Wings TRIZ Cases
- Variable Porosity Aircraft Surface for Drag Reduction
Actuator-driven sliding layers adjust pore alignment to mitigate transonic shock and reduce cruise drag across varying flight regimes.
- Aircraft Fuel Tank Access Cover Panel Sealing Design
Segmented inner and outer cover plates with floating nut plates prevent fuel leakage while allowing easy disassembly for maintenance.
- Integrally Stiffened Panel Inverted Pocket Joint Buckling
Inverted pocket geometry at stiffener intersections prevents buckling deformation without adding structural reinforcement weight.
- Aircraft High-Lift Flap Fairing with Integrated Flow Control
Integrated fairing channels air from pressure side to suction side, preventing flow separation during slow flight without adding complex external mechanisms.
- Wing Detachment Assembly Manual Release Mechanism
A wing detachment assembly uses a press-fitting member to drive a fastening member away from a mounting groove for quick manual release.
- Aircraft Floor Sandwich Panel with Integrated Reinforcing Structures
Honeycomb sandwich panels integrate reinforcing structures into core recesses, enabling direct module attachment without altering floor frame geometry.
- Composite Multispar Torsion Box Integration
A composite multispar torsion box structure uses integrated U and C shaped elements to form a single unitary assembly.