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Testing and quality

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Acceleration (g)<br />

40<br />

30<br />

20<br />

10<br />

0<br />

–10<br />

–20<br />

–30<br />

–40<br />

–50<br />

–60<br />

0 10 20 30 40<br />

Time (s)<br />

50 60 70<br />

2 Time traces of accelerometers showing implausible excursions in negative direction<br />

<strong>and</strong> clipping at –50 g.<br />

Signals of the accelerometer<br />

The accelerometer signals were not<br />

optimal either (see 2); they showed<br />

numerous implausible excursions in the<br />

negative direction <strong>and</strong> substantial<br />

clipping at approximately –50g. Nevertheless,<br />

in the frequency domain, the<br />

results obtained with the accelerometers<br />

were quite well defined compared with<br />

the results from strain gauges <strong>and</strong> were<br />

therefore used for further investigations.<br />

Resonance detection using<br />

spectrograms<br />

Spectrograms are a common method for<br />

displaying characteristics of transient<br />

vibration signals. Figure 3 shows an<br />

2500<br />

2000<br />

1500<br />

Frequency (Hz) 3000<br />

1000<br />

500<br />

Example 1: f = 1150 Hz<br />

(2-diameter mode,<br />

excitation by 23rd order)<br />

Example 2: f = 900 Hz<br />

(0-diameter mode,<br />

excitation by 21st order)<br />

example. The vibration levels are color<br />

coded <strong>and</strong> displayed as a function of<br />

time (= x-axis) <strong>and</strong> frequency (= y-axis).<br />

In the spectrogram of an accelerometer<br />

signal depicted in 3, the impeller natural<br />

frequencies are evident as horizontal,<br />

slightly fanned-out yellow-red shades<br />

(marked with red arrows in 3). The frequency<br />

b<strong>and</strong>width of the yellow-red<br />

shades is more than 100 Hz wide, indicating<br />

that the corresponding resonances<br />

feature considerable damping. A resonance<br />

with low damping would be<br />

evident by a rather narrow resonance<br />

b<strong>and</strong>width; no such feature crops up in<br />

the spectrogram of 3. Wherever the fanlike<br />

excitation frequencies of the rotor-<br />

0 10 20 30 40<br />

Time (s)<br />

50 60 70<br />

5-D<br />

3 Spectrogram of the accelerometer signal Acc1 (Ramp with decreasing speed; frequency<br />

b<strong>and</strong>s indicating resonances (yellow-red shades) marked by red arrows, resonances coinciding<br />

with a speed order line (circled in blue).<br />

4-D<br />

3-D<br />

2-D<br />

0-D<br />

1-D<br />

Deflection (–)<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

–0.2<br />

–0.4<br />

–0.6<br />

–0.8<br />

–1.0<br />

stator interaction coincide with a natural<br />

frequency of the impeller (see bluecircled<br />

lines), the corresponding resonance<br />

is excited. However, thanks to substantial<br />

damping, the amplification of<br />

the amplitude is not significant, <strong>and</strong> no<br />

fatigue damage is expected due to these<br />

resonances.<br />

Deflection shape identification<br />

It is well known that any given excitation<br />

order of the stationary components can<br />

excite only certain mode shapes of the<br />

impeller (Tanaka, 1990). Once the resonance<br />

frequencies of the impeller have<br />

been identified from the spectrogram,<br />

measured data <strong>and</strong> theoretically<br />

computed rotor vibrations can be<br />

matched in order to determine the corresponding<br />

mode shapes of the impeller.<br />

Following are two examples:<br />

• Example 1: Two-diameter mode at<br />

f=1150 Hz excited by the 23rd order:<br />

The frequency response function<br />

between two accelerometer signals is<br />

computed <strong>and</strong> averaged for the time<br />

segment in which a certain resonance<br />

mode is excited by the suitable excitation<br />

order. Then, the ratio of<br />

vibration amplitudes <strong>and</strong> the phase<br />

difference can be determined at the<br />

resonance frequency (f = 1150 Hz); at<br />

this frequency, the coherence should<br />

be reasonably good. The amplitude<br />

ratios <strong>and</strong> the relative phase at the<br />

measurement points are then animated<br />

synchronously with the theoretical<br />

vibration mode shape, the amplitude<br />

<strong>and</strong> phase of which are manually<br />

adapted to match the measured data.<br />

Using this methodology, it was<br />

TESTING AND QUALITY<br />

0 50 100 150 200 250 300 350<br />

Wheel circumference (º)<br />

4 Instantaneous deflection of mode shape with two nodal diameters.<br />

Red: measured vibration signals; blue: theoretical mode shape.<br />

Sulzer Technical Review 1/2011 |<br />

15

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