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MASCOT SIGNED

Modular multilevel cost Analysis Software for COmposite smarT fuselage

Total Cost €

EC-Contrib. €

Partnership

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MASCOT project word cloud

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

beam level regarding module structural expressed obtain upper interface repair fastener multidisciplinary optimization object health cad bayesian linked manager deals computed gasket informations paint manufacturing analogous rivet inclusion tool man machine filling concerning contains bottomup data software levels parametric collect floor endowed shm benefit skin materials material connected structure honeycomb estimate sealant geometrical model pressure collects frame lower interfaced carry final hour gui stringer historical components fuselage raw entire maintenance hours bdddsa routes details tree doublers procedure quick dynamic estimation composite bulkhea monitoring drivers

Project "MASCOT" data sheet

The following table provides information about the project.

Coordinator	UNIVERSITA DEGLI STUDI DI FERRARA Organization address address: VIA ARIOSTO 35 city: FERRARA postcode: 44121 website: www.unife.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	404˙532 €
EC max contribution	400˙000 € (99%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP09-2018-02
Funding Scheme	CS2-RIA
Starting year	2019
Duration (year-month-day)	from 2019-10-01 to 2021-09-30

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	UNIVERSITA DEGLI STUDI DI FERRARA UNIVERSITA DEGLI STUDI DI FERRARA Organization address address: VIA ARIOSTO 35 city: FERRARA postcode: 44121 website: www.unife.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 (FERRARA)	coordinator	128˙000.00
2	SKY TECHNOLOGY SRL SKY TECHNOLOGY SRL Organization address address: VIA FRANCESCO GONIN 55 city: MILANO postcode: 20147 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (MILANO)	participant	104˙000.00
3	UNIVERSITA DEGLI STUDI DELLA CAMPANIA LUIGI VANVITELLI UNIVERSITA DEGLI STUDI DELLA CAMPANIA LUIGI VANVITELLI Organization address address: VIALE ABRAMO LINCOLN 5 city: CASERTA postcode: 81100 website: www.unina2.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 (CASERTA)	participant	88˙000.00
4	PLYFORM COMPOSITES SRL PLYFORM COMPOSITES SRL Organization address address: VIA MIRABELLA 12 city: VARALLO POMBIA postcode: 28040 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (VARALLO POMBIA)	participant	80˙000.00

Map

Project objective

The objective of the proposal is to set up a three-level-parameter cost estimation method that allows the determination of the final cost for the fuselage design under analysis. The tree-structure of the procedure allows a quick, easy and friendly-user inclusion of the main parameters determining the final cost of a fuselage both at the raw material level and at the component level and at the fuselage level. Level 0 contains information concerning the raw materials (rivet, fastener, composite raw material, honeycomb, gasket, sealant, paint), level 1 collects informations regarding the components (stringer, skin, frame, doublers, floor-beam, pressure bulkhea) and level 2 deals with the fuselage as entire object. The upper levels are connected to the lower levels by manufacturing routes that are expressed in terms of hours and hour cost (that is man-hours and machine-hours), and in terms of manufacturing technology. Each of the three levels collects informations and details to estimate the cost. Some of these parameters can be set as cost drivers in order to carry out both the analogous method and the parameter method. Levels 0 and 1 can collect historical data that will be used by the analogous method. The entire fuselage is thus defined by filling the three levels and the estimated cost can be computed by one of the methods (Analogous, Parametric o BottomUp). At level 1 the software will allow the maintenance and repair parameters to be interfaced to the Structural Health Monitoring (SHM) system in order to estimate the SHM technology cost and its cost benefit on manufacturing, maintenance and repair. A Bayesian based Dynamic Data Driven Application System (BDDDSA), developed by the Topic Manager, will be also integrated to the software. The cost estimation module will be endowed with GUI interface. It will be linked to CAD model to obtain geometrical parameters at each level. The module will also be interfaced to a multidisciplinary optimization tool.

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