Claims
- 1. An ultralight coaxial rotor aircraft comprising
a frame, an engine, a coaxial rotor set tiltable with respect to the aircraft, at least one yaw paddle, a handlebar control, whereby pitch and roll control is by tilting the rotor set, and yaw control is by actuation of the yaw paddles.
Parent Case Info
[0001] This application claims priority of U.S. provisional application Serial No. 60/268,978, filed Feb. 14, 2001, which is hereby incorporated herein by reference for the teachings consistent herewith, and this disclosure shall control in case of any inconsistency.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60268978 |
Feb 2001 |
US |