MX371351B - Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg. - Google Patents
Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg.Info
- Publication number
- MX371351B MX371351B MX2015008509A MX2015008509A MX371351B MX 371351 B MX371351 B MX 371351B MX 2015008509 A MX2015008509 A MX 2015008509A MX 2015008509 A MX2015008509 A MX 2015008509A MX 371351 B MX371351 B MX 371351B
- Authority
- MX
- Mexico
- Prior art keywords
- curved
- fabricating
- composite
- prepreg tape
- carrier
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 3
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000003351 stiffener Substances 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
-
- 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
- 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
- B29C70/06—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
-
- 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
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
-
- 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
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
Es proporcionado un método de fabricación de un refuerzo compuesto que tiene un alma curveada y al menos una pestaña curveada. Una longitud sustancialmente recta de cinta unidireccional de prepreg (30) es colocada sobre un portador (32). Al menos la pestaña curveada es formada al utilizar el portador para orientar una primera porción de la cinta sobre una primera superficie de herramienta curveada. El alma curveada es formada al utilizar el portador para formar una segunda porción de la cinta sobre una segunda superficie de herramienta curveada.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/736,021 US9387657B2 (en) | 2010-11-12 | 2013-01-07 | Method of fabricating a curved composite structure using composite prepreg tape |
PCT/US2013/070918 WO2014107241A1 (en) | 2013-01-07 | 2013-11-20 | Method of fabricating a curved composite structure using composite prepreg tape |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2015008509A MX2015008509A (es) | 2016-01-20 |
MX371351B true MX371351B (es) | 2020-01-27 |
Family
ID=49684099
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015008509A MX371351B (es) | 2013-01-07 | 2013-11-20 | Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg. |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP2941345B1 (es) |
JP (1) | JP6353465B2 (es) |
KR (1) | KR102143668B1 (es) |
CN (1) | CN104903081B (es) |
BR (1) | BR112015013772B1 (es) |
CA (1) | CA2890761C (es) |
MX (1) | MX371351B (es) |
RU (1) | RU2631296C2 (es) |
WO (1) | WO2014107241A1 (es) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9387657B2 (en) | 2010-11-12 | 2016-07-12 | The Boeing Company | Method of fabricating a curved composite structure using composite prepreg tape |
US9701067B2 (en) | 2010-11-12 | 2017-07-11 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
WO2015053869A1 (en) * | 2013-10-07 | 2015-04-16 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
US10800111B2 (en) | 2015-06-16 | 2020-10-13 | The Boeing Company | Composite structure fabrication systems and methods |
JP7240559B2 (ja) * | 2020-03-31 | 2023-03-15 | 川崎重工業株式会社 | 航空機部品の中間生成品の製造方法および航空機部品 |
KR20230121031A (ko) * | 2020-09-17 | 2023-08-17 | 아이코맷 리미티드 | 테이프 배치 헤드 |
CN113334764B (zh) * | 2021-07-08 | 2023-07-04 | 上海交通大学 | 一种纤维横向铺带3d打印方法 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0773886B2 (ja) * | 1986-07-03 | 1995-08-09 | 東芝ケミカル株式会社 | 繊維強化プラスチック積層板からなるスペーサの製造方法 |
GB8629267D0 (en) * | 1986-12-08 | 1987-02-11 | Westland Plc | Laying pre-impregnated fibre reinforced material on surface |
US4961700A (en) * | 1988-12-15 | 1990-10-09 | Owens-Corning Fiberglas Corporation | Shaping means for the production of fiber-reinforced preform articles |
SU1805605A1 (ru) * | 1991-02-25 | 1996-07-20 | Киевский механический завод им.О.К.Антонова | Способ формования листовых деталей из композитов с синусоидальными гофрами |
JPH11158764A (ja) * | 1997-11-27 | 1999-06-15 | Nippon Resibon Corp | 強化繊維シート |
US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
US7943076B1 (en) * | 2005-05-03 | 2011-05-17 | The Boeing Company | Method of manufacturing curved composite structural elements |
DE102005044823B3 (de) * | 2005-09-20 | 2007-05-16 | Airbus Gmbh | Verfahren und Vorrichtung zum Aufbringen dünner Materiallagen auf eine Reliefform |
US7968169B2 (en) * | 2007-08-07 | 2011-06-28 | The Boeing Company | Compound contoured composite beams and fabrication methods |
JP5324788B2 (ja) * | 2008-01-09 | 2013-10-23 | 有限会社アズモ技研 | 繊維強化プラスチック、その製造方法、およびその製造キット |
JP2009221390A (ja) * | 2008-03-18 | 2009-10-01 | Jamco Corp | 複合材連続成形用プリプレグピールプライ |
US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US9278484B2 (en) * | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
US8709576B2 (en) * | 2008-11-21 | 2014-04-29 | Airbus Operations (Sas) | Curved structural part made of composite material and a process for manufacturing such a part |
US8551380B2 (en) * | 2010-11-12 | 2013-10-08 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
-
2013
- 2013-11-20 BR BR112015013772-5A patent/BR112015013772B1/pt active IP Right Grant
- 2013-11-20 JP JP2015551675A patent/JP6353465B2/ja active Active
- 2013-11-20 MX MX2015008509A patent/MX371351B/es active IP Right Grant
- 2013-11-20 WO PCT/US2013/070918 patent/WO2014107241A1/en active Application Filing
- 2013-11-20 RU RU2015117413A patent/RU2631296C2/ru active
- 2013-11-20 CA CA2890761A patent/CA2890761C/en active Active
- 2013-11-20 EP EP13799170.9A patent/EP2941345B1/en active Active
- 2013-11-20 CN CN201380069595.XA patent/CN104903081B/zh active Active
- 2013-11-20 KR KR1020157014303A patent/KR102143668B1/ko active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
BR112015013772A2 (pt) | 2017-07-11 |
JP2016501756A (ja) | 2016-01-21 |
MX2015008509A (es) | 2016-01-20 |
JP6353465B2 (ja) | 2018-07-04 |
KR20150104085A (ko) | 2015-09-14 |
BR112015013772B1 (pt) | 2021-06-08 |
CA2890761C (en) | 2017-08-22 |
CA2890761A1 (en) | 2014-07-10 |
CN104903081A (zh) | 2015-09-09 |
RU2631296C2 (ru) | 2017-09-20 |
EP2941345B1 (en) | 2021-10-20 |
EP2941345A1 (en) | 2015-11-11 |
RU2015117413A (ru) | 2017-02-09 |
WO2014107241A1 (en) | 2014-07-10 |
KR102143668B1 (ko) | 2020-08-12 |
CN104903081B (zh) | 2018-03-13 |
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Legal Events
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FG | Grant or registration |