Tail Function; Gb B. Rc Functions Of The Helicopter; Technical Data - Carson SA315B Lama Betriebsanleitung

b. RC Functions of the Helicopter
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.
GB
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.
c. Technical Data
Principal rotor diameter
Length
Height
Weight
Battery charger „LiPo Balance"
Input:
Output:
32 CARSON Air Zermatt SA 315B „Lama" 50 050 7041
emote control
tral position.
del helicopter
e control takes
wards and back-
not spring
lly drawn
s
570 mm
860 mm
365 mm
1080 g
100 - 240 V/ AC, 50 - 60 Hz
0.4 A
R ll f Roll function i
(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.