|
Number of Motor Poles |
Synch |
Induction |
Synch |
Induction |
|
|
50 hz |
50 hz |
60 hz |
60 hz |
|
4 |
1500 |
1475 |
1800 |
1775 |
|
6 |
1000 |
985 |
1200 |
1185 |
|
8 |
750 |
740 |
900 |
885 |
|
10 |
600 |
590 |
720 |
710 |
|
12 |
500 |
492 |
600 |
590 |
|
14 |
428 |
422 |
514 |
506 |
Quotation:
Start up torque curve (at highest suction pressure) with estimated bypass line pressure losses
Full horsepower torque effort curve
Part load torque effort curves (highest power of each single acting step)
+10% of max horsepower for nameplate power (may be inclusive of service factor)
Shaft diameter to be no less than compressor shaft diameter (keyless shaft)
Purchase (confirming quotation data):
*Start up torque curve (at highest suction pressure) with actual bypass line pressure losses
Full horsepower torque effort curve
Part load torque effort curves (highest power of each single acting step)
+10% of max horsepower for nameplate power (may be inclusive of service factor)
Shaft diameter to be no less than compressor shaft diameter (keyless shaft)
Studies necessary:
Motor start up analysis - Does the motor have enough torque to reach full speed fast (before the high inrush current overheats the motor)
This is done by the motor supplier and requires the compressor inertia value from the start up curve or mass elastic data, the coupling inertia, inertia from any added flywheel or crankshaft detuner
Current pulsation analysis (66% or less for induction motors, per NEMA MG-1) (by motor supplier)
Torsional analysis
Lateral analysis may be necessary depending upon lengths
Data necessary for Torsional from Motor Supplier:
Mass elastic data (inertia and shaft stiffness)
Shaft detail drawing for vibratory stress calculations
Minimum additional inertia (flywheel) to limit current pulsations (66% or less)
*Generating Final Start Up Torque Curve:
Run start up curve at highest suction pressure (or settle out pressure) and default pressure loss settings of 25 psi times the number of stages
Load cylinders if manual capacity devices are used, and unload cylinders if pneumatic capacity devices are used (suction valve unloaders and pneumatic pockets)
Apply the "flow at startup" value from the start up torque data to size the bypass line
Calculate the bypass line pressure drop at the "flow at startup" (from final stage cylinder discharge flange through vessels, coolers, bypass line, bypass valve, suction scrubber, suction vessel to first stage cylinder suction flange)
Provide the final flywheel inertia from the torsional analysis and current pulsation analysis for the final start up torque calculation
Rerun the start up curve with the calculated bypass line losses
Start up torque is used to determine if an engine starter, or electric motor driver has enough torque to start a compressor. Refer to Starting Torque topic for more specific information on starting torque curves and data.
Ariel
Corporation Application Manual
11 November 2011