Propulsion and Fluid Systems Design Engineer

General Qualifications

• Graduated from universities' Departments of Mechanical, Aerospace, Automotive, Aviation, or Space Engineering,
• Preferably holding a master's degree in these fields,
• Proficient in engineering disciplines such as statics, dynamics, strength of materials, materials science, thermodynamics, heat transfer, and fluid mechanics,
• Experienced in the design of aviation engines and subsystems,
• Experienced in the design of hydraulic and pneumatic systems,
• Knowledgeable about aviation standards, product qualification, and certification processes,
• Proficient in at least one CAD modeling software (preferably Catia),
• Capable of designing systems and subsystems based on requirements,
• Knowledgeable in geometric dimensioning and tolerancing,
• Able to use applied engineering tools and systems,
• Familiar with literature review processes and capable of conducting detailed literature research,
• Strong problem-solving skills,
• Adequate technical English proficiency,
• Good command of MS Office applications,
• Open to innovation and continuously eager to improve oneself,
• Good communication skills and able to work collaboratively in a team,
• Able to adapt to a high work pace and flexible working hours,
• Able to coordinate and collaborate with other teams related to their areas of responsibility.
   

Job Description

Considering project dynamics and active division of labor requirements, the following assignments will be carried out:

• Extracting system requirements compliant with aviation standards,
• Creating and reporting system architectures,
• Designing hydraulic and pneumatic systems (fuel, air, oil, etc.) and their components,
• Selecting components for hydraulic and pneumatic systems and determining suitable requirements for them,
• Defining necessary subsystem requirements for engine integration into the aircraft (cooling system, exhaust, engine mounts, air intakes, etc.),
• Designing parts required for subsystems and engine integration,
• Designing and testing the engine exhaust system considering thermal variables,
• Identifying propeller and related subsystems and conducting design work for integration,
• Performing lifespan calculations for products,
• Ensuring verification of system products through testing, analysis, and simulation methods,
• Providing support in integration, technical documentation, manufacturing processes, and product lifecycle stages.