Projectiles TRIZ Cases
- Supersonic Projectile Stabilization Cone Design
Aerodynamic cone stabilizer with cylindrical bearing surface ensures supersonic projectile trajectory stability.
- Projectile Fins with Spiracles for Launch Pressure Relief
Spiracles in hinged fins vent trapped gases, preventing fin bending at the muzzle brake.
- Trimmable Tail Kit Rudder Drag Reduction
Dynamic trimmable rudders reduce drag from aggressive strakes by decoupling rotational control, extending effective range of gun-fired munitions.
- Guidance Unit Motor Shielding Against Launch Inertia
A guidance unit motor rotates within a rigidly attached bearing to shield internal components from inertial loads.
- Projectile Fin Deployment via Centrifugal and Aerodynamic Forces
Centrifugal and aerodynamic forces rotate rotatable fins from launch to flight position, eliminating springs or active drive elements.
- Articulated Missile Nosecone Actuation System
Nested concentric motors and bearings articulate the nosecone through a central aperture, preserving aerodynamic integrity while transmitting control signals.
- Rotatable Lock Mechanism for Missile Fin Shafts
A rotatable lock mechanism uses a solenoid actuator to translate rings and bearing balls, locking fin shafts with high stiffness.