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Paul MAURY

COLOMIERS

En résumé

Mes compétences :
Modélisation
Simulation
Optimisation
Calcul De Structure Aéronautique
Abaqus

Entreprises

  • DATADVANCE - Account Manager

    2017 - maintenant
  • Segula Defence & Space - Responsable de l'unité Calcul et Système

    2016 - 2017
  • Alten - Simulation Technical Leader

    Boulogne-Billancourt 2014 - maintenant My previous main missions in GECI were reconducted , including team management of 4 stress Enginneers :

    Others missions added are:

    .Transnational activities, to harmonize and share also in germany
    .Management of skill matrix for Simulation Skills
    .Pre-Sales tasks
  • Alten - A330 NEO PYLON STRESS LEADER

    Boulogne-Billancourt 2014 - 2014 This mission was integrated in my last position of Simulation Stress leader, I was asked on this determinated period to prepare and secure ALTEN Stress Technical Team on the field in the way to win call for tender.

    I was supporting from front Office (Airbus Site), Airbus stress leader in the pre-MG3 maturity gate by :
    .Proposing Method&Tools from our capitalization and my last experiences,
    .Using best practises from other program A380, A350 (Dynamic thrust links calculation, Wing and engine mount stress status)

    In this period, I also managed a team of 5 stress located in back office :
    . answering technical issues in FEM modelling, analytical calculation
    . providing work load and reporting to project manager
    .etc ...

  • GECI Systemes - Head of the numerical simulation department

    Paris 2010 - 2014 • Operational manager of a team of 4 engineers dealing with technical issues requiring tight constraints (time or technical) -> Task Force
    • Technical support transverse FEM on GECI’s WPs
    • Choice of the best-adapted tools and anticipation of tough issues with the relevant project managers.
    • Validation of key deliverables, maturity gate
    • Internal instruction on various tools (PATRAN/NASTRAN, ABAQUS) for project engineers
    • Tools and methods’ development: Process automation (Python, VBA, Fortran)
    • Temporary instructor at ICAM (Toulouse) and Master 2 program (Paul Sabatier University): practical work on finite elements, recruitment assistance
    • Tool and business technical watch: benchmarking of new solutions prior to project deployment
    • HPC management of the unit
  • GECI Systemes - Stress Leader

    Paris 2008 - 2009 Stress Leader architecture Pylon A320Neo/A30X for AIRBUS EDSI A30X research
    • Technical monitoring of a team of 5 calculation engineers on stress issues (completion and check-up of deliverables according to the guidelines and business rules)
    • Study of various architectures (Core, Fan, Hybrid) to assist in decision-making on the baseline concept
    • Structural design and metal fatigue (vibratory dynamics, linear and non-linear buckling, post buckling, thermo elastic, PRA)
    • Management of global and local models using NASTRAN, linear and non-linear condensation
    • Management of global and local models using ABAQUS, SUBMODELING and of DMIG NASTRAN

  • GECI Systemes - Stress Engineer - FEM Expert

    Paris 2006 - 2008 DFEM focal point on AIRBUS ST ELOI site TWYEK Mats A350
    • Focal point GECI project for linear MEF activities and non-linear DFEM 3D activities using NASTRAN and ABAQUS
    • Expertise on potential dynamic coupling issues between RR engines and primary structure -> dynamic validation of the concept

  • GECI Systemes - Stress Engineer - FEM Expert

    Paris 2005 - 2006 For AIRBUS Toulouse - TWYEK - A380 Pylon


    • Dynamic studies on thrust engine links of A380 Pylon, DFEM linear and non linear
    • Correlation with bench and data testing
    • Weight saving on Engines mounts fittings, non linear DFEM



  • GECI Systemes - Stress Engineer

    Paris 2004 - 2005 For LATECOERE Toulouse - F7X STUB

    • Substantiation sizing loop - DFEM for FTD sizing
    • Structure sizing metallic - Static, Dynamic, Buckling - Analytic &FEM
  • EUROSIM -MECALOG - Stress Engineer

    2003 - 2004 For SOCATA Tarbes (65) - F7X

    • Modeling a crack fatigue propagation on a stiffened panel of Falcon 900 to correlate methods used on F7X

  • RETEC - Stress Engineer

    2000 - 2003 For EUROCOPTER (Marignane – 13)

    • Dynamic analysis on NH 90- Static and Fatigue sizing
    • Static and fatigue sizing of transmission housing box on GAZELLE, DAUPHIN et SUPER PUMA
    • Trade off on convertible helicopter
  • ECAM - Designer

    1998 - 2000 For LATECOERE Toulouse- A340 500/600


    - Design drawings using CADDS5 parametric tools

Formations

  • IUP GMP (Toulouse)

    Toulouse 1994 - 1997 Conception des Systèmes Mécaniques et Aeronautique

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