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MISSP SIGNED

Manufacturing of Integral Stiffened Skin Panels

Total Cost €

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EC-Contrib. €

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Partnership

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Project "MISSP" data sheet

The following table provides information about the project.

Coordinator
SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIALE SONACA SA 

Organization address
address: ROUTE NATIONALE CINQ PARK INDUSTRIEL
city: GOSSELIES
postcode: 6041
website: www.sonaca.com

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 Belgium [BE]
 Project website http://missp.eu/index.php/project
 Total cost 899˙742 €
 EC max contribution 899˙742 € (100%)
 Programme 1. H2020-EU.3.4.5.4. (ITD Airframe)
 Code Call H2020-CS2-CFP04-2016-02
 Funding Scheme CS2-RIA
 Starting year 2017
 Duration (year-month-day) from 2017-05-01   to  2020-02-29

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIALE SONACA SA BE (GOSSELIES) coordinator 423˙180.00
2    3D METAL FORMING BV NL (LELYSTAD) participant 305˙000.00
3    CENTRE DE RECHERCHES METALLURGIQUES ASBL BE (BRUXELLES) participant 171˙562.00
4    CENTRE D'ETUDES WALLON D'ASSEMBLAGEET CONTROLE DES MATERIAUX ASBL BE (OUGREE) participant 0.00

Map

 Project objective

MISSP (Manufacturing of Integral Stiffened Skin Panels) project aims at proposing new manufacturing concepts for metallic aircraft cargo doors. The main objective of this project will be to develop cheaper and greener structures as an alternative to CFRP doors but also applicable for any stiffened skin panel structure. This will be made possible by the use of advanced materials, manufacturing techniques and design concepts. Expensive and polluting chemical milling operations shall be replaced by flat mechanical machining, while multi-parts riveted components shall be replaced by more integrated structures reducing the number of parts and the time-consuming mechanical riveting assembly processes The project will be divided into 3 main technical work packages, followed by a cost and performance analysis. The first work package shall focus on the manufacturing of the external door skin with the aim of replacing the chemically milled pockets by mechanically machined ones. Both stretch-forming on tailored tool blocks and high energy hydroforming alternative will be investigated. In the second work package, stringers shall be integrated to the Al-Mg-Sc 5028 skin by flat welding (FSW or LBW) followed by creep forming. Finally, the third package shall be dedicated to the manufacturing of an integral structure, drastically limiting the number of assembly operations. To this aim, an innovative solution is proposed: a plate shall be deformed by high energy hydroforming and subsequently machined into the final cargo door integral structure. To support the advanced manufacturing technologies proposed in this challenging project, use shall be made of numerical modelling that will help designing appropriated tools and optimizing process parameters to achieve high quality demonstrators that shall be delivered to the topic manager.

 Publications

year authors and title journal last update
List of publications.
2017 Marchal Yves, Oud Marcel, Groenenveld Hugo and Godet Stéphane
High speed forming, a smart way to manufacture complex parts with high performance alloys
published pages: , ISSN: , DOI:
2020-04-08

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

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