Aircraft Navigation Control TRIZ Cases
- Turbojet Outlet Mixer Protrusions for Static Pressure Reduction
Guiding protrusions direct exchange airflow toward cold lobes, minimizing outlet static pressure and energy losses.
- Convertiplane Rotor Tilting Mechanism for Lift and Stability
Tilting rotors within semi-wing openings generate lift while reducing noise, resolving wing shielding effects during mode transitions.
- Aerospace Plane Wing Body Design with Retractable Intake Doors
Retractable engine intake doors seal off airflow when the engine shuts down, reducing drag and improving fuel efficiency.
- Aircraft Clutch Synchronization for Secondary Thrust
Clutch system synchronizes secondary thrust with powerplant via controlled engagement timing, preventing overheating during extended periods.
- Axially Stacked Motor Modules With Clutch for VTOL Propulsion
Clutch arrangements selectively couple axially stacked motor modules to a driveshaft, resolving reliability-complexity contradictions in VTOL propulsion.
- Temperature-Responsive Rocket Nozzle Throat Adaptation
A rocket nozzle throat adjusts diameter via temperature-responsive materials to maintain thrust efficiency during propellant depletion.
- VTOL Aircraft Thrust Augmentation via Segmented Ejectors
Segmented thrust augmentation systems distribute fluid streams across distributed thrusters to balance force vectors during vertical take-off and landing operations.
- Four-Axis Thrust Vectoring for Air Vehicle Attitude Stabilization
Segmented thrust generators adjust force magnitude and direction independently to counteract external disturbances and restore original position.
- HPVO Propulsion System with Differential Speed Fan for Stealth and Efficiency
A differential speed fan integrated into the aircraft hull reduces drag and noise while maintaining structural integrity.
- UAM Balance Control via Cloud Occupant Data
Cloud-connected balance control manages seat positions and motor power to resolve stability-complexity trade-offs in urban air mobility aircraft.