Loïc CHAVERON

En résumé

Entreprises

• PORTALLIANCE - Stress Engineer

  2013 - maintenant => Beluga XL, WP10 fuselage and Main Cargo Door structure sizing & justification (2 years) ;
  * Calculation in accordance with AIRBUS method (Hand & FEM calculation) ;
  * Interfaces concept and implementation (Backup structure at latch & Hinge interfaces) ;
  * Tasks management and engineers support
  
  => A330 neo, technical support on engine pylon structure (6 months) ;
  * Development and optimization of calculation method ;
  * Stress sheets checking
  * Interfaces concept and implementation
  
  => A330 neo, MLGB Sizing & justification mod ELAF (5 months) ;
  * Calculation in accordance with AIRBUS method ;
  * PSN tools
  * Justification dossiers
  
  => A350-1000, engine pylon structure sizing & justification (18 months). ;
  * Calculation in accordance with AIRBUS method :
  * Metallic primary structure, isogrid panel, ribs and titanium spar ;
  * Composite primary structure, spars using the FEM and ISAMI (plain strength module, filled hole, Open hole, damage tolerance and edge impact) ;
  * Metallic secondary structure, lugs, machined supports and corner fittings ;
  * Systems, fuel pipes, bleed air and hydraulic. ;
  * FEM
  * Mesh 2D et 3D ;
  * SOL101, SOL105 and SOL106 including contacts. ;
  * Particular Risks Analysis FBO and fire on metallic and composite parts ;
  * Interfaces concept and implementation
  * Tasks management and engineers support ;
  * C maturity Validation and justification Stress dossiers preparation

• AUSY - Stress Engineer

  Sèvres Cedex 2011 - 2013 => A320 neo, engine pylon secondary structure sizing and justification. (14 months). ;
  * Machined supports, metallic angle and composite panels using FEM and ISAMI Calculation using AIRBUS method. ;
  * FEM, mesh 2D and 3D (SOL101, 105 and 106 including contacts) ;
  * Interfaces Concept and implementation ;
  * B & C maturity Validation and justification Stress dossiers preparation
  
  => A380-800e, Lower shell static Serial Repair Manual (6 months). ;
  * lightning strike, skin & stringer repair Calculation in accordance with SRM AIRBUS method ;
  * SRM dossiers.
  
  => A380-800e, forward lower shell static certification dossiers (8 months) ;
  * Static calculation in accordance with AIRBUS method ;
  * PSN tools
  * FEM modification
  * certification dossiers.

• AKKA - Designer

  Paris 2007 - 2011 => A350-900, in charge of Keel Beam design (2 years) ;
  * Design principle ;
  * composite and metallic primary structure Design (panels, Fittings, Shear webs) ;
  * B & C maturity Validation
  
  => A380, forward lower shell Brackets installation (17 months) ;
  * secondary structures design and drawings
  * Memos Analysis, configuration management

• ECM - Designer

  velizy villacoublay 2006 - 2007 => A380, nose fuselage frames design (18 months) ;
  * primary structures design and drawings

Formations

• Université Toulouse 3 Paul Sabatier

  Toulouse 2009 - 2012 Mechanical engineer (Conservatoire national des arts et métiers)

• Université Toulouse 3 Paul Sabatier

  Toulouse 2005 - 2006 License Pro Ingénierie simultanée et travail collaboratif

• Lycée Pierre Paul Riquet

  St Orens De Gameville 2003 - 2005

• Lycée Saint Joseph

  Toulouse 2000 - 2004

Réseau

Pas de contact professionnel