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Technical leadership of Mechanical Design Engineering teams (Work Units) responsible for Compressor, Combustion Chamber, Turbine – Static / Rotative Parts.
Cooperate with Design Office Manager in creation of new Mechanical Design Organization within Safran Aircraft Engines Poland – collaboration contracts, technical specifications, remote teams management policy, work coordination, hiring.
Supervise, track and report progress of activities and projects within Work Unit of Design Office.
Full accountability for agreeing the new activities, defining deadlines, tracking and reporting work progress in direct contact with the external customer.
Technical validation of work related to non-conformity assessment of aero engines components.
Preparation of strength analyses (static, LCF, HCF, fatigue, overspeed, FBO, crack propagation) of aero engine components using FEA (Ansys Workbench) and analytical methods.
Defining technical solutions (request for drawing change, Production Permit, process optimization) to eliminate non-conformities on products.
Day-to-day cooperation with internal and external stakeholders from design, technology, quality, and manufacturing at various stages of implementation and serial production.
Must:
Language: English, C1.
Master degree in engineering.
Teamwork, analytical thinking, self-motivation, ‘can-do attitude, and decision-making skills.
Ability of technical drawing interpretation.
In-depth understanding of the Theory of Elasticity, Fatigue Strength, and related challenges.
Professional experience as a mechanical engineer / stress engineer preferably in aerospace industry.
Strong technical and team leader skills.
Ability to empower and motivate people.
Ansys or Patran or Abaqus or Hyperworks Experience.
Nice to have:
Catia V5 experience.
Solid Edge Experience.
Language: French.
Design and GD&T experience will be considered a plus.
Knowledge of design and operation of aircraft engines.