Stress Engineer

1w1 week ago

Airbus

Beijing, CN · Full-time · CNY 350,000 – CNY 550,000

About this role

The jobholder provides stress validation to the design solutions addressing NC and Concessions occurred during manufacturing in Airbus plants. Working with Airbus design office, provide stress justification for the modifications of all Airbus programs. This role ensures structural integrity across production processes.

Perform detail stressing of components and mechanisms according with Airbus procedures, standards and methods. Analyze and validate Metal &/or Composites / Hybrids structures at component level for static strength, F&DT, producing relevant strength margins or reserve factors according to validated Airbus methods.

Analyze static strength and dynamic capabilities with provided loads to calculate strength margins and generate reports. Apply finite element method or classical analysis methods to predict failure modes of aircraft metallic and composite structures. Generate fatigue spectrum from aircraft cycle definition files for fatigue and damage tolerance analysis.

Support manufacturing with stress analysis of non-conformity for element parts and assembly. Operate in a multicultural and international environment at Airbus Beijing Engineering Centre. Airbus fosters flexible working arrangements and commits to workforce diversity and inclusive practices.

Requirements

Bachelor and above degree major in mechanical design or aircraft design or mechanical engineering
Minimum 2 years experience of static strength analysis for metal or composite structure
Experience of fatigue and damage tolerance (crack propagation) analysis
Good technical understanding of aircraft structure analysis, repair, or plant engineering
Good at Patran, Nastran, Hyperworks
Good level of English skills in both writing and speaking
Capability in programming like VBA, Python
Good interpersonal communication skills in a multicultural and international environment

Responsibilities

Provide stress validation to design solutions addressing NC and concessions during manufacturing
Provide stress justification for modifications of all Airbus programs working with design office
Perform detail stressing of components and mechanisms according to Airbus procedures, standards and methods
Analyze and validate metal, composites or hybrid structures at component level for static strength and F&DT
Analyze static strength and dynamic capabilities with provided loads to calculate strength margins and generate reports
Apply finite element method or classical analysis methods to predict failure modes of aircraft structures
Generate fatigue spectrum from aircraft cycle definition files to perform fatigue and damage tolerance analysis
Support manufacturing with stress analysis of non-conformities for element parts and assemblies