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COMBUSS SIGNED

Composite tooling for business jet lower wing stiffened panel manufacturing

Total Cost €

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EC-Contrib. €

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Partnership

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Project "COMBUSS" data sheet

The following table provides information about the project.

Coordinator
OFFICINE MECCANICHE IRPINE SRL 

Organization address
address: AREA INDUSTRIALE CALAGGIO SNC
city: LACEDONIA AV
postcode: 83046
website: www.omi-mf.it

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Italy [IT]
 Total cost 740˙956 €
 EC max contribution 599˙519 € (81%)
 Programme 1. H2020-EU.3.4.5.4. (ITD Airframe)
 Code Call H2020-CS2-CFP07-2017-02
 Funding Scheme CS2-IA
 Starting year 2018
 Duration (year-month-day) from 2018-11-01   to  2020-06-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    OFFICINE MECCANICHE IRPINE SRL IT (LACEDONIA AV) coordinator 330˙019.00
2    TWI LIMITED UK (CAMBRIDGE) participant 149˙375.00
3    BRUNEL UNIVERSITY LONDON UK (UXBRIDGE) participant 120˙125.00

Map

 Project objective

The aim of the COMBUSS project is to develop, design, manufacture and deliver to the Topic Manager facilities, all the prototype subcomponent manufacturing tooling needed to manufacture the stiffeners and panel of lower wing (including all auxiliary tools). COMBUSS project will design the tooling system which will incorporate self-heated capability with multiple heating zones and advanced thermal management.

The activities will start with the provision of definitions and specifications by the Topic Manager (TM). The mould materials will be optimised for long life and improved productivity. It will feature built-in quality assurance tools to guarantee reliable processing of the selected material systems according to technical specifications. After the TM’s approval of the design, the tool will be fabricated, checked for conformance with the specification, transported to the TM premises and commissioned. The partners will provide full documentation on the tooling system and its use and will support the TM with the demonstrator fabrication.

The COMBUSS system, as the main output of the project, will be realized in line with the “most innovative expectations” of the call, as it will present a comprehensive tooling solution for improved cost (tooling materials and manufacturing method), eco-design (out-of-autoclave processing, low thermal mass and easy modification of tooling, waste reduction in process), energy savings (self-heating and multi-zone configuration of tooling), manufacturing process simplification (robust process thermal control), production time savings (faster heating rates, cure process optimization) and Aeronautical quality standards (on-line quality control) in composites manufacturing. The COMBUSS system is intended to be used directly at the flight-worthy demonstrator at the Topic Manager premises as a first step of the system exploitation.

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The information about "COMBUSS" are provided by the European Opendata Portal: CORDIS opendata.

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