Technical group leader of 20+ engineers.Responsible of system architecture definition and development (preliminary design solutions, conception, specification, V&V and safety activities) of Fan Pitch Actuation Systems for future aircraft engines. Several projects in parallel from 2024 test demonstrations to 2033+ new solutions maturation.

Group leader (5 p.) of the team in charge of the architecture and safety analysis of the RISE engine (preliminary design project).

In charge of engine or sub-systems architecture in preliminary design phase : - Needs capture- Global architecture definition- Solutions trading- Safety activities (failure analysis) to help define the best architecture

Group leader (5 p.) for external systems aerodynamic design of the Silvercrest engine.

Design optimization of external parts of aircraft engines (air intake, nacelle, nozzle, secondary duct, scoops, etc): - CAD, meshing, numerical simulations, post-processing and optimization- Validation and calibration through mock-up and engine tests

Turbopropeller inlet aerodynamics optimization by mesh morphing and CFD

Prediction of new technologies development and production costs.