Rotational Systems Design Engineer

 General Qualities

• Graduated from Mechanical Engineering, Aircraft and Space Engineering, Aeronautical and Space Engineering departments of universities with at least a bachelor's degree,
• Strong theoretical background in Machine Dynamics, Mechanical Vibrations and Strength,
• Experienced in 3D modeling (preferably CATIA V5) programs,
• Predominant in finite elements software,
• Experienced in structural and life cycle analysis,
• Advanced level of technical English,
• In knowledge of aerospace and military standards (competence in industrial standards for rotor dynamics such as API Standards, knowledge of standard procedures and acceptance criterias),
• Capable of using MS Office programs,
• To be able of reporting and making written and oral presentations of the researches and the methods that he/she had developed,
• Prone to teamwork and has strong communication skills,
• Men must be free from the military service for at least 2 years, 

We are looking for a ‘’ Rotational Systems Design Engineer'' with the qualifications above.

 

Preffered Qualifications

• Master's or PhD degree in Mechanical, Aeronautical, Aerospace engineering departments of universities,
• Worked on advanced mechanical design, elasticity, advanced mechanical vibrations and finite element analysis
• Strong theoretical background in dynamics of rotating machines, simulation of bearing characteristics, design of rotor bearing systems and vibration analysis,
• Applied experience in rotational systems; in knowledge and experience of dinamical tests including bearing design and modelling, weight balancing, designing measurments with performing them, and analyzing test results,
• Know/uses a software program for the design, analysis and optimization of rotational systems ( shaft, gear, etc. ) in aircraft,
• In knowledge of geometrical dimensioning and tolerancing according to international standards.

Job Description

Considering the project dynamics, the following assignments will be made;

• Designing rotor-bearing systems in compliance with the technical requirements of the project and taking over system and subsystem design responsibilities,
• Determinating the bearing locations, critical speeds (Campbell diagram) and vibration calculations-analyses in the moving mechanisms of the aircraft.
• Designing shafts; performing statical, dynamical and life calculations and analysis,
• Deciding on the most appropriate design solution by evaluating the materials and manufacturing methods,
• Making the necessary technical documentation.