Engineering vacancy with Airbus in China

If you are interested, please email your CV to Zijun.Jin@airbus.com.

ABEC-001 Stress Engineer 应力分析工程师

Common Requirement

• The basic knowledge of the aircraft structure (or at least the slim beam/thin shell structure) is a plus
• Could work with people in a team and have the commitment to one’s work
• Could explain technical details and communicate in English, the capability to communicate with international customers is a plus
• A quick learner and a technical thinking inclination are quite preferred

Detailed technical requirements

Static

• Good knowledge on Material Mechanics, solid command of basic concepts (material properties, beam theory, failure criterion, buckling, etc); knowledge of Elastic Mechanics is a plus
• Experience of metal static analysis, especially on buckling and joint; experience of analysis on aircraft structure or the slim beam/thin shell structure is appreciated
• Capable to build calculation model from real structure, capable to perform hand calculations, good command of MS Excel with VBA programming as a plus

Composite

• Knowledge on composite material, manufacturing and characteristics, sandwich structures, sizing composite structure, composite structure test or NDI (non destructive inspection) for composite structure
• Basic knowledge of composite CLA (classic laminate theory, such tape/fabric properties, ABD matrix, CLA assumption, etc)
• Experience of composite structure modeling/Analysis in Patran/Nastran, with laminate modeler as a plus.

FEM

• work experience with constantly FEM modeling and analysis, meshing skill is strongly requested, using Patran/Natran is a plus    
• Basics of FEM theory and corresponding numerical knowledge, experience of the FEM source coding is preferred and a plus
• If candidate's major FEM experience is Patran/Nastran, then she/he should have:
• Basics of the element properties and definition (including the RBE and MPC), the load/constraint definition, the material properties definition, composite knowledge is a plus
• Basics of the common solution series and subcase control (especially SOL101 and SOL105)  in Nastran analysis, analysis deck format
• Basics of the Nastran operation environment especially the UNIX system.
• Work experience of the preprocess especially the mesh work, the post-processing, especially the free body load extraction, fringe, marker and cursor operation in Patran etc, with PCL program capability as a plus

F&DT

• Basics Mechanics theory background, especially on Fracture mechanics, be familiar of basic concepts of Fatigue and Damage Tolerance.
• Fatigue and Crack Growth analysis experience, could perform fatigue and damage analysis with different tools
• Capable of how to select of critical damage locations (on A/C structures is a plus)