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November 2018

66 \

World Cement

a holistic vision of the asset’s condition. Variables

have always been analysed in the past; however, with

vibrational analysis data included, the client can make

more informed decisions.

Case study 1: Increase gear mesh frequency

output shaft gear box findings

Goals

z

To identify the main factors in the increment of

gear mesh frequency (GMF) output shaft gearbox

and the transitions to the bull gear’s housing.

z

Show the correlation analysis between mechanical

and process variables.

Observations: unbalancing power – correlation analysis

z

The surge of 67X into the gear bull is caused by the

GMF output shaft gearbox.

z

The increase of value of this frequency in the bull

gear (both housings) is consistent with the increase

of GMF output shaft gearbox.

z

The frequency is transmitted through the shaft.

z

With these observations, it is important to now

look for a cause of the increase of GMF (Point 12)

output shaft gearbox.

Conclusion

z

Increase of GMF output shaft gearbox (Point 12): a

potential relationship was detected but it was not

possible to confirmm as its repetitiveness has not

been proven.

z

Correlation signals (pressure) system anti-cranking:

1

it was possible to identify areas of operation of the

system, but it was not possible to correlate it with

vibrational increases.

z

Operational information analysis: it becomes

necessary to have a greater number of key

operational variables available, besides knowing

details of the operation of auxiliary systems, in

this case of anti-cranking. At the moment, the

analyses are limited and inconclusive. SKF has

been able to see a high potential in predicting

events detrimental to the equipment and

production.

Case study 2: Determination of pre- and

post-failure phases by means of dependent

variables

Goals

z

Identify an early start point of the fault that has

already occurred.

z

Show the potential of the correlation analysis

between mechanical and process variables by

identifying early signs of failure.

Figure 9. Determination of the evolution of the fault

for sensor 14.

Figure 6. Identification of correlation zones.

Figure 7. Determination of correlation for both zones.

Figure 8. Vibrational register of fault on sensors 13 and 14.

Figure 5. The crossover of unbalanced power and high

GMF frequency values on sensor 12 (red spot).