Miettinen Paper on AE

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    Miettinen, J., Pataniitty, P. Acoustic Emission in Monitoring Extremely Slowly Rotating Rolling

    Bearing. In: Proceedings of COMADEM 99. Oxford, Coxmoor Publishing Company. 1999. ISBN1-901892-13-1. pp. 289-297.

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    Acoustic Emission in Monitoring Extremely

    Slowly Rotating Rolling Bearing

    Juha Miettinen*and Pentti Pataniitty

    **

    *

    Tampere University of Technology, Machine DesignP.O. Box 589, SF-33101 Tampere, Finland

    email: [email protected]**

    Acutest Oy, Hermiankatu 8 D

    SF-33720 Tampere, Finland

    email: [email protected]

    Abstract: There are not international standards or universally accepted limit values available, that classify

    rotating machines as slow or high speed machines. The old international standard ISO 2372, which has been

    replaced with the new ISO 10816 standard, gave the vibration velocity severity ranges for different classes

    of machines. The old standard covered machines with rotational speeds from 600 rpm to 12000 rpm. Thenew standard does not contain any rotational speed limits. Sometimes the limit for low-speed rotating

    machines is set to 20 rpm or 30 rpm. In industry, it is easy to find machinery where the rotational speed in

    continuous running is lower than 2 rpm.

    In the condition monitoring of rotating machines, it is common practice to measure the vibration velocity or

    acceleration. At very low frequency, the vibration velocity amplitude becomes weak and therefore

    displacement measurement can sometimes be a suitable vibration measurement parameter. When the rolling

    element in the rolling bearing passes the early-stage fault in the case of an extremely low rotational speed,

    the energy that the collision generates is very low. In that case, the defect is difficult to detect in the

    frequency domain but can possibly be seen in the time domain.

    The frequency bandwidth of acoustic emission (AE) measurement method is typically in the range 100 kHz

    to 1 MHz. In that range, vibrations occur in a material by fracture of crystallites, crack nucleation and

    growth, several mechanisms involving dislocations, phase transformations in materials, boiling and

    electrical discharges. Each of these mechanisms is characterised by a rapid collective motion of a group of

    atoms.

    The present paper describes the use of the acoustic emission method in the monitoring of faults in an

    extremely slowly rotating rolling bearing. The introduction describes the principle of the measurement

    method of acoustic emission and the analysis methods used for the acoustic emission signal. The paper

    contains the results of AE measurements where the rotational speed of the shaft was from 0.5 rpm to 5 rpm.

    The measurements were carried out using a laboratory test rig with grease lubricated spherical roller

    bearings of an inner diameter of 130 mm and a load of 70 kN. Prior to testing the test bearing had beennaturally damaged on its outer race during normal use in industry. The results of the acoustic emission

    measurement have been compared with the results of low-frequency vibration measurements, which have

    been carried out in the same test arrangement. The paper gives an example where acoustic emission

    measurements have been used in industry, in the monitoring of slowly rotating machinery.

    Keywords: acoustic emission, vibration measurement, slowly rotating bearings

    1. Introduction

    Acoustic emission can be described as a shock wave inside a material, which is under stress. The shock

    wave causes the surface of the material to move, and this movement is measured with a very sensitive

    sensor. The shock, or transient elastic wave, is generated by a rapid release of energy from a local source

    within the material. The sources of acoustic emission (AE) comprise different mechanisms of deformation

    and fracture including the fracture of crystallites, crack nucleation and growth, several mechanisms

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    involving dislocations, phase transformations in materials, boiling and electrical discharges. Each of these

    mechanisms is characterised by a rapid collective motion of a group of atoms (Beattie, 1983). The intensity

    of acoustic emission vibration, often called AE activity, depends on the type of material and on the

    properties of the material. In Table 1 (Miller, 1987), some factors that affect the relative amplitude of the

    acoustic emission response are presented.

    Table 1. Factors that affect the relative amplitude of the acoustic emission response (Miller, 1987).Factors that tend to increase the acoustic emission

    response amplitude

    Factors that tend to decrease the acoustic emission

    response amplitude

    High strength

    High strain rate

    Low temperature

    Anisotropy

    Nonhomogeneity

    Thick sections

    Brittle failure

    (cleavage)

    Material containing

    discontinuities

    Martensite phase

    transformations

    Crack propagation

    Cast materials

    Large grain size

    Mechanically induced

    twinning

    Low strength

    Low strain rate

    High temperature

    Isotropy

    Homogeneity

    Thin sections

    Ductile failure

    (shear)

    Material without

    discontinuities

    Diffusion-controlled

    phase transformations

    Plastic deformations

    Wrought materials

    Small grain size

    Thermally induced

    twinning

    A particular feature, which affects the activity of the acoustic emission, is called the Kaiser effect. The

    Kaiser effect means that when a defined stress has been applied on the material and it has caused acoustic

    emission, additional emission will not be induced in to the material until defined level of stress has been

    exceeded, even if the load is completely removed and then reapplied (Miller, 1987). Because of the Kaiser

    effect, each AE wave can occur only once. The Kaisen phenomenon has a special effect on the crack

    nucleation and growth. It can also affect the AE activity caused by a fault in a bearing when a rolling

    element is passing the fault and causes stress in the material.

    In order to evaluate the significance of an AE source and to interpret the AE signal, different parameters can

    be extracted from the signal. The signal waveform depends on the characteristics of the source, on the pathof the signal from the source to the sensor, on the characteristics of the sensor and on the measurement

    system. The parameters, which will be extracted from the signal, are depending on the type of the signal.

    From a burst type of signal, typical extracted parameters are the duration time of the AE event, the emission

    counts, the emission event energy, the emission signal amplitude and the peak amplitude, the emission

    signal rise time or the signal decay time, see Fig. 1.

    Fig. 1. An AE burst signal and the characteristic parameters of the signal.

    If the examined AE signal is longer and contains a lot of emission bursts like the signal shown in Figure 2,

    one way to characterise the signal is to calculate statistical values from the time signal. These values express

    if the signal is peaked or not. Typical statistical values are the standard deviation of the signal, the kurtosisvalue of the signal, the variance value of the signal, the skewness value of the signal, the signal peak-to-peak

    value and the acoustic emission signal root mean square (RMS) value that describes the signal energy

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    content (Li, 1995). One way to characterise the signal is to count the pulses per time unit; for example

    pulses/second. This way to monitor the signal is very suitable for continuous measurement because the data,

    which is stored, contains only a fractional part of the amount of the data that is stored if the AE time signal

    is measured. The pulse count data is easier to handle in the industrial environment. In some studies an AE

    time signal area summation technique has been used (Tan, 1990).

    Fig. 2. A long AE time signal, which contains a lot of emission bursts.

    2. Acoustic emission in the monitoring of faults of rolling bearings

    When the rolling element passes the fault in a bearing, it excites vibration, which can be measured by avibration measurement sensor. The common practice is to measure the vibration displacement, velocity or

    acceleration. The velocity amplitude is almost independent from the vibration frequency in the range 10 Hz -

    2 kHz. The vibration velocity describes very well the general condition of the rotating machine. For that

    reason, vibration velocity measurement is the most common measurement parameter in condition monitoring

    of rotating machinery. At higher frequencies, the vibration displacement amplitude becomes very low but

    the vibration acceleration rises to a high level. For machines rotating at high speed with a rolling bearing

    failure at a very early stage, the measurement of the vibration acceleration is usually a more reliable

    indicator (Berry, 1991).

    The type of the spectrum, which the defective rolling bearing generates, depends on the severity of the fault.

    We can find out basically four types of spectrums. These spectrums can contain random ultrasonicfrequencies, natural frequencies of bearing components, bearing rotational defect frequencies and sum and

    difference frequencies which are born when the different frequencies modulate with each other (Berry,

    1991). Random ultrasonic frequencies appear typically at an early stage of the fault, and can dramatically

    rise just before the seizure of the bearing. The natural frequencies of the mounted bearing are utilised when

    vibration acceleration is measured using enveloping techniques.

    The main difference between the acoustic emission and the low frequency vibration is that for low

    frequency vibration we already need a defect in the bearing which excites the vibration when a rolling

    element is passing it but acoustic emission vibration is exited just when the crack is formed. Therefore, in

    principle, the acoustic emission should indicate damage in the bearing at a very early stage. In practice, the

    situation of course is not so clear. When the rolling bearing is running, the lubrication situation is not always

    fully flooded but very often the bearing is running under some degree of starved condition. Starvedlubricated situation means metallic contacts, micro fractures, and micro plastic deformations, which all can

    generate acoustic emission.

    2.1 Technique to measure acoustic emission

    The substantial difference in the AE measurement technique, compared with the low frequency

    measurement techniques, is in mounting the measurement sensor. Acoustic emission monitoring is

    nondirectional. Most AE sources appear to act as point sources. The point sources radiate energy in

    spherical wavefronts, and therefore the sensor can be located anywhere in the vicinity of the AE source and

    it can detect the acoustic emission signal. This is in contrast to other measurement methods of mechanical

    vibration, in which the direction of the sensor has a strong influence. The vibration measurement sensors arevery insensitive in other directions than the measurement direction so as result we get the vibration in the

    direction of the measurement axle of the sensor.

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    Although the AE measurement is nondirectional, it must be taken into consideration that every boundary

    surface affects damping on the high frequency vibration signal. Therefore, the sensor should be located as

    close as possible to the expected emission source, normally on the load side of the bearing. In addition, it is

    very important to use a contact grease between the sensor and the fitting surface.

    Because the levels of the voltage in the acoustic emission measurement are very low, great care must be

    taken to minimise the affect of disturbances from the environment on the measurement. Strong electricaldisturbances can cause, for example, magnetic fields, eddy current fields, inverters of the electrical motors

    and fluorescent lamps. The so called background noise, which means the acoustic emission generated for

    example from pressure vessels, welding, hydraulic and mechanical noise, fretting and deformations by heat

    expansion, can disturb the AE measurements, especially in field environments. The disturbances can affect

    the measurement results, they can not always be easily explained. The disturbances are especially harmful,

    when the rotational speed of the bearing is low and when the emission level from the bearing is low

    (McFadden, 1984). The background noise can affect the AE measurement in that way, that even if the signal

    is very clear when the rotational speed is low the signal can become ambiguous when the rotational speed

    and the background noise is higher (Smith, 1982).

    The frequency bandwidth in acoustic emission measurement is typically in the range 100 kHz to 1 GHz. The

    sensors are generally of piezoelectric type. The difference between the normal accelerometer and the AEsensor is that AE sensor does not have any mass attached on the piezoelectric crystal. The frequency

    response of the AE sensor is strongly non-linear and therefore the measurement of the spectrum in the case

    of acoustic emission is not very suitable. In Figure 3 is a graph of a typical frequency response of an AE

    sensor presented (B&K, 1984). The normal way to do the measurement is to use a narrow band-pass filterwhich centre frequency is the same as the resonance frequency of the sensor.

    Fig. 3. A typical frequency response of an AE transducer (B&K type 8313).

    3. An example of the acoustic emission monitoring of slowly rotating rolling bearings in the

    paper industry

    The example is from a Finnish paper plant. The AE monitoring system is installed for monitoring the

    support bearings of the lime sludge reburning kiln, Fig. 4 a and Fig. 4 b. The kiln is supported with six

    bearing pairs, total number of the bearings being 12. The rotational speed of the kiln is 8 rpm. During 10

    years running there has happened over 16 bearing faults, which have caused unsystematical shutdowns and

    losses of production. The principle of the AE measurement in this case is continuos pulse count method. The

    AE sensors were of piezoelectric type and their sensitivity was highest at the frequency of about 150 kHz.

    The lower frequencies until 100 kHz are filtered out.

    After some time the measurement system was taken in to use the pulse count level from the bearing number

    8 started to rise from its normal level. That situation is shown in Fig. 5 a. After running of 20 days the pulse

    count level started to rise again very strongly which is shown in Fig. 5 b. The kiln was stopped according to

    the normal maintenance plan and the bearing was removed. That maintenance operation did not affect anycosts in the production. After the removal of the bearing the pulse count level dropped to a level about 100

    pulses/300s.

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    a) b)

    Fig. 4. The lime sludge reburning kiln (a) and the supporting bearing (b).

    a) b)

    Fig. 5. The AE pulse count level of the bearing number 8 starts to rise slowly (a) and after 20 days operation

    the level started to rise very strongly (b).

    4. The measurements in the laboratory

    The aim of the laboratory measurements was to test the acoustic emission measurement with extremely lowrotational speed of a rolling bearing. For the sake of comparison, some low frequency vibration

    measurement methods were included in the measurements. These methods were the envelope spectrum

    method, the peak value method, the method of derivation of the acceleration signal and the time signal of

    vibration acceleration.

    4.1 Measurement arrangement

    The measurements were carried out with a test rig, which is shown in Fig. 6. The type of the test bearings

    and the support bearings of the rig was two-row spherical roller bearing. The bearing application was the

    same as in a normal railway wagon. Every housing includes two bearings and one of the test bearings was

    damaged. The damage was followed from the normal use of the bearing and the damaged bearing was found

    in normal maintenance operation of the wagon bearings. The test bearing represents a typical faulted bearing

    in that usage. The load of the test bearings during the measurement was 70 kN per housing and it was static

    and pure radial. That load is the same as the maximum static load per one housing when the wagon is loaded

    full. The type of the grease in the test bearings was NLGI grade 1.5 lithium complex soap with synthetic

    base oil.

    The AE sensor was mounted on the bearing housing with a 150 mm long wave-guide, which was fitted with

    screw fastening. The AE sensor was of piezoelectric type and the signal was filtered with narrow band-pass

    filter which centre frequency was 150 kHz or 240 kHz. The methods for analyse of the AE signal were the

    pulse count method and the time signal of acoustic emission vibration. The pulses where counted in the unit

    of pulses/one second. From the time signal, the cycle time of the fault frequency of the bearing was defined

    when it was possible. The rotational speed in the measurements was from 0.5 rpm to 5 rpm. With lowfrequency measurement methods, the rotational speed was so low when the fault still could be detected.

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    Fig. 6. The test rig of the bearings in the laboratory.

    5. Results

    In the results are shown the AE pulse count and the AE time signal measurements when bearing rotational

    speed has been 0.5 rpm, 0.85 rpm, 1.4 rpm and 5 rpm. In the end of this chapter, also some results of the

    measurements of low frequency vibration are shown.

    In generally the fault was identified in all AE measurements. In some of the cases, the background noise

    appeared so strongly that it was difficult to find out the cycle time of the fault. In Fig. 7 are shown the

    results when rotational speed was 0.5 rpm. The fault cycle time can be identified very clearly from the time

    signal and from the pulse count results. The background noise with that a slow rotational speed is low

    comparing it for example between the results when the rotational speed was 0.85 rpm, which is shown in

    Fig. 8. Because of the low background noise, the fault cycle time can be identified more clearly from the AE

    time signal measurement when the rotational speed was 0.5 rpm than 0.85 rpm. The time of the pulse count

    measurement is much longer than the time of the AE time signal measurement. From the long-time pulse

    count results it is possible to find out time intervals where the cycle time of the fault can be easily identified

    despite of the background noise, which can be seen from Fig. 8.

    AE pulse count AE time signal

    Fig. 7. The AE pulse count and the AE time signal results with a rotational speed of 0.5 rpm.

    AE pulse count AE time signal

    Fig. 8. The AE pulse count and the AE time signal results with a rotational speed of 0.85 rpm.

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    In Fig. 9 the AE pulse count and time signal results when rotational speed was 1.4 rpm are presented. The

    background noise in these measurements was so high that it was a little bit difficult to find out the cycle time

    of the fault frequency from the AE time signal. The background noise disturbed also the pulse count

    measurement and therefore the cycle time could not be identified as well as in that case when the rotational

    seed was lower, which is shown in Fig. 7.

    AE pulse count AE time signal

    Fig. 9. The AE pulse count and the AE time signal results with a rotational speed of 1.4 rpm.

    In Fig. 10 the AE pulse count and time signal results when rotational speed was 5 rpm are presented. In thismeasurement, the emission from the fault is so strong that the background noise does not disturb the

    measurement. The cycle time of the fault frequency can be identified very clearly from the time signal. The

    AE pulse count was measured in the unit pulses/one second. When the cycle time of the fault frequency

    approaches the time interval of the pulse count measurement, the cycle time of the fault can not be anymore

    identified from the pulse count results. This is shown in Fig. 10. In the pulse count result the cycle time of

    the rotation of the shaft can be seen very clearly but the cycle time of the fault frequency can not be

    identified.

    AE pulse count AE time signal

    Fig. 10. The AE pulse count and the AE time signal results with a rotational speed of 5 rpm.

    The character of the AE emission depends for example on the size and on the shape of the fault on the

    rolling surface. In Fig. 11 is shown one AE pulse cluster, which has been taken from the result of the time

    signal measurement shown in Fig. 10. From the fault in the bearing, a pulse cluster is generated, which inthis case consists of eight short-duration AE bursts. This kind of pulse cluster has a different shape than for

    example the acceleration signal in the low frequency area generated from the same fault.

    Fig. 11. The AE pulse cluster from the fault in the bearing.

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    That is one difficulty in the pulse count technique or for example in the peak value technique in analyses of

    the AE signal. If the cycle time of the fault is short, it may be difficult to find out an adequate time interval

    for the measurement so that the different clusters will not be mixed together in the measurement. That

    makes it difficult to identify the passing frequency of the fault. One possibility in this case is to follow the

    AE pulse count overall level or the AE activity RMS value.

    5.1 Results of the low frequency measurement

    The same damaged bearing was measured also with the low frequency measurement methods. The methods,

    which were included in the measurements, were the envelope spectrum method, the peak value method, and

    the method of derivation of the acceleration signal and the pure time signal of acceleration. Some view of

    the suitability of the low frequency measurement methods in this case is shown in Fig. 12. In these

    measurements, the most sensitive low frequency measurement method was the envelope based spectrum

    measurement method. In Fig. 12 methods have been arranged based on the property of detecting the fault

    from the spectrum and from the time signal. The grades have been estimated. Envelope method was scored

    as a highest, because it could detect the fault in a lowest rotational speed. The limit of the rotational speed

    when the fault was detected was with envelope method 10 rpm and with the other methods 20 rpm.

    Fig. 12. The suitability of low frequency measurement methods to detect the fault in the bearing. The

    methods are arranged based on the property of detecting the fault from the spectrum and from the time

    signal. The grades have been estimated. Envelope method was scored as a highest, because it could detect

    the fault in a lowest rotational speed.

    Conclusions

    The acoustic emission measurement has been tested to detect the fault of a rolling bearing, which is rotating

    with extremely slowly rotational speed. The rotational speed in the measurements has been from 0.5 rpm to

    5 rpm.

    The study denoted that the acoustic emission measurement is a very sensitive method to detect the fault in abearing which is rotating with an extremely slowly rotational speed. With the AE method, the fault in the

    bearing could be identified with the slowest rotational speed, which was used in the measurements. With the

    lowest speed the fault was clearly identified from the AE time signal and from the results of the AE pulse

    count method.

    The voltage levels in the AE measurements are very low therefore, the influence of the external disturbances

    on the measurement must be taken in the consideration. The external disturbances can be caused by other

    emission sources than from the rotation of the bearing. In addition, the high rotational speed can cause

    background noise, which can make it difficult to identify the cycle time of the fault frequency.

    The pulse count method is convenient principle for monitoring the rolling bearing when the rotational speed

    is extremely slow. The measurement time in pulse count is long, very often continuous. From those long

    time measurement results, it is possible to find out time intervals of that kind from where the cycle time of

    the fault frequency can be clearly identified. The pulse count method has also the advantage that the size of

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    the measurement file stays reasonable. Instead, in the measurement of the AE time signal the data file can

    grow up so large that it is troublesome to process.

    When the rotational speed was higher, the cycle time of the bearing fault frequency could be identified best

    from AE time signal. With higher rotational speed, the collision of the rolling element on the fault creates so

    high emission energy that the background noise does not disturb the identification of the cycle time of the

    fault. The measurement time interval in the pulse count method is limiting its use in identifying the faultcycle time when the rotational speed is high. The character of the AE emission is depending for example on

    the size and on the shape of the fault on the rolling surface. When the rolling element passes the fault it

    builds up an emission burst cluster. In this case, it is difficult to choice the right time interval for pulse count

    method and it is possible that the different emission clusters are mixed together.

    The measurements were carried out also with low frequency measurement methods. The limit of the

    rotational speed when the fault still could be reliable identified with those methods was between 10 rpm and

    20 rpm.

    Acknowledgements

    This study is a part of the Finnish project Condition Monitoring of Grease Lubricated Rolling Bearings"which is included in the international COST 516 GRIT research programme. The authors are grateful for the

    financial and technical support from the following companies and institutions: The Technology

    Development Centre of Finland (Tekes), SKF Engineering & Research Centre B.V. in The Netherlands, the

    Finnish companies Mobil Oil oy ab, Rautaruukki Steel, VR Ltd., Acutest Oy and the Finnish Maintenance

    Society.

    References

    Beattie, A G (1983) Acoustic emission, principles and instrumentation. Journal of Acoustic Emission,

    Volume 2, Number 1/2, pp. 95-128.

    Berry, James E (1991) How to track rolling element bearing health with vibration signature analysis. Sound

    and Vibration, November, pp. 24-35.

    Brel & Kjr (B&K)(1984) Instruction Manual. Acoustic Emission Transducers and Preamplifiers. Revision

    March 1984. 17 p.

    Li, C James, Li, S Y (1995) Acoustic emission analysis for bearing condition monitoring. Wear 185, pp. 67-

    74.

    McFadden, P D, Smith, J D (1984) Acoustic emission transducers for the vibration monitoring of bearings at

    low speeds. Proceedings of the Institution of Mechanical Engineers, Part C, Vol 198 No 8, pp 127-130.

    Miller, R K, (Technical Editor), McIntire, P (Editor) (1987) Nondestructive Testing Handbook. Volume 5:

    Acoustic Emission Testing. American Society for Nondestructive Testing. 603 p. ISBN 0-931403-02-2.

    Smith, J D (1982) Vibration monitoring of bearings at low speeds. Tribology International, Volume 15,

    Number 3, June, pp. 139-144.

    Tan, C C (1990) Application of Acoustic Emission to the Detection of Bearing Failures. Proceeding of the

    Tribology Conference, Brisbane 3-5 December 1990. The Institution of Engineers Australia, pp. 110-114.

    Tandon, N and Nakra, B C (1990) Defect Detection in Rolling Element Bearings by Acoustic Emission

    Method. Journal of Acoustic Emission. Volume 9 Number 1, pp. 25-28.