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ENERCON E-82 E4 - Safe Stopping Procedures

ENERCON E-82 E4
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6.5 Safe stopping of the wind energy converter
The ENERCON wind energy converter can be stopped by manual intervention or automatically by
the control system.
The causes are divided into groups by risk.
Wind energy converter stop during
Normal operationFault
Emergency stop,
rotor lock,
rotor brake
e.g. -2° limit switch,
vibration sensor,
grid failure,
overspeed,
pitch unit malfunction
e.g. load shedding,
data bus fault,
generator air gap,
bearing overtemperature,
capacitor fault
e.g. tower oscillations,
storm, lack of wind,
overtemperature,
grid fault
e.g. manual stopping,
shadow shutdown
Switching of
pitch motors to
capacitor boxes
Emergency pitching
into feathered position
and activation of
the rotor brake
Switching of
pitch motors to
capacitor boxes
Emergency pitching
into feathered position
Emergency
pitching
into feathered
position
Pitching to 60°
(idle mode)
Pitching into
feathered position
Fig. 5: Overview of stopping procedures
Stopping the wind energy converter by means of pitch control
In the event on a fault that is not safety-relevant, the WEC control system pitches the rotor blades
out of the wind, causing the rotor blades not to generate any lift and bringing the wind energy con‐
verter to a safe stop.
Emergency pitching
For emergency pitching, the pitch motors are supplied with power by the capacitor boxes. The rotor
blades move automatically and independently of each other into a position in which they do not
generate any lift; this is called the feathered position.
Since the three pitch units are interconnected but also operate independently of each other, if one
component fails, the remaining pitch units can still function and stop the rotor.
Emergency braking
If a person presses an emergency stop button, or if the rotor lock is used while the rotor is turning,
the control system initiates an emergency braking procedure.
This means that in addition to the emergency pitching of the rotor blades, the rotor brake is ap‐
plied. The rotor is decelerated from rated speed to a standstill within 10 to 15 seconds.
Control system
D0376616-2 / DA 17 of 21