Carson Electric dual-rotor helicopter RtF (500507041) 500507041 데이터 시트

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500507041
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32
GB
CARSON Air Zermatt SA 315B „Lama“ 50 050 7041
b. RC Functions of the Helicopter
c. Technical Data
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 back-
wards 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 opposed 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. In 
order for the model to be able to rotate around the vertical axis (rotor 
shaft), the rotors must run at slightly different speeds. The resulting 
torque introduces the rotation. 
At less speed of the steering rotor compared to the bearing rotor, the 
torque of the bearing rotor is greater, the helicopter turns around the 
vertical axis in the direction of rotation of the steering rotor. At higher 
speed of the steering rotor, the torque of the bearing rotor is less than 
that of the steering rotor and the helicopter turns in the direction of 
the bearing rotor.
The tail function is controlled with the right control lever. If the lever is 
moved to the left, the tip of the fuselage turns to the left. If you move 
the lever to the right, the tip of the fuselage likewise turns to the right.
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. The lower rotor rotation tips slightly downwards and 
the model tilts around the transverse axis. 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.
Principal rotor diameter 
570 mm
Length 860 
mm
Height 365 
mm
Weight  
1080 g
Battery charger „LiPo Balance“
Input:  
100 - 240 V/ AC, 50 - 60 Hz
Output:  
7.4 V und 11.1 V/ 0.8 A
emote control
tral position.
del helicopter 
e control takes 
wards and back-
not spring 
lly drawn 
R ll f
i
Trans
verse
 axis
(Nick
)
Ve
rt
ic
a
l a
xi
s
(T
a
il
)
Hori
zont
al 
axis (
Roll)