Manuel Martin de la Escalera Hernandez

Project: AIRBUS A330NEO and BOEING 777X Engine Exhaust Nacelles (MRB Department). Customer: SAFRAN Nacelles (France). Static and Fatigue strength justification of different metallic parts damages and deviations through concessions. Linear and Buckling FEM Analysis through MSC Patran global and detailed FEMs. SRM analysis analysis to justify ADL/RDL diagrams and repairs. Verification technical approval signature (VT signature) in A330Neo and B777X programs.

Project: AIRBUS A350XWB Horizontal Stabilizer and Elevator (SRM Department). Customer: AIRBUS Getafe (Spain). Linear and Buckling FEM Analysis through MSC Patran and ABAQUS DFEMs. Static and Fatigue strength analysis to justify ADL/RDL diagrams and repairs ot the metallic fittings and composite parts using different ISAMI modules. SRM Validation reports.

Project: AIRBUS A350XWB- Horizontal Stabilizer and Elevator (Stress and MRB Department) and A330 Main Landing Doors. Linear and Buckling FEM Analysis through MSC Patran and ABAQUS DFEMs. Static strength analysis of different metallic and composite parts. A350XWB and A330 Concesions of metallic fittings and composite parts justifying different damages and deviations. Certification reports of A350XWB-1000 and 900 HTP and Elevator parts.

Project: 190E2 Executive Jet Horizontal and Vertical Stabilizer GFEM Optimization and Update of the Horizontal and Vertical Stabilizer through MSC Patran-Nastran Analysis of the Horizontal Stabilizer GFEM stiffness to satisfy the aero-elastic requirements. Linear and Buckling GFEM Analysis through MSC Patran. Creation of tools to generate the HS element properties by Microsoft Office Excel Macros. Static strength calculations of metallic parts.

Project: AIRBUS A350XWB Horizontal Stabilizer and Wing Trailing Edge. Linear and Buckling FEM Analysis through MSC Patran and ABAQUS DFEMs. Static analysis of different metallic and composite parts using ISAMI. Concesions of metallic fittings justifying different damages and deviations. Result post-processing using Microsoft Office Excel (Visual Basic). MAT-C and First Flight Validation Reports.

Project: AW169 and NH90 (Internship). Customer: AGUSTAWESTLAND (Cascina Costa di Samarate, Italy). Modeling and Sizing of the different components of the hydraulic system parts (Hydraulic pumps, pipes, hoses, valves…). Verify the capability of the helicopter to carry out the required flight maneuvers depending on the different parameters of the hydraulic system (temperature, pressure, the flow-rate of the fluid).

Thanks to a double certificate program between Universidad Pontificia de Comillas de Madrid