The emergency
generator manufacturer was developing a new line of
mid-range (50 – 200 kW) emergency generators, powered by
automotive derivative engines running on natural gas rather
than diesel and operating at 3600 RPM rather than 1800 RPM.
The advantages are greatly reduced size and weight of
the generator set.
Reliability problems were encountered with
the prototype units. Bearing failures were occurring
too early and rotors were rubbing on the stators causing
catastrophic failures.
The manufacturer requested assistance in data
acquisition and analysis.
The generator manufacturer had already acquired data
indicating a rotor critical speed near 1.5X RPM.
The entire unit was mounted on rubber isolators.
The initial readings were taken on the
generator set with a full range of load conditions.
The outboard end of the generator generated the
highest vibration amplitudes in the vertical direction due
to 1X RPM sources and was not load dependent. The horizontal direction vibration was dominated at low loads
by 1X RPM vibration but was dominated by 1.5X RPM vibration
at high loads.
˝X RPM harmonics are characteristic of V6
reciprocating engines. The intensity of these pulses increases significantly with
load. This
coincides with the findings that the 1.5X RPM amplitude
increases significantly with load.
The rotor/stator contact was likely a result of
excessive rotor deformation when the rotor critical at 1.5X
RPM was excited by high load 1/2X RPM harmonics from the
engine. Also these pulses often excite torsional natural frequencies
of attached machinery.
To determine if torsional natural
frequencies were excited, a spectrum/sideband analysis was
performed on the signal generated from the 14 generator fan
blades as they passed a photo cell.
The high resolution spectrum is included along with
the “zoom” view of the data which clearly shows
sidebands spaced at 1.5X RPM (90 Hz). The sidebands are caused by torsional vibration of the rotor.
The
new rotor configuration was tested in February.
Results showed that the 1X RPM vibration on the
generator was significantly reduced in the vertical
direction as a result of the balancing.
The natural frequency of the rotor assembly was also
shifted away from the 1.5X RPM frequency sufficiently to
reduce the 1.5X RPM vibration amplitude significantly.
The rotor/stator contact problem was eliminated.