Aircraft Stabilisation TRIZ Cases
- Tapered Mounting Assembly for Torsional Load and Bolt Fatigue
A tapered socket, boss, and interlocking features replace close-fit sanding and fatigue-prone bolts while reacting bending, torsional, and axial loads.
- Laser Rangefinder Flight Control Rigging for Precise Alignment
Laser rangefinders replace visual rigging checks to align aircraft control surfaces more accurately while reducing fall and moving-surface hazards.
- UAV Propeller Tilting for Position Movement Without Pitching
Tilting propeller shafts and a flywheel stabilizer let a UAV move laterally without pitching, improving docking accuracy and image quality.
- Double-Wall Aircraft Leading Edge for Lightweight Flow Control
An integrated double-wall leading edge uses molded stiffeners, micro pores, and plenum openings to cut HLFC weight and assembly complexity.
- THSA Upper Attachment With Dynamic Recess to Eliminate Backlash
A biasing mechanism lets the THSA tie-bar recess stay clear in normal use, then close under axial load to stop backlash and flutter.
- Takeoff Trim Using Stabilizer-Elevator Pitch Moment Split
Combining stabilizer and elevator trim shares tail pitching moment, cuts stabilizer travel, and lowers uncontrollable pitch risk at takeoff.
- Aircraft Elevator Authority Limits for Horizontal Tail Load Relief
Dynamic elevator limits based on stabilizer angle, Mach, and airspeed reduce horizontal tail loads without sacrificing pitch control.