Press Forming

The stamp forming process for thermoplastic composites is well suited for automated high volume production. It is for example applied to manufacture large series of clips and brackets used in aeronautical structures. Application of the technology is, however, not straightforward as it largely relies on specific (and often inaccessible) knowhow and requires relatively large investment costs.

Contact: Mark Bouwman

Business Development and Lab Operations

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To establish processing guidelines and design tools for the high-precision stamp forming of thermoplastic composites.

Keywords: consolidation, stamp forming, molding, residual stresses, warpage, defects


Process window optimization and tool design are critical steps in the development of a new thermoplastic composite part, especially when stamp forming is used. For example, mold cavity design is not straight-forward when complex three-dimensional shells are manufactured. Fiber reorientation due to double curvature, followed by local thickening of the material, needs to be predicted to avoid a non-uniform pressure distribution. The occurrence of defects such as wrinkles is ideally prevented by i.e. a well-chosen blank holder design, but if unavoidable, the effect on the part performance should be known.


The basic principles behind the forming behavior of thermoplastic composites are identified and translated to predictive (numerical) models. The research includes further work on the characterization and description of the behavior of thermoplastic composites in melt conditions, extending previous work on continuous fiber reinforced thermoplastics to discontinuously reinforced polymers and hybrid combinations of these materials. Subsequently, the material performance is captured as a function of the process parameters, which allows for both the consistent design of a new part as well as the optimization of an existing process chain.

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  • Interested in application of the developed knowledge? Please contact Sebastiaan Wijskamp.