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TRIMIS

Injection Moulding with Continuous Local Reinforcements

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€586 239
EU Contribution
€503 375
Project Acronym
IMCoLoR
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP03-2016-01
Link to CORDIS
Objectives

In the IMCoLoR project the scroll of an air cycle machine is manufactured with an injection moulding process with the local integration of continuous carbon fibre reinforcements. The local reinforcements are placed along the main load paths in order to lead to a higher pressure and temperature resistance of the scroll than for a short carbon fibre reinforced scroll as manufactured in CleanSky I. Consequently, with this method also new generation aluminium scrolls can be replaced by a thermoplastic scroll reducing weight and cost and preventing the need of hazardous surface treatments.

Methodology

For the local reinforcement of the injection moulded scroll a two-step process will be developed. In a first step, a 3D reinforcement structure from aligned pre-impregnated continuous carbon fibres (Tape) will be manufactured with the AFPT process. A removable core system will be implemented as a tool for the lay-up process. This allows the load adapted design of the reinforcements. In a second step, the reinforcement structure will be fixed inside an injection mould and will be over injected by injection moulding. The aim of the tool design is to enable a complete enclosure of the reinforcement structure. Therefore, the fixation system is embedded into the injection mould and consists of movable fixation elements that can fix and release the reinforcement structure. When the fixations are released they move backwards and are completely embedded in the mold. This enables the complete enclosure of the reinforcement inside the part without yhe build up of gaps. The exact position of the reinforcement can be adjusted with the fixations.

Non-destructive and destructive test methods will be implemented in order to evaluate the processing quality and the mechanical performance of the part.

A demonstrator will be manufactured with the developed technology and a final evaluation of the process in terms of an industrialization of the process will be done.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.6.

Partners

Lead Organisation
Organisation
Technische Universitaet Muenchen
Address
Arcisstrasse 21, 80333 MUENCHEN, Germany
Organisation website
EU Contribution
€251 775
Partner Organisations
Organisation
Apppex Product Development, Prototypes, Parts Gmbh
Address
STUTTGARTER STR. 7, 80807 MUNCHEN, Germany
EU Contribution
€158 988
Organisation
Fischer Advanced Composite Components Ag
Address
Fischerstr. 9, 192 RIED / INNKREIS, Austria
Organisation website
EU Contribution
€37 363
Organisation
Stichting Thermoplastic Compositesresearch Center
Address
PALATIJN 15, 7521 ENSCHEDE, Netherlands
EU Contribution
€55 250

Technologies

Technology Theme
Composite materials
Technology
Composite materials for structural purposes in the aircraft
Development phase
Demonstration/prototyping/Pilot Production

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