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Role Purpose
To perform stress activities, carrying out challenging analysis and calculations on a wide range of state of the art aerospace components. The role offers opportunities for developing skills, knowledge and experience in this exciting industry.
Principal Responsibilities/Accountabilities
* Delivering design solutions by carrying out structural & thermal analysis of aero engine and/or naval marine components
* Linear/Nonlinear stress analysis of rotating/static components.
* Ensure stress reports meet the appropriate levels of quality and robustness and confirm that defined requirements are met.
* Ensure that all project stakeholders have the right information at the right time, through pro‑active communication.
* Support other team members with ongoing/future work packages.
Baseline Responsibilities
* Technical support and execution for all stress/lifing activities such as:
* Application of Vibration (Campbell Diagram) analysis, creep analysis.
* Application of Low cycle fatigue (LCF), High cycle fatigue (HCF), creep, corrosion, erosion and crack propagation assessment of rotating machinery.
* Damage and Tolerance/Melt anomaly methods.
* Support thermo‑mechanical solutions.
* Contribute to development of best practices and productivity improvements.
Experience
Applicants should have a proven background in gas turbines or naval marine applications at component level.
Ability To
* Quickly understand problems, set priorities.
* Actively lead various tasks and issues while continuously working towards improvements.
* Drive technical delivery through adherence to key processes (safety, concessions, lifing, etc.).
* Understand complex system interactions.
* Interpret technical analysis, draw out key issues and present to project for review.
* Develop technical solutions, compliant with requirements, and make technical recommendations.
* Develop solutions, based on experience, in new product designs.
Knowledge
* Demonstrate a good understanding of all aspects of aero engine or naval marine components.
* Understand the Safety Process for in‑service engines.
* Understand the behaviour and limitations of aerospace materials.
* Understand component lifing strategies and limitations.
* Knowledge on system behaviour under impact loading.
* Knowledge of composite failure & analysis methods.
Tool Knowledge
Experience of one or more of these is essential: ANSYS, PLM, UG NX, LS‑Dyna, ICEM Meshing, ABAQUS, HYPERWORKS, SCO3. Desirable: NASTRAN, PATRAN, Simcenter.
Qualifications
Masters degree in Engineering (e.g. Aeronautical, Mechanical or Aerospace Engineering) or equivalent experience in an OEM.
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