Turbofan Analysis Simulation and Modeling Engineer

GENERAL QUALIFICATIONS

• Graduated from Mechanical, Aerospace, Aeronautical, Manufacturing, Automotive, or Mechatronics Engineering departments,
• Possesses a theoretical background in strength, heat transfer, statics, dynamics, vibration, fatigue, and materials,
• Experienced in finite element analysis (preferably using ANSYS),
• Proficient in engineering software such as ANSYS, MATLAB, and CAD tools,
• Knowledgeable about the working principles of turbofan engines and their components under high temperature, vibration, and mechanical durability conditions,
• Technically competent to understand aerospace standards and regulations (e.g., FAA, EASA, MIL, SAE) and proficient in technical English,
• Skilled in using general engineering tools and software (e.g., MS Office),
• Follows industry developments and has an innovative mindset,
• Able to work in coordination with other teams related to responsibilities,
• Possesses strong communication skills and is inclined to teamwork,
• For male candidates, has no military obligation for at least 2 years,
• Resides or is willing to reside in Istanbul.

PREFERABLY

• Holds a Master's or Ph.D. degree in Mechanical, Aerospace, Aeronautical, Manufacturing, Automotive, or Mechatronics Engineering,
• Has at least 2 years of relevant work or project experience,
• Knowledgeable in structural analysis, structural optimization, and load distribution of engine components,
• Familiar with rotor dynamics concepts such as Campbell diagrams, Bode diagrams, critical speeds, and node points,
• Experienced in analysis topics like multi-body dynamics and fluid-structure interaction,
• Proficient in finite element analysis software, particularly in thermal, static, modal, and harmonic modules.
• We are looking for a "Turbofan Analysis, Simulation, and Modeling Engineer" to join our team with these qualifications.

JOB DESCRIPTION

• Considering project dynamics, the following assignments will be made:
• Conducting overspeed, over-temperature, and burst analyses of fan and compressor rotor stages in turbofan engines in compliance with engine regulations,
• Performing structural strength analyses of engine structures in case of fan blade detachment,
• Examining the behavior of rotating components under thermal and mechanical loads and determining tip clearances under operating conditions,
• Identifying critical loading conditions and requirements of turbofan engine components considering high maneuverability of the aircraft,
• Modeling high-speed aviation bearings, determining speed-dependent stiffness and damping coefficients, performing macro and micro modifications, and calculating lifespan based on aircraft mission profiles,
• Conducting structural and thermal strength analyses of afterburner system components unique to turbofan engines,
• Performing thermal, fatigue, and creep analyses of turbine stator and rotor components under high temperatures and developing cooling designs accordingly,
• Conducting rotor dynamic analyses of nested shafts, examining their interactions, creating critical speed maps, and shifting critical speeds beyond operational ranges,
• Carrying out analysis of engine components in conceptual design processes of the developing turbofan architecture to guide detailed design efforts,
• Documenting all analysis, simulation, and modeling studies,
• Collaborating with design teams to develop and optimize engine components to meet system-level requirements and performance targets,
• Assisting in analysis and test correlation to validate system performance and identify areas for improvement,
• Contributing to strategies such as weight reduction, material changes, additional safety measures, and design modifications to identify potential risks in system design and operation, ensuring engine reliability and safety.