10
GB
CARSON UL-Copter C35 50 050 7029
The following functions are controlled
with the two remote control levers of
the portable transmitter.
For every control function there is a trim slider on the
remote control transmitter which permits minor
corrections of the neutral position.
Pitch function
(ascend / descend)
The pitch function controls the flying height of this model
helicopter over a common variation in speed of the two
rotors. The control takes place with the left control lever.
To do this, move it forwards and backwards in a
continuously variable fashion. Contrary to the other control
functions this lever does not spring back into the middle
position. If the control lever is totally drawn towards the back,
then the motors are off and the rotors stand still. If the control
lever is pushed forward then the motor starts running and the
rotors run with increasing speed depending on the lever
position.
In the middle position of the control lever, the helicopter should
hover at a fixed height.
Tail function
(Rudder function)
The tail function causes a rotation of the model around the
vertical axis. Since the helicopter has two rotors, no torque
ensues around the vertical axis at the same speed of the rotors
(rotor shaft). The helicopter also therefore requires no tail rotor
for stabilization.
Roll function
(Aileron function)
The roll function causes the lateral flight of the helicopter.
The control takes place with the right control lever.
If the lever is moved to the left, then the model hovers laterally
to the left. Moving the lever to the right makes the model move
laterally to the right.
Nick function
(Elevator function)
The nick function causes forwards and backwards flight of the
helicopter. When the nose drops downwards, a part of the lift is
transferred into forwards thrust.
If conversely the nose is raised, then the model flies backward.
the control takes place with the right control lever.
Press the lever forward to introduce forwards flight, pull back to
have the model fly backwards.
b. RC Functions of the Helicopter
c. Technical Data
Principal rotor diameter
2 x 350 mm
Length 420
mm
Height 160
mm
Weight
260 g
Battery charger „Lipo Balance“
Input:
100-240 V/ AC, 50-60 Hz
Output:
7.4 V und 11.1 V/ 0.3 A – 1.2 A
Horizontal axis
(Roll)
V
ertical axis
(T
ail)
Transverse
axis (Nick)
Содержание UL-COPTER C35 RTF
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