AU6617690A - Reinforced composite structural members - Google Patents
Reinforced composite structural membersInfo
- Publication number
- AU6617690A AU6617690A AU66176/90A AU6617690A AU6617690A AU 6617690 A AU6617690 A AU 6617690A AU 66176/90 A AU66176/90 A AU 66176/90A AU 6617690 A AU6617690 A AU 6617690A AU 6617690 A AU6617690 A AU 6617690A
- Authority
- AU
- Australia
- Prior art keywords
- reinforced composite
- structural members
- composite structural
- reinforced
- members
- 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.)
- Abandoned
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
- B29C70/06—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
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- 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
- B29C70/202—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 arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
-
- 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
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
-
- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Woven Fabrics (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8924590 | 1989-11-01 | ||
GB898924590A GB8924590D0 (en) | 1989-11-01 | 1989-11-01 | Reinforced composite structural members |
Publications (1)
Publication Number | Publication Date |
---|---|
AU6617690A true AU6617690A (en) | 1991-05-31 |
Family
ID=10665522
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU66176/90A Abandoned AU6617690A (en) | 1989-11-01 | 1990-11-01 | Reinforced composite structural members |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0500604A1 (de) |
JP (1) | JPH05501385A (de) |
AU (1) | AU6617690A (de) |
GB (2) | GB8924590D0 (de) |
WO (1) | WO1991006421A1 (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9117863D0 (en) * | 1991-08-19 | 1991-10-09 | Cambridge Consultants | Fibre preforms for structural composite components |
DE4342575A1 (de) * | 1993-10-12 | 1995-04-13 | Textilma Ag | Textileinlage zur Herstellung eines Faserverbundwerkstoffes sowie Faserverbundwerkstoff |
FR2998602B1 (fr) * | 2012-11-28 | 2015-06-05 | Lr Etanco Atel | Systeme d'isolation de batiments par l'exterieur. |
CA2922198C (en) | 2013-09-04 | 2021-06-15 | Biteam Ab | Method and means for weaving a 3d fabric, 3d fabric items thereof and their use |
CN112936912B (zh) * | 2021-04-12 | 2023-08-25 | 江苏集萃碳纤维及复合材料应用技术研究院有限公司 | 复合材料传动轴及其成型方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2334645C3 (de) * | 1973-07-07 | 1983-04-07 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8000 München | Verfahren zur Herstellung eines Trägers aus Faserverbundprofil |
JPS5841950A (ja) * | 1981-08-31 | 1983-03-11 | 東レ株式会社 | 繊維強化樹脂用補強基材 |
FR2564490B1 (fr) * | 1984-05-15 | 1986-09-19 | Aerospatiale | Perfectionnements aux profiles composites tricotes en trois dimensions et procede pour leur fabrication |
US4606961A (en) * | 1984-10-09 | 1986-08-19 | The Boeing Company | Discretely stiffened composite panel |
JPS61179731A (ja) * | 1984-12-29 | 1986-08-12 | 日本マイヤー株式会社 | 三次元構造材料 |
EP0236500B1 (de) * | 1985-09-13 | 1990-01-31 | Shikishima Canvas Kabushiki Kaisha | Faserstruktur zur verstärkung von baumaterial |
FR2602248B1 (fr) * | 1986-08-01 | 1989-11-24 | Brochier Sa | Structure textile multidimensionnelle pour le renforcement de materiaux stratifies et procede et metier a tisser permettant l'obtention d'une telle structure |
JPS63152637A (ja) * | 1986-12-16 | 1988-06-25 | Toray Ind Inc | 樹脂の補強用プリフオ−ム材 |
IT1218653B (it) * | 1987-04-08 | 1990-04-19 | Ferrari Spa Esercizio Fabbrich | Elemento strutturale portante composito per carrozzerie di veicoli e procedimento per la sua fabbricazione |
EP0329434B1 (de) * | 1988-02-19 | 1993-07-28 | Mitsubishi Jukogyo Kabushiki Kaisha | Textile Struktur für das Verstärken von Bauelementen, wie Balken, aus Verbundwerkstoffen und Verfahren zur Herstellung derselben |
JPH0823095B2 (ja) * | 1989-06-06 | 1996-03-06 | 東レ株式会社 | 補強繊維織物 |
-
1989
- 1989-11-01 GB GB898924590A patent/GB8924590D0/en active Pending
-
1990
- 1990-11-01 WO PCT/GB1990/001671 patent/WO1991006421A1/en not_active Application Discontinuation
- 1990-11-01 AU AU66176/90A patent/AU6617690A/en not_active Abandoned
- 1990-11-01 EP EP19900916108 patent/EP0500604A1/de not_active Withdrawn
- 1990-11-01 JP JP51485190A patent/JPH05501385A/ja active Pending
-
1992
- 1992-05-01 GB GB9209556A patent/GB2253639B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB9209556D0 (en) | 1992-07-08 |
JPH05501385A (ja) | 1993-03-18 |
WO1991006421A1 (en) | 1991-05-16 |
EP0500604A1 (de) | 1992-09-02 |
GB8924590D0 (en) | 1989-12-20 |
GB2253639B (en) | 1994-06-29 |
GB2253639A (en) | 1992-09-16 |
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