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Aude LUPPI

Courbevoie

Electionseuropéennes 2024

RETROUVEZ GRATUITEMENTLe résultat des européennes à Toulouse ainsi que le résultat des européennes en Haute-Garonne.

En résumé

November 2011 – Present

Structural stress engineer in FDT for P3 Voith (Toulouse, France):
- FDT analyses performed on A350XWB-1000 Nose Landing Gear Bay (NLGB) and NLG Roof Panel: comparison between -900 & -1000 on FDT equivalent stresses (to conserve actual geometry), damage tolerance analysis
- Optimization on A350XWB-900 Door surrounding (Nose Fuselage): Isami frame study, damage tolerance analyses (1 month)
- Concessions on A320 Family Center Wing Box: geometrical check (1 month)

February 2007 – October 2011

Structural stress engineer in FDT for Altran Sud Ouest (Toulouse, France):
- FDT leader (of 5 persons) on A350XWB-900 Spoilers (calculations of metallic fittings: lugs, junctions, current areas, fasteners, justification dossiers) from July 2009
- 2 years experience on Extension Service Goal for A320 on Center Wing Box (fatigue full test scale: gauges, inspection program, repairs catalogue, artificial damages)

Entreprises

  • Assystem Canada - Tress Engineer: Fatigue & Damage Tolerance

    Courbevoie 2013 - maintenant

  • P3Voith - Stress Engineer: Fatigue & Damage Tolerance

    2011 - 2013 - FDT analyses performed on A350XWB-1000 Nose Landing Gear Bay (NLGB) and NLG Roof Panel: comparison between -900 & -1000 on FDT equivalent stresses (to conserve actual geometry), damage tolerance analysis
    - Optimization on A350XWB-900 Door surrounding (Nose Fuselage): Isami frame study, damage tolerance analyses (1 month)
    - Concessions on A320 Family Center Wing Box: geometrical check (1 month)

  • Altran SO - Stress Engineer: Fatigue & Damage Tolerance

    Vélizy-Villacoublay 2007 - 2011
    - FDT leader (of 5 persons) on A350XWB-900 Spoilers (calculations of metallic fittings: lugs, junctions, current areas, fasteners, justification dossiers) from July 2009
    - 2 years experience on Extension Service Goal for A320 on Center Wing Box (fatigue full test scale: gauges, inspection program, repairs catalogue, artificial damages)

  • EADS SOCATA - Stage de fin d'études

    Blagnac 2006 - 2006 Février – Juillet 2006
    Stage de fin d’études pendant 5 mois à la SOCATA (EADS) à Tarbes (65) : formalisation et fiabilisation de l’expérience SOCATA en fatigue et tolérances aux dommages (méthode et outils).

Formations

  • Ecole EPF

    Sceaux 2001 - 2006 Option Aéronautique et Espace

Réseau

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