ARMD™ 5.7
Module Description of ROTLAT™ (Rotor Dynamics)
One of the main ARMD modules is ROTLAT, which is a finite
element based software for performing damped and undamped critical
speeds, mode shapes, stability, unbalance response, and time-transient
response.
ROTLAT's modeling capabilities include:
- solid, hollow, tapered, and stepped type elements
- cylindrical, conical, tilting-pad, and rolling element type bearings
- gravitational loading
- bearing elevation
- gyroscopic effects
- flexible coupling, casing, foundation flexibility
- material damping in the shaft and foundation


ROTLAT consists of four sub-modules (ROSTAB, ROTORMAP,
ROSYNC, RORESP) integrated by ROTLAT's module messenger.
The messenger controls the sub-modules to provide a complete lateral vibration
analysis environment.
The four sub-modules are embedded in the rotor dynamics environment in order to
solve different problems. Look through the following examples; you are certainly
convinced of the powerful simulation technology. If you use the Internet Explorer 6.0,
you should check the image set-up to ensure the correct resolution for
the enlarged images (Help).
ROTLAT analyses results include:
1. Stability Analysis (ROSTAB + ROTORMAP)
natural frequencies and mode shapes
growth factors / damping ratios
rotor orbit directions
bearing reaction forces
shaft weight, deflection, and centerline slope
stability map and critical speed map (ROTORMAP)
2. Unbalance Response Analysis (ROSYNC)
(synchronous response)
multiple unbalance forces
magnitude and phase
dynamic forces and moments
vibratory amplitudes and orbits
forces and moments transmitted to bearings and
foundation
foundation vibratory amplitudes
3. Time-Transient Response Analysis (RORESP)
(non-synchronous response)
gravitational and external force:
sinusoidal, step, ramp, and pulse type
lateral amplitudes
rotor orbits
dynamic forces and moments
dynamic stresses


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