Havacılık Projeleri

Aircraft Engine Blade System

This project introduces three key innovations in engine blade technology: a Staggered Axial Alignment where 32 blades are fixed along a 50 cm line on the shaft like a screw thread, 3 aerodynamic slits to optimize surface pressure, and a three-part segmented tip with a 2-degree angular difference to reduce vortices. This integrated architecture provides higher thrust at the same RPM, achieving maximum performance and fuel efficiency.

Helicopter Blade And Propeller System

This project is a next-generation helicopter technology built on five core innovations that enable flight without a traditional tail rotor. The system features 10 aerodynamic slots to double lift, a double-layered blade structure for increased capacity, double-forked tips for quiet efficiency, spiral geometry to eliminate vibration, and angular tilted positioning to trap high-pressure air under the blades. All maneuver and direction control is managed by an internal secondary blade mechanism at the rotor's center.

The Active Rotation Disk System (A.R.D.S.)

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