Reely SKY 23 26 60 Bedienungsanleitung Seite 22

Main rotor
Causes the lift, propulsion and lateral flight of the model in dependence of the blade angle of the rotor blades to the plane of rotation.
Tail boom
Fuselage arm to which the tail rotor is attached.
Tail rotor
The rotary motion of the main rotor causes the fuselage to rotate anticlockwise about the yaw axis.
The tail rotor, whose plane of rotation is perpendicular to the plane of rotation of the main rotor, works against this rotation
of the fuselage.
In addition, the rotation about the yaw axis can be induced with the tail rotor.
Inch
Unit of length in the USA and Great Britain. 1 inch = 25.4 mm
Nick
Rotary motion about the pitch axis; the pilot tilts the machine with the nose downward to induce propulsion.
Pitch
Collective adjustment of the blade angle of the rotary blades for more or less lift.
RC model
"Radio controlled," more precisely: "Remotely controlled" model, thus "radio-controlled" or "remote control" model.
Roll
Rotary motion about the longitudinal axis. Lateral tilting of the helicopter induces lateral flight.
Fins
Perpendicular fins on the tail boom (corresponding to the fin surface on the fixed wing model) stabilizes level flight.
Servo
Servo-motor that mechanically, by means of levers, carries out a control function.
Servo-lever (servo-arm)
Lever, disc or cross with 4 control levers that conveys the rotary motion of the servo-motor via adjustment levers to the steering (control
movements).
Flybar paddle
The flybar paddles are at the ends of the two paddle bars. These are in the plane of rotation of the main rotor, perpendicular right and left to the
longitudinal axis of the rotor blades, and stabilize the rotation.
Swashplate
The adjustable angle of the swashplate to the rotation axis of the main rotor causes a cyclical change of the setting
angle of the rotor blades.
Depending on where in the revolution the greatest blade angle of attack (highest lift) is reached, the helicopter flies
forwards, backwards or sideways.
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6. v
ol
1. c
OMMande
Conséquences des actionnements du manche de commande sur le vol
(données directionnelles envisagées dans la direction de vol)
Montée
Descente
Pivotement à gauche
(rotor arrière)
Pivotement à gauche
(rotor arrière)
Tangage : Vol avant
(descendre le nez)
Tangage vol arrière
(relever le nez)
Roulis gauche
Roulis droit
Manche de commande
droit vers l'avant
Manche de commande
droit vers l'arrière
Manche de commande
gauche vers la gauche
Manche de commande
gauche vers la droite
Manche de commande
gauche vers l'avant
Manche de commande
gauche vers l'arrière
Manche de commande
droit vers la gauche
Manche de commande
droit vers la droite
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