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Advanced Integrated
Composite Tail Cone

project deals with aircraft composite structure
development and production

Technologies


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Through Thickness Reinforcement (TTR)

The ADVITAC project will study composite reinforcement using tufting for the creation of one-shot rivet-less fully integrated structures. Investigation of the structural behaviour of tufted composites offers very useful information to allow a greater understanding of the technology and also to provide faster paths to certification of tufted composite structures.

Progress beyond the state of the art expected from the project:

Tufting of composite T-joint

  • Optimisation of the distribution and density of Z-reinforcement
  • Tool design issues for implementation of TTR
  • Investigation of the distribution of the TTR on the interplay between through thickness and inplane permeability
  • Investigation of the effects of TTR on infusion
  • Failure management with selective use of TTR and/or nano-particles

The first step will be the investigation of the requirements needed to certify a new manufacturing technology like tufting, in collaboration with an industrial partner. The second step will be the manufacture of typical skin to stiffeners joints representative of the structural elements found in a tail cone and the testing of the joints.

Another aspect related to tufting (or stitching) is the development of specialised tooling necessary during the insertion of the through thickness reinforcement and transfer of the structure to the infusion/injection tool. This is described further in the section related to Moulding.

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News & Events

  • 8th February 2011

    25-26th May 2010 Technical meeting (Cranfield University)

    Read more

  • 8th February 2011

    23rd-24th September 2010 Progress meeting (NLR, The Netherlands)

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Project partners

DAHER NLR Tecnalia Corporación Tecnológica Cranfield University CORIOLIS composites
FFT: Free Field Technologies EMBRAER RECOMET IMPLEX SLR HONEYWELL