NOUS Composites Research Hub « [Di tutti gli esseri...] il più veloce è l'intelletto (νοῦς), perché corre ovunque.
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NOUS Composites Research Hub « [Di tutti gli esseri...] il più veloce è l'intelletto (νοῦς), perché corre ovunque. » Diogene Laerzio (I,35) Overview on our Solutions in Composites Manufacturing Background and Mission Overview on our Solutions in Composites Manufacturing Equipment and Engineering SW Market & Partners Aerospace Industry & Composites Thermoplastic vs. Thermoset Composites Technology - Targeted Innovation A Look to the Future 2014 NOUS Proprietary Background and Mission Overview on our Solutions in Composites Manufacturing NOUS Composites Research Hub was born 2012 from an innovation driven joint venture between Novotech s.r.l. and Compositi Avanzati s.r.l. with the aim to improve existing technologies and develop new solutions in design and manufacturing of composite materials. Thanks to a continuous exchange of engineering expertise and manufacturing capabilities a Team composed by valued researchers coming from Universities and Research Centres aspires to create a Centre of Excellence in the research and design of composites in Southern Europe. 2014 NOUS Proprietary Equipment and Engineering SW Overview on our Solutions in Composites Manufacturing Composites Manufacturing Process with: ABB IRB-6640/205/2.75 standard robot 8-fibre placement head, developed by Coriolis Composites s.a.s. (Quéven, France), mounted on a linear axis with a working length of 3m. The heating of the material can be performed by a 3kW laser (LDM 3000-100) or Infra-Red lamp; Hypaject MKIII Injection Thermostatted System up to 10bar Injection Pressure for RTM; 2 Freezers for Resin Prepreg Storage 1.0mx3.0m and 1.0mx1.8m; Redundant Vacuum Infusion Systems; Extractor Bench for Sanding Dust (Composites Tooling); Bench for Cutting composites. Product Design Simulation Process with: 2014 NOUS Proprietary Hot Press for RTM and CM with plates of 1.2mx1.8m, 400°C Insulated Plates; Composite Curing Oven 400°+/-2°C Uniformity Temperature of 1.0mx1.0mx1.2m with Vacuum Line; Background and Mission - NOVOTECH s.r.l. Overview on our Solutions in Composites Manufacturing Novotech s.r.l. is an engineering innovation partner for companies in the aerospace field and advanced technology industries. The Company has been founded in 1983 as spinoff consulting engineering company from the Department of Aerospace Engineering of the University of Naples “Federico II”. It still maintains roots and backbone with scientific institutions, as Universities and Research Centres, keeping a strong link and continuing relationship, especially, but not exclusively, in the aerospace field. Continual Novotech s.r.l. research leads to advanced, more robust solutions for even the most complex engineering problems. As a proof of such spirit, recently the Company decided to invest on innovative techniques for manufacturing of composites equipping itself of an Automated Fiber Placement machine. 2014 NOUS Proprietary Background and Mission - NOVOTECH s.r.l. Overview on our Solutions in Composites Manufacturing Since 1983 Novotech s.r.l. is aimed to Provide technical-scientific support (Aeroelastic and Acoustics Certification) and advanced testing support (Ground Vibration Tests, Noise Tests, Landing Gear Drop Tests) to SMEs as Partenavia, Generalavia, Sky Arrow, TECNAM, OMA SUD, Vulcanair and others. Develop technical-scientific partnerships on specific technological tasks with big aerospace industries: Aeritalia/Alenia Aermacchi: internal noise (ATR), advanced F.E.A. on metal-CFRP structures, European Research Programs; Alfa Romeo Avio/Fiat Avio: advanced F.E.A. on turbine components; AgustaWestland: advanced F.E.A. on metal-CFRP structures; Magnaghi Aeronautica: Crashworthiness of tanks, advanced F.E.A. on composite structures (Bombardier); DEMA: Aeroelastic calculations for gust loads on Bombardier G-7000. Work for the cross-sector technology transfer (Aerospace, Automotive, Railway, Naval and Civil Engineering) for some specific issues within its main competences. 2014 NOUS Proprietary Background and Mission - NOVOTECH s.r.l. Overview on our Solutions in Composites Manufacturing Novotech s.r.l. has always been involved in research projects in partnership with Universities, Research Centers and companies concerning design, testing and manufacturing of aeronautical structures as MESEMA (Magnetoelastic Energy Systems for Even More Electric Aircraft) FP6-AST3-CT-2003-502915, SARISTU (Smart Intelligent Aircraft Structures) FP7-AAT-2011-RTD-1, etc. In addition to these ongoing activities, Novotech s.r.l. has attended directly in the following research projects: ASAM: Advanced Simulation of Aircraft Mechanisms - EU Project (Call identifier: SP1JTI-CS-2013-01-GRA-02-023/Topic number: JTI-CS-2013-1-GRA-02-023); LAMITECH: Innovative Testing Methods for Automatic Layering of Hybrid Composite Materials (Program Contract Apulia Region - Alenia Aermacchi S.p.A.); PROALATECH: Structural Characterization and Repair Solutions Analysis of Innovative CFRP Empennages (Program Contract Apulia Region - Alenia Aermacchi S.p.A.); FACE : Friendly Aircraft Cabin Environment - EU Project (G4RD-CT2002-00764). 2014 NOUS Proprietary Background and Mission - Compositi Avanzati s.r.l. Overview on our Solutions in Composites Manufacturing Compositi Avanzati s.r.l. is a manufacturing firm which deals in design, development and production of composite components, either for structural or non-structural applications, through the Resin Transfer Moulding (RTM) process and other closed mould technologies. The main company business is the production of Carbon Fibre Reinforced Polymers (CFRP) for the aerospace industry either with thermosetting or thermoplastic matrices. Side production sectors are the naval, railway and automotive industries. The use of the closed mould technologies permits the realisation of composite elements with complex shape, tight dimensional tolerance, embedded inserts, high quality finished surfaces, excellent reproducibility on a part to part basis and environmental compliance. Besides manufacturing and quality control, Compositi Avanzati s.r.l. accomplishes the design of the elements to be realised by RTM or other closed mould processes, as well as a significant R&D activity to continuously improve the production process. Recently, Compositi Avanzati s.r.l. has provided to University of Naples “Federico II” a set of composite stiffened panels manufactured with RTM technique for an International Research and Technology Project concerning Aircraft Expedient Repairs. 2014 NOUS Proprietary Markets & Partners Overview on our Solutions in Composites Manufacturing Applications demanding low weight, high stiffness-to-weight and strength-to-weight as well as high productivity rates are the key targets for us. Markets Partners 2014 NOUS Proprietary Aerospace Industry & Composites trend STATUS AND TARGETS FOR COST OF COMPOSITE STRUCTURES Source: Composites Forecasts & Consulting Overview on our Solutions in Composites Manufacturing Today, metallic structures are being replaced by composites for vehicle weight reduction and resultant fuel savings. The costs of composite components have to be reduced down to the level known from conventional metal structures. This can only be achieved through changes in materials and manufacturing processes. 2014 NOUS Proprietary Thermoplastic vs. Thermoset Composites Thermoplastics are typically 4-times tougher than comparable thermosets, which results in more impact resistance and damage tolerance. are relatively insensitive to aircraft fluids and chemical attack, and with one exception (PEIs), insensitive to moisture. offer substantial reductions in flammability, smoke and toxicity performance. also exhibit a near-infinite shelf life at room temperature. The potential value that thermoplastics bring to the aerospace market becomes more apparent when neat resin performance characteristics are compared with raw material costs. Source: Composites Forecasts & Consulting LLC Overview on our Solutions in Composites Manufacturing Many TP polymers have raw material prices comparable to, and the high tensile strength of, common thermosetting resins. 2014 NOUS Proprietary High-Performance Composite - May 2011 Thermoplastic vs. Thermoset Composites Overview on our Solutions in Composites Manufacturing PEEK, PPS, PEI and PC show many favorable characteristics for application in both aerospace structures and interior components: The cost of finished TPs components can be roughly 20 to 40% lower than competing TS due to reduced handling, processing and assembly costs. TPs offer the option to fuse or weld molded subcomponents, which can reduce assembly weight and stress concentrations by eliminating fasteners and adhesives. For high-temperature applications, PPS, PEI and PEEK polymers also offer excellent thermal stability - beyond the capabilities of high-temperature epoxy TS (~180°C/~350°F). At elevated temperatures, PEEK and PPS TPs, priced between $4 and $72/lb ($9 and $160/kg) can offer potentially substantial savings compared to BMI and PI TS, priced between $42 and $400/lb ($92 and $880/kg). 2014 NOUS Proprietary Technology - Targeted Innovation Overview on our Solutions in Composites Manufacturing 00 Compression Moulding Process Resin Transfer Moulding Process Injection Moulding Process 2014 NOUS Proprietary Automated Fiber Placement Process Design & Manufacturing of Composite Layups by Compression Moulding Technique Overview on our Solutions in Composites Manufacturing Compression Moulding is a closed mould process in which a moulding charge is squeezed into a preheated mould taking a shape of the mould cavity and cured by the heat and pressure applied to the material. The process involves the following steps: A pre-weighed measure of a polymer assorted with slices reinforcing fibers, hardening agent, anti-adhesive agent and pigment is positioned into the lower half of the mould. The mould cavity is filled by forcing and pressing on the charge and thereby the upperhalf of the mould shift downwards. With the help of the ejector pin the mould is opened and the part is removed. This method is capable of reproducing fiber-reinforced plastic parts in significant volumes, with high quality finish surfaces, repeatability and speed. 2014 NOUS Proprietary Design & Manufacturing of Composite Layups by Resin Transfer Moulding Technique Overview on our Solutions in Composites Manufacturing This method offers high precision moulded parts and enables integrated solutions offering high quality and repeatability beyond a reduction of weight, costs and assembly time. Exploded view of components used in RTM process 2014 NOUS Proprietary View as built of Composite Stiffened Panels (TS) samples manufactured by RTM process for an International R&T Project with University of Naples “Federico II” Design & Manufacturing of Composite Layups by Resin Transfer Moulding Technique Overview on our Solutions in Composites Manufacturing TEST TRIAL: DESIGN AND DEVELOPMENT OF A RIB MANUFACTURED BY RTM PROCESS 2014 NOUS Proprietary Design & Manufacturing of Composite Layups by Injection Moulding Technique Overview on our Solutions in Composites Manufacturing Injection Moulding is a process in which molten polymer is forced under high pressure into a mold cavity through an opening (sprue). Injection Moulding is highly productive method providing high accuracy and control of shape of the manufactured parts. The method is profitable in mass production of large number of identical parts. Thermoplastics commonly used Injection Molding are PP, PC, ABS, N6. in ONGOING RESEARCH & DEVELOPMENT PROJECT : DEVELOPMENT OF A THERMOPLASTIC COMPOSITE SEAT ARMREST Injection speeds are typically 1 to 5 seconds, and as many as 2,000 small parts can be produced per hour in some multiple-cavity molds. Finite Element Analysis 2014 NOUS Proprietary Design & Manufacturing of Composite Layups by Automated Fiber Placement Technique Overview on our Solutions in Composites Manufacturing From this year NOUS is involved in research projects dealing with the investigation and characterization of innovative configurations and processing of CFRP multi-layer materials to manufacture with automated technology (LAMITECH Research: Program Contract Apulia Region - Alenia Aermacchi S.p.A.). . With an ABB IRB-6640/205Kg/2.75m standard robot having an 8-fibre placement head, mounted on a linear axis with a working length of 3m, we are able to process TS, TP and DF composite materials. TEST TRIAL: FLAT COMPOSITE PANEL WITH A RAMP The heating of the material can be performed by a 3kW laser or IR device. 2014 NOUS Proprietary DF 25’ for 16 plies (750 mm x 750 mm) TP 50’ for 16 plies (1500 mm x1500 mm) Design & Manufacturing of Composite Layups by Automated Fiber Placement Technique Overview on our Solutions in Composites Manufacturing COMPARISON OF DIFFERENT MANUFACTURING TECHNOLOGIES FOR CFRP FUSELAGE PANELS MULTI-LAYER MATERIALS DOUBLE CURVATURE COMPOSITE PANEL WITH RAMP Test trial CONCEPT, DESIGN AND FEASIBILITY STUDY 2014 NOUS Proprietary MANUFACTURING Design & AFP Manufacturing of Composite Parts Overview on our Solutions in Composites Manufacturing 2014 NOUS Proprietary Activities in Development Overview on our Solutions in Composites Manufacturing Production of a standard sandwich-structured composite with AFP procedure OOA Acceptance with AFP machine Productivity Test - Lamination of flat panels Productivity Test – Lamination of stringers for fuselage Productivity Test – Lamination of windows frame 2014 NOUS Proprietary Activities in Development Overview on our Solutions in Composites Manufacturing Rotating Positionner Vertical spindle axis interpolated with robot axis. ► Motorized head-stock. ► Handling capacity: 3 000 kg. ► Max tool diameter: 3 meters. ► Gear box reduction that has to be defined before being ordered: ► Max tool inertia 6000 m²kg, max speed 8 rpm and max acceleration 45°/s². ► Or max tool inertia 1500 kgm², max speed 16 rpm and max acceleration 90°/s². ► This payload on the positioner is only an approximate value regarding the final usage. For each mold, the load, inertia and torques have to be checked separately ► Repeatability: ±0.05 mm at 500 mm radius. ► The positioner is fixed to the ground nearby the linear axis. ► Customer color RAL. ► Foundations are not included in this option. ► Fixation by welding the linear unit to HEB beam integrated into the ground, into concrete with minimal characteristic C 20/25 thickness 220 mm. Customer foundation studies must be communicated to Coriolis in advance. ► HMI and software functionality, installation. ► Energy, air and vacuum supply system for Customer are available on request. 2014 NOUS Proprietary A Look to the Future Overview on our Solutions in Composites Manufacturing Out of autoclave solutions Multifunctional composites Increase capabilities in manufacturing even more complex shapes Analytical tools to support manufacturing processes Consolidation and reduction in parts required to produce assemblies 2014 NOUS Proprietary Thank you for your attention If You Want To Go Fast, Go Alone. If You Want To Go Far, Go Together. 2014 NOUS Proprietary