Ingeniero de materiales y procesos. composites

Parametric Study of Carbon Fibre Reinforced Thermoplastic Processing (Numerical Study). Responsible for:
•	Process window definition for AFP with in situ consolidation assisted by laser and welding processes.
•	Non-dimensional heat transfer equation using Eulerian Formulation reaching an abacus able to modify several parameters at once.
•	Powerful and less time-consuming tool - written in Matlab and Comsol M. - for design purposes.
Microstructural material characterisation and micro-scale heat transfer calculations. Responsible for:
•	Digitalization of the micro-architecture of composite tapes using the Hough Transform (Matlab code).
•	Heat transfer problem solved at the micro-scale level coupling conductive and radiative models (Matlab and FreeFem++).
•	Laser beam characterization depending on the irradiation angle (AFP process-oriented).

Parametric Study of Carbon Fibre Reinforced Thermoplastic Processing (Numerical Study). Responsible for:
•	Process window definition for AFP with in situ consolidation assisted by laser and welding processes.
•	Non-dimensional heat transfer equation using Eulerian Formulation reaching an abacus able to modify several parameters at once.
•	Powerful and less time-consuming tool - written in Matlab and Comsol M. - for design purposes.
Microstructural material characterisation and micro-scale heat transfer calculations. Responsible for:
•	Digitalization of the micro-architecture of composite tapes using the Hough Transform (Matlab code).
•	Heat transfer problem solved at the micro-scale level coupling conductive and radiative models (Matlab and FreeFem++).
•	Laser beam characterization depending on the irradiation angle (AFP process-oriented).

Designing and implementing series line of production of strakes and beams for A320NEO engines. Responsible for:
•	Design of the Resin Transfer Moulding (RTM) process of the strakes and beams for the A320NEO Fan Cowl.
•	Ply-model design from a solid model provided by the client. Optimization of unfolding models from CatiaV (Composites Design).
•	Solution for interferences between parts and RTM tooling from preliminary models. 
•	Optimization of the pattern cutting (dry fibre) for very large rates of production and potentially large amount of scrap (CNC). 
•	Hot-forming press optimization thanks to experimental development of shorter cycles. Double rate of production reached.

Designing and implementing series line of production of strakes and beams for A320NEO engines. Responsible for:
•	Design of the Resin Transfer Moulding (RTM) process of the strakes and beams for the A320NEO Fan Cowl.
•	Ply-model design from a solid model provided by the client. Optimization of unfolding models from CatiaV (Composites Design).
•	Solution for interferences between parts and RTM tooling from preliminary models. 
•	Optimization of the pattern cutting (dry fibre) for very large rates of production and potentially large amount of scrap (CNC). 
•	Hot-forming press optimization thanks to experimental development of shorter cycles. Double rate of production reached.

The technological centre of composites created by Airbus-Spain and the Spanish Government participates in a large number of projects within the composites field mainly oriented to the aerospace sector.
High Deposition Prepreg (FACTORIA Project - CEDETI) (Jun16 – Mar19):
•	Complete review of the manufacturing process of a lifting surface made from carbon fibre, typically horizontal tailplane (HTP) or wing covers. 12M€ budget.
•	New material composition and formats. Responsible for the material characterization and feedback to the provider and project partner (Hexcel) to improve the material quality. 
•	Responsible for the requirements of the mechanical and chemical test campaign, as well as a member of the group responsible for the presentation and interpretation of the results. Budget about 500K€.
•	Responsible for the new hot-forming process development for T-shaped stringers. Definition of the Roll Feet Forming (RFF) process, patented by Airbus and FIDAMC. Besides, part of the team in charge of the hot-forming press requirements and acceptance tests.
•	New AFP Head by the project partner Mtorres. Responsible for the ply-model review (CatiaV) and work following before acceptance tests. Excellent results obtained with rates over 300kg/h (current highest rates about 40kg/h).
•	Responsible for the supervision of tooling design and manufacturing. Very strict tolerances in interferences between tooling and the composite fresh/cured parts.
•	Co-lead the execution of an 18-meters-length demonstrator of a co-cured CFRP lifting surface plus stringers. 
•	Leading a team of +10 blue collars. 
Natural Laminar Flow HTP (Airbus Operations) (Nov17 - Jun18):
•	Development of an HTP with natural laminar flow requirements. Project Manager.
•	Responsible for the manufacturing execution. 
•	Due to the high-curvature surfaces and very strict tolerance requirements on manufacturing it has been necessary accurate measurements for final quality control. For this purpose a 3D model generated from million of points (meshed and refined using CatiaV) obtained by laser measurement is compared with the nominal model. 
•	Thanks to this excellent work It has been reached the next TRL of this technology, consequently a larger budget for the next trials, about 5M€.
Super-structure of the submarine S-80  (NAVANTIA) (Nov15 - Jun16): 
•	Definition of the process of the composite structure made from dry glass fibre using a Liquid Resin Infusion method. 
•	Member of the team responsible for the mechanical test campaign definition. 
•	Supporting the composite structure analysis.
One-Shot Feasibility Trials (Airbus Operations) (Jun16 - Dic16)
•	Responsible for the research of an easier demolding process in a multi-spar HTP box. 
•	It has been reduced the complexity and cost of tools for this fabrication. 
•	Project management and technical support to the design and manufacturing departments.
MotoStudent Electrical Competition (Collaboration with Polytechnical University of Madrid) (Jun16 - Jun18)
•	Development of a lightweight, high performance and design flexible shock damper employing a non-excentric carbon fibre spring, based on metallic Belleville disc springs. 
•	Supporting and training the Composites Group (3 people) of this team.
•	Third Place Winner. Best Technological Innovation. 
Dornier Wal (UAV - replica) Structure Manufacturing (Fidamc Internal Project) (Jun18 – Feb19)
•	Lead the design and manufacturing process of a UAV carbon fibre structure. All the solid parts, assembly design and ply models have been designed using CATIA V. 
•	Training and supervision of a team (4 people) formed by interns.

The technological centre of composites created by Airbus-Spain and the Spanish Government participates in a large number of projects within the composites field mainly oriented to the aerospace sector.
High Deposition Prepreg (FACTORIA Project - CEDETI) (Jun16 – Mar19):
•	Complete review of the manufacturing process of a lifting surface made from carbon fibre, typically horizontal tailplane (HTP) or wing covers. 12M€ budget.
•	New material composition and formats. Responsible for the material characterization and feedback to the provider and project partner (Hexcel) to improve the material quality. 
•	Responsible for the requirements of the mechanical and chemical test campaign, as well as a member of the group responsible for the presentation and interpretation of the results. Budget about 500K€.
•	Responsible for the new hot-forming process development for T-shaped stringers. Definition of the Roll Feet Forming (RFF) process, patented by Airbus and FIDAMC. Besides, part of the team in charge of the hot-forming press requirements and acceptance tests.
•	New AFP Head by the project partner Mtorres. Responsible for the ply-model review (CatiaV) and work following before acceptance tests. Excellent results obtained with rates over 300kg/h (current highest rates about 40kg/h).
•	Responsible for the supervision of tooling design and manufacturing. Very strict tolerances in interferences between tooling and the composite fresh/cured parts.
•	Co-lead the execution of an 18-meters-length demonstrator of a co-cured CFRP lifting surface plus stringers. 
•	Leading a team of +10 blue collars. 
Natural Laminar Flow HTP (Airbus Operations) (Nov17 - Jun18):
•	Development of an HTP with natural laminar flow requirements. Project Manager.
•	Responsible for the manufacturing execution. 
•	Due to the high-curvature surfaces and very strict tolerance requirements on manufacturing it has been necessary accurate measurements for final quality control. For this purpose a 3D model generated from million of points (meshed and refined using CatiaV) obtained by laser measurement is compared with the nominal model. 
•	Thanks to this excellent work It has been reached the next TRL of this technology, consequently a larger budget for the next trials, about 5M€.
Super-structure of the submarine S-80  (NAVANTIA) (Nov15 - Jun16): 
•	Definition of the process of the composite structure made from dry glass fibre using a Liquid Resin Infusion method. 
•	Member of the team responsible for the mechanical test campaign definition. 
•	Supporting the composite structure analysis.
One-Shot Feasibility Trials (Airbus Operations) (Jun16 - Dic16)
•	Responsible for the research of an easier demolding process in a multi-spar HTP box. 
•	It has been reduced the complexity and cost of tools for this fabrication. 
•	Project management and technical support to the design and manufacturing departments.
MotoStudent Electrical Competition (Collaboration with Polytechnical University of Madrid) (Jun16 - Jun18)
•	Development of a lightweight, high performance and design flexible shock damper employing a non-excentric carbon fibre spring, based on metallic Belleville disc springs. 
•	Supporting and training the Composites Group (3 people) of this team.
•	Third Place Winner. Best Technological Innovation. 
Dornier Wal (UAV - replica) Structure Manufacturing (Fidamc Internal Project) (Jun18 – Feb19)
•	Lead the design and manufacturing process of a UAV carbon fibre structure. All the solid parts, assembly design and ply models have been designed using CATIA V. 
•	Training and supervision of a team (4 people) formed by interns.

Thesis: “Lightning Strike Test Study”. Challenging project in collaboration with Airbus Defence and Space, based on a comparison between Non-Destructive inspections and
thermography records during a Lightning Strike Test (LST).

Thesis: “Lightning Strike Test Study”. Challenging project in collaboration with Airbus Defence and Space, based on a comparison between Non-Destructive inspections and
thermography records during a Lightning Strike Test (LST).

Thesis: “The Executive Aviation in Cuatro Vientos”. Project-based on a study about how to move the executive aviation at the airport of Cuatro Vientos, placed in Madrid.
Conducted rigorous design of the new structure of the airport and business plan.
Reached saving’s amount of 212 million euros for the Spanish government- community of Madrid. ”

Thesis: “The Executive Aviation in Cuatro Vientos”. Project-based on a study about how to move the executive aviation at the airport of Cuatro Vientos, placed in Madrid.
Conducted rigorous design of the new structure of the airport and business plan.
Reached saving’s amount of 212 million euros for the Spanish government- community of Madrid. ”

Thesis: “Study of air traffic between Latin America and Spain”. Performed an economical study trying to map and statistically summarise the vast amount of airplane traffic between Spain and the broad geographical region of Latin America.

Thesis: “Study of air traffic between Latin America and Spain”. Performed an economical study trying to map and statistically summarise the vast amount of airplane traffic between Spain and the broad geographical region of Latin America.