An Introduction to AET Reading 2004-01

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    An Introduction to

    Acoustic Emission Testing, AET

    2014-JuneFacilitators: Fion Zhang/ Charliechong

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    http://wins-ndt.com/oil-chem/spherical-tanks/

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    http://www.smt.sandvik.com/en/search/?q=stress+corrosion+cracking

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    Speaker: Fion Zhang2014/6/13

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    Contents:

    1. AE Codes and Standards ASTM

    ASME V

    2. Reading 01,

    3. Reading 02,4. Reading 03,

    5. Others reading.

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    ASME V Article Numbers:

    Gen Article 1RT Article 2

    Nil Article 3

    UT Article 4 for welds

    UT Article 5 for materialsPT Article 6

    MT Article 7

    ET Article 8

    Visual Article 9

    LT Article 10

    AE Article 11 (FRP) /Article 12 (Metallic) / Article 13 (Continuous)

    Qualif. Article 14

    ACFM Article 15

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    ASTM Standards

    1. ASTM E 1930 Standard Practice for Examination of Liquid-FilledAtmospheric and Low-Pressure Metal Storage Tanks Using Acoustic

    Emission

    2. ASTM E 569 Standard Practice for Acoustic Emission Monitoring of

    Structures During Controlled Stimulation3. ASTM E 749-96 is a standard practice of AE monitoring of continuous

    welding

    4. ASTM F914 governs the procedures for examining insulated aerial

    personnel devices.

    5. ASTM E 1932 for the AE examination of small parts,

    6. ASTM E1419-00 for the method of examining seamless, gas-filled,

    pressure vessels.

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    Others Reading

    http://www.globalspec.com/reference/63985/203279/Chapter-10-Acoustic-Emission-Testing

    http://www.corrosionsource.com/(S(vf34kqncr0uklwzu0ioy5dz2))/FreeContent/3/Combatting+Liq

    uid+Metal+Attack+by+Mercury+in+Ethylene+and+Cryogenic+Gas+PlantsTask+1+-+Non-

    Destructive+Testing

    http://www.ndt.net/ndtaz/index.php?id=2

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    Typical AET Signal

    https://dspace.lib.cranfield.ac.uk/bitstream/1826/2196/1/Acoustic%20Emission%20Waveform%20Changes%202006.pdf

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    Typical AET Signal

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    Study Note 1:

    http://www.geocities.ws/raobpc/AET.html

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    What is AE

    Acoustic emission is the technical term for the noise emitted by materials andstructures when they are subjected to stress. Types of stresses can be

    mechanical, thermal or chemical. This emission is caused by the rapid

    release of energy within a material due to events such as crack initiation and

    growth, crack opening and closure, dislocation movement, twinning, and

    phase transformation in monolithic materials and fiber breakage and fiber-

    matrix debonding in composites.

    The subsequent extension occurring under an applied stress generates

    transient elastic waves which propagate through the solid to the surfacewhere they can be detected by one or more sensors. The sensor is a

    transducer that converts the mechanical wave into an electrical signal. In this

    way information about the existence and location of possible sources is

    obtained. Acoustic emission may be described as the "sound" emanatingfrom regions of localized deformation within a material.

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    Until about 1973, acoustic emission technology was primarily employed in the

    non-destructive testing of such structures as pipelines, heat exchangers,

    storage tanks, pressure vessels, and coolant circuits of nuclear reactor plants.However, this technique was soon applied to the detection of defects in

    rotating equipment bearings.

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    Acoustic Emission

    Acoustic Emission (AE) refers to generation of transient elastic waves

    during rapid release of energy from localized sources within a material.

    The source of these emissions in metals is closely associated with the

    dislocation movement accompanying plastic deformation and with the

    initiation and extension of cracks in a structure under stress.,

    /()..

    Other sources of AE are: melting, phase transformation, thermal stresses,

    cool down cracking and stress build up, twinning, fiber breakage and fiber-matrix debonding in composites.

    :

    ,,,,-

    http://www.geocities.ws/raobpc/AET.html

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    AE Technique

    The AE technique (AET) is based on the detection and conversion of high

    frequency elastic waves emanating from the source to electrical signals. This

    is accomplished by directly coupling piezoelectric transducers on the surface

    of the structure under test and loading the structure. The output of the

    piezoelectric sensors (during stimulus) is amplified through a low-noise

    preamplifier, filtered to remove any extraneous noise and further processedby suitable electronics. AET can non-destructively predict early failure of

    structures. Further, a whole structure can be monitored from a few locations

    and while the structure is in operation. AET is widely used in industries for

    detection of faults or leakage in pressure vessels, tanks, and piping systemsand also for on-line monitoring welding and corrosion. The difference

    between AET and other non-destructive testing (NDT) techniques is that AET

    detects activities inside materials, while other techniques attempt to examine

    the internal structures of materials by sending and receiving some form ofenergy.

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    Types of AET

    Acoustic emissions are broadly classified into two major types namely;

    continuous type and

    burst type.

    The waveform of continuous type AE signal is similar to Gaussian random

    noise, but the amplitude varies with acoustic emission activity. In metalsand alloys, this form of emission is considered to be associated with the

    motion of dislocations. Burst type emissions are short duration pulses and

    are associated with discrete release of high amplitude strain energy. In

    metals, the burst type emissions are generated by twinning, micro yielding,development of cracks.

    Continuos type (Gaussian random noise) Motion of dislocation,

    Burst type (discrete high amplitude strain energy)

    twinning, microyielding, development of cracks

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    AET Set-up

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    Continuous type- Gaussian random noise

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    Continuous type

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    Discrete Burst Type

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    Discrete Burst Type

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    Kaiser Effect

    Plastic deformation is the primary source of AE in loaded metallic structures.

    An important feature affecting the AE during deformation of a material isKaiser Effect, which states that additional AE occurs only when the stress

    level exceeds previous stress level. A similar effect for composites is termed

    as 'Falicity effect'.

    Key words:

    Kaiser effect

    Falicity effect

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    Kaiser Effect- which states that additional AE occurs only when the stress

    level exceeds previous stress level. A similar effect for composites is termed

    as 'Falicity effect'.

    http://www.ndt.net/ndtaz/content.php?id=476

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    AE Parameters

    Various parameters used in AET include: AE burst, threshold, ring down

    count, cumulative counts, event duration, peak amplitude, rise time, energyand rms voltage etc. Typical AE system consists of signal detection,

    amplification & enhancement, data acquisition, processing and analysis units.

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    Sensors / Source Location Identification

    The most commonly used sensors are resonance type piezoelectric

    transducers with proper couplants. In some applications where sensorscannot be fixed directly, waveguides are used. Sensors are calibrated for

    frequency response and sensitivity before any application. The AE

    technique captures the parameters and correlates with the defect

    formation and failures. When more than one sensors is used,

    AE source can be located based by measuring the signals arrival time to

    each sensor. By comparing the signals arrival time at different sensors,

    the source location can be calculated through triangulation andother methods.

    AE sources are usually classified based on activity and intensity

    . A source is considered to be active if its event count continues to

    increase with stimulus. A source is considered to be critically active if the rate of change of its

    count or emission rate consistently increases with increasing stimulation

    .

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    AET Advantages

    AE testing is a powerful aid to materials testing and the study of deformation,

    fatigue crack growth, fracture, oxidation and corrosion. It gives an immediateindication of the response and behaviour of a material under stress, intimately

    connected with strength, damage and failure. A major advantage of AE

    testing is that it does not require access to the whole examination area. In

    large structures / vessels permanent sensors can be mounted for periodicinspection for leak detection and structural integrity monitoring.

    Typical advantages of AE technique include:

    1. high sensitivity,2. early and rapid detection of defects, leaks, cracks etc.,

    3. on-line monitoring,

    4. location of defective regions,

    5. minimization of plant downtime for inspection,6. no need for scanning the whole structural surface and

    7. minor disturbance of insulation.

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    AET Limitations

    On the negative side;

    AET requires stimulus.

    AE technique can only (1) qualitatively estimate the damage and predict (2)

    how long the components will last. So,

    other NDT methods are still needed for thorough examinations and forobtaining quantitative information.

    Plant environments are usually very noisy and the AE signals are usually

    very weak. This situation calls for incorporation of signal discrimination and

    noise reduction methods. In this regard, signal processing and frequencydomain analysis are expected to improve the situation.

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    A Few Typical Applications

    Detection and location of leak paths in end-shield of reactors (frequencyanalysis)

    Identification of leaking pressure tube in reactors

    Condition monitoring of 17 m Horton sphere during hydro testing (24

    sensors) On-line monitoring of welding process and fuel end-cap welds

    Monitoring stress corrosion cracking, fatigue crack growth

    Studying plastic deformation behaviour and fracture of SS304, SS316,

    Inconel, PE-16 etc Monitoring of oxidation process and spalling behaviour of metals and

    alloys

    A ti E i i T ti li ti t it bl f

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    Acoustic Emission Testing applications are most suitable for:

    1. Aboveground Storage Tank Screening for Corrosion & Leaks

    2. Pressure Containment Vessels (Columns, Bullets, Cat Crackers)3. Horton Spheres & legs

    4. Fiberglass Reinforced Plastic Tanks and Piping

    5. Offshore Platform Monitoring

    6. Nuclear components inspection7. Tube Trailers

    8. Railroad tank cars

    9. Bridge Critical Members monitoring

    10. Pre- & Post-Stressed Concrete Beams11. Reactor Piping

    12. High Energy Seam Welded Hot Reheat Piping Systems in Power Plants.

    13. On-Stream Monitoring

    14. Remote Long Term Monitoring

    http://www.techcorr.com/services/Inspection-and-Testing/Acoustic-Emission-Testing.cfm

    A ti E i i T ti Ad t

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    Acoustic Emission Testing Advantages

    1. Compared to conventional inspection methods the advantages of the

    Acoustic Emission Testing technique are:2. Tank bottom Testing without removal of product.

    3. Inspection of Insulated Piping & Vessels

    4. Real time monitoring during cool-down & start-ups

    5. Real Time Monitoring Saves Money6. Real Time Monitoring Improves Safety

    T k AET

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    Tank AET

    E d f R di

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    End of Reading

    Study Note 2:

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    Study Note 2:

    Sidney Mindess

    University of British Columbia

    Chapter 16: Acoustic Emission Methods

    16

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    16

    Acoustic Emission

    Methods

    http://unina.stidue.net/Politecnico%20di%20Milano/Inge

    gneria%20Strutturale/Corsi/Felicetti%20-

    %20Structural%20assessment%20and%20residual%20

    bearing%20capacity/books/Handbook%20of%20NDT%

    20of%20Concrete/1485_C16.pdf

    Dam

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    Dam

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    Dam

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    Dam

    16 1 Introduction

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    16.1 Introduction

    16.2 Historical Background

    16.3 Theoretical Considerations16.4 Evaluation of Acoustic Emission Signals

    16.5 Instrumentation and Test Procedures

    16.6 Parameters Affecting Acoustic Emissions from Concrete

    The Kaiser Effect Effect of Loading Devices SignalAttenuation Specimen Geometry Type of aggregate Concrete Strength

    16.7 Laboratory Studies of Acoustic Emission

    Fracture Mechanics Studies Type of Cracks Fracture Process

    Zone (Crack Source) Location Strength vs. Acoustic Emission

    Relationships Drying Shrinkage Fiber Reinforced Cements

    and Concretes High Alumina Cement Thermal Cracking

    Bond in Reinforced Concrete Corrosion of Reinforcing Steel

    in Concrete

    16.8 Field Studies of Acoustic Emission

    16.9 Conclusions

    Foreword:

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    Foreword:

    Acoustic emission refers to the sounds, both audible and sub-audible, that are

    generated when a material undergoes irreversible changes, such as thosedue to cracking. Acoustic emissions (AE) from concrete have been studied for

    the past 30 years, and can provide useful information on concrete properties.

    This review deals with the parameters affecting acoustic emissions from

    concrete, including discussions of the Kaiser effect, specimen geometry, andconcrete properties. There follows an extensive discussion of the use of AE to

    monitor cracking in concrete, whether due to (1) externally applied loads, (2)

    drying shrinkage, or (3) thermal stresses. AE studies on reinforced concrete

    are also described. While AE is very useful laboratory technique for the studyof concrete properties, its use in the field remains problematic.

    16 1 Introduction

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    16.1 Introduction

    It is common experience that the failure of a concrete specimen under load is

    accompanied by a considerable amount of audible noise. In certaincircumstances, some audible noise is generated even before ultimate failure

    occurs. With very simple equipment a microphone placed against the

    specimen, an amplifier, and an oscillograph subaudible sounds can be

    detected at stress levels of perhaps 50% of the ultimate strength; with thesophisticated equipment available today, sound can be detected at much

    lower loads, in some cases below 10% of the ultimate strength. These sounds,

    both audible and subaudible, are referred to as acoustic emission. In general,

    acoustic emissions are defined as the class of phenomena whereby transientelastic waves are generated by the rapid release of energy from localized

    sources within a material. These waves propagate through the material, and

    their arrival at the surfaces can be detected by piezoelectric transducers.

    Keywords: Audible & Sub-audible sounds

    Acoustic emissions, which occur in most materials, are caused by irreversible

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    , , y

    changes, such as (1) dislocation movement, (2) twinning, (3) phase

    transformations, (4) crack initiation, and propagation, (5) debonding betweencontinuous and dispersed phases in composite materials, and so on.

    In concrete, since the first three of these mechanisms do not occur, acoustic

    emission is due primarily to:

    1. Cracking processes

    2. Slip between concrete and steel reinforcement

    3. Fracture or debonding of fibers in fiber-reinforced concrete

    16.2 Historical Background

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    g

    The initial published studies of acoustic emission phenomena, in the early

    1940s, dealt with the problem of predicting rockbursts in mines; this techniqueis still very widely used in the field of rock mechanics, in both field and

    laboratory studies. The first significant investigation of acoustic emission from

    metals (steel, zinc, aluminum, copper, and lead) was carried out by Kaiser.

    Among many other things, he observed what has since become known as the

    Kaiser effect: the absence of detectable acoustic emission at a fixed

    sensitivity level, until previously applied stress levels are exceeded. While

    this effect is not present in all materials, it is a very important observation, and

    it will be referred to again later in this review. The first study of acoustic

    emission from concrete specimens under stress appears to have been carried

    out by Rsch, who noted that during cycles of loading and unloading below

    about 70 to 85% of the ultimate failure load, acoustic emissions were

    produced only when the previous maximum load was reached (the Kaiser

    effect). At about the same time, but independently, LHermite also measured

    acoustic emission from concrete, finding that a sharp increase in acoustic

    emission coincided with the point at which Poissons ratio also began to

    increase (i.e., at the onset of significant matrix cracking in the concrete).

    In 1965, however, Robinson used more sensitive equipment to show that

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    acoustic emission occurred at much lower load levels than had been reported

    earlier, and hence, could be used to monitor earlier microcracking (such asthat involved in the growth of bond cracks in the interfacial region between

    cement and aggregate). In 1970, Wells built a still more sensitive apparatus,

    with which he could monitor acoustic emissions in the frequency range from

    about 2 to 20 kHz. However, he was unable to obtain truly reproducible

    records for the various specimen types that he tested, probably due to the

    difficulties in eliminating external noise from the testing machine. Also in 1970,

    Green reported a much more extensive series of tests, recording acoustic

    emission frequencies up to 100 kHz. Green was the first to show clearly that

    acoustic emissions from concrete are related to failure processes within the

    material; using source location techniques, he was also able to determine the

    locations of defects. It was this work that indicated that acoustic emissions

    could be used as an early warning of failure. Green also noted the Kaiser

    effect, which suggested to him that acoustic emission techniques could be

    used to indicate the previous maximum stress to which the concrete had been

    subjected. As we will see below, however, a true Kaiser effect appears not to

    exist for concrete.

    Green also noted the Kaiser effect, which suggested to him that acoustic

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    emission techniques could be used to indicate the previous maximum stress

    to which the concrete had been subjected. As we will see below, however, a

    true Kaiser effect appears not to exist for concrete.

    Nevertheless, even after this pioneering work, progress in applying acoustic

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    emission techniques remains slow. An extensive review by Diederichs et al.

    (et al means: and others), covers the literature on acoustic emissions from

    concrete up to 1983. However, as late as 1976, Malhotra noted that there was

    little published data in this area, and that acoustic emission methods are in

    their infancy. Even in January, 1988, a thorough computer-aided search of

    the literature found only some 90 papers dealing with acoustic emissions from

    concrete over about the previous 10 years; while this is almost certainly not a

    complete list, it does indicate that there is much work to be carried out before

    acoustic emission monitoring becomes a common technique for testing

    concrete. Indeed, there are still no standard test methods which have even

    been suggested for this purpose.

    16.3 Theoretical Considerations

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    When an acoustic emission event occurs at a source with the material, due to

    (1) inelastic deformation or (2) to cracking, the stress waves travel directly

    from the source to the receiver as body waves. Surface waves may then arise

    from mode conversion. When the stress waves arrive at the receiver, the

    transducer responds to the surface motions that occur.

    It should be noted that the signal captured by the recording device may be

    affected by:

    the nature of the stress pulse generated by the source,

    the geometry of the test specimen, and

    the characteristics of the receiver,

    making it difficult to interpret the recorded waveforms.

    Two basic types of acoustic emission signals can be generated (Figure 16.1):

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    Continuous emission is a qualitative description of the sustained signal

    level produced by rapidly occurring acoustic emission events. These are

    generated by events such as plastic deformations in metals, which occur

    in a reasonably continuous manner.

    Burt emission is a qualitative description of the discrete signal related to

    an individual emission event occurring within the matrial,1 such as that

    which may occur during crack growth or fracture in brittle materials.

    These burst signals are characteristic of the acoustic emission events

    resulting from the loading of cementitious materials.

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    FIGURE 16.1 The two basic types of acoustic emission signals. (A) Continuous

    emission. (B) Burst emission.

    16.4 Evaluation of Acoustic Emission Signals

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    A typical acoustic emission signal from concrete is shown in Figure 16.2.12

    However, when such acoustic events are examined in much greater detail, asshown in Figure 16.3,13 the complexity of the signal becomes even more

    apparent; the scatter in noise, shown in Figure 16.3, makes it difficult to

    determine exactly the time of arrival of the signal; this means that very

    sophisticated equipment must be used to get the most information out of theacoustic emission signals. In addition, to obtain reasonable sensitivity, the

    acoustic emission signals must be amplified. In concrete, typically, system

    gains in the range of 80 to 100 decibels (dB) are used.

    FIGURE 16.2 A typical acoustic emission signal from concrete. (From

    Berthelot J M et al private communication 1987 With permission )

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    Berthelot, J.M. et al., private communication, 1987. With permission.)

    FIGURE 16.3 Typical view of an acoustic emission event as displayed in an

    oscilloscope screen (Adapted from Maji A and Shah S P Exp Mech 26

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    oscilloscope screen. (Adapted from Maji, A. and Shah, S.P., Exp. Mech., 26,

    1, 1988, p. 27.)

    FIGURE 16.2 A typical acoustic emission signal from concrete. (From

    Berthelot J M et al private communication 1987 With permission )

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    Berthelot, J.M. et al., private communication, 1987. With permission.)

    There are a number of different ways in which acoustic emission signals may

    be evaluated

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    be evaluated.

    Acoustic Emission Counting (ring-down counting)

    This is the simplest way in which an acoustic emission event may be

    characterized. It is the number of times the acoustic emission signal exceeds

    a preset threshold during any selected portion of a test, and is illustrated in

    Figure 16.4. A monitoring system may record:

    FIGURE 16.4 The principle of acoustic emission counting (ring-down counting).

    1. The total number of counts (e.g., 13 counts in Figure 16.4). Since the

    shape of a burst emission is generally a damped sinusoid pulses of higher

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    shape of a burst emission is generally a damped sinusoid, pulses of higher

    amplitude will generate more counts.

    2. The count rate. This is the number of counts per unit of time; it is

    particularly useful when very large numbers of counts are recorded.

    3. The mean pulse amplitude. This may be determined by using a root-mean

    square meter, and is an indication of the amount of energy being

    dissipated.

    Clearly, the information obtained using this method of analysis depends upon

    both the gain and the threshold setting. Ring-down counting is affected

    greatly by the characteristics of the transducer, and the geometry of the

    test specimen (which may cause internal reflections) and may not be

    indicative of the nature of the acoustic emission event. In addition, there is

    no obvious way of determining the amount of energy released by a single

    event, or the total number of separate acoustic events giving rise to thecounts.

    Event counting Circuitry is available which counts each acoustic emission

    event only once by recognizing the end of each burst emission in terms of a

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    event only once, by recognizing the end of each burst emission in terms of a

    predetermined length of time since the last count (i.e., since the most recent

    crossing of the threshold). In Figure 16.4, for instance, the number of events

    is three. This method records the number of events, which may be very

    important, but provides no information about the amplitudes involved.

    Rise time This is the interval between the time of first occurrence ofsignals above the level of the background noise and the time at which the

    maximum amplitude is reached. This may assist in determining the type of

    damage mechanism.

    Signal duration This is the duration of a single acoustic emission event;

    this too may be related to the type of damage mechanism.

    Amplitude distribution This provides the distribution of peak amplitudes.

    This may assist in identifying the sources of the emission events that are

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    This may assist in identifying the sources of the emission events that are

    occurring.

    Frequency analysis This refers to the frequency spectrum of individual

    acoustic emission events. This technique, generally requiring a fast Fourier

    transformation analysis of the acoustic emission waves, may help

    discriminate between different types of events. Unfortunately, a frequencyanalysis may sometimes simply be a function of the response of the

    transducer, and thus reveal little of the true nature of the pulse.

    Energy analysisThis is an indication of the energy released by an

    acoustic emission event; it may be measured in a number of ways, depending

    on the equipment, but it is essentially the area under the amplitude vs. time

    curve (Figure 16.4) for each burst. Alternatively, the area under the envelope

    of the amplitude vs. time curve may be measured for each burst.

    Defect location By using a number of transducers to monitor acoustic

    emission events, and determining the time differences between the detection

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    e ss o e e ts, a d dete g t e t e d e e ces bet ee t e detect o

    of each event at different transducer positions, the location of the acoustic

    emission event may be determined by using triangulation techniques. Work

    by Maji and Shah, for instance, has indicated that this technique may be

    accurate to within about 5 mm.

    Analysis of the wave-form Most recently, it has been suggested that an

    elaborate signals processing technique (deconvolution) applied to the wave-

    form of an acoustic emission event can provide information regarding the

    volume, orientation, and type of microcrack. Ideally, since all of these

    methods of data analysis provide different information, one would wish to

    measure them all. However, this is neither necessary nor economically

    feasible. In the discussion that follows, it will become clear that the more

    elaborate methods of analysis are useful in fundamental laboratory

    investigations, but may be inappropriate for practical applications.

    Signal Evaluation:Analysis of the wave-form

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    http://sirius.mtm.kuleuven.be/Research/NDT/AcousticEmissions/index.html

    Signal Evaluation:Acoustic Emission Counting (ring-down counting)

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    Ring-down count= 13

    Signal Evaluation: Raise Time/ Event Counts/ Signal Duration

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    Raise time

    mV/s

    Signal duration s

    Event counts = 3 in unit time

    Signal Evaluation:Amplitude Distribution- Triangulation to locate source

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    Signal Evaluation:Amplitude Distribution- Triangulation to locate source

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    http://iopscience.iop.org/0964-1726/21/3/035009;jsessionid=DE0B79359A6ADDA1365CAC54ABA381A2.c2

    Signal Evaluation: Frequency analysis

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    Signal Evaluation:

    Energy analysis- it is essentially the area under the amplitude vs. time curve

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    Note: all areas under curves or only areas above threshold.

    Signal Evaluation: Raise Time/ Event Counts/ Signal Duration

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    ring-down counting

    Signal Evaluation: Raise Time/ Event Counts/ Signal Duration

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    16.5 Instrumentation and Test Procedures

    Instrumentation (and, where necessary, the associated computer software) is

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    ( , y, p )

    available, from a number of different manufacturers, to carry out all of themethods of signal analysis described above. It might be added that advances

    in instrumentation have outpaced our understanding of the nature of the

    elastic waves resulting from microcracking in concrete. The main elements of

    a modern acoustic emission detection system are shown schematically inFigure 16.5.

    FIGURE 16.5 The main elements of a modern acoustic emission detection system.

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    A brief description of the most important parts of this system is as follows:

    1. Transducers: Piezoelectric transducers (generally made of lead zirconate

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    titanate, PZT) are used to convert the surface displacements into electricsignals. The voltage output from the transducers is directly proportional to

    the strain in the PZT, which depends in turn on the amplitude of the

    surface waves. Since these transducers are high impedance devices, they

    yield relatively low signals, typically less than 100V. There are basicallytwo types of transducers. (a) Wide-band transducers are sensitive to

    acoustic events with frequency responses covering a wide range, often

    several hundred kHz. (b) Narrow-band transducers are restricted to a

    much narrower range of frequencies, using bandpass filters. Of course, thetransducers must be properly coupled to the specimen, often using some

    form of silicone grease as the coupling medium.

    PZT:- If the p.d or the stress is changing the resulting effect also changes. Therefore if

    an alternating potential difference with a frequency equal to the resonant frequency of

    the crystal is applied across it the crystal will oscillate. A number of crystalline

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    y pp y y

    materials show this effect examples of these are quartz, barium titanate, lithiumsulphate, lead metaniobate, lead zirconate titanate (PZT) and polyvinylidine difluoride.

    Piezoelectric transducers can act as both as a transmitter and a detector of vibrations.

    However there are certain conditions. The crystal must stop vibrating as soon as the

    alternating potential difference is switched off so that they can detect the reflected

    pulse. For this reason a piece of damping material with an acoustic impedance the

    same as that of the crystal is mounted at the back of the crystal. (See Figure 2).The

    transducer is made with a crystal that has a thickness of one half of the

    wavelength of the ultrasound, resonating at its fundamental frequency. A layer of

    gel is needed between the transducer and the body to get good acoustic coupling (seeacoustic impedance).

    http://www.schoolphysics.co.uk/age16-19/Medical%20physics/text/Piezoelectric_transducer/index.html

    The transducer is made with a crystal that has a thickness of one half of the

    wavelength of the ultrasound, resonating at its fundamental frequency.

    Example: Frequency= 519Hz Wavelength = Speed/ frequency =

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    Example: Frequency= 519Hz, Wavelength = Speed/ frequency =

    5890/519=11.35mm. The thickness of the transducer= 5.7mm approx.

    s= 5890m/s

    http://www.olympus-ims.com/en/ndt-tutorials/thickness-gage/appendices-velocities/

    AET

    Transducer

    In 0 1KHz~2 0KHz

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    In 0.1KHz 2.0KHz

    UT Transducers 2.0~5.0 MHz

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    2. Preamplifier: Because of the low voltage output, the leads from the

    transducer to the preamplifier must be as short as possible; often, the

    preamplifier is integrated within the transducer itself. Typically, the gain in the

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    preamplifier is integrated within the transducer itself. Typically, the gain in the

    preamplifier is in the range 40 to 60 dB. (Note: The decibel scale measuresonly relative amplitudes. Using this scale:

    where Vis the output amplitude and Vi is the input amplitude. That is, a gainof 40 dB will increase the input amplitude by a factor of 100; a gain of 60 dB

    will increase the input amplitude by a factor of 1000, and so on.)

    3. Passband filters are used to suppress the acoustic emission signals that

    lie outside of the frequency range of interest.

    4. The main amplifier further amplifies the signals, typically with a gain of an

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    p p g , yp y g

    additional 20 to 60 dB.5. The discriminator is used to set the threshold voltage above which signals

    are counted.

    The remainder of the electronic equipment depends upon the way in whichthe acoustic emission data are to be recorded, analyzed, and displayed.

    Acoustic emission testing may be carried out in the laboratory or in the field.

    Basically, one or more acoustic emission transducers are attached to thespecimen. The specimen is then loaded slowly, and the resulting acoustic

    emissions are recorded.

    There are generally two categories of tests:

    1. To use the acoustic emission signals to learn something about the internal

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    structure of the material, and how structural changes (i.e., damage) occurduring the process of loading. In this case, the specimens are generally

    loaded to failure.

    2. To establish whether the material or the structure meet certain design or

    fabrication criteria. In this case, the load is increased only to somepredetermined level (proof loading). The amount and nature of the

    acoustic emissions may be used to establish the integrity of the specimen

    or structure, and may also sometimes be used to predict the service life.

    16.6 Parameters Affecting Acoustic Emissions from Concrete

    16.6.1 The Kaiser Effect

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    The earliest acoustic emission studies of concrete, such as the work of Rsch,indicated that a true Kaiser effect (see above) exists for concrete; that is,

    acoustic emissions were found not to occur in concrete that had been

    unloaded until the previously applied maximum stress had been exceeded on

    reloading. This was true, however, only for stress levels below about 75 to85% of the ultimate strength of the material; for higher stresses, acoustic

    emissions began again at stresses somewhat lower than the previous

    maximum stress. Subsequently, a number of other investigators have also

    concluded that concrete exhibits a Kaiser effect, at least for stresses belowthe peak stress of the material.

    Key points:

    For concrete This was true, however, only for stress levels below about 75 to85% of the ultimate strength of the material

    Spooner and Dougill confirmed that this effect did not occur beyond the peak

    of the stress-strain curve (i.e., in the descending portion of the stress-strain

    curve), where acoustic emissions occurred again before the previous

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    maximum strain was reached. It has also been suggested that a form of theKaiser effect occurs as well for cyclic thermal stresses in concrete, and for

    drying and wetting cycles. On the other hand, Nielsen and Griffin have

    reported that the Kaiser effect is only a very temporary effect in concrete; with

    only a few hours of rest between loading cycles, acoustic emissions are againrecorded during reloading to the previous maximum stress. They therefore

    concluded that the Kaiser effect is not a reliable indicator of the loading

    history for plain concrete. Thus, it is unlikely that the Kaiser effect could be

    used in practice to determine the previous maximum stress that a structuralmember has been subjected to.

    Kaiser Effect- Concrete that this effect did notoccur beyond the

    peak of the stress-

    strain curve (i.e., in

    the descending

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    For concrete This

    was true, however,only for stress

    levels below about

    75 to 85% of the

    ultimate strength

    of the material

    portion of the stress-strain curve), where

    acoustic emissions

    occurred again

    before the previous

    maximum strain was

    reached.

    Spooner and Dougill conclusion on Kaiser Effect- Concrete:

    They therefore concluded that the Kaiser effect is not a

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    y

    reliable indicator of the loading history for plain concrete.

    16.6.2 Effect of Loading Devices

    As is well known, the end restraint of a compression specimen of concrete

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    due to the friction between the ends of the specimen and the loading platenscan have a considerable effect on the apparent strength of the concrete.

    These differences are also reflected in the acoustic emissions measured

    when different types of loading devices are used. For instance, in

    compression testing with stiff steel platens, most of the acoustic emissionappears at stresses beyond about half of the ultimate stress; with more

    flexible platens, such as brush platens, significant acoustic emission appears

    at about 20% of the ultimate stress. This undoubtedly reflects the different

    crack patterns that develop with different types of platens, but it nonethelessmakes inter-laboratory comparisons, and indeed even studies on different

    specimen geometries within the same laboratory, very difficult.

    16.6.3 Signal Attenuation

    The elastic stress waves that are generated by cracking attenuate as they

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    propagate through the concrete. Thus, large acoustic emission events thattake place in the concrete far from a pick-up transducer may not exceed the

    threshold excitation voltage due to this attenuation, while much smaller

    events may be recorded if they occur close to the transducer. Very little

    information is available on acoustic emission attenuation rates in concrete. Ithas been shown that more mature cements show an increasing capacity to

    transmit acoustic emissions.20 Related to this, Mindess23 has suggested that

    the total counts to failure for concrete specimens in compression are much

    higher for older specimens, which may also be explained by the bettertransmission through older concretes.

    As a practical matter, the maximum distance between piezoelectric

    transducers, or between the transducers and the source of the acoustic

    emission event, should not be very large. Berthelot and Robert required an

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    array of transducers arranged in a 40-cm square mesh to locate acousticemission events reasonably accurately. They found that for ordinary concrete,

    with a fifth transducer placed in the center of the 40 x 40-cm square mesh,

    only about 40% of the events detected by the central transducer were also

    detected by the four transducers at the corners; with high strength concrete,this proportion increased to 60 to 70%. Rossi also found that a 40-cm square

    mesh was needed for a proper determination of acoustic emission events.

    Although more distant events can, of course, be recorded, there is no way of

    knowing how many events are lost due to attenuation. This is an area thatrequires much more study.

    16.6.4 Specimen Geometry

    It has been shown that smaller specimens appear to give rise to greater

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    levels of acoustic emission than do larger ones. The reasons for this are notclear, although the observation may be related to the attenuation effect

    described above. After an acoustic emission event occurs, the stress waves

    not only travel from the source to the sensor, but also undergo (1) reflection,

    (2) diffraction, and (3) mode conversions within the material. The basicproblem of wave propagation within a bounded solid certainly requires further

    study, but there have apparently been no comparative tests on different

    specimen geometries.

    16.6.5 Type of Aggregate

    It is not certain whether the mineralogy of the aggregate has any effect on

    ti i i It h b t d th t t ith ll

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    acoustic emission. It has been reported that concretes with a smallermaximum aggregate size produce a greater number of acoustic emission

    counts than those with a larger aggregate size;10 however, the total energy

    released by the finer aggregate concrete is reduced. This is attributed to the

    observation that concretes made with smaller aggregates start to crack atlower stresses; in concretes with larger aggregate particles, on the other hand,

    individual acoustic events emit higher energies. For concretes made with

    lightweight aggregates, the total number of counts is also greater than for

    normal weight concrete, perhaps because of cracking occurring in the

    aggregates themselves.

    16.6.6 Concrete Strength

    It has been shown that the total number of counts to the maximum load is

    t f hi h t th t H ti d li f

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    greater for higher strength concretes. However, as was mentioned earlier, forsimilar strength levels the total counts to failure appears to be much higher for

    older concretes.

    16.7 Laboratory Studies of Acoustic Emission

    By far the greatest number of acoustic emission studies of concrete have

    b i d t i th l b t d h b l l th ti l i

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    been carried out in the laboratory, and have been largely theoretical innature:

    1. To determine whether acoustic emission analysis could be applied to

    cementitious systems2. To learn something about crack propagation in concrete

    16.7.1 Fracture Mechanics Studies

    A number of studies have shown that acoustic emission can be related to

    crack growth or fracture mechanics parameters in cements mortars and

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    crack growth or fracture mechanics parameters in cements, mortars, andoncretes. Evans et al. showed that acoustic emission could be correlated with

    crack velocity in mortars. Morita and Kato and Nadeau, Bennett, and

    Mindess20 were able to relate total acoustic emission counts to Kc (the

    fracture toughness). In addition, Lenain and Bunsell found that the number ofemissions could be related to the sixth power of the stress intensity factor, K.

    Izumi et al. showed that acoustic emissions could also be related to the strain

    energy release rate, G. In all cases, however, these correlations are purely

    empirical; no one has yet developed a fundamental relationship between

    acoustic emission events and fracture parameters, and it is unlikely that such

    a relationship exists.

    16.7.2 Type of Cracks

    A number of attempts have been made to relate acoustic events of different

    frequencies or of different energies to different types of cracking in concrete

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    frequencies, or of different energies, to different types of cracking in concrete.For instance, Saeki et al.,31 by looking at the energy levels of the acoustic

    emissions at different levels of loading, concluded that the first stage of

    cracking, due to the development of bond cracks between the cement paste

    and the aggregate, emitted high energy signals; the second stage, which they

    termed crack arrest, emitted low energy signals; the final stage, in which

    cracks extended through the mortar, was again associated with high energy

    acoustic events. Similarly, Tanigawa and Kobayashi32 used acoustic

    energies to distinguish the onset of the proportional limit, the initiation stress

    and the critical stress. On the other hand, Tanigawa et al.11 tried to relate

    the fracture type (pore closure, tensile cracking, and shear slip) to the power

    spectra and frequency components of the acoustic events. The difficulty with

    these and similar approaches is that they tried to relate differences in the

    recorded acoustic events to preconceived notions of the

    nature of cracking in concrete; direct cause and effect relationships were

    never observed.

    16.7.3 Fracture Process Zone (Crack Source) Location

    Perhaps the greatest current interest in acoustic emission analysis is its use

    in locating fracture processes and in monitoring the damage that concreted k Ok d t l 33 34 h d th t th l ti f

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    in locating fracture processes, and in monitoring the damage that concreteundergoes as cracks progress. Okada et al.33,34 showed that the location of

    crack sources obtained from differences in the arrival times of acoustic

    emissions was in good agreement with the observed fracture surface. At

    about the same time, Chhuy et al.35 and Lenain and Bunsell29 were able to

    determine the length of the damaged zone ahead of the tip of a propagating

    crack using one-dimensional acoustic emission location techniques. In

    subsequent work, Chhuy et al.,36 using more elaborate equipment and

    analytical techniques, were able to determine damage both before the

    initiation of a visible crack and after subsequent crack extension. Berthelot

    and Robert24,37 and Rossi25 used acoustic emission to monitor concrete

    damage as well.

    They found that, while the number of acoustic events showed the progression

    of damage both ahead and behind the crack front, this technique alone could

    not provide a quantitative description of the cracking. However, using more

    elaborate techniques including amplitude analysis and measurements of

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    elaborate techniques, including amplitude analysis and measurements ofsignal duration, Berthelot and Robert24 concluded that acoustic emission

    testing is practically the only technique which can provide a quantitative

    description of the progression in real time of concrete damage within test

    specimens. Later, much more sophisticated signals processing techniqueswere applied to acoustic emission analysis. In 1981, Michaels et al.15 and

    Niwa et al.38 developed deconvolution techniques to analyze

    acoustic waveforms, in order to provide a stress-time history of the source of

    an acoustic event. Similar deconvolution techniques were subsequently usedby Maji and Shah13,39 to determine the volume, orientation and type of

    microcrack, as well as the source of the acoustic events. Such sophisticated

    techniques have the potential eventually to be used to provide a detailed

    picture of the fracture processes occurring within concrete specimens.

    16.7.4 Strength vs. Acoustic Emission Relationships

    Since concrete quality is most frequently characterized by its strength, many

    studies have been directed towards determining a relationship betweenti i i ti it d t th F i t T i d

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    studies have been directed towards determining a relationship betweenacoustic emission activity and strength. For instance, Tanigawa and

    Kobayashi32 concluded that the compressive strength of concrete can be

    approximately estimated by the accumulated AE counts at relatively low

    stress level. Indeed, they suggested that acoustic emission techniques might

    provide a useful nondestructive test method for concrete strength. Earlier,

    Fertis40 had concluded that acoustic emissions could be used to determine

    not only strength, but also static and dynamic material behavior. Rebic,41 too,

    found that there is a relationship between the critical load at which the

    concrete begins to be damaged, which can be determined from acoustic

    emission measurements, and the ultimate strength; thus, acoustic emission

    analysis might be used as a predictor of concrete strength. Sadowska-Boczar

    et al.42 tried to quantify the strength vs. acoustic emission relationship using

    the equation

    Sadowska-Boczar et al.42 tried to quantify the strength vs. acoustic emission

    relationship using the equation:

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    Where:

    Fr is the rupture strength,Fp is the stress corresponding to the first acoustic emission signal, and

    a and b are constants for a given material and loading conditions.

    Using this linear relationship, which they found to fit their data reasonably well,

    they suggested that the observation of acoustic emissions at low stresses

    would permit an estimation of strength, as well as providing some

    characterization of porosity and critical flaw size.

    Unfortunately, the routine use of

    acoustic emissions as an

    estimator of strength seems to be

    an unlikely prospect in large part

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    an unlikely prospect, in large partbecause of the scatter in the data,

    as has been noted by Fertis.40 As

    an example of the scatter in data.

    Figure 16.623 indicates thevariability in the strength vs. total

    acoustic emission counts

    relationship; the within-batch

    variability is even more severe, asshown in Figure 16.7.23

    FIGURE 16.6 Logarithm of total acoustic emission counts vs.

    compressive strength of concrete cubes. (From Mindess, S., Int.

    J. Cem. Comp. Lightweight Concr., 4, 173, 1982. Withpermission.)

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    FIGURE 16.7 Within-batch variability of total acoustic emission counts vs. applied compressive

    stress on concretecubes. (From Mindess, S., Int. J. Cem. Comp. Lightweight Concr., 4, 173,

    1982. With permission.)

    16.7.5 Drying Shrinkage

    16.7.6 Fiber Reinforced Cements and Concretes

    16.7.7 High Alumina Cement

    16.7.8 Thermal Cracking

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    16.7.8 Thermal Cracking16.7.9 Bond in Reinforced Concrete

    16.7.10 Corrosion of Reinforcing Steel in Concrete

    Read text for details

    http://unina.stidue.net/Politecnico%20di%20Milano/Inge

    gneria%20Strutturale/Corsi/Felicetti%20-

    %20Structural%20assessment%20and%20residual%20

    bearing%20capacity/books/Handbook%20of%20NDT%

    20of%20Concrete/1485_C16.pdf

    16.8 Field Studies of Acoustic Emission

    As shown in the previous section, acoustic emission analysis has been used

    in the laboratory to study a wide range of problems. Unfortunately, its use

    in the field has been severely limited; only a very few papers on field

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    in the field has been severely limited; only a very few papers on field

    application have appeared, and these are largely speculation on future

    possibilities. The way in which acoustic emission data might be used to

    provide information about the condition of a specimen or a structure has

    been described by Cole;54 his analysis may be summarized as follows:

    1. Is there any acoustic emission at a certain load level? If no, then no

    damage is occurring under these conditions; if yes, then damage is

    occurring.

    2. Is acoustic emission continuing while the load is held constant at the

    maximum load level? If no, no damage due to creep is occurring; if yes,

    creep damage is occurring. Further, if the count rate is increasing, then

    failure may occur fairly soon.

    3. Have high amplitude acoustic emissions events occurred? If no, individual

    fracture events have been relatively minor; if yes, major fracture events

    have occurred.

    4. Does acoustic emission occur if the structure has been unloaded and is? f

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    then reloaded to the previous maximum load? If no, there is no damage or

    crack propagation under low cycle fatigue; if yes, internal damage exists

    and the damage sites continue to spread even under low loads.

    5. Does the acoustic emission occur only from a particular area? Ifno, theentire structure is being damaged; if yes, the damage is localized.

    6. Is the acoustic emission in a local area very localized? if no, damage is

    dispersed over a significant area; if yes, there is a highly localized stress

    concentration causing the damage.

    16.9 Conclusions

    From the discussion above, it appears that acoustic emission techniques may

    be very useful in the laboratory to supplement other measurements of

    concrete properties. However, their use in the field remains problematic.

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    concrete properties. However, their use in the field remains problematic.

    Many of the earlier studies held out high hopes for acoustic emission

    monitoring of structures. For instance, McCabe et al.17 suggested that, if a

    structure was loaded, the absence of acoustic emissions would indicate that it

    was safe under the existing load conditions; a low level of acoustic emissions

    would indicate that the structure should be monitored carefully, while a high

    level of acoustic emission could indicate that the structure was unsafe. But

    this is hardly a satisfactory approach, since it does not provide any help with

    quantitative analysis. In any event, even the sophisticated (and expensive)

    equipment now available still provides uncertain results when applied to

    structures, because of our lack of knowledge about the characteristics of

    acoustic emissions due to different causes, and because of the possibility of

    extraneous noise (vibration, loading devices, and so on).

    Another serious drawback is that acoustic emissions are only generated

    when the loads on a structure are increased, and this poses considerable

    practical problems. Thus, one must still conclude, with regret, that acoustic

    emission analysis has not yet been well developed as a technique for thel ti f h t ki l i t i t t 18

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    y y p qevaluation of phenomena taking place in concrete in structures.18

    End of Reading

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    Study Note 3:

    Introduction to Acoustic Emission Testinghttp://www.ndt-ed.org/EducationResources/CommunityCollege/Other%20Methods/AE/AE_Intro.htm

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    Acoustic Emission (AE) refers to the generation of transient elastic waves

    produced by a sudden redistribution of stress in a material. When a

    structure is subjected to an external stimulus (change in pressure, load, or

    temperature), localized sources trigger the release of energy, in the form ofstress waves which propagate to the surface and are recorded by sensors

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    stress waves, which propagate to the surface and are recorded by sensors.

    With the right equipment and setup, motions on the order of picometers

    (10-12 m) can be identified. Sources of AE vary from natural events like:

    1. earthquakes and rock bursts to

    2. the initiation and growth of cracks,

    3. slip and dislocation movements,

    4. melting,5. twinning, and

    6. phase transformations

    in metals. In composites, matrix cracking and fiber breakage and de-bondingcontribute to acoustic emissions.

    AEs have also been measured and recorded in polymers, wood, and

    concrete, among other materials. Detection and analysis of AE signals can

    supply valuable information regarding the origin and importance of a

    discontinuity in a material. Because of the versatility of Acoustic EmissionTesting (AET)

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    Testing (AET),

    It has many industrial applications e.g.

    1. assessing structural integrity,

    2. detecting flaws,

    3. testing for leaks, or

    4. monitoring weld quality and5. is used extensively as a research tool.

    Twinning

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    AET

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    Acoustic Emission is unlike most other nondestructive testing (NDT)

    techniques in two regards. The first difference pertains to the origin of the

    signal. Instead of supplying energy to the object under examination, AET

    simply listens for the energy released by the object.AE tests are oftenperformed on structures while in operation, as this provides adequate loading

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    performed on structures while in operation, as this provides adequate loading

    for propagating defects and triggering acoustic emissions.

    The second difference is that AET deals with dynamic processes, or changes,

    in a material. This is particularly meaningful because only active features (e.g.

    crack growth) are highlighted. The ability to discern between developing and

    stagnant defects is significant. However, it is possible for flaws to go

    undetected altogether if the loading is not high enough to cause an acoustic

    event.

    Furthermore, AE testing usually provides an immediate indication relating to

    the strength or risk of failure of a component. Other advantages of AET

    include fast and complete volumetric inspection using multiple sensors,permanent sensor mounting for process control, and no need to disassemble

    and clean a specimen.

    Unfortunately, AE systems can only qualitatively gauge how much damage is

    contained in a structure. In order to obtain quantitative results about size,

    depth, and overall acceptability of a part, other NDT methods (often ultrasonic

    testing) are necessary. Another drawback of AE stems from loud serviceenvironments which contribute extraneous noise to the signals. For

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    environments which contribute extraneous noise to the signals. For

    successful applications, signal discrimination and noise reduction are crucial.

    A Brief History of AE Testing

    Although acoustic emissions can be created in a controlled environment, they

    can also occur naturally. Therefore, as a means of quality control, the origin of

    AE is hard to pinpoint. As early as 6,500 BC, potters were known to listen for

    dibl d d i th li f th i i i if i t t l

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    audible sounds during the cooling of their ceramics, signifying structural

    failure. In metal working, the term "tin cry" (audible emissions produced by the

    mechanical twinning of pure tin during plastic deformation) was coined

    around 3,700 BC by tin smelters in Asia Minor. The first documented

    observations of AE appear to have been made in the 8th century by Arabian

    alchemist Jabir ibn Hayyan. In a book, Hayyan wrote that Jupiter (tin) gives

    off a harsh sound when worked, while Mars (iron) sounds much during

    forging. Many texts in the late 19th century referred to the audible emissionsmade by materials such as tin, iron, cadmium and zinc. One noteworthy

    correlation between different metals and their acoustic emissions came from

    Czochralski, who witnessed the relationship between tin and zinc cry and

    twinning. Later, Albert Portevin and Francois Le Chatelier observed AEemissions from a stressed Al-Cu-Mn (Aluminum-Copper-Manganese) alloy.

    The next 20 years brought further verification with the work of Robert

    Anderson (tensile testing of an aluminum alloy beyond its yield point), Erich

    Scheil (linked the formation of martensite in steel to audible noise), and

    Friedrich Forster, who with Scheil related an audible noise to the formation ofmartensite in high-nickel steel. Experimentation continued throughout the

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    g p g

    mid-1900s, culminating in the PhD thesis written by Joseph Kaiser entitled

    "Results and Conclusions from Measurements of Sound in Metallic Materials

    under Tensile Stress. Soon after becoming aware of Kaisers efforts,Bradford Schofield initiated the first research program in the United States to

    look at the materials engineering applications of AE. Fittingly, Kaisers

    research is generally recognized as the beginning of modern day acoustic

    emission testing.

    Theory - AE Sources

    As mentioned in the Introduction, acoustic emissions can result from the

    initiation and growth of cracks, slip and dislocation movements, twinning, or

    phase transformations in metals. In any case, AEs originate with stress.

    When a stress is exerted on a material a strain is induced in the material as

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    When a stress is exerted on a material, a strain is induced in the material as

    well. Depending on the magnitude of the stress and the properties of the

    material, an object may return to its original dimensions or be permanently

    deformed after the stress is removed. These two conditions are known aselastic and plastic deformation, respectively.

    The most detectible acoustic emissions take place when a loaded material

    undergoes plastic deformation or when a material is loaded at or near its yield

    stress. On the microscopic level, as plastic deformation occurs, atomic planes

    slip past each other through the movement of dislocations. These atomic-scale deformations release energy in the form of elastic waves which can be

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    thought of as naturally generated ultrasound traveling through the object.

    When cracks exist in a metal, the stress levels present in front of the crack tip

    can be several times higher than the surrounding area. Therefore, AE activitywill also be observed when the material ahead of the crack tip undergoes

    plastic deformation (micro-yielding).

    Two sources of fatigue cracks also cause AEs. The first source is emissive

    particles (e.g. nonmetallic inclusions) at the origin of the crack tip. Since these

    particles are less ductile than the surrounding material, they tend to break

    more easily when the metal is strained, resulting in an AE signal. The secondsource is the propagation of the crack tip that occurs through the movement

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    of dislocations and small-scale cleavage produced by triaxial stresses.

    The amount of energy released by an acoustic emission and the amplitude of

    the waveform are related to the magnitude and velocity of the source event.The amplitude of the emission is proportional to the velocity of crack

    propagation and the amount of surface area created. Large, discrete crack

    jumps will produce larger AE signals than cracks that propagate slowly over

    the same distance.Detection and conversion of these elastic waves to electrical signals is the

    basis of AE testing. Analysis of these signals yield valuable information

    regarding the origin and importance of a discontinuity in a material. As

    discussed in the following section, specialized equipment is necessary todetect the wave energy and decipher which signals are meaningful.

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    Activity of AE Sources in Structural Loading

    AE signals generated under different loading patterns can provide valuable

    information concerning the structural integrity of a material. Load levels that

    have been previously exerted on a material do not produce AE activity. In

    other words discontinuities created in a material do not expand or move until

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    other words, discontinuities created in a material do not expand or move until

    that former stress is exceeded. This phenomenon, known as the Kaiser Effect,

    can be seen in the load versus AE plot to the right. As the object is loaded,

    acoustic emission events accumulate (segment AB). When the load isremoved and reapplied (segment BCB), AE events do not occur again until

    the load at point B is exceeded. As the load exerted on the material is

    increased again (BD), AEs are generated and stop when the load is removed.

    However, at point F, the applied load is high enough to cause significantemissions even though the previous maximum load (D) was not reached.

    This phenomenon is known as the Felicity Effect. This effect can be

    quantified using the Felicity Ratio, which is the load where considerable AE

    resumes, divided by the maximum applied load (F/D).

    Kaiser/Felicity effects

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    Felicity effect F/D

    Kaiser effect

    Knowledge of the Kaiser Effect and Felicity Effect can be used to determine if

    major structural defects are present. This can be achieved by applying

    constant loads (relative to the design loads exerted on the material) and

    listening to see if emissions continue to occur while the load is held. Asshown in the figure, if AE signals continue to be detected during the holding

    f th l d (GH) it i lik l th t b t ti l t t l d f t t

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    of these loads (GH), it is likely that substantial structural defects are present.

    In addition, a material may contain critical defects if an identical load is

    reapplied and AE signals continue to be detected. Another guidelinegoverning AEs is the Dunegan corollary, which states that if acoustic

    emissions are observed prior to a previous maximum load, some type of new

    damage must have occurred. (Note: Time dependent processes like corrosion

    and hydrogen embrittlement tend to render the Kaiser Effect useless)

    Dict:

    Corollary: something that results from something else.

    Emissions are observed prior to a previous maximum load;

    Felicity effect,

    Dunegan corollary

    K d

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    Keywords:

    Kaiser effect,

    Felicity effect,

    Dunegan corollary

    Noise

    The sensitivity of an acoustic emission system is often limited by the amount

    of background noise nearby. Noise in AE testing refers to any undesirable

    signals detected by the sensors. Examples of these signals include frictionalsources (e.g. loose bolts or movable connectors that shift when exposed to

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    ( g p

    wind loads) and impact sources (e.g. rain, flying objects or wind-driven dust)

    in bridges. Sources of noise may also be present in applications where the

    area being tested may be disturbed by mechanical vibrations (e.g. pumps).To compensate for the effects of background noise, various procedures can

    be implemented. Some possible approaches involve fabricating special

    sensors with electronic gates for noise blocking, taking precautions to place

    sensors as far away as possible from noise sources, and electronic filtering(either using signal arrival times or differences in the spectral content of true

    AE signals and background noise).

    Pseudo Sources

    In addition to the AE source mechanisms described above, pseudo source

    mechanisms produce AE signals that are detected by AE equipment.

    Examples include liquefaction and solidification, friction in rotating bearings,solid-solid phase transformations, leaks, cavitation, and the realignment or

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    growth of magnetic domains (See Barkhausen Effect).

    Wave Propagation

    A primitive wave released at the AE source

    is illustrated in the figure right. The

    displacement waveform is a step-likefunction corresponding to the permanent

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    change associated with the source process.

    The analogous velocity and stress

    waveforms are essentially pulse-like. Thewidth and height of the primitive pulse

    depend on the dynamics of the source

    process. Source processes such as

    microscopic crack jumps and precipitatefractures are usually completed in a fraction

    of a microsecond or a few microseconds,

    which explains why the pulse is short in

    duration. The amplitude and energy of theprimitive pulse vary over an enormous range

    from submicroscopic dislocation movements

    to gross crack jumps.

    Primitive AE wave

    released at a source. The

    primitive wave is

    essentially a stress pulsecorresponding to a

    permanent displacement

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    permanent displacement

    of the material. The

    ordinate quantities refer toa point in the material.

    Waves radiates from the

    source in all directions, often

    having a strong directionality

    depending on the nature of thesource process, as shown in

    the second figure Rapid

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    the second figure. Rapid

    movement is necessary if a

    sizeable amount of the elasticenergy liberated during

    deformation is to appear as an

    acoustic emission.

    Angular dependence of acoustic emission radiated from a growing

    microcrack. Most of the energy is directed in the 90 and 270o directions,

    perpendicular to the crack surfaces.

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    Angular dependence of acoustic emission radiated from a growing

    microcrack. Most of the energy is directed in the 90 and 270o directions,

    perpendicular to the crack surfaces.

    As these primitive waves travel through a material, their form is changed

    considerably. Elastic wave source and elastic wave motion theories are being

    investigated to determine the complicated relationship between the AE

    source pulse and the corresponding movement at the detection site. Theultimate goal of studies of the interaction between elastic waves and material

    structure is to accurately develop a description of the source event from the

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    structure is to accurately develop a description of the source event from the

    output signal of a distant sensor.

    However, most materials-oriented researchers and NDT inspectors are not

    concerned with the intricate knowledge of each source event. Instead, they

    are primarily interested in the broader, statistical aspects of AE. Because of

    this, they prefer to use narrow band (resonant) sensors which detect only asmall portion of the broadband of frequencies emitted by an AE. These

    sensors are capable of measuring hundreds of signals each second, in

    contrast to the more expensive high-fidelity sensors used in source function

    analysis. More information on sensors will be discussed later in theEquipment section.

    The signal that is detected by a sensor is a combination of many parts of the

    waveform initially emitted. Acoustic emission source motion is completed in a

    few millionths of a second. As the AE leaves the source, the waveform travels

    in a spherically spreading pattern and is reflected off the boundaries of theobject. Signals that are in phase with each other as they reach the sensor

    produce constructive interference which usually results in the highest peak of

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    p y g p

    the waveform being detected. The typical time interval from when an AE wave

    reflects around the test piece (repeatedly exciting the sensor) until it decays,ranges from the order of 100 microseconds in a highly damped, nonmetallic

    material to tens of milliseconds in a lightly damped metallic material.

    Decay Time:highly damped, nonmetallic material order of 100 microseconds (s-6)

    lightly damped metallic material tens of milliseconds (s-3)

    Decay time

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    y

    Decay Time:

    highly damped, nonmetallic material order of 100 microseconds (s-6)lightly damped metallic material tens of milliseconds (s-3)

    Attenuation

    The intensity of an AE signal detected by a sensor is considerably lower than

    the intensity that would have been observed in the close proximity of the

    source. This is due to attenuation. There are three main causes of attenuation,beginning with geometric spreading. As an AE spreads from its source in a

    plate like material its amplitude decays by 30% every time it doubles its

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    plate-like material, its amplitude decays by 30% every time it doubles its

    distance from the source. In three-dimensional structures, the signal decays

    on the order of 50%. This can be traced back to the simple conservation ofenergy. Another cause of attenuation is material damping, as alluded to in the

    previous paragraph. While an AE wave passes through a material, its elastic

    and kinetic energies are absorbed and converted into heat. The third cause of

    attenuation is wave scattering. Geometric discontinuities (e.g. twinboundaries, nonmetallic inclusions, or grain boundaries) and structural

    boundaries both reflect some of the wave energy that was initially transmitted.

    Attenuation:

    Spread (30% for 2D, 50% for 3D for each doubling of distance from source),

    Material damping,

    Wave scattering at interfaces

    Attenuation:

    1. Spread (30% for 2D, 50% for 3D for each doubling of distance from

    source),

    2. Material damping,3. Wave scattering at interfaces

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    1

    2

    3

    3

    Measurements of the effects of attenuation on an AE signal can be performed

    with a simple apparatus known as a Hsu-Nielson Source. This consists of a

    mechanical pencil with either 0.3 or 0.5 mm 2H lead that is passed through a

    cone-shaped Teflon shoe designed to place the lead in contact with thesurface of a material at a 30 degree angle. When the pencil lead is pressed

    and broken against the material, it creates a small, local deformation that is

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    relieved in the form of a stress wave, similar to the type of AE signal produced

    by a crack. By using this method, simulated AE sources can be created atvarious sites on a structure to determine the optimal position for the

    placement of sensors and to ensure that all areas of interest are within the

    detection range of the sensor or sensors.

    http://www.ndt.net/ndtaz/content.php?id=474

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    Wave Mode and Velocity

    As mentioned earlier, using AE inspection in conjunction with other NDE

    techniques can be an effective method in gauging the location and nature of

    defects. Since source locations are determined by the time required for thewave to travel through the material to a sensor, it is important that the velocity

    of the propagating waves be accurately calculated This is not an easy task

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    of the propagating waves be accurately calculated. This is not an easy task

    since wave propagation depends on the material in question and the wave

    mode being detected. For many applications, Lamb waves are of primaryconcern because they are able to give the best indication of wave

    propagation from a source whose distance from the sensor is larger than the

    thickness of the material. For additional information on Lamb waves, see the

    wave mode page in the Ultrasonic Inspection section.

    Equipment- Probe

    Case

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    Damping

    materials

    Wear plate

    Electrode

    Piezoelectric element

    Couplants

    Specimen

    Equipment- Probe

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    Equipment

    Acoustic emission testing can be performed in the field with portable

    instruments or in a stationary laboratory setting. Typically, systems contain a

    sensor, preamplifier, filter, and amplifier, along with measurement, display,and storage equipment (e.g. oscilloscopes, voltmeters, and personal

    computers). Acoustic emission sensors respond to dynamic motion that is

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    p ) p y

    caused by an AE event. This is achieved through transducers which convert

    mechanical movement into an electrical voltage signal. The transducerelement in an AE sensor is almost always a piezoelectric crystal, which is

    commonly made from a ceramic such as Lead Zirconate Titanate (PZT).

    Transducers are selected based on operating frequency, sensitivity and

    environmental characteristics, and are grouped into two classes: resonantand broadband. The majority of AE equipment is responsive to movement in

    its typical operating frequency range of 30 kHz to 1 MHz. For materials with

    high attenuation (e.g. plastic composites), lower frequencies may be used to

    better distinguish AE signals. The opposite holds true as well.

    Key Points:

    Two classes: resonant and broadband.

    The majority of AE equipment is responsive to movement in its typicaloperating frequency range of 30 kHz to 1 MHz.

    For materials with high attenuation (e.g. plastic composites), lower

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    g ( g p p ),

    frequencies may be used to better distinguish AE signals. The opposite

    holds true as well.

    Ideally, the AE signal that reaches the mainframe will be free of background

    noise and electromagnetic interference. Unfortunately, this is not realistic.

    However, sensors and preamplifiers are designed to help eliminate unwanted

    signals. First, the preamplifier boosts the voltage to provide gain and cabledrive capability. To minimize interference, a preamplifier is placed close to the

    transducer; in fact, many transducers today are equipped with integrated

    preamplifiers Next the signal is relayed to a bandpass filter for elimination of

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    preamplifiers. Next, the signal is relayed to a bandpass filter for elimination of

    low frequencies (common to background noise) and high frequencies.Following completion of this process, the signal travels to the acoustic system

    mainframe and eventually to a computer or similar device for analysis and

    storage. Depending on noise conditions, further filtering or amplification at the

    mainframe may still be necessary.

    Schematic Diagram of a Basic Four-channel Acoustic Emission Testing

    System

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    FIGURE 16.5 The main elements of a modern acoustic emission detection system.

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    After passing the AE system mainframe, the signal comes to a

    detection/measurement circuit as shown in the figure directly above. Note that

    multiple-measurement circuits can be used in multiple sensor/channel

    systems for source location purposes (to be described later). At themeasurement circuitry, the shape of the conditioned signal is compared with a

    threshold voltage value that has been programmed by the operator. Signals

    are either continuous (analogous to Gaussian random noise with amplitudes

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    are either continuous (analogous to Gaussian, random noise with amplitudes

    varying according to the magnitude of the AE events) or burst-type. Each time

    the threshold voltage is exceeded, the measurement circuit releases a digital

    pulse. The first pulse is used to signify the beginning of a hit. (A hit is used to

    describe the AE event that is detected by a particular sensor. One AE event

    ca