Dec 15, 2015
n
4a) Result trim run:Trial mass is removed:Result is calculated by rotating by 110°, multiplying mass by 5
Balancing result
Field balancing - Complete procedure
A
B
Let rotor disk roll freelyStatically balance mass if required
Initial unbalance run
4b) Result trim runTrial mass remains in place:Result is calculated by rotating by 110°, multiplying mass by 0.36
Rule :
Leave start field !
Optimal balancing result
n+1
n
n
4a) Result trim run:Trial mass is removed:Result is calculated by rotating by 110°, multiplying mass by 5
Balancing result
n.Check balancing result
D
C
B
A
Evaluation of overall vibra-tion according to ISO 10816Check whether balance grade has been reached, ISO 1940
Document results
G 2.5
2. When in doubt, check whether vibration caused by unbalance
f [Hz]
v[mm/s]
t [s]
max. value in spectrum > 50%
v[mm/s]
fn
D
C
B
A
1. Preparation for balancing
Overall vibration measurement according to ISO vRMS10...1000 Hz determine balancing direction and maximum valueevaluate according to ISO 10816Define levels, anglesEnter valuesDetermine causes
Balancing problems: overhung rotors
Allocation of measurement planes, standard caseWide rotor disks: static + dynamic unbalance
A B
B A
Direct drive: Use motor radiator fin as balancing plane B
B A
„Emergency balance“ for narrow impeller
A B
Special case: narrow impeller
Large couple unbalance, small static unbalance,possibly exchange A B
A B
BA
Aids for distributing and mounting masses
70°
55g
90°
0°180°
270°
70° mu
Only particular correction masses are available
Fixed angles for mounting( number of rotor blades )
Angle not ascertainable,
accessible externally only
nur außen zugänglich
Correction using fixed locations
90°
0°180°
N° 3 80° 36 g
N° 2 40° 13 g
9 blades
4
5
6
7
8
9
1
2
3
70°
Accelerometer A
Trigger sensor
Trigger mark
Measuring plane A
Measuring plane BBalancing plane B
Balancing plane A
Mounting angle
B
A
A
T
A
B
0°
Trigger angle A
Accelerometer B
Mounting angle, measuring & balancing planes