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Modular multilevel cost Analysis Software for COmposite smarT fuselage

Project description

Monolithic fuselage barrels that eliminate joints and bolts

Polymer composites are now routinely used in numerous aircraft components to reduce weight, fuel consumption and emissions while imparting properties such as corrosion and fatigue resistance. They have also made it possible to produce monolithic fuselage barrels that eliminate joints and bolts. The European aerospace industry is now targeting a smart, multifunctional thermoplastic composite-based fuselage barrel. To get it off the ground, the EU-funded MASCOT project is developing a multilevel cost analysis software platform to be linked to an optimisation tool. It will consider costs of raw materials, individual components, and the fuselage overall. In addition, it will assess total manufacturing hours and man- or machine-hours. Finally, the software will also account for structural health monitoring costs as well as maintenance and repair.

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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Programme(s)

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Topic(s)

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Funding Scheme

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CS2-RIA - Research and Innovation action

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Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) H2020-CS2-CFP09-2018-02

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Coordinator

UNIVERSITA DEGLI STUDI DI FERRARA
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 128 000,00
Address
VIA ARIOSTO 35
44121 Ferrara
Italy

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Region
Nord-Est Emilia-Romagna Ferrara
Activity type
Higher or Secondary Education Establishments
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 128 053,75

Participants (3)

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