GB1038883A - Improvements in or relating to the manufacture of reinforced plastics tubes - Google Patents
Improvements in or relating to the manufacture of reinforced plastics tubesInfo
- Publication number
- GB1038883A GB1038883A GB3986263A GB3986263A GB1038883A GB 1038883 A GB1038883 A GB 1038883A GB 3986263 A GB3986263 A GB 3986263A GB 3986263 A GB3986263 A GB 3986263A GB 1038883 A GB1038883 A GB 1038883A
- Authority
- GB
- United Kingdom
- Prior art keywords
- core
- tube
- resin
- wound
- passes
- 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.)
- Expired
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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
-
- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
1,038,883. Pipe-making apparatus. C. GADANI, and U. GADANI, [trading as C.I.M.E.M. DI F. ILI GADANI]. Oct. 9, 1963 [Oct. 18, 1962], No. 39862/63. Heading F2P. Reinforced plastics tubes are made by extruding a plastics core, having a coefficient of thermal expansion greater than that of the reinforced resin to be used, from an extrusion press, winding a reinforcing glass fibre ribbon on to the core, depositing a layer of resin on the glass fibre windings to impregnate the same, subjecting the tube to thermosetting by heating to cause the core to dilate and compress the resin-impregnated windings and cooling the whole so that the core contracts to a greater extent than the tube and can be detached therefrom. A core 4 (Fig. 1a not shown), e.g. of polyvinyl chloride, cellulose acetate or polystyrene is continuously extruded from a worm extruder 1 preferably through a rotary head 2, passes through a cooling chamber 3, a support 5 and a caterpillar conveyer 7 or a helicoidal roller conveyer mounted on a rotating support 6, through further supports 5 (Fig. 1b and through a winding device 8. Said device 8 comprises a rotating collar 33 carrying arms 34, 35 arranged at 45 degrees to the direction of travel of the core, said arms carrying pivots on which are rotatably mounted drums 36, 37 holding a continuous ribbon 9 of glass fibre felt. Two arms 44, 45 extend from the arms 34, 35 and bear guiding rollers 42, 43. The collar 33 is rotated in the same direction as the core but at a lower speed by speed varying device 29. The core is thus wound with spirals of predetermined angle. The wound core then passes through two more supports 5 and through a covering device 38 comprising an internal cylinder 12 carrying a concertina'd fabric sheath 13 and surrounded by a protecting cylinder 14, the whole being connected to a rotating collar 11. The sheath 13 is applied to the tube to ensure that the glass fibres stay in position and so that the tube wall is completely formed and has a high degree of finish. The wound core then passes to an impregnation device which, as described comprises two feed tubes 17, 18 having resin spraying nozzles and situated above the machine, and a pressure roller 16 adjacent the wound core. Resin in the form of a catalyst and a polymerization-accelerating agent falls separately from each tube 17, 18 between the roller and wound core and evenly impregnates the reinforcement. The tube then passes through a calibrating ring 20 mounted on a rotary ring 19 and passes through a furnace (Fig. 1c, not shown) wherein the diameter of the core is increased to exert pressure on the wound layers and reaches a conveying frame 25 (Fig. 1d, not shown) wherein a distancer 26 and a circular saw 24 serve to cut the tube into predetermined lengths. As the tube cools the core contracts to a greater extent than that of the reinforced resin and can be extracted. The core can be recovered and recycled. The resins used for manufacture of the reinforced tube may be polyesters, epoxy resins, silicon resins, phenolic resins, acrylic resins.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2045962 | 1962-10-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1038883A true GB1038883A (en) | 1966-08-10 |
Family
ID=11167259
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3986263A Expired GB1038883A (en) | 1962-10-18 | 1963-10-09 | Improvements in or relating to the manufacture of reinforced plastics tubes |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH415030A (en) |
FR (1) | FR1378299A (en) |
GB (1) | GB1038883A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008133748A2 (en) | 2006-12-14 | 2008-11-06 | The Boeing Company | Method and related tool for minimizing fiber distortion during fabrication of one-piece composite barrel section |
WO2010084423A2 (en) * | 2009-01-21 | 2010-07-29 | Composites Atlantic Limited | Process for reducing wrinkles in composite laminated structures |
CN114173597A (en) * | 2019-08-02 | 2022-03-11 | 爱德兰丝株式会社 | Method for manufacturing wig and wig |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2735538A1 (en) * | 1977-08-06 | 1979-02-15 | Bayer Ag | FIBER COMPOSITE PROFILES |
-
1963
- 1963-10-01 CH CH1208463A patent/CH415030A/en unknown
- 1963-10-02 FR FR44054A patent/FR1378299A/en not_active Expired
- 1963-10-09 GB GB3986263A patent/GB1038883A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008133748A2 (en) | 2006-12-14 | 2008-11-06 | The Boeing Company | Method and related tool for minimizing fiber distortion during fabrication of one-piece composite barrel section |
WO2008133748A3 (en) * | 2006-12-14 | 2008-12-18 | Boeing Co | Method and related tool for minimizing fiber distortion during fabrication of one-piece composite barrel section |
EP2452807A1 (en) * | 2006-12-14 | 2012-05-16 | The Boeing Company | Method for minimizing fiber distortion during fabrication of one-piece composite barrel section |
WO2010084423A2 (en) * | 2009-01-21 | 2010-07-29 | Composites Atlantic Limited | Process for reducing wrinkles in composite laminated structures |
WO2010084423A3 (en) * | 2009-01-21 | 2010-09-30 | Composites Atlantic Limited | Process for reducing wrinkles in composite laminated structures |
CN114173597A (en) * | 2019-08-02 | 2022-03-11 | 爱德兰丝株式会社 | Method for manufacturing wig and wig |
Also Published As
Publication number | Publication date |
---|---|
CH415030A (en) | 1966-06-15 |
FR1378299A (en) | 1964-11-13 |
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