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Résumé de l'offre
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Type de contrat:
CDI / Permanent -
Lieu:
Pune -
Niveau d'expérience:
6 à 10 ans -
Publiée le:
3/29/2024
Description de l'offre
Type d'emploi : CDI / Permanent
Description de l'offre
Job Description:
Job scope (core activities):
• Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs
• Extraction of loads, stresses, generation of spectra and mission files
• Extraction of material data, geometry details and fastener specifications from part & assembly drawings
• Application of appropriate static, fatigue and damage tolerance design values from standard references
• Creation of FEMs using geometric data from part & assembly drawings
• Sizing of primary and secondary parts for static and fatigue requirements
• Fastener load extraction and joint analysis
• RF calculation for different failure modes such as strength, buckling, shear panel failure, damage tolerance etc.
• Low RF mitigations using classical or numerical methods
• Preparation of stress certification dossiers, ACD4 and ACD6
Profil souhaité
Qualification : B.E / M. E. in Mechanical / Aeronautical Engineering
Graduate / Post Graduate Engineer (Aerospace Engineering / Mechanical Engineering).
Experience Range : 6 - 9 years of experience in static analysis
Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities
Minimum 3 years’ experience in leading team.
Experience in High Lift is an advantage
Keyskills :
- Tools : Patran/Nastran, Hypermesh, ISAMI (preferred)
- Advanced Knowledge of Microsoft Office Software
- Sound knowledge of structural design principles, aircraft loads and aircraft structures
- Experience in static, fatigue and damage tolerance analysis of aircraft structural components
- Knowledge of Airbus internal Static manuals, methods and policies mandatory
- Advanced knowledge of hand and classic calculation methods (e.g. HSB, Bruhn…)
- Background in design and sizing of aircraft primary structure components and parts
- Ability to liaise/negotiate with design, stress, EU teams and customer services
- Certification requirements and experience with stress dossiers
- Finite element method / finite element analysis (FEM / FEA)
- Knowledge in Metallic / CFRP aircraft structure
- Very good analytical and reasoning skills