UniCopter ~ Vibration - Rotor Induced - Control
Overview:
Objective: To overcoming vibration, particularly rotor to rotor, by Direct Confrontation not by Accommodation.
Objective: By short duration increase in thrust (not: to increase the maximum lift coefficient)
Working Papers:
|
|
DESIGN: |
MAKE: |
|
BUY: |
|
Items:
DESIGN:
|
|
Name |
Item |
|
|
Higher Harmonic Control: |
|
|
|
UniCopter ~ Rotor - Disk - Lateral Dissymmetry of Lift |
|
|
|
UniCopter ~ Control - Flight - Swishring - Fixed Azimuth Overview |
|
|
|
UniCopter ~ Control - Flight - Swishring - Variable Azimuth Overview |
|
|
|
UniCopter ~ Control - Flight - Swishring - Split Harmonic Control |
|
|
|
UniCopter ~ Control - Flight - Swishring |
|
|
|
OTHER: Aerodynamics - Vibration - Rotor Induced - Higher Harmonic Control |
|
|
|
Individual Blade Control: |
|
|
|
UniCopter ~ Vibration - Rotor Induced - Control - Output - Boundary Layer Control |
|
|
|
UniCopter ~ Vibration - Rotor Induced - Control - Output - Lower Surface Flap(s) |
|
|
|
UniCopter ~ Vibration - Rotor Induced - Control - Closed-Loop Controller |
|
|
|
OTHER: Aerodynamics - Vibration - Rotor Induced - Individual Blade Control |
|
|
|
UniCopter ~ Vibration - Rotor Induced - Control - High Frequency Leading & Trailing Edge Flaps |
|
|
|
UniCopter ~ Vibration - Rotor Induced - Control - High Frequency Modifiable Tip Control |
|
|
|
Additional Means of Reducing Vibration: |
|
|
|
UniCopter ~ Pusher Prop - General - Pusher Prop Assist |
|
|
|
OTHER: Aerodynamics ~ Rotor Concept - Active Blade Twist [ABT] |
|
|
|
Short wings under hubs and/or extended and webbed rotor hubs |
|
Back to top | SynchroLite Home Page | UniCopter Home Page | Nemesis Home Page
Last Revised: January 28, 2007
