3121865B1 (fr) * | 2021-04-14 | 2023-12-15 | Safran Aircraft Engines | Procédé de fabrication d’une aube creuse de turbomachine |
| US11920493B2 (en) | 2022-02-25 | 2024-03-05 | General Electric Company | Airfoil having a structural cell and method of forming |
| CN114635217B (zh) * | 2022-03-09 | 2023-05-09 | 南京玻璃纤维研究设计院有限公司 | 一种三维机织复合材料风扇流道平台预制件及其制备方法 |
| CN116604840A (zh) * | 2023-04-27 | 2023-08-18 | 中国航发北京航空材料研究院 | 一种双层结构复合材料包容机匣及其制备方法 |
| US12359570B2 (en) | 2023-10-27 | 2025-07-15 | General Electric Company | Composite airfoil assembly for a turbine engine |
| US12234745B1 (en) | 2023-11-03 | 2025-02-25 | General Electric Company | Variable pitch airfoil |
| US12215592B1 (en) | 2024-02-07 | 2025-02-04 | General Electric Company | Preform for making a casing structure for turbine engines |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3102559A (en) * | 1959-12-24 | 1963-09-03 | Raymond Dev Ind Inc | Woven honeycomb cellular fabrics |
| US5080142A (en) * | 1989-04-06 | 1992-01-14 | Hitco | Integrally woven multi-apertured multi-layer angle interlock fabrics |
| US5358758A (en) * | 1989-12-06 | 1994-10-25 | Albany International Corp. | Structural member |
| JPH03234840A (ja) * | 1990-02-05 | 1991-10-18 | Shikishima Kanbasu Kk | 筒状織物および該織物を用いた複合材料 |
| US5451448A (en) * | 1993-07-01 | 1995-09-19 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Flexible ceramic thermal protection system resistant to high aeroacoustic noise comprising a three-dimensional woven-fiber structure having a multilayer top fabric layer, a bottom fabric layer and an intermediate rib fabric layer |
| US6446675B1 (en) * | 2001-07-05 | 2002-09-10 | Albany International Techniweave, Inc. | Minimum distortion 3D woven preforms |
| DK1892071T4 (en) * | 2003-03-06 | 2018-10-15 | Vestas Wind Sys As | Process for preparing a preform |
| FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
| US7712488B2 (en) * | 2008-03-31 | 2010-05-11 | Albany Engineered Composites, Inc. | Fiber architecture for Pi-preforms |
| FR2939130B1 (fr) * | 2008-11-28 | 2011-09-16 | Snecma Propulsion Solide | Procede de fabrication de piece de forme de forme complexe en materiau composite. |
| FR2939153B1 (fr) * | 2008-11-28 | 2011-12-09 | Snecma Propulsion Solide | Realisation d'une structure fibreuse a epaisseur evolutive par tissage 3d |
| FR2946999B1 (fr) * | 2009-06-18 | 2019-08-09 | Safran Aircraft Engines | Element de distributeur de turbine en cmc, procede pour sa fabrication, et distributeur et turbine a gaz l'incorporant. |
| US7836917B1 (en) * | 2009-11-18 | 2010-11-23 | Paradox LLC | Weaving connectors for three dimensional textile products |
| FR2953885B1 (fr) * | 2009-12-14 | 2012-02-10 | Snecma | Aube de turbomachine en materiau composite et procede pour sa fabrication |
| FR2955609B1 (fr) * | 2010-01-26 | 2012-04-27 | Snecma | Aube composite a canaux internes |
| FR2957093B1 (fr) * | 2010-03-02 | 2012-03-23 | Snecma | Preforme fibreuse pour un secteur d'anneau de turbine et son procede de fabrication. |
| US10280537B2 (en) | 2011-12-14 | 2019-05-07 | Sanfran Aircraft Engines | Fiber structure woven as a single piece by 3D weaving and application to the manufacturing of composite material part |
-
2012
- 2012-04-26 FR FR1253881A patent/FR2989977B1/fr active Active
-
2013
- 2013-04-17 WO PCT/FR2013/050841 patent/WO2013160584A1/fr not_active Ceased
- 2013-04-17 CN CN201380026193.1A patent/CN104395515B/zh active Active
- 2013-04-17 BR BR112014026522-4A patent/BR112014026522B1/pt active IP Right Grant
- 2013-04-17 US US14/397,052 patent/US10145039B2/en active Active
- 2013-04-17 RU RU2014147441A patent/RU2623921C2/ru active
- 2013-04-17 JP JP2015507575A patent/JP6105051B2/ja active Active
- 2013-04-17 CA CA2871168A patent/CA2871168C/fr active Active
- 2013-04-17 EP EP13722490.3A patent/EP2841631B1/fr active Active
-
2018
- 2018-09-21 US US16/138,529 patent/US10724159B2/en active Active
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