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TRIMIS

Direct filament wound rotor carbon resin sleeves by bulk curing and layer-by-layer Electron beam polymerisation

Project

E-SLEEVE - Direct filament wound rotor carbon resin sleeves by bulk curing and layer-by-layer Electron beam polymerisation


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/09/2012,
End date: 01/07/2014

Status: Finished
Funding details:
Total cost:
€199 100
EU Contribution:
€149 325

Overview

Objectives:

E_SLEEVE activities dealt with the design, set-up and demonstration of two distinct processes for the filament winding of the required carbon composite retaining sleeve, to be realised directly integrated onto the high speed motocompressor rotor of air conditioning systems used in aircraft application.

The first one used Cyanate Ester resin and subsequent bulk curing, the second one used specific resins for high temperature use and for direct layer-by-layer curing to be performed via low energy Electron beam, simultaneously to the filament winding process itself.

Each process was validated by manufacturing the required five sleeves directly on the rotor sub-assembly.

Next Technology Tecnotessile had internal expertise and equipment from previous projects and commissions allowing to fulfil the Topic expectations. Two European-level experts in layer-by-layer E-beam curing for aerospace applications were involved to advise on resin formulation and provide support to process design and set-up and to validation activities. Further industrial up-scaling scenarios with cost analysis were produced for both processes and full collaboration with Topic Manager on exploitation and dissemination activities was provided.

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