GOALS
The project has been carried out in collaboration between FIDAMC and Airbus Defense and Space
A fully integrated component with skin, stiffeners and spar has been produced in only one shot by co-consolidation methodology and is representative of a cockpit frame assembled in the structural cockpit demonstrator of the regional aircraft project.
These cabin frames are currently being tested in ADS facilities.
RESULTS
- Design and manufacturing modular tooling to manufacture both frames symmetric and drawing with a solution to facilitate the heat transfer.
- Development of a new repair system “in service”, with local heating, for thermoplastic stiffened structure.
- Successful stiffened frames symmetric and drawing manufacturing with high integration by co- consolidation process..