Composites Design and Manufacture (BEng) - MATS 324
Filament windingFibre placementTape layingPultrusionTube rolling.

PowerPoint presentation (412KB)

Filament winding [1-8 and Ăström pp 241-251].

Filament winding is a process in which continuous fibre reinforcements are precisely positioned in a pre-determined pattern on a rotating mandrel (the mould tool for filament winding). Filament winding machines are normally computer numerically controlled (CNC) to permit highly automated production of axisymmetric components.  A simple machine may have just two motions (degree-of-freedom): rotation of the mandrel and translation of a feed eye along an axis parallel to the machine axis. The complexity of the machine is characterised by the number of degrees of freedom: some machines may have up to six separately controlled axes (usually three orthogonal and three rotational axes).   

Design of filament wound components

The winding pattern for a filament wound component (typical product configurations include shafts, cylinders, domed ends, flywheels and spheres) may be:

Netting analysis is a simple approach to the design and structural analysis of filament wound components. The analysis assumes that:

Eckold [9] devotes a couple of pages to netting analysis. Evans and Gibson [10] have "shown that the stable angle of inclination of the fibres, where no strain-induced fibre rotations occur, deviates from the so-called 'ideal' fibre angle predicted by netting analysis by an amount that depends on the matrix-to-reinforcement-stiffness ratio. When the initial angle of inclination of the fibres deviates from the stable angle, the application of strain produces fibre rotation and nonlinear stress–strain relations result. Analytical expressions for the stress–strain relations have been obtained; they show the interaction of the parameters that control the shape of the stress–strain curves".

Manufacture

The fibres are supplied on creels.  Fibre tension is critical to the operation of a filament winding machine, so it is normal to have fibre tensioners (closed-loop controlled servo-driven "dancers") in the feed line. The tension required is dependent on the type of fibre, the part diameter and the winding pattern selected. The tension directly affects both fibre volume fraction and void content and, in turn, influences the stiffness and strength of the composite part.  It is difficult to maintain fibre tension on flat surfaces and hence axial (0°) winding is not a preferred orientation on cylinders.

The fibres are impregnated with resin by (a) immersion, (b) passing over a resin-wetted drum, or (c) injection into a die, before being led to a feed eye where a controlled band-width is set prior to positioning fibres on the mandrel.  The simplest fibre orientation to realise is the geodesic path which assumes non-slip winding.  Once winding has commenced this imposes a fixed fibre path at any point dictated by the Clairaut angle ( r.sin α = constant), where r is local radius, α is local angle.  At bosses, α = arcsin (rb/r) where rb = angle at the boss (the polar opening).  By exploiting friction, it is possible to achieve non-geodesic winding within limits.

Once the fibre package is positioned, the resin is taken to full cure, often by heating in an oven.  The final stage is mandrel removal to leave the desired hollow component.  This may be achieved by hydraulic rams for extracting steel mandrels.  For more complex structures, the mandrel may be a low melting point material (e.g. metal alloy) or a water soluble salt (e.g. leachable plaster) which can be washed out or a collapsible rubber or a non re-useable foam.  In some cases, where a liner is required for minimal gas permeability the liner may also function as the mandrel and hence not need to be removed.

It is possible to filament wind with prepreg tapes or with thermoplastic matrix composites.  The higher tack of prepreg resin, or cooling of the molten thermoplastic, permits greater deviations from the geodesic path.

Applications

Typical applications for filament wound structures include rocket motors, launch tubes, pressure vessels, storage tanks and pipes, drive shafts and fishing rods.

Covington and Baumgardner [11] reported the development of prototype fibreglass helicopter rotor blades using filament winding techniques.  A Goldsworthy Orbital Pin Winding machine for high volume production of blades with longitudinal unidirectional reinforcement could lay approximetely 40 kg/hour of fibreglass using 16 strands of 60-end count prepreg roving.  The machine was 14 m long, 4.5 m wide and weighed 13 tonnes.  Addition of a second winding head could almost double production rates.   A McClean-Anderson tube winding machine could lay in excess of 27 kg/hour of a similar prepreg roving.

McLarty [12] analysed the feasibility of filament winding on a hull shaped mandrel in such a way as to cover the mandrel with fibres at a variety of angles to yield a structure conforming to the contours of the mandrel.  The feasibility was verified by winding a 1/48 scale hull.  It was concluded that 62m ship hulls could be produced.  Chappelear et al [13] conducted further study toward the filament winding of a 46m glass reinforced plastics ship hull, and developed a 1/5 scale mandrel for the proposed MSH mine sweeper-hunter for the United States Navy.

Hunting Engineering used multiple mandrels to filament wind the tubes for the Light Anti-armour Weapon (LAW) at a rate of a nesting pair every four minutes (if my memory serves me well!) in combination with a continuous curing oven such that the mandrels circulated through the machine. 

Entec built "the world’s largest five-axis filament winding machine" [8] to produce wind turbine blades 45.72 m long with a diameter of 8.23 m and a weight in excess of 36 Mg.

San Diego Composites have recently announced [14, 15] the successful manufacture of a toroidal composite tank fabricated using automated fibre winding technology. Their website includes images of the winding machine, the completed component and stills from a video of the pressure test.

Suppliers of filament winding machines and control software

References
  1. ST Peters, WD Humphrey and RF Foral, Filament winding composite structure fabrication,
    SAMPE, Covina CA, 1991. ISBN 0-938994-55-7. Second edition, 1999. ISBN 0-938994-81-6.  UOP Library
  2. MS Babu, G Srikanth and S Biswas, Composite fabrication by filament winding - an insight, Technology Information, Forecasting and Assessment Council (TIFAC India), 2009.
  3. S Baksi, PR Basak and S Biswas, Innovation in filament winding – an Indian experience, Technology Information, Forecasting and Assessment Council (TIFAC India), 2009.
  4. J Colton, Filament winding (for ENG 4793: Composite Materials and Processes), Georgia Institute of Technology, undated - accessed 12:57 on 23 October 2009.
  5. S Koussios, OK Bergsma and A Beukers, Filament winding
    Part 1: determination of wound body related parameters, part 2: generic kinematic model and its solutions
    Composites Part A: Applied Science and Manufacturing, 2004, A35(2), 181-212.
  6. VV Vasiliev, VA Barynin and AF Rasin, Anisogrid lattice structures – survey of development and application,
    Composite Structures, November-December 2001, 54(2-3), 361-370.
  7. Advanced Composites: Manufacturing - Filament Winding Process, Addax, undated, - accessed 13:00 on 23 October 2009.
  8. Filament Winding, Entec Composite Machines Inc, undated - accessed 13:04 on 23 October 2009.
  9. G Eckold, Mechanics of materials behaviour, Chapter 3 in Design and Manufacture of Composite Structures, Woodhead Publishing, Cambridge, 1994 pages 86-88.  ISBN 1-85573-051-0.
  10. JT Evans and AG Gibson, Composite angle ply laminates and netting analysis, Proceedings of the Royal Society, Part A: Mathematical, Physical and Engineering Sciences, 8 December 2002, 459(2028), 3079-3088.
  11. CE Covington and PS Baumgardner, Design and production of fibreglass helicopter rotor blades, In EM Lenoe, DW Oplinger and JJ Burke (editors), Fibrous Composites in Structural Design, Plenum, New York and London, 1980, pages 497-513.
  12. DN Chappelear, T Aochi and RJ Milligan, Filament winding of a ship hull, Lockheed report LMSC-D945 402, October 1983. AD A134 577.
  13. JL McLarty, Feasibility of filament winding large ship hulls, McClean-Anderson report J2016, December 1981. AD A125 771.
  14. San Diego Composites successfully manufactures and tests a composite toroidal tank fabricated using automated fiber winding technology, San Diego Composites Inc, 07 October 2009.
  15. Toroidal Test Tank Delivers Better Resistance, NetComposites, 23 October 2009.

Video

  1. Filament winding a composite bottle (Crossfire on YouTube)
  2. Burst test of a composite toroidal pressure vessel (San Diego Composites Inc).

Fibre placement (Ăström pp 262, pp 292)

Fibre placement is a process in which a multi-axis robot is used to wet-wind yarn or roving around a series of pins (or similar restraints within a mould) in a predetermined pattern.  The name fibre placement is often taken to include filament winding.  The restraints around which the fibres are wound permit the construction of parts without the limitations of geodesic paths.  The process has been used to produce Geoform (filament wound lattice-work towers where mandrel coverage is only in specific bands) and has potential for automotive space frames.  The process is perhaps more applicable to thermoplastic matrix composites where on-line consolidation and cooling permit its use without the requirement for the fibre restraints.

Tape laying (Ăström pp 211-212)

Tape laying is a computer-numerically controlled (CNC) technique similar to fibre placement with the obvious difference that (prepreg) reinforcement tapes are laid.  The fibre delivery system usually employs a Cartesian framework for gross positioning (rather than a primarily rotational axis robot) with rotational freedoms close to the work-piece.  It may be used for thermoset or thermoplastic matrix composites but is usually limited to flat or low curvature surfaces.  It is often associated with high quality aerospace composites such as flight control surfaces and wing skins.

Pultrusion (Ăström pp 282-286 and Teel website)

The pultrusion process produces continuous lengths of constant cross-section solid or hollow composite profile.  The process is normally undertaken with thermoset resins, but pultrusion with thermoplastics is possible (albeit somewhat different in implementation).  The reinforcement is supplied as yarn or roving.  The fibres are impregnated with resin (by immersion, or by passing over a resin-wetted drum, or by injection into the die) before being pulled through a heated die.  High resin shrinkage is advantageous in this process as it reduces friction in the die (hence polyester resins are easier to process than epoxy resins).  Reinforcement tension is controlled as in filament winding.    After leaving the die, the profile is usually air-cooled before being gripped for pulling by hand-over-hand hydraulic clamps or conveyor belt/caterpillar track systems. To ensure a clean cut, the profile is usually gripped by a moving cut-off machine which travels fixed at a constant position on the profile to make the cut ("flying cutter") before returning to the start point.  The process is described in the following Figure:


Figure from http://www.acmanet.org/pic/images/schematic.jpg (no longer online)
Click on the image to go to the Pultrusion Industry Council/Composite Fabricators Association page

Quinn [P1] and Hartley [P2] have produced design manuals for pultruded profiles.  Design of pultruded profiles tends to seek uniform thickness in order to achieve uniform cooling and hence minimise residual stress.  For the manufacture of hollow profiles, it is necessary to arrange the fibre feed such that a cantilevered mandrel can enter the die from the fibre-feed end.

Applications of pultrusion include panels – beams – gratings – ladders - tool handles - ski poles – kites - hand rails – light poles – electrical insulators and enclosures – roll-up doors.  During construction of the Channel Tunnel, 450 km of cable trays were produced by pultrusion. The Maunsell Structural Plastics (MSP) Advanced Composites Construction System (ACCS = interlocking "standard" pultruded box-sections ) was used for the A19 Tees Viaduct deck enclosure, and for the construction of the Aberfeldy Bridge in Scotland and the Bonds Mill Lift Bridge in Gloucestershire (about one mile from the M4 at Junction 13).  Hollaway has monitored the creep performance of the Bonds Mill Lift Bridge.

Variants on the pultrusion process include:

Suppliers of pultrusion machines
Suppliers of pultruded sections

P1. JA Quinn, Design Manual: Engineered Composite Profiles, Fibreforce Composites, Runcorn, 1988.
P2. JR Hartley, Composite Profiles, November 2002. Download zipped 1.51MB PDF file Design Manual
P3. Pultrusion of Glass Fiber Composites, Owens Corning Technical Paper 58644, no date (available as a 230 KB PDF from http://www.owenscorning.com/ via a secure server ☺ )

Tube rolling

Tube rolling is a technique where pre-preg blanks are formed onto a mandrel and consolidated normally using shrink-wrap.  The process is most often used to manufacture fishing rod blanks.  Tube rolling companies include Hardy Advanced Composites and Kilwell FibreTube (New Zealand)

Centrifugal casting

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Updated by John Summerscales on 12-Feb-2014 12:14. Terms and conditions. Errors and omissions. Corrections.