IThe IIAMS project is related to the advanced low-weight and high-performance structures domain. More specifically, it is included inside the ITD Airframe development area and it involves the manufacturing and assembling of a new concept of a composite wing box structure that will be tested on the turboprop aircraft prototype of the programme. The main objective is develop an innovative pilot system able to manufacture an integrated R/H and L/H composite wing box structure according with JTI-CS2-2017-CFP07-AIR-02-53 topic specifications. This pilot system will be based on Out of Autoclave resin infusion technology, and its ultimate purpose is to demonstrate that an alternative technology (to prepreg + autoclave) with lower costs, reduced lead times and lesser environmental footprint can achieve similar design tolerances and quality levels. The result of this development will also allow portability. Mtorres will optimise its AFP technology to manufacture with the maximum productivity the spar and stringers to simplify the movement of the hot forming station. They propose to use a light table design to enable the human collaboration with robots as well as to facilitate the direct taping of dry fibres on the mould. Mtorres will use multi-function connections and optimise the ancillaries to simplify the subsequent infusion and curing processes. The infusion process will be simulated using specific software and CFD to avoid dry spots, increase the speed, minimise waste materials, decrease the exothermal risk and viscosity development. Then, experimental trials will be carried out using a precise control of the temperature and measuring the resin and hardener flows. It will be validated the use of self-heated mould and blankets but also "onsite" air ovens that can be placed on top of the tools during the cure process. It will be design, build and test lightweight tooling and modular and collapsible moulds to facilitate the demoulding process.

SMART-LAYUP activities described in the present proposal will contribute to develop and validate an advanced process of hybrid materials automated lay-up for manufacturing of regional aircraft composite fuselage which allows a significant reduction of the overall production costs and manufacturing flow. After a developmental phase to be performed at MTORRES site, the innovative process and related machine will be validated and costs assessed through the execution of dedicated lay-up tests and fabrication of fuselage demonstrators at Topic Manager plant.

In the aerospace industry very high quality standards have to be met. For the manufacturing of carbon fibre parts this is currently solved through extended end-of-line inspection in combination with re-work processes to deal with defective parts. Also, in-situ visual inspection is used for quality control, which is currently causing huge productivity losses (30%-50%) during lay-up and has become a real bottleneck in carbon fibre parts manufacturing. The project will provide a solution by developing inline quality control methods for the key process steps: automatic lay-up (dry fibre placement and automatic dry material placement) and curing. At the system level decision support systems will be developed that assist human decision-making when assessing defects and when planning the part flow through the production line. These will be supported by simulation tools for part verification and logistical planning. The future manufacturing of the A320neo wing covers will be provide the background for the developments. Each such wing cover consists of two parts, that each cost several hundred thousand Euros in manufacturing. Assuming the planned production rates of 60 planes per month from 2025, savings of 150 MEUR in production costs can be obtained per year. The consortium consists of all key players that will play a future role in the manufacturing of such large carbon fibre parts. Airbus with its research centers Airbus Group Innovations and FIDAMC will play a leading role in the consortium as far as the multi-stage manufacturing process is concerned. Machine builders (MTorres, Danobat) and research centers will develop the inline quality control, while Dassault Systémes will provide simulation support.

Development of key technologies to address a new wing design for a HER aircraft maturing up to TRL5: manufacturing, assembly, structural concepts and processes, concept studies, configuration and architecture trade offs for a full wing component are part of the activity. As a physical demonstration concept, the detail design and manufacturing of the relevant components of a centre wing section of a HER Aircraft will be addressed. Conceptual wing studies: configuration and architecture (structural arrangement, Systems allocation and disposition, flight control system) trade offs for a full wing. Full wing structural arrangement mock up for innovative wing concepts, Structural and Multidisciplinary Optimization studies for definition of the optimal structural configuration of wing. Demonstration platform: wingbox, high lift devices, control surfaces, load alleviation devices focusing on the centre section as a demonstration platform: - Integrated Centre section wing box structure with the inner Propulsion stage: Full span (pylon to pylon) torsion box concept representative of more ambitious tip 2 tip concept. Multispar concept, Access manholes and panels, Sustainable aviation fuel and Integrated Fuel vent systems. - Inner section Leading Edges, Integrated Inductive ice protection system integration, Multifunctionality: erosion, impact, Lightning, ice protection, Morphing concepts, Functional tests, Bird strike tests (virtual or real) - Inner section Flap and high lift solutions: Integrated flap solutions. Multifunctionality application to flap. Key processing technologies: Low cost-high integrated out of autoclave technologies. Dry fiber placement and liquid resin infusion for integrated multispar torsion box. Thermoplastic composites processing: In situ consolidation for integrated flap skin and Leading edge applications. Thermoplastic welding and co-consolidation for Integration. Bonding technologies exploration towards certifiable solutions.