sampath singh

Airbus Hydraulic & Highlift Systems Bremen •FEM for linear and non-linear stress analysis using PATRAN, NASTRAN. •Life estimation of equipment using the endurance profiles •Fatigue and damage tolerances calculation and life estimation of coiled pipes using AFI methodology. • Part of the stress team to find the Root cause analysis for fractured or damaged equipment. • Supporting the qualification of hydraulic equipment’s according to RTCA DO-160 by reviewing the stress justification reports from suppliers.

Masterarbeit Thema :FEM-Simulation von Wälzlagern an der gebauten Nockenwelle * Untersuchung möglicher Arten der FE-Simulationen eines Wälzlagers und die Auswirkung auf die Nockenwelle. * Empfehlung für das update des Mahle Simulations- Standards Nockenwelle.

Masterarbeit Thema :FEM-Simulation von Wälzlagern an der gebauten Nockenwelle * Untersuchung möglicher Arten der FE-Simulationen eines Wälzlagers und die Auswirkung auf die Nockenwelle. * Empfehlung für das update des Mahle Simulations- Standards Nockenwelle.

Forschung und Entwicklung von Diskrete-Element-Methode mit EDEM, Visual Studio C++ und MATLAB und Erzeugen von Makros mit Visual Basic.

Studentische Hilfskraft für Einführung in der Bruchmechanik Kurs

Period of activity : 09/2012 – 07/2013 Topic “787-9 Nacelle Structure Analysis“ • Static, Fatigue and Finite Element Analysis of composite and metallic aircraft structures. • Creation of structural analysis reports for various components using numerical and analytical hand calculation methods. • Collaborating with the design teams and performing strength analysis calculations thereby meeting the manufacturing requirements. • CAD/FEM Tools: PATRAN, CATIA v5, HSB, Bruhn, Microsoft Office.

Period of activity : 10/2011 – 09/2012 Topic “A350 XWB Wing Upper Cover Analysis“(FERCHAU Engineering GmbH) • Composite Structural Repair Assessment on A350 Wing upper cover (Concession Work) • Designing the composite structures for wing upper cover by meeting the manufacturing requirements. • Fatigue and Damage Tolerance analysis • Sizing study of Bolted joints on composite and metallic structures using Airbus tools. • CAD/FEM Tools: PATRAN, NASTRAN, Airbus CBJT Tools, ISAMI, Microsoft Office.

Initial Learning Program in New Product Developement Field.

Bruchmechanik, Finite Element Methoden, nicht linear solid Mechanik, Struktural Mechanik, Constitutive Material Modelling, Partielle Differetialgleichungen, Wisschenschaftliche Rechnen. Abschluss Note: 2,4 Masterarbeit: FEM-Simulation von Wälzlagern an der gebauten Nockenwelle

Festkörpermechanik, Struktural Mechanik, Thermodynamik, Quality management, Project management, Intellectual Property Rights. (Abschluss Note: 7,8 - First Class with Distinction) Bachelorarbeit: Effective methodologies for supplier selection and order quantity allocations.