GB1038883A - Improvements in or relating to the manufacture of reinforced plastics tubes - Google Patents

Improvements in or relating to the manufacture of reinforced plastics tubes

Info

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
Application number
GB3986263A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB1038883A publication Critical patent/GB1038883A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/60Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous 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.
GB3986263A 1962-10-18 1963-10-09 Improvements in or relating to the manufacture of reinforced plastics tubes Expired GB1038883A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2735538A1 (en) * 1977-08-06 1979-02-15 Bayer Ag FIBER COMPOSITE PROFILES

Cited By (6)

* Cited by examiner, † Cited by third party
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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