Wing Adjustments TRIZ Cases
- Closed Wing Aircraft Structural Bracing via Fuselage Interconnections
A closed wing aircraft configuration uses structural interconnections between multiple wings to enhance stiffness and aerodynamic performance.
- Variable Incidence Wing Aircraft Stowage Mode
A variable incidence wing aircraft pivots its assembly between perpendicular and parallel orientations to enable compact stowage.
- Aircraft Stowable Wing Assembly with Offset Driveshaft
Offset driveshaft misaligns gearbox during rotation cycle, enabling compact aircraft storage without complex alignment controls.
- Morphing Wing Segmented Feathers for UAV Adaptability
Segmented feathers and pivots adjust sweep angles, reducing complexity while maintaining adaptability.
- Variable-Shape Aerodynamic Fairing for Aircraft Flap Actuator
Telescopic modules retract during takeoff to avoid engine blast vibrations, then extend for optimal cruise drag reduction.
- Active Suspension Aircraft Wing-to-Fuselage Joint
Segmented actuators adjust relative positions to suppress flutter and reduce fuselage deformation.
- Movable Fuselage for Aircraft Weight and Balance Management
A movable fuselage positioning mechanism shifts the aircraft center of gravity relative to the wing assembly.
- Vehicle Readiness Control via Actuator Orientation
A control system mechanically orients vehicle parts using actuators to secure the asset against environmental threats.
- Movable Wingtip Retracting Mechanism for Hangar Access
Roller assemblies translate wingtips into stowed positions under fixed wings, enabling hangar entry without compromising structural integrity.
- Polymer Foam Adaptive Actuator for Wing Shape Adjustment
A polymer foam adaptive actuator adjusts wing shape and size to optimize aerodynamic properties.
- Aircraft Wing Camber Adjustment via Coupled Droop Panel and Flap
A camber adjustment system pivots a droop panel through an arcuate track coupler linked to the flap.