Descripción del trabajo - Senior Static Stress Engineer (m/w/d)
Founded in 1962, SOGECLAIR is a group of engineering companies specializing in high technologies. With an international presence, SOGECLAIR has extended its influence beyond national borders, reinforcing its ability to innovate and collaborate with partners worldwide.
SOGECLAIR DIGITAL ENGINEERING consolidates and develops engineering projects within the group, featuring a diversity of areas of expertise. As a company with a human dimension, SOGECLAIR and its teams of experts offer a wide range of mechanical engineering skills, from research and development to service support.
As a designer of innovative, high value-added products and solutions, SOGECLAIR DIGITAL ENGINEERING brings its high-tech engineering skills to the cutting-edge aeronautical, space, rail and naval sectors.
We are looking for a Senior Static Stress Engineer with 10 years of proven experience in the aerospace industry. Candidates should be proficient in the following tasks:
Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs
Extraction of loads, stresses, generation of spectra and mission file.
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
Minimum 10 years' of experience in static analysis
Degree in (Aerospace Engineering or similar
Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities.
Minimum 10 years’ experience in leading team.
Professional experience in Patran/Nastran, Hypermesh, ISAMI
Fluency in Spanish and English
Experience in both metallic and composite material.
Sound knowledge of structural design principles, aircraft loads and aircraft structures
Experience in static, fatigue and damage tolerance analysis of aircraft structural components (Airbus methods and tools preferable)
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)
Very good analytical and reasoning skills
Strategic career progression with international mobility opportunities
Advanced training and leadership development in high-profile aerospace programs
Empowering team culture with direct impact and cross-functional collaboration and more
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