Stress engineer (static and f&dt)

-Structural analysis (Static and Fatigue and Damage Tolerance) from A350XWB-900/-1000 slats and A220-300 Fixed Leading Edge in Sonaca for Airbus Operations.

-Certification of new loop loads and configurations as well as non-conformity reviews (NCR) and failure modes.

-Work with SONIA and Nastran/Patran program for modelling design, load inputs, generation, processing, post-process, display and results presentation

-Work with CATIA program for FEM remeshing.

-Non-linear analyses using con Nastran/Patran (SOL106) ; FEM model modification such as Load factors, Non-Linear stiffness curve in fasteners , elastoplastic material...

-Study and analysis of all joints in A220-300 leading edge components. Mitigations carried out where needed (load redistribution, improvement of allowables...)

-7 months working in Customer installations (Belgium). After that, working for them in Madrid Offices.

-Service Request (SR) resolution about aircraft systems and structures for Airbus Defence & Space Customers in Backoffice. L&M Aircrafts: C-212, CN-235, C295

-Service Bulletin (SB) scrutiny with SMART program.

-Operating with CRM and maintenance manuals such as AMM, MRBR, MRBD, CMM, etc, ,besides, IPC, Sprint.net.

-After-sales documentary management of bulletins (SB), AOT, OIT, SIL, etc, in Front Office for L&M (C-212; CN-235 and C295)

Stress engineer in Structural Repair Maintenance C295 and CN-235 to Airbus Defence & Space.

-Structural static analysis using HSD, ESDU (longitudinal beam, frames, fuselage, wing, ribs, spars, skins,...)

-Structural books to static calculation by hand such as Bruhn, Niu, Roark...

-Work with Legacy tools (Crippling, Uniones, Aida, FLEXA,FITAN, Panal, Panco, FREM, Pretension,...)

-Flap sizing calculation

-Rivets and removable joints calculation to structural items.

-Work with analysis files from Structures Calculation program such as Nastran/Patran to analyze GFEM and DFEM.

-Calculation files post-processing from Airbus D&S in wing structure such as ARBUS, COSTI...

-Mechanical desig tool Catia V5.

-Sprint.net for drawings 2D and configuration.

Stress Engineer on the Project of Horizontal Tail Plane (HTP) modifications in A330 working for Airbus Operations.

Work with several programs for Structures Calculation:
- Nastran/Patran
- Isami
- VBA Excel
- ACD tool

Aeronautical Design Engineer on the Project to optimize passenger’s door of A330 (S.18) for Airbus Operations.

- Mechanical Design: Using the following tools:

• CATIA V5: Draftings, assemblies and installation of components made by sheets, injection molding
for plastics, maching.

• SPRINT : "Drawing set" Documentation for Airbus operations.

• EPD CONNECT (Optegra) : Implementation of PS and Vault handling for Airbus operations.

- Study of product structure of DMU. Configuration. Changes of effectivity. Documental correction.

- Collaboration and support in different projects design about modifications from time to time: SRM, Belly Fairing Design, installation of water waste tank S18, etc

Research and development of an internal project about rear auxiliary propulsion in R&D Department which belongs to Aeronautics, Space and Defense subsection., focusing on:

- Research and development of a new propulsion system, searching an innovative product.

- Conceptual and preliminary design of the structure, using CATIA V5.

- Calculation: Structural loads analysis and impact on the structure, using Nastran/Patran.

-Analytical pre-dimensioning in composite material for S19 from A330. Analysis of A330 documentation and failure modes, 

- Work closely with the documentation, draftings, SRM, component documents of A330/A340 fuselage.

- Work with advanced tools for generation and processing of Finite Element Models such as Nastran/Patran.

- Application of technical requirements on the new design consisted on composite materials for a passenger aircraft.

- Analysis of failure modes in order to achieve finally an optimized design.

- Graduated with honors from the final thesis project.

Work with CATIA V5 during 650 hours. Some practices in electrical design, tools design, composites, sheet and maching design.		               

Plan 2000 Engineering.

Graduated with honors from the final thesis project “Alternativa al diseño actual del revestimiento de la sección S19 metálico de los aviones A330/A340:  Revestimiento en CFRP” at Airbus Operations S.L