Structural engineer
Alb*** ***** (XX años)
Space Structural Optimization Engineer en CITD
Carlos III University of Madrid - UC3M
Madrid,
Madrid
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Experiencia
Space Structural Optimization Engineer
CITD
sep 2017
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Actualmente
Space structure analysis and additive manufacturing in Airbus Space projects. • Structural analysis of JUICE spacecraft (primary and secondary structure) in CDR and MRR phases. • Structural topology optimization of parts for additive manufacturing. • Structural analysis of H3 launch vehicle Payload Adapter Fitting (PAF) for HTV-X spacecraft. • Design and analysis of MGSE and test set-ups. • Static and dynamic analysis. • Performing testing phase of Jason-CS/Sentinel-6 spacecraft. • Creation and validation of FEM models. • Documentation: structural analysis report.
Space Structural Engineer
ATOS
dic 2016
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sep 2017
Space structure analysis in Airbus Space projects. • Structural analysis of JUICE spacecraft in PDR phase. • Structural analyses of Jason-CS/Sentinel-6 spacecraft in CDR phase. • Static and dynamic analysis. • Creation and validation of FEM models. • Fatigue analysis of cleats. • Documentation: structural analysis report.
F&DT Stress Engineer
ATOS
abr 2016
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dic 2016
Fatigue and damage tolerance analyses. • F&DT analyses of A350-900 XWB S19 (MSN5 and MSN74). • Analyses of spectra, fatigue lives and crack propagations. • Metallic frames and joints analyses (inner caps, support holes, mouse holes and skin joint). • Knowledge of ISAMI (F&DT modules). • Documentation: certification reports and ACDs.
Stress Engineer
ATOS
nov 2012
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mar 2016
Airbus A380 structures analysis. • Modifications and concessions of Airbus A380 (section 19, 19.1 and HTP). • Parametric evaluation of rear corner splices (Section 19). • Studies of the Section 19 upper corner skin area residual strength, as result of the appearance of some cracks. • Creation and modification of FEM models. • Justification of section 19.1 parts which have been affected by curing cycle deviation. • Pull-through justification of the frame-skin joint of Section 19. • Frame riveting justification of Section 19 for aircraft A380-800, adding global thermal loads. • Study for the replacement of BMI to Epoxy in Section 19.1. • Justification of section 19 for Russian Certification (loop loads) • Correlation of GFEM and test results. • Development of tools for data processing by VBA/Excel. • Airbus tools knowledge. • Documentation.
Formación
Degree in Mechanical Engineering
Carlos III University of Madrid - UC3M
sep 2008
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jul 2013
Idiomas
Spanish - Native language
English - Upper intermediate level
French - Upper intermediate level
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