Description courte : Location: Beijing (Shunyi) Starting date: ASAP The job context is related to the turbo propeller engine design activities with 2 modules concerned: the flame tube and the power turbine. Missions -To support the Chief Technical Officer and the Deputy Chief Technical Officer to manage transversally the numerical methods and be creative to find new propositions and technical solutions, -With specifications and interfaces given by mother companies, the objective is to lead and improve numerical computations and parts design with the support of the technical leader and his team to achieve the final objective given by Mother Companies, -To study on AI driven data collection and AI enabled turbine design
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