Whole Engine Thermal Analysis

* Thermo-mechanical analysis for the calculation of component temperatures and displacements to support the design and lifing of these components
* Generating thermo-mechanical models including setting up the proper heat transfer boundary conditions, e.g. relation between external flow pattern and convective heat transfer coefficient

* Analysis of relative movements and optimisation of seal and tip clearances on whole engine level
* Defining and analysing validation and approval tests
* Interaction with other technical units, particularly as regards component design and thermal analysis
* Compile technical reports for engine certification and approval of design changes

VORAUSSETZUNGEN:

* Expertise and know-how in the field of heat transfer, thermo-mechanical analysis, and fluid dynamics as well as state-of-the-art engineering tools such as FEM and CFD
* Knowledge of Thermal system functionality, including component temperature prediction, boundary condition management and thermo-mechanical behaviour
* Ability to calculate component and assembly thermal and thermo-mechanical behaviours, including numerical modelling, and support the definition of engineering architecture at whole system level to achieve optimum component temperature and assembly clearance control
* Above-average academic track record, with Diploma or Master‘s degree (or equivalent) in Mechanical/Aerospace Engineering or comparable qualifications
* Demonstrable expertise relating to turbo engines, gas turbines and/or aero-engines
* Fluent English

We welcome your application. Please inform us about your charge rate including all expenses and your earliest availability.

EINSATZBEREICHE:

Luft- und Raumfahrttechnik, Ingenieurwesen/Technik, Sonstiges