Aircraft Navigation Control TRIZ Cases

Fluid jet propulsion replaces mechanical actuators to reduce power consumption during orbital changes.

Pivotable panels on an omnidirectional thrust mechanism redirect compressed gas to generate multi-directional forces.

Segmenting a single central airflow into multiple jet streams via lateral guiding outlets reduces vehicle weight while maintaining flight stability.

Strategic flow channels modify shock formations and separation regions, eliminating vibration and buffet on transonic aerospace vehicles.

Segmented pivotable vanes in the divergent nozzle section redirect exhaust flow for enhanced aircraft maneuverability while reducing system complexity.

Radial protrusion on the rotation shaft guides combustion gases away from the gas seal member to reduce direct thermal exposure.

An operating map guides air vehicles through low Reynolds number regimes by controlling angle of attack and speed.

Collapsible lift propellers reduce electrical power consumption and drag by dynamically adjusting blade orientation via torsion springs.

Dual-temperature planar jets direct airflow over a wing to generate vertical lift for low thrust-to-weight ratio aircraft.

Segmented rectangular nacelles with rotatable inlet slats and exhaust flaps resolve drag and yawing moment trade-offs while reducing air turbulence.

A hybrid air transport vehicle integrates side rotors and a rear rotor with a retractable fixed wing to enable autonomous vertical takeoff and horizontal flight.

Segmented access doors open in opposite directions to bypass rotor assemblies, resolving vehicle size versus loading access trade-offs.

Aircraft use swiveling jet engines to generate pitch and yaw torques via thrust vectoring.