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Plesea DRAGOS

TOULOUSE

En résumé

Master Administration d'Entreprise IAE TOULOUSE 2008-2010(CAAE/MAE2)
Ingénieur études aéronautique calcul fatigue - Chef de projet
Developpement projet "near shore" - Roumanie
Fondateur INFOMEC SISTEMArray

Mes compétences :
Aéronautique
Mécanique
Externalisation
OFFSHORE

Entreprises

  • Aeronatical Company Toulouse - AERONAUTICAL STRESS ENGINEER

    2008 - maintenant Performing the certification phase in fatigue and damage tolerance analysis of A330 GMF NLGB structure elements: panels, formed and machined frames,crossbeam of S12 floor
    Coordinating and performing:
    single load path analysis and multiple load path analysis on PSE and SSE of A330 GMF;
    crack propagation analysis and residual strength calculations;
    splicings calculations on panels and frame junctions areas;
    fatigue stress reports for both phases: justification and certification for metallic elements of A330 GMF;
    In charge of SRM phase of NLGB A330 GMF

  • INBIS UK - AERONAUTICAL STRESS ENGINEER

    2006 - 2006 Certification phase in fatigue and damage tolerance analysis of the A380 Leading and Buttstrap Trailling Edge
    A fatigue and damage tolerance analyis,using DAMTOL system (Ciscan&Seqdam)made for the joggle and bolted joints contained by the structure;

  • INFOMEC SISTEM - Managing Director

    2006 - maintenant Fondator of romanien engineering consultancy company INFOMECSISTEM

    The geographical membership of Romania to Europe and its cultural and linguistic proximity with France, as well as the excellent training level of its Engineers and Frameworks, represent true advantages for the Rumanian medium of business.
    INFOMEC SISTEM provides a “consulting” activity for the companies interested by “Near Shore” towards Romania.
    INFOMEC SISTEM’s business model was planned so that the Rumanian Engineers (who wish to remain in their country and to make a career there) can work for distant and local Customers.
    www.infomecsistem.com

  • ASSYSTEM - AERONAUTICAL STRESS ENGINEER

    Courbevoie 2003 - 2008 FATIGUE & DAMAGE TOLERANCE STRESS A330 GMF, 400M , A380 & A380F - 800 DEPARTEMENT
    Participation on justification phase in fatigue and damage tolerance analysis of the 400M Sponson structure;
    Certification phase in fatigue and damage tolerance analysis of the A380 Leading and Buttstrap Trailling Edge
    A fatigue and damage tolerance analyis,using DAMTOL system (Ciscan&Seqdam)made for the joggle and bolted joints contained by the structure;
    Project leader of 5 fatigue stress engineers working on NOSE LOWER STRUCTURE (NLS) A380 Pax
    Coordinating the certification phase in fatigue and damage tolerance analysis of all A380 Nose fairing structure elements: panels, formed and machined frames, frontal and lateral boxes, NLS doors attachment fittings on fuselage, radome junctions;
    Coordinating and performing:
    single load path analysis and multiple load path analysis on PSE and SSE of A380 NLS;
    crack propagation analysis and residual strength calculations;
    splicings calculations on panels and frame junctions areas;
    fatigue stress reports for both phases: justification and certification for metallic elements of NLS A380;
    Participation on fatigue spectrum elaboration;
    Participation on pre-dimensioning and justification phases of NLS structure;
    Project leader of 2 persons for the NOSE LOWER A380 F- 800 Frighter structure
    Coordinating and performing pre-dimensioning of A380 F-800 Frighter structure;
    Coordinating and performing comparison between the loading behavior of A380 F-800 Frighter/ A380 Pax structures;Load manipulation of the global FEM;
    Participation on certification phase of the main landing gear of the A340;
    Performing statique stress reports for the certification of junction door/frame;

Formations

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