Aircraft Stabilisation TRIZ Cases
- Flexible Drive Shaft Coupling for Aircraft Control Surfaces
A coupling assembly with rotatable balls connects a flexible drive shaft to an actuator assembly.
- Aircraft Elevator Fairing Design Minimizing Fuselage Gap
Design procedure shapes fairing to minimize gap with fuselage during elevator movement, reducing parasitic aerodynamic resistance.
- Flap Actuator Redundant Load Path Design
Segmented hydraulic architecture reduces line complexity while the roller clutch maintains flap position under aerodynamic forces.
- Aircraft Stabilizer Energy Attenuation via Adaptable Sections
Integrating an adaptable section into the stabilizer structure eliminates tail skids, reducing drag and weight while maintaining energy absorption capability.