Maxime Philipot

Calculation Engineer in the Aero- & Thermodynamic department of MAN Diesel & Turbo SE Responsible for the design of integrally geared compressors for Oil & Gas Industry Looking for compromise in thermodynamics, mechanics & systems to reach best efficiency at low cost and with maximum safety Take part in compressor performance test, cost optimization projects and software development

Engineering consultant within the Aero- & Thermodynamic department of MAN Diesel & Turbo SE in Berlin Calculation of the design of integrally geared compressors for Oil & Gas Industry Looking for compromise in thermodynamics, mechanics & systems to reach best efficiency at low cost and with maximum safety Take part in software development

Engineering Consultant working within the Compressor Rig Testing departement of MTU Aero Engines, Munich, Germany. Intermediary with Engine Performance department and Performance department of MTU's Customer. Validation of real-time and post-processing performance calculation corresponding to rig testing.

Master's Thesis (Diplomarbeit) on Aircraft Engines Performance Engine Performance department Subject matter: A Method for On- and Off-board Diagnostics of Aircraft Engine Performance based on a Linear Operating Behaviour Application on the latest Eurofighter Typhoon's engine, EJ200

Internship on Aircraft Engines Development Combustor Department Subject matter: Combustor optimisation using CFD Methods (Computational Fluid Dynamics) CFD Simulations using different calculation methods to compare cooling efficiencies of different combustor geometries

Working as a blue-collar worker. The goal was to learn the functioning of a company and experience team work.

Aerospace and Energy Engineering (Luft- und Raumfahrttechnik und Energietechnik): Thermodynamics, Aero Propulsion, Engine Performance, Numerical Methods for Real Flow in Turbomachinery... Lectures mainly attended at IST (Insitute of Jet Propulsion and Turbomachinery) - All lectures, exams in german

Propulsion engineering: Fluids mechanics, Thermodynamics, Combustion, Turbomachinery, Heat transfer, Programming, Numerical Methods (FEM) - One-year project-study on a test bed for a helicopter combustion chamber from TURBOMECA. It consists in proportioning and designing the test bed.