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COMBUSS SIGNED

Composite tooling for business jet lower wing stiffened panel manufacturing

Total Cost €

EC-Contrib. €

Partnership

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COMBUSS project word cloud

Explore the words cloud of the COMBUSS project. It provides you a very rough idea of what is the project "COMBUSS" about.

heating intended tools auxiliary zone solution specifications optimization multiple thermal full cure time documentation self tm line life combuss faster manufacture manager quality savings conformance zones waste aeronautical simplification prototype commissioned standards capability materials facilities first composites realized autoclave flight stiffeners modification fabricated start demonstrator wing energy panel incorporate eco subcomponent rates checked transported configuration expectations assurance mass heated worthy tooling premises material mould lower innovative tool productivity guarantee provision specification approval definitions output manufacturing fabrication

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 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.	IT (LACEDONIA AV)	coordinator	330˙019.00
2	TWI LIMITED TWI LIMITED Organization address address: GRANTA PARK GREAT ABINGTON city: CAMBRIDGE postcode: CB21 6AL website: www.twi.co.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (CAMBRIDGE)	participant	149˙375.00
3	BRUNEL UNIVERSITY LONDON BRUNEL UNIVERSITY LONDON Organization address address: KINGSTON LANE city: UXBRIDGE postcode: UB8 3PH website: www.brunel.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	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.