APPLICATIONS

• Structure link parts
• Aircraft and rotorcraft rods
• Structure rods for satellites

CONCEPT

The proposed rods are tapped in extremities and without metallic inserts. Threads are obtained without any machining in one time.

This very original patented manufacturing mode allows to have particularly very light products. This process will be decline to composite nuts and swrew

EXEMPLE

• 30 kN Traction and Compression
• Lenght : 400 mm
• Diameter : 25 mm
• 2 x M8 at extremities
• Weight : 104 g