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TRIMIS

New Hybrid Thermoplastic Composite Aerostructures manufactured by Out of Autoclave Continuous Automated Technologies

NHYTE

New Hybrid Thermoplastic Composite Aerostructures manufactured by Out of Autoclave Continuous Automated Technologies

Link to CORDIS:
Objectives: 

NHYTE project aims at developing and demonstrating concepts and methodologies enabling the realization of innovative integrated aero-structures, made of a new hybrid thermoplastic matrix composite material with multifunctional capabilities.

The high-performing material proposed, based on a commercial PEEK-Carbon Fiber Prepreg with addition of amorphous (PEI) films, answers to the needs to have reduced weight and consequently reduced fuel consumptions and emissions on an aircraft, as well as reduced manufacturing and operational costs. Demonstration aero-structures will be fabricated by an innovative working cell implementing an advanced continuous automated production process, including: automated hybrid material fabrication; manufacturing of skin panels by automated fiber placement in-situ consolidation process; fabrication of stringers by continuous forming; component assembly by induction welding. The innovative material, conceived and patented by a partner of the Consortium, is an example of multifunctional composite, since it returns both functions of toughness improvement (multilayer material) and process simplification.

This concept on one side will provide an advantage from the structural point of view, in terms of better impact damage performance; while on the other side major advantages will result on processing simplification, in particular including improved cycle times and lower energy consumptions, since it does not require the use of an autoclave curing phase. As of today, its usage has been limited to fabricate panels, only at laboratory level; hence, a suitable improvement finalized to process in industrial environment is needed.

Proposed process techniques and assembly will be the first step towards the industrial application of the innovative material. Consortium has set a target for weight saving not less than 5% for primary structures. Further reduction of full life cycle cost is expected from scrape material and end of life structures recycling.

Institution Type:
Institution Name: 
European Commission
Type of funding:
Lead Organisation: 

Novotech Aerospace Advanced Technology Srl

Address: 
VIA COSTANZI 3
74024 MANDURIA (TA)
Italy
EU Contribution: 
€1,350,000
Partner Organisations: 

Universite De Bretagne Sud

Address: 
RUE ARMAND GUILLEMOT 27
56100 LORIENT
France
EU Contribution: 
€350,000

University Of Bath

Address: 
Claverton Down
Bath
BA2 7AY
United Kingdom
EU Contribution: 
€554,440

Centro Di Ricerche Europeo Di Tecnologie Design E Materiali

Address: 
Strada Statale 7 Per Mesagne Km 7.3
72100 Brindisi
Italy
EU Contribution: 
€585,313

Lgai Technological Center Sa

Address: 
Campus Universidat Autonoma De Barcelona Facultad De Medicina
8193 Cerdanyola Barcelona
Spain
EU Contribution: 
€683,293

Easn Technology Innovation Services Bvba

Address: 
Terweidenstraat 28
3440 Budingen
Belgium
EU Contribution: 
€120,000

Leonardo - Societa Per Azioni

Address: 
Piazza Monte Grappa 4
195 Roma
Italy
EU Contribution: 
€1,164,186

Panepistimio Patron

Address: 
University Campus- Rio
26500 Patras
Greece
EU Contribution: 
€443,125
Technologies: 
Development phase: