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Projecte llegit

Títol: Aircraft Cabin Layout Check - Development of a tool for the adaptation of Aircraft Loading in case of Shear Exceedances

Estudiants que han llegit aquest projecte:

Director/a: MELLIBOVSKY ELSTEIN, FERNANDO PABLO

Departament: FIS

Títol: Aircraft Cabin Layout Check - Development of a tool for the adaptation of Aircraft Loading in case of Shear Exceedances

Data inici oferta: 17-07-2023     Data finalització oferta: 17-03-2024


Estudis d'assignació del projecte:
    GR ENG SIST AEROESP
Tipus: Individual
 
Lloc de realització: EETAC
 
Nom del segon director/a (UPC): Tim Köhler
Departament 2n director/a:
 
Paraules clau:
Aircraft, Shear, Fuselage, Certification, Tool
 
Descripció del contingut i pla d'activitats:
 
Overview (resum en anglès):
Airbus currently offers a wide range of cabin configurations, fuel tanks and cargo compartments for each of its aircraft models. All these configuration differences must be subjected to an amount of studies to ensure the operability and safety of the aircraft. One of the most critical and rigorous studies that each aircraft must overcome is the level of fuselage shear.

The study consists of ensuring that the amount of shear suffered by the fuselage is lower than or equal to the safety values stipulated by Airbus. This verification process takes a long time and by that increases the computational and monetary costs for the company.

This thesis deals with the development, implementation and verification of a new tool in order to offer solutions when the shear of an aircraft exceeds the reference and safety values. The aim is to reduce the amount of time and expenses for the certification of the aircrafts.

First of all, the software that Airbus currently uses to calculate all the shear levels of the fuselage has been analyzed in detail. In a second step all requirements for the new tool development are discussed and reviewed with the Airbus stakeholders. After that the requested software is generated including the corresponding User Interface.

Then the new tool has to be checked by a series of tests and certifications in order to ensure its operability in the industrial context by helping in the certification process of an aircraft.

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