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Fabien BOUTEILLE

Paris

En résumé

GENERAL SKILLS

• 15 years professional experience in various areas of aeronautics and space:
• Modeling and mesh generation for Numerical simulations.
• Design catia V5 fundamental and surface R18-R21.
• Geometric Dimensioning and Tolerancing (Y14.5 2009)
• Project Follow-up
• The ability to read engineering drawing, good vision in space 3D.

PROFESSIONAL SKILLS MECHANICAL DESIGNER

• Designing according to Bombardier Aerospace Standards
• Manufacturing process: parts, mold, trim and assy jig
• Mechanical design support for new and existing products
• Generation of part drawings, assembly drawings and drawings 2D
• Creating and checking Engineering Change Requests (ECRs)
• Geometric Dimensioning and Tolerancing (Y14.5 2009)

PROFESSIONAL SKILLS MESH GENERATION

• Topology of structured mesh ( Patch grid technical and chimera technical)
Topology of unstructured mesh (surfacic mesh, volumic mesh, prismatic layer,refinement local, density box, wake, scripting).
• Surface wrapping, geometry discretization
• Check shapes and simplification of geometric and CAD geometry repair. Using Catia v5.
• Identify and optimization the mesh constraints, ensure the mesh quality and compatibility
with CFD codes and balance to find between the grid accuracy and computational
duration.
• Definition of processes to be respected to reach computation convergence.

COMPUTER SKILLS

• ICEMCFD ANSYS V12, 13, 14 Hexa, and Tetra, Scripting.
• CATIA V 5 Fundamental R20, and Surface Design R21
• Solid Work, Pointwise: notion
• Numeric code NSU3D, CFD++, ELSA: notion
• Programming language Python, batch: notion
• Environment system Linux, Unix, Windows
• Excel, Word, PowerPoint, and Client Mail.

Mes compétences :
Catia v5
Ansys workbench
Icem CFD
CFD
Bash
Aéronautique
Python
Catia Fundamentals R20
Microsoft Office
Tolérancement géométrique
Microsoft Excel
Aerospace
Aérodynamique
Catia Surface Design R21
Environnement linux
Maillage Non Structuré (Tetra)
Maillage Structuré (Hexa)

Entreprises

  • Akka Technologies - Designer Catia V5

    Paris 2014 - maintenant Design cabin cockpit interior Catia V5 surface: The Challenger CL650 Vision Flight Deck is introduced as an Interior upgrade to current CL605, The baseline aircraft cockpit is modified to introduce enhanced styling.

    Realisation:
    • Study and design 3D model of center pedestal console part, windows post and bottom glareshield cockpit, analysis interface point. Structural requirement, aesthetic requirement, material process & part, robustness requirement, interface and tolerance.
    • Study SOCD (Source Control Drawing) and drawing 2D model.

  • Akka Technologies - Mesh designer, Aircraft Aerodynamics Engineer Military Projects (ITAR)

    Paris 2013 - 2014 Realisation:
    • Aircraft primary simplification of geometric design using Catia v5.19 for meshing.
    • Realization of a tetrahedral mesh in ICEMCFD, study on mesh topology
    • Establishment process mesh CFD:
     surfacique mesh
     volumique mesh
     prismatic layer
    • Realization of tetrahedral mesh special, air operable door, observation windows, camera, drop hatch, lunch tubes, emergency equipment, antenna. Design specialized modifications that maximize the effectiveness of mission equipment, while minimizing the impact on flight performance.
    • Realization of tetrahedral mesh special military program CF-188 Hornet. Study military equipment (lunch missile trajectory of the missile and prediction, additional tank)
    • Complete autonomy on tasks management. Always meet expectation on schedule

    Technical environment:
    • ICEMCFD ANSYS Hexa, and Tetra, Scripting.
    • CATIA V5
    • CFD++

  • Akka Technologies - Mesh Designer, Aircraft Aerodynamics Engineer Global 7000 -8000

    Paris 2011 - 2012 Realisation:
    • Aircraft primary simplification of geometric design using Catia v5 for meshing.
    • Realization of a tetrahedral mesh in ICEMCFD for :
     study stability and control landing, take off configuration high lift and for ground effect.
     analysis performance high speed, low speed.
     Meshing for computation high lift design
     study landing gear at different phase of deployment, completely retracted and full extended, door deployed.
     efficiency rudder
     for study Longitudinal (consumption, stability) and lateral (stability, maneuverability)

    • Polar Running with the aerodynamic calculation code NSU3D
    • Complete autonomy on tasks management. Always meet expectation on schedule

    Technical environment:
    • ICEMCFD ANSYS Hexa, and Tetra, Scripting.
    • CATIA V5
    • code NSU3D

  • Aeroconseil - Mesh designer, Maillage CFD / Études Aérodynamiques

    Blagnac 2001 - 2011 Mesh designer CFD for Aerodynamics

    Realisation:
    • Responsible for and contribution to the process of definition of unstructured and structured hexahedral topology for the calculation code FLUENT, CFD + +, ELSA, internal and external aerodynamics.
    • Provide study on mesh topology, unstructured and structured.
    • Provide ICEMCFD trainings for contractors and also checking processes are correctly implemented for meshing

    Project: Airbus program A320 NEO
    • Optimize entire nacelle mesh for the A320 NEO :
     External part – pylon/strut, nacelle, air intake, fan cowl
     Internal part : inlets / outlets exhausting for air system flows, ventilation intake

    Project: Airbus program A400M
    • Mesh for optimization for engine propeller

    Project: EADS/ Astrium NT6
    • Plane powered by aircraft and rocket engine dedicated to sub orbital flight: the different flight phases imply to produce a mesh that is adapted to each calculation.

    Project: Daher/ Socata TBM 900
    • Provide new design due to engine change: TBM 850 aerodynamics to be modified (new calculation depending on tetrahedral mesh)

    Project: Safran/ Aircelle
    • Air intake design methodology development for “Aircelle” (Establishment of an automatic mesh generator, in the case of an optimization study nacelle lines): insert parametrical data in the tool to create geometric mesh in order to produce an automatism which take nacellist criteria into consideration. (Geometric input / ouput Fluent solver)

    Project: EADS/ MBDA:
    • Set up a hexahedral topology for an aerodynamic study of drone the Talarion, M.A.L.E. (Moyenne Altitude Longue Endurance)
    • Preliminary study.

Formations

  • IUT De Bourgogne (Auxerre)

    Auxerre 1997 - 1999 BTS CPI
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