Objective Considering handling, costs and metallographic results multifilament alumina fibres were found to lead to best results within the investment casting process.Starting up with four different matrix alloys the AlZn6Mg1Ag1 showed best results in the MMC in case of best compatibility with the fibres.For optimisation of the alloy in the reinforced and the unreinforced status parameters and parameter windows for casting and heat treatment were defined:- Techniques for manufacturing performs for the considered geometries (unidirectional, windings) with defined fibre orientation and fibre content were found and optimised for all specimen and components within the project;- During the project the process parameters were continuously adapted and optimised on the two following production routes:a) Gas pressure infiltration (FIBRECAST) and;b) Autoclave gas pressure infiltration (MIT).* FIBRECAST: Based on the common investment casting process the requirements of the low gas pressure infiltration lead to an optimised ceramic mould with specially developed layers and to a casting unit. This includes casting in a vacuum chamber, starting the infiltration at a low environmental pressure.MIT: the autoclave gas pressure infiltration was adapted to ceramic shell moulds. This included the development of a gas-tight sealing for ceramic moulds.The monitoring of process parameters and comparison with results of mechanical testing and micro structural investigations led to optimised process parameter windows.A comparison with regard to handling and costs led to the decision to favour the FIBRECAST infiltration route.Micromechanical models were developed especially for continuous fibre MMCs. The data derived from mechanical testing was used to validate the computed results of the micromechanical modelling.Based on the verified mechanical properties of the MMCs in the reinforced and unreinforced sections the models were employed for numerical simulation of axial tensions and compressions, torsion, bending and the effects of pressure and temperature. Correlation of mechanical properties predicted by modelling with the data derived from the mechanical testing was used to extend the existing micromechanical models to include more realistic representations of the composite microstructure.To supply more information to designers of continuous fibre MMCs tests on corrosion behaviour, stress corrosion cracking, coefficient of thermal expansion and fracture mechanisms were executed.Based on the previously measured mechanical, physical and physico-chemical properties, the micro mechanical modelling and the requirements of the process two real components were defined and designed.Representing a typical rib structure for aerospace applications an H-shaped MMC part was designed, produced and tested.A flange connector for an uptake riser for offshore application was selected as the most appropriate candidate for the real tubular component.* In addition to common ND testing methods such as X-ray radiography, ultrasonic technique and dye penetration the method of 3-D non-destructive testing was scaled up to the geometric requirements making it possible to test longer components and with a higher resolution.Correlation of measured mechanical properties (especially compression strength) to predicted properties by modelling considering possible infiltration defects and misalignment of fibres led to information about tolerable defects depending on the required properties of the MMC.On the laboratory scale methods of separation of matrix and fibres by using external forces were successfully applied and showed a very high separation grade. In case of silicon contamination the alloy cannot be reused for MMC production, but can be introduced into the conventional secondary aluminium cycle. All employed procedures need a high technical expenditure. The volume of recyclable MMCs available will define the economic viability.Objectives and content A survey of engineering structure materials has shown the imperative need to save further weight and to increase performance without increasing the cost beyond reason. High performance requirements in combination with complex shapes bring conventional materials as steel, titanium and aluminium alloys close to their performance limits. With lot sizes from 500 to 20 pieces those parts are mostly produced by expensive mechanical milling or die forging, often as a number of individual pieces to be assembled later on. Only a minor proportion is made near net shape by casting. The group of aluminium matrix composites with a continuous fibre reinforcement is most efficient for ultra high strength, stiffness and fatigue requirements. Yet their application is still limited due to both technologically and economically inefficient manufacturing processes. The overall objective of the proposed project is to develop and verify a technically and economically efficient manufacturing process for aluminium components with selective reinforcement and to improve the performance and acceptance of this advanced material using a tubular and a rib component for demonstration. The project aims at the industry-scale verification of a combined filament winding/liquid metal infiltration process and consequently makes the high technological potential of fibre MMCs economically available ensuring highest possible design freedom. The proposed work programme comprises three main stages: Elaboration of the materials and the process routes, Development of a test component and Production of two real representative components. The development of components follows an integrated approach of a 'total life cycle of products', i.e. the entire component life starting with an appropriate design, manufacture, post processing, testing under real service conditions and recycling will be covered by the tasks of the work programme. Besides others, a new contactless ND inspection method will be developed and used. The partnership comprises 5 industrial enterprises and 2 universities from 5 EU countries (including one less developed region, Ireland) and CH. Their business fields reflect the total life cycle of a product starting with the design through manufacture and testing upon application and recycling. 6 of the partners collaborated successfully within the FIBRECAST project providing an ideal base for a smooth co-operation in the proposed project. The size of the companies varies from S1 to S7, involving 3 SMEs. The project will be managed by Partner 1 who already co-ordinated the FIBRECAST project. Fields of science engineering and technologymechanical engineeringmanufacturing engineeringengineering and technologyenvironmental engineeringwaste managementwaste treatment processesrecyclingengineering and technologymaterials engineeringcompositesnatural scienceschemical sciencesinorganic chemistrypost-transition metalsengineering and technologymaterials engineeringceramics Programme(s) FP4-BRITE/EURAM 3 - Specific research and technological development programme in the field of industrial and materials technologies, 1994-1998 Topic(s) 0201 - Materials engineering Call for proposal Data not available Funding Scheme CSC - Cost-sharing contracts Coordinator AACHEN UNIVERSITY OF TECHNOLOGY Address Intzestrasse 5 52072 Aachen Germany See on map EU contribution € 0,00 Participants (6) Sort alphabetically Sort by EU Contribution Expand all Collapse all AEROSPATIALE MATRA SA France EU contribution € 0,00 Address 12,rue pasteur 92152 Suresnes See on map Feinguss Blank GmbH Germany EU contribution € 0,00 Address 18,industriestraße 18 88499 Riedlingen See on map IMPERIAL COLLEGE OF SCIENCE, TECHNOLOGY AND MEDICINE United Kingdom EU contribution € 0,00 Address Royal school of mines, prince consort road SW7 2BP London See on map KEMA Nederland BV Netherlands EU contribution € 0,00 Address 310,utrechtseweg 310 6812 AR Arnhem See on map MARINE COMPUTATION SERVICES LTD. Ireland EU contribution € 0,00 Address Merchants road lismoyle house 90 Galway See on map Moser Glaser Plasma AG Switzerland EU contribution € 0,00 Address 24,hofackerstrasse 24 24 4132 Muttenz See on map