The structure of military UAV meets GB/T 19520.12-2009 standard and relevant military standards, adapted to airborne, ship-borne, vehicular and ground station environments.
The military UAV accessory structure meets GB/T 19520.12-2009 standard and relevant military standards, and adapts to the environmental requirements of airborne, ship-borne, vehicular and ground station room. High structural rigidity and lightweight were the key design requirements.
PROTOTYPE PRODUCTION
The complex geometry of the UAV chassis required 5-axis simultaneous machining to achieve the required tolerances in a single setup. This minimized fixturing error and maintained the tight dimensional relationships between mounting interfaces.
Titanium alloy inserts were integrated into the aluminum chassis at high-stress points. The combined assembly provides a high strength-to-weight ratio meeting military shock and vibration specifications.
