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Job Description: Tasks As a Fatigue & Damage Tolerance Analysis Engineer, you will develop the following challenging tasks and activities: Analyze and validate metallic, composite & hybrid structures for Fatigue and Damage Tolerance (F&DT), using Airbus Defence & Space methods, to assess design solutions for a whole range of tasks, potentially from concept and structural development to certification and in-service maintenance Sizing of the structural components, parts and assemblies from Fatigue point of view Definition of fatigue loading spectra for lightweight structures in military programs Determination of fatigue allowable stress levels for sizing Selection of manufacturing technologies, materials and standards during the sizing Support the structural design process to ensure required quality is achieved for F&DT within direct area of responsibility Definition and establishment of the certification/qualification fatigue documents Definition of inspection programs based on fracture mechanic approaches Structural test definition, support and analysis of the tests Participation in the development of the technological areas of engineering and manufacturing Support to develop of the Digital Design workflow Influence areas F&DT engineers work in cooperation with many stakeholders of the company, including: Engineering and Technologies: Structural and System installations design, Materials & Processes, Weight and Balance, Standardization and Research & Development Operations: Manufacturing Engineering, Maintenance Services: Back office of Services Engineering, Maintainability, Technical Publications, Services Bulletins
Job Responsibility:
Analyze and validate metallic, composite & hybrid structures for Fatigue and Damage Tolerance (F&DT), using Airbus Defence & Space methods, to assess design solutions for a whole range of tasks, potentially from concept and structural development to certification and in-service maintenance
Sizing of the structural components, parts and assemblies from Fatigue point of view
Definition of fatigue loading spectra for lightweight structures in military programs
Determination of fatigue allowable stress levels for sizing
Selection of manufacturing technologies, materials and standards during the sizing
Support the structural design process to ensure required quality is achieved for F&DT within direct area of responsibility
Definition and establishment of the certification/qualification fatigue documents
Definition of inspection programs based on fracture mechanic approaches
Structural test definition, support and analysis of the tests
Participation in the development of the technological areas of engineering and manufacturing
Support to develop of the Digital Design workflow
Requirements:
University Aeronautical Engineering Degree or equivalent
At least 1 year of experience in F&DT Structural Analysis of airframe components, mainly but not limited to metallic structures
Knowledge of structural analysis in general and design details of airframe
at least basic experience in stress/fatigue tools (standard Finite Element Method codes and software packages)
Knowledge of standard references: books, papers, standards, etc
Metallic and composite materials behavior knowledge
Fluent English language
What we offer:
Vacation days plus additional days-off along the year
Attractive salary
Hybrid model of working when possible, promoting the work-life balance
Collective transport service in some sites
Benefits such as health insurance, employee stock options, retirement plan, or study grants
On-site facilities (among others): free canteen, kindergarten, medical office
Possibility to collaborate in different social and corporate social responsibility initiatives
Excellent upskilling opportunities and great development prospects in a multicultural environment