The primary objective of this project is the utilization of gear mechanisms within a power transmission system designed to actuate aircraft control surfaces. As the system lacks redundancy, the design process will strongly prioritize weight reduction, cost-effectiveness, and structural simplicity.

Within the scope of the project, the objective is to achieve the necessary torque conversion via gear sets, ensuring that the motion from the actuator is transmitted to the control surfaces with maximum precision and high mechanical efficiency. Prospective candidates involved in this project will design a highly functional and compact mechanism within the framework of domestic technology production, and will execute the initial prototype production of the developed system utilizing a 3D printer.

Criteria and Expectations

• A strong interest in designing lightweight power transmission systems (within a maximum limit of 3 kg) that exhibit high mechanical efficiency (90% and above).
• High motivation for continuous self-development regarding manufacturing methods, material selection, Finite Element Analysis (FEA), and fatigue analysis specific to gear mechanisms.
• The capability to work towards system design objectives that ensure minimum backlash and maximum precision (±0.5 degree angular tolerance).
• The ability to select materials and systems suitable for severe environmental conditions (temperature ranges from -40°C to +60°C, dust and moisture protection compliant with IP67 standards, and corrosion resistance in saline environments).
• Demonstrated aptitude for learning and effectively utilizing specialized design and analysis software such as Romax and KISSsoft.

Relevant Academic Departments

• Mechanical Engineering
• Aeronautical Engineering
• Aerospace Engineering
• Mechatronics Engineering