Community Research and Development Information Service - CORDIS


The aim of this CfP is to manufacture a curved stiffened structure in thermoplastic representative of an aero-structure (i.e wing, fuselage panel or engine cowling) preferably with double curvature using thermoplastic high strength material (i.e PEEK) and an advanced pre-industrial “in situ consolidation” process through adaptation and enhancements of existing machine into a more advanced prototype.  Please refer for the full and formal topic description to Annex III of the Clean Sky 2 Work Plan 2014-2015 Amendment nr. 1  Version 3 (see under the tab "Topic Conditions and Documents")

Record Number: 669123 / Last updated on: 2015-05-26