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Resin-transfer moulding

The liquid resin is then injected into the mould, typically from the bottom mould, assisted by pressure and vacuum to aid in providing an even resin distribution and achieving the removal of voids. A key processing consideration here is that the resin flow should match the wetting out and impregnation of the reinforcement. [Pg.393]

Quality-control tests and important process variables [Pg.393]

Typically vinyl ester, epoxy-resin and polyester systems with cure promoters are used at room temperature or under heated conditions. [Pg.393]

MOULD HALVES CLOSED —RESIN INJECTED AT BOTTOM-VACUUM APPLIED AT TOP — RISER TUBES PINCHED OFF AS RESIN RISES AND IS ALLOWED TO CURE-THEN MOULD OPENED AND PART RELEASED [Pg.394]

Cure kinetics and chemorheological models are key for characterizing and modelling RTM processes. For example, Lobo (1992) utilized the following kinetic and chemorheological models for a vinyl ester RTM resin. The kinetic model is given by [Pg.394]

This process is almost as versatile as contact moulding as regards selection of resin and reinforcement, and therefore the possible range of properties. Its primary advantage is that of reproducibility and reduced labour, though this is offset by increased tooling cost as it is a closed mould technique. [Pg.275]

Because the resin is injected into a mould containing the fabric, the key need is for good vet-out betvreen the resin and the rovings as the resin needs to dissolve the binder (finish) w hich holds the rovings in a bundle. [Pg.275]

Most fibres are designated as epoxy or polyester-compatible, but if other resins are to be used then the material suppliers need to be consulted as to the appropriate combination of fibre and resin. [Pg.275]

The best vray of checking compatibility is to compare the properties of the fibre/resin combination with a known combination either from this book or by measurement. [Pg.275]

A thermoplastic or thermoset binder can be used to bind layers of fabric or fibre bundles together. This allows specific orientations to be achieved and placing of local reinforcement as required by the design. [Pg.275]

RIM is a relatively new process. It can be used for processing of unfilled resin as well as fibre-reinforced composites. The process was discussed in Chapter 1. The process is similar to RTM (discussed previously) with some variation in mould release and reinforcement sizing to optimise resin chemistry with the process. The low viscosity reactant systems facilitate composite materials production, so-called structural RIM composites [19, 20] in which continuous fibre reinforcement mats are placed in mould cavities before injection. Capital investment and operational cost in RIM are therefore much less than those for conventional injection moulding. Polymerisation of a monomer is usually initiated by heat. However, in RIM, the polymerisation is initiated by impingement mixing (not by heat). Hence it is possible to activate polymerisation at relatively low temperature. Unlike RTM, in RIM the mould-fill times are very low ( 1 s) and a cycle time of 60 s is typical. The process is used for the rapid and automated production of large, thin and complex-shaped parts. [Pg.294]


For some years there has been concern at the amount of styrene vapour in workshops preparing reinforced polyester laminates. More recently this has increased interest in polyester-polyurethane hybrids and in the further development of closed moulding and resin transfer moulding techniques as well as greater use of lower styrene levels. [Pg.708]

Mcllhagger, A., Brown, D., and Hill, B. (2000). The development of a dielectric system for the on-line cure monitoring of the resin transfer moulding process. Composites Part A Appl. Sci. Manuf. 31(12), 1373-1381. [Pg.832]

Low clamping pressures only are needed, and this in turn means that quite large products can be made on inexpensive plant. By varying the raw materials it is possible to produce either rigid or flexible articles, microcellular or otherwise, and (if required) to include fillers or reinforcing sections. Thermosets other than polyurethane can be used—like epoxides and polyesters (with the latter, the process is known also as resin transfer moulding ). [Pg.149]

Abraham, D. Matthews, S. Mcllhagger, R. A comparison of physical properties of glass fiber epoxy composites produced by wet layup with autoclave consolidation and resin transfer moulding. Compos. Pt. A 1998, 29 (7), 795-801. [Pg.2322]

In resin-transfer moulding (RTM) there is typically a two-part mould, which forms a cavity corresponding to the final product shape. In the process, as shown in Figure 6.11, reinforcement, typically being a woven roving, cloth or mat, is placed (dry) in the female cavity, and then the male half is placed into position. [Pg.393]

Figure 6.11. A schematic diagram of resin-transfer moulding. Figure 6.11. A schematic diagram of resin-transfer moulding.
The use of these sensors is not restricted to high-performance composites, but can be extended to on-line monitoring of resin-transfer moulding (McIUiagger et al, 2000) and glass-polyester prepreg composite cure (Kim and Lee, 2002). [Pg.428]

In Resin Transfer Moulding preformed Carbon fibre and fabrics are placed in a mould along with the other components required to make the product. The mould is closed and premixed epoxy resin is injected into the fibrous mat. [Pg.22]

Damage tolerance of fibre reinforced thermoplastic composites Processing of polymer matrices using resin transfer moulding Fractal analysis of wear in short-fibre reinforced thermoplastic composites Rheology flow behavior of associative polymers in coating applications Kevlar-thermoplastic composites... [Pg.72]

Figure 3.6 Vacuum-assisted resin transfer moulding (VARTM). Figure 3.6 Vacuum-assisted resin transfer moulding (VARTM).
Figure 3.10 Compression resin transfer moulding (CRTM). Figure 3.10 Compression resin transfer moulding (CRTM).
Lowe JR, Owen MJ, Rudd CD. Void fonnation resin transfer moulding. In Proceedings of the 4th international conference on automated composites, ICAC95. Nottingham, Institute of Materials 1995. pp. 227—34. [Pg.73]

Scott FN, Heath R. Resin transfer moulding for civil aircraft manufacture. SAMPE European Chapter 1992. pp. 235—47. [Pg.74]

Kendall KN, Rudd CD, Owen MJ, Middleton V. Characterisation of the resin transfer moulding process. Compos Manuf 1992 3(2) 235—49. [Pg.74]

Ferland P, Guittard D, Trochu E. Concurrent methods for permeability measurement in resin transfer moulding. ModeUing and simulation of resin transfer moulding. Polym Compos 1996 17(l) 149-53. [Pg.74]

Lui B, Bickerton S, Advani G. Modelling and simulation of resin transfer moulding-gate control, venting and dry spot prediction. Compos Part A 19% 27a(2) 135—41. [Pg.74]

Potter KD. The early history of the resin transfer moulding process for aerospace applications. Compos Part A Appl Sci Manuf May 1999 30(5) 619—21. [Pg.74]

Bickerton S, Kelly P. Compression resin transfer moulding (CRTM) in polymer matrix composites. In Advani S, Hsiao K-T, editors. Manufacturing techniques for polymer matrix composites (PMCs). Cambridge (UK) Woodhead Publishing Limited 2012. [Pg.74]

Hamidi YK, Aktas L, Cengiz Allan M. Formation of microscopic voids in resin transfer moulded composites. J Eng Mater Technol Trans ASME 2004 126 420-6. [Pg.113]

Resin transfer moulding (RTM) As above, but long fibre reinforcement preform cut to shape and placed in cavity instead of using premixed short fibres. One half of mould cavity can be flexible Large, complex shapes for automotive and aerospace use. Relatively fast cycles... [Pg.34]

A further development is resin transfer moulding (RTM), in which long fibre reinforcement fabrics are cut to shape as preforms and placed in the mould cavity, before the resin is injected. This is potentially a slow process and one alternative is for the preforms to be made rapidly by spraying short fibres onto a suitably shaped pattern coated with an adhesive or binder. [Pg.37]


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