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Jimmy LENCLUME

TOULOUSE

En résumé

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Mes compétences :
Patran
Visual Basic for Applications
NASTRAN
Microsoft Word
Microsoft PowerPoint
Microsoft Office
Microsoft Excel
CATIA
Finite elements
Structure analysis
Project management

Entreprises

  • ST3D on behalf Spirit AeroSystem - Stress analyst

    2012 - maintenant A350 program: Forward Lower Shell Justification and certification

    - Frame 41 to 45 analysis with ISAMI-CFRP module (Composite + metallic). ;
    - Shear-web, strut/Frame junction and splice analysis (EPTool, filled hole). ;
    - Impact of loaded bracket on skin and frame analysis.
    - System holes in skin analyses (ISAMI Open Hole et Rib Bay Buckling) ;
    - Concession T300 et T390 (SAP)
    - Method presentation (power point)
    - Stress report (Word)

  • ST3D on behalf AEROSUD AVIATION - Team Leader

    2010 - 2011 Team leader on two Work-package (Stairs case lining and Load Master Workstation, 5 pers).
    - Projected schedulle realization;
    - Organisation of stress and design progress meeting.
    - Progress meeting with customers
    - Check and validation of the analyses.

    Management staff (10 pers.):
    - Focal point for ST3D employer on Aerosud site.
    - Achievment exit interview and annual monitoring
    - Check and validation of hours worked for time sheet.
    - Identify customer needs and propose new resources

    Stress analyst (A400M program):
    - New design study of stair case lining and load master to sustain decompression load.
    - Finites elements modelling.
    - Analytical analysis tool preparation (excel VBA)

  • ST3D on behalf Airbus Group - Stress analyst

    2007 - 2010 A400M program: Galley cockpit Justification (Installation system)

    - Galley modelling with patran.
    - FEM validation check.
    - Dynamique analysis (sol103)
    - Static analysis on composite (Hill criteria, tenon-mortesis junction) and metallic part (Von Mises, flange bending and buckling)

    A380 program: Nose fuselage system bracket Certification (loop2 step 2)

    - Dynamic and static bracket or support analyses (FEM, analytical)
    - Stress report

  • ST3D - Stress analyst

    2007 - 2007 A400M program: Lateral console and center piedestal (cockpit )

    - FEM update for dynamic analysis.
    - Structure rigidity study to prevent the natural frequency of the structure do not match
         a frequency range encountered by the aircraft in service

Formations

Réseau

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