High-Performance Composites

JUL 2014

High-Performance Composites is read by qualified composites industry professionals in the fields of continuous carbon fiber and other high-performance composites as well as the associated end-markets of aerospace, military, and automotive.

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3 4 | H I G H - P E R F O R M A N C E C O M P O S I T E S T he Thermoplastic Affordable Primary Aircraft Struc- ture (TAPAS) consortium was launched in The Neth- erlands in 2009 with the goal of developing new ther- moplastic composite materials and processes for use in Airbus (Toulouse, France) aerostructures. The con- sortium is starting its second phase of application and mate- rial development, and its members hope, by 2017, to bring to market a thermoplastic composite fuselage and torsion-box concept that proves the viability of thermoplastics in com- mercial aerostructures. In addition to Airbus, the TAPAS consortium comprises a number of composite material suppliers, composite parts manufacturers and academic research institutions based in The Netherlands. They include project lead Fokker Aerostruc- tures (Hoogeveen), the Airborne Technology Center and Kok & Van Engelen (both based in The Hague), Dutch Thermoplastic Components (Alkmaar), Technobis Fibre Technologies (Uit- geest), TenCate Advanced Composites (Nijverdal), KE-works, CoDeT and Technische Universiteit Delft (all based in Delft), the University of Twente (Enschede) and the National Aero- space Laboratory, in Amsterdam. Arnt Offringa, director R&D; at Fokker, says that under the frst phase of the program, called TAPAS 1, the consortium TAPAS 2: Next steps in thermoplastic aerostructures TAPAS 1 successes set stage for TAPAS 2 The TAPAS 1 12m/39-ft thermoplastic composite torsion box (top photo), is shown during maximum load testing performed in July 2012. TAPAS 2 participants have been asked to take this structure to technology readiness level (TRL) 6 by 2015. The photo immediately above shows the TAPAS 1 thermoplastic composite fuselage skin demonstrator and the engineers who built it. TAPAS 2 partners will more closely evaluate minimum skin thickness requirements for it in the hope of proving its viability for use in new commercial aircraft. Source: Fokker Aerostructures Source: Fokker Aerostructures FEATURE / RESEARCH UPDATE BY JEFF SLOAN 0714HPC UpdateTapas-OK.indd 34 6/17/2014 10:45:34 AM

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