GENERAL INFORMATION

• Customer: AIRBUS OPERATIONS
• Technologies: Fatigue and Damage Tolerance Analysis, Finite Element Method, Non-Linear Analysis

DESCRIPTION

• Fatigue and damage tolerance analysis
• FEM modelling (GFEM and DFEM)
• Non-linear simulation of structures
• Process optimisation, automation and scheduling
• Definition of calculation methodologies

PROJECTS

• -1000 Step 7.1: Fatigue analysis and damage tolerance of frames (Milled Frames FR95 to FR98)
• -900 MSN006-073: Fatigue analysis and damage tolerance of RCF (Rear Corner Frames)
• -900 RPB MSN460: Fatigue analysis and damage tolerance of frames and THSA Fitting (Milled Frames FR95 to FR98)
• -900 RPB MSN460: Fatigue analysis and damage tolerance of frame 102
• -900 & 1000 RPB Shift: Fatigue analysis and damage tolerance of frames and other components
• -900 MSN316: Fatigue analysis and damage tolerance of frames and other components
• 1000 MSN216 ULR: Fatigue analysis and damage tolerance of frames and other components -900 MSN316: Fatigue analysis and damage tolerance of frames and other components
• -1000 MSN216 ULR: Fatigue and damage tolerance analysis of hardware. Windmilling analysis
• -1000 MSN88: Fatigue analysis and damage tolerance of interface hardware between S19 and S191, Y-Bolt and other components.
• Development of non-linear FEM models:
  • Stringer Run Out Root Joint (strength and fracture analysis using Virtual Crack Closure Technique – VCCT method.
  • Non-linear detail model (Abaqus) MSN006
  • Detailed analysis of the skin-frame foot connection
  • HTP Step 6