vibration
Case Report
Measurement and Analysis of Inadequate Friction Mechanisms
in Liquid-Buffered Mechanical Seals Utilizing Acoustic
Emission Technique
Manuel Medina-Arenas 1, Fabian Sopp 1,* , Johannes Stolle 1, Matthias Schley 1, RenéKamieth 2
and Florian Wassermann 3
Citation: Medina-Arenas, M.; Sopp,
F.; Stolle, J.; Schley, M.; Kamieth, R.;
Wassermann, F. Measurement and
Analysis of Inadequate Friction
Mechanisms in Liquid-Buffered
Mechanical Seals Utilizing Acoustic
Emission Technique. Vibration 2021,4,
263–283. https://doi.org/10.3390/
vibration4010018
Academic Editors: Pawel
H. Malinowski and Julian
Sierra Perez
Received: 14 January 2021
Accepted: 16 March 2021
Published: 18 March 2021
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4.0/).
1
Functional Division Engineering & Technical Expertise, BASF SE, Carl-Bosch-Straße 38, 67063 Ludwigshafen
[email protected] (M.S.)
2Chair of Engineering Design & Product Reliability, Institut für Maschinenkonstruktion und Systemtechnik,
3
Operating Division Intermediates, BASF SE, Carl-Bosch-Straße 38, 67063 Ludwigshafen am Rhein, Germany;
*Correspondence: [email protected]; Tel.: +49-621-60-40778
Abstract:
Mechanical seals play an important role in the reliability of a process. Currently, the condi-
tion monitoring of mechanical seals is restricted due to the limitations of the traditional monitoring
methods, including classical vibration analysis. For this reason, the objective of the present work
is the detection and analysis of friction mechanisms inside a mechanical seal that are unfavorable
and induce fault conditions using the acoustic emission technique, which allows the measurement of
high-frequency vibrations that arise due to material fatigue processes on a microscopic scale. For this
purpose, several fault condition modes were induced on a test rig of an agitator vessel system with a
double-acting mechanical seal and its buffer fluid system. It was possible to detect the presence of
inadequate friction mechanisms due to the absence and limited use of lubrication, as well as the pres-
ence of abrasive wear, by measuring a change in the properties of the acoustic emissions. Operation
under fault condition modes was analyzed using the acoustic emission technique before an increase
in the leakage rate was evaluated using traditional monitoring methods. The high friction due to the
deficient lubrication was characterized by a pattern in the high-frequency range that consisted of the
harmonics of a fundamental frequency of about 33 kHz. These results demonstrate the feasibility of a
condition monitoring system for mechanical seals using the acoustic emission technique.
Keywords:
mechanical seal; acoustic emissions; friction mechanism; high frequency; condition
monitoring
1. Introduction
1.1. Research Goals
Rotating equipment plays an important role for many applications in the process
industry because its functionality is crucial for the productivity and safety of plants and,
thus, business success. The components of each piece of equipment must be highly
reliable in order to reduce downtime costs. Even more challenging is the avoidance of
unplanned plant shutdowns resulting from equipment failure, especially failure of single
key components. One such key component is the mechanical seal often used as shaft
sealing in process machinery applications such as in agitator vessel systems [1].
There are several useful measurement techniques, whereas the following are the most
promising possibilities:
•classical vibration analysis;
•thermal imaging;
Vibration 2021,4, 263–283. https://doi.org/10.3390/vibration4010018 https://www.mdpi.com/journal/vibration
Vibration 2021,4264
•acoustic measurements;
•the acoustic emission technique.
Currently, condition monitoring and the early detection of damage to rotating equip-
ment are primarily based on classical vibration analysis according to DIN ISO 10816 [
2
].
This standard prescribes a measuring range of 10–1000 Hz, within which the RMS (root
mean square) value of the vibration velocity is determined. For this scalar value, specifi-
cations are given regarding the maximum acceptable values. In addition, there are also
analysis methods, such as spectral and envelope analysis, in which vibrations of up to
approximately 15 kHz are typically included. This enables the drawing of conclusions
on untypical mechanical behavior by correlating these conspicuous frequencies with the
dominant rotation frequency (e.g., rolling element bearing frequencies). This shows the lim-
itations of classical vibration analysis, which relies on distinct kinematics and comparably
high rotational speeds or undesirable long acquisition times.
In some applications, thermal imaging is used to detect damages and faulty behav-
ior. For the presented case of mechanical seals in a heated environment, the technique
cannot be employed reliably, as not only parts are impacted by friction heat up, but also
their surroundings. For precise measurements in this context, another technique may
be preferred.
Acoustic measurements can be used for vibration measurement. Microphones pick
up sound vibrations that are emitted by the machinery. It is possible to measure high
frequencies, but inevitable noise from the environment has to be filtered out. This leads to
an approach that measures the relevant vibrations more closely to their source.
When microscopic phenomena are dominant and vibration emissions are significantly
determined by material characteristics that are also independent of the shaft rotational
speed [
3
], high-frequency vibrations are the result. One promising approach for detecting
and analyzing such phenomena is known as the acoustic emission technique (AET). How-
ever, the costs and the necessary resource intensity of this application are higher than other
approaches [4].
The goal of this paper is to present an approach of using the AET for the monitoring
of mechanical seals in process industry.
1.2. Basics of Mechanical Seals
Mechanical seals are widely used in process engineering [
1
]. They serve as a barrier
to prevent the escape of fluid from inside a vessel to the surrounding environment by
obstructing the passageway between the machine housing and the rotating shaft. In most
cases within the process industry, this represents a safety-relevant feature [
5
]. Moreover,
premature mechanical seal failure can lead to high follow-up costs and irreparable damage
to the machine or plant or even endanger people and the environment [
1
]. Fault-free
operation of the mechanical seal must be ensured as unplanned shutdowns usually result
in higher maintenance costs than regular maintenance downtimes. Appropriate monitoring
methods provide continuous information on the condition of the mechanical seal. Thus,
unplanned maintenance activities can be prevented and an extension of the time intervals
between regular services can be achieved [5].
Mechanical seals generally consist of two major components: a rotating seal ring
attached to the shaft and a stationary seal ring inserted into the seal housing. Both rings
are aligned to each other so that their end faces meet. The resulting hollow cylinder space
between the two rings is called the sealing gap. To fulfill the function of the mechanical seals,
the following additional elements are required: secondary seals, springs and components
for transmitting the torque of the shaft. The use of one or two pairs of seal rings in a
mechanical seal depends on its application. These types of seals are called single or double-
acting mechanical seals respectively. In Figure 1, the two main components are highlighted
by color and the additional elements are schematically depicted.
Vibration 2021,4265
Vibration 2021, 4 FOR PEER REVIEW 3
or double-acting mechanical seals respectively. In Figure 1, the two main components are
highlighted by color and the additional elements are schematically depicted.
Figure 1. Schematic illustration of the main components of an exemplary mechanical seal. The rotating sealing unit is
marked purple and the stationary sealing unit is marked green.
One common version is the liquid-buffered mechanical seal, which entails a barrier
fluid system as another important component. This dissipates the heat generated by
frictional processes within the sealing gap and lubricates the faces of the seal rings to
hinder them from touching each other. Thus, the barrier fluid functions as a coolant and
lubricant of the mechanical seal. The circulation of the barrier fluid through the
mechanical seal is normally performed by a circulation pump or by the thermosyphon
principle. The latter is defined as the natural circulation of a liquid in a closed circuit due
to temperature-driven density differences. It is physically impossible to ensure operation
without leakage, as the barrier fluid provides the barrier needed to keep the seal rings
separated and to prevent the escape of the fluid to be sealed to the surroundings. Thus,
the leakage rate must always be kept as low as possible. To ensure that the permissible
leakage rate is as low as possible, the seal ring faces are subjected to a lapping process and
the sealing gap is designed to be very small by choosing the pretensioning of both rings
with respect to the rotational speed, seal ring materials and seal ring diameter. Mechanical
seals also comprise a drain hole in the housing, where an inadmissible increase of the
leakage rate can be determined by visually detecting the presence of barrier fluid there.
The frictional behavior inside the sealing gap is depicted in Figure 2 as a function of the
relative velocity between the seal rings (sliding velocity), the applied load and the
dynamic viscosity of the barrier-fluid. For liquid-buffered mechanical seals, three
lubrication states can occur: boundary (BL), mixed (ML) or hydrodynamic (HL) lubrication.
The progress between these states is represented by the Stribeck curve [6]. The lubricating
film thickness in ML corresponds approximately to the average roughness of the two
friction partners and represents the best compromise in terms of wear and leakage.
However, operation in ML depends significantly on the operation conditions. If high loads
or low speeds are present, the seal ring surfaces are not completely separated and high wear
is expected due to the increased interaction between the asperities of the surfaces at a
microscopic level. On the other hand, if low loads and high speeds occur, the lubricating
film thickness exceeds the surface roughness and the leakage rate increases significantly.
The transition from BL to an unlubricated condition (also called dry running) is marked by
a drastic increase in wear rate [6].
Figure 1.
Schematic illustration of the main components of an exemplary mechanical seal. The rotating sealing unit is
marked purple and the stationary sealing unit is marked green.
One common version is the liquid-buffered mechanical seal, which entails a barrier
fluid system as another important component. This dissipates the heat generated by
frictional processes within the sealing gap and lubricates the faces of the seal rings to
hinder them from touching each other. Thus, the barrier fluid functions as a coolant and
lubricant of the mechanical seal. The circulation of the barrier fluid through the mechanical
seal is normally performed by a circulation pump or by the thermosyphon principle. The
latter is defined as the natural circulation of a liquid in a closed circuit due to temperature-
driven density differences. It is physically impossible to ensure operation without leakage,
as the barrier fluid provides the barrier needed to keep the seal rings separated and to
prevent the escape of the fluid to be sealed to the surroundings. Thus, the leakage rate
must always be kept as low as possible. To ensure that the permissible leakage rate is
as low as possible, the seal ring faces are subjected to a lapping process and the sealing
gap is designed to be very small by choosing the pretensioning of both rings with respect
to the rotational speed, seal ring materials and seal ring diameter. Mechanical seals also
comprise a drain hole in the housing, where an inadmissible increase of the leakage rate
can be determined by visually detecting the presence of barrier fluid there. The frictional
behavior inside the sealing gap is depicted in Figure 2as a function of the relative velocity
between the seal rings (sliding velocity), the applied load and the dynamic viscosity of
the barrier-fluid. For liquid-buffered mechanical seals, three lubrication states can occur:
boundary (BL), mixed (ML) or hydrodynamic (HL) lubrication. The progress between
these states is represented by the Stribeck curve [
6
]. The lubricating film thickness in
ML corresponds approximately to the average roughness of the two friction partners and
represents the best compromise in terms of wear and leakage. However, operation in ML
depends significantly on the operation conditions. If high loads or low speeds are present,
the seal ring surfaces are not completely separated and high wear is expected due to the
increased interaction between the asperities of the surfaces at a microscopic level. On the
other hand, if low loads and high speeds occur, the lubricating film thickness exceeds the
surface roughness and the leakage rate increases significantly. The transition from BL to an
unlubricated condition (also called dry running) is marked by a drastic increase in wear
rate [6].
Vibration 2021,4266
Vibration 2021, 4 FOR PEER REVIEW 4
Figure 2. Stribeck curve, according to [6].
If the operation conditions do not match the specific conditions for which the
mechanical seal was intended, the seal may experience partial damage or total failure. For
example, the mechanical seal experiences unstable conditions at start-up and shutdown
as well as when problems in the barrier fluid system occur. For this reason, one of the
most common causes of damage to mechanical seals is inappropriate lubrication.
Towsyfyan [7] gathered the results of a survey about the reasons for mechanical seal
failures in centrifugal pumps and found that dry running (in almost 25% of all cases) and
abrasive wear (in approximately 16% of all cases) were the main factors that lead to failure.
This information coincides with the long-term data collected by practical experience
within the BASF SE community in the area of process machinery and maintenance,
specifically in the Rotating Equipment department.
Without a change of the system’s operating conditions, violent fluctuations of the
leakage rate are indications of malfunctions in the performance of or even damage to the
mechanical seal [8]. The presence of an inadmissibly high leakage rate may indicate a
complete failure of the mechanical seals and therefore it must be replaced. Most
mechanical seal damage is due to inadmissible friction between the seal rings. Given that
the quality of the lubrication in the sealing gap is associated with a higher generation of
friction between the seal rings, unfavorable lubrication conditions can lead to seal damage
[7]. These friction mechanisms can be associated with acoustic emissions (AE) [9].
The mechanical seal itself is a tribological system, in which the energy released is
mainly converted into heat and (only to a lesser extent) into AE [9]. The characteristic
frequency of the excited vibrations in a tribological system is determined only by the
natural frequency of the integral system and not by the vibration characteristic of each
subcomponent. The intensity of the AE emitted due to the friction process is influenced
by the composition of the materials, the roughness of the surface and the speed of the
relative motion. Nonetheless, the frequency of the excited vibrations remains dependent
on the rigidity of the tribological system [4]. When observed on a microscopic level, the
collisions between the surface irregularities of the seal ring faces, which are spread over
the entire contact surface, excite the natural frequencies of the individual asperities. The
frequency ranges excited here depend on the properties of the individual asperities, such
as height, width, cross-sectional area and modulus of elasticity of the material [9]. As hard
material particles can cause abrasive wear on the surface of softer seal ring materials and
thus lead to the formation of microcracks and spalling on the surface of both seal rings
[10], potential abrasive particles inside the sealing gap must be conveyed away by the
barrier fluid flow and filtered in the barrier fluid system. This helps to avoid additional
damage to the sealing components caused by particle erosion.
Figure 2. Stribeck curve, according to [6].
If the operation conditions do not match the specific conditions for which the me-
chanical seal was intended, the seal may experience partial damage or total failure. For
example, the mechanical seal experiences unstable conditions at start-up and shutdown as
well as when problems in the barrier fluid system occur. For this reason, one of the most
common causes of damage to mechanical seals is inappropriate lubrication. Towsyfyan [
7
]
gathered the results of a survey about the reasons for mechanical seal failures in centrifugal
pumps and found that dry running (in almost 25% of all cases) and abrasive wear (in
approximately 16% of all cases) were the main factors that lead to failure. This information
coincides with the long-term data collected by practical experience within the BASF SE
community in the area of process machinery and maintenance, specifically in the Rotating
Equipment department.
Without a change of the system’s operating conditions, violent fluctuations of the
leakage rate are indications of malfunctions in the performance of or even damage to the
mechanical seal [
8
]. The presence of an inadmissibly high leakage rate may indicate a
complete failure of the mechanical seals and therefore it must be replaced. Most mechanical
seal damage is due to inadmissible friction between the seal rings. Given that the quality of
the lubrication in the sealing gap is associated with a higher generation of friction between
the seal rings, unfavorable lubrication conditions can lead to seal damage [
7
]. These friction
mechanisms can be associated with acoustic emissions (AE) [9].
The mechanical seal itself is a tribological system, in which the energy released is
mainly converted into heat and (only to a lesser extent) into AE [
9
]. The characteristic
frequency of the excited vibrations in a tribological system is determined only by the
natural frequency of the integral system and not by the vibration characteristic of each
subcomponent. The intensity of the AE emitted due to the friction process is influenced
by the composition of the materials, the roughness of the surface and the speed of the
relative motion. Nonetheless, the frequency of the excited vibrations remains dependent
on the rigidity of the tribological system [
4
]. When observed on a microscopic level, the
collisions between the surface irregularities of the seal ring faces, which are spread over
the entire contact surface, excite the natural frequencies of the individual asperities. The
frequency ranges excited here depend on the properties of the individual asperities, such
as height, width, cross-sectional area and modulus of elasticity of the material [
9
]. As hard
material particles can cause abrasive wear on the surface of softer seal ring materials and
thus lead to the formation of microcracks and spalling on the surface of both seal rings [
10
],
Vibration 2021,4267
potential abrasive particles inside the sealing gap must be conveyed away by the barrier
fluid flow and filtered in the barrier fluid system. This helps to avoid additional damage to
the sealing components caused by particle erosion.
1.3. Preceding Research in Wear Detection Relating to Mechanical Seals
Zou and Green [
11
] were able to successfully detect unwanted contact between two
seal ring faces in real time using eddy current proximity probes. Anderson et al. [
12
]
suggested a monitoring system that could be applied retroactively to field operation to
detect the contact of two seal ring faces and measure its severity. This method was based
on the detection of actively generated ultrasonic transverse waves reflected from the faces
of the seal rings.
Miettinen and Siekkinen [
13
] were able to detect a change in the RMS value of the AE
signals between normal running, leakage and dry running conditions of a double-acting
mechanical seal applied on a centrifugal pump. Mba et al. [
14
] successfully assessed the
applicability of the AE measurement to detect the onset and duration of contact between
the seal rings. Moreover, Towsyfyan [
7
] studied the response of the AE signals to changes
in the lubrication states due to changes in the operation conditions. They reported the
possibility of identifying the states using a combination of RMS and kurtosis values of the
AE signals. In addition, they suggested that the direct interaction of asperities generates
high-frequency AE signals (between 50 and 300 kHz). Furthermore, the influence of the
rotational speed of the shaft and the barrier fluid system pressures on the vibrational
behavior of mechanical seals was investigated. They found that, at low rotational speeds,
AE amplitude values are higher with increasing seal pressures due to greater friction
between the seal ring faces. Hase et al. [
10
] summarized the result of different literature into
an overview of the frequency spectra of wear-emitted AE. Significant differences between
the investigations appear to be dependent on the utilized type of sensor, measuring system
and the experimental conditions. According to Hase et al. [
10
], a dependence between the
distribution of the AE frequencies and the type of wear can be found. Almeida et al. [
15
]
analyzed the damage process of a ceramic matrix composite during fatigue and found
that the AE measurements provide information about the severity, type and onset of the
damage. Ferrer et al. [
16
] investigated the AE that originated due to slip events resulting
from contact between the surface asperities. Chung et al. [
17
] investigated a method based
on AE measurements for monitoring the wear caused by hard particles that slide between
two surfaces. The frequency spectra show excitation of the frequencies between about
100 and 400 kHz with a large peak at 200 kHz. According to Chung et al. [
17
], noise
emissions result from rolling and from the collision of the abrasive particles between
the sliding surfaces. Ramadan et al. [
18
] characterized the frequency spectra of the AE
generated by crack growth and propagation and breakage in high-strength steel. The
growth and propagation of cracks were characterized by a frequency range of 100 to
600 kHz with a large peak at 200 kHz.
Based on the above-mentioned studies, this work describes a novel approach for
monitoring failure modes due to inadequate friction processes inside mechanical seals
using the AET. For this purpose, typical failure condition modes (namely dry running,
insertion of abrasive particles into the buffer fluid flow and a total failure in the buffer fluid
system) of a double-acting mechanical seal mounted on a test agitator vessel system were
induced. The emitted AE were simultaneously recorded and analyzed. It was possible to
detect unfavorable friction processes due to the aforementioned failure modes at an early
stage. Indicators for premature failure of the utilized mechanical seal were found.
2. Acoustic Emission Technique
The acoustic emission technique (AET) is a non-destructive testing method for the
measurement and assessment of high-frequency vibrations in the range of 0.2 MHz to
2 MHz. Scruby et al. [
19
] define acoustic emission (AE) as a “spontaneous release of a
structure-borne transient wave in a solid as a consequence of a sudden local stress change”.
Vibration 2021,4268
This local change in the stress energy can occur as a result of damage, such as cracks or
plastic deformation. Any physical event that causes an AE is addressed as an AE event,
whereas an AE source is defined as the spatial element from which one or more AE events
arise. The transient wave propagates through the solid and on the surface in all directions
depending only on the component geometry and material characteristics. An AE exceeding
a certain amount of energy can be detected by an AE sensor whose measuring method is
based on the piezoelectric effect. A detected transient wave is usually referred to as a hit. A
single AE event may result in multiple hits [
19
]. The formation, propagation and detection
of AE are illustrated in Figure 3. In this work, the AE activity is defined as the occurrence
of AE events exceeding the minimum detectable amount of energy specified by the utilized
AE sensor. Thus, a high AE activity means that many hits have been detected in a short
amount of time.
Vibration 2021, 4 FOR PEER REVIEW 6
event, whereas an AE source is defined as the spatial element from which one or more AE
events arise. The transient wave propagates through the solid and on the surface in all
directions depending only on the component geometry and material characteristics. An
AE exceeding a certain amount of energy can be detected by an AE sensor whose
measuring method is based on the piezoelectric effect. A detected transient wave is
usually referred to as a hit. A single AE event may result in multiple hits [19]. The
formation, propagation and detection of AE are illustrated in Figure 3. In this work, the
AE activity is defined as the occurrence of AE events exceeding the minimum detectable
amount of energy specified by the utilized AE sensor. Thus, a high AE activity means that
many hits have been detected in a short amount of time.
Figure 3. Principles of AE formation, propagation and detection.
To prevent the recording of disturbing background noises, a threshold filter is typically
used whereby only AE with higher amplitudes are recorded. The threshold can be user-
adjustable, fixed or automatically adjustable. The recording of the signal starts when the
amplitude of a hit exceeds the threshold level and ends when it falls below the threshold
again. The waveform is then used to determine the so-called AE parameters (see Figure 4),
such as the maximum amplitude or the hit duration. Utilizing a fast Fourier
transformation (FFT), the spectrum of the signal can be determined, which can then be
used to create additional parameters including the peak or median frequency; these are
known as transient parameters (TR parameters) [20]. In non-destructive testing, different
damage generation mechanisms can be distinguished using these parameter sets. The
amplitudes of the AE signals are given in decibel AE (dB
AE
) with a reference voltage of 1
µV [21]. Figure 4 shows a summary of the signal processing of AE measurements.
Figure 4. Schematic representation of the signal processing according to [20].
3. Experimental Setup
The test rig consists of an agitator vessel system with a double-acting liquid-buffered
mechanical seal. The agitator vessel is equipped with a tubular baffle. To vary the shaft
Figure 3. Principles of AE formation, propagation and detection.
To prevent the recording of disturbing background noises, a threshold filter is typ-
ically used whereby only AE with higher amplitudes are recorded. The threshold can
be user-adjustable, fixed or automatically adjustable. The recording of the signal starts
when the amplitude of a hit exceeds the threshold level and ends when it falls below the
threshold again. The waveform is then used to determine the so-called AE parameters
(see Figure 4), such as the maximum amplitude or the hit duration. Utilizing a fast Fourier
transformation (FFT), the spectrum of the signal can be determined, which can then be
used to create additional parameters including the peak or median frequency; these are
known as transient parameters (TR parameters) [
20
]. In non-destructive testing, different
damage generation mechanisms can be distinguished using these parameter sets. The
amplitudes of the AE signals are given in decibel AE (dB
AE
) with a reference voltage of
1µV [21]. Figure 4shows a summary of the signal processing of AE measurements.
Vibration 2021, 4 FOR PEER REVIEW 6
event, whereas an AE source is defined as the spatial element from which one or more AE
events arise. The transient wave propagates through the solid and on the surface in all
directions depending only on the component geometry and material characteristics. An
AE exceeding a certain amount of energy can be detected by an AE sensor whose
measuring method is based on the piezoelectric effect. A detected transient wave is
usually referred to as a hit. A single AE event may result in multiple hits [19]. The
formation, propagation and detection of AE are illustrated in Figure 3. In this work, the
AE activity is defined as the occurrence of AE events exceeding the minimum detectable
amount of energy specified by the utilized AE sensor. Thus, a high AE activity means that
many hits have been detected in a short amount of time.
Figure 3. Principles of AE formation, propagation and detection.
To prevent the recording of disturbing background noises, a threshold filter is typically
used whereby only AE with higher amplitudes are recorded. The threshold can be user-
adjustable, fixed or automatically adjustable. The recording of the signal starts when the
amplitude of a hit exceeds the threshold level and ends when it falls below the threshold
again. The waveform is then used to determine the so-called AE parameters (see Figure 4),
such as the maximum amplitude or the hit duration. Utilizing a fast Fourier
transformation (FFT), the spectrum of the signal can be determined, which can then be
used to create additional parameters including the peak or median frequency; these are
known as transient parameters (TR parameters) [20]. In non-destructive testing, different
damage generation mechanisms can be distinguished using these parameter sets. The
amplitudes of the AE signals are given in decibel AE (dB
AE
) with a reference voltage of 1
µV [21]. Figure 4 shows a summary of the signal processing of AE measurements.
Figure 4. Schematic representation of the signal processing according to [20].
3. Experimental Setup
The test rig consists of an agitator vessel system with a double-acting liquid-buffered
mechanical seal. The agitator vessel is equipped with a tubular baffle. To vary the shaft
Figure 4. Schematic representation of the signal processing according to [20].
Vibration 2021,4269
3. Experimental Setup
The test rig consists of an agitator vessel system with a double-acting liquid-buffered
mechanical seal. The agitator vessel is equipped with a tubular baffle. To vary the shaft
speed, the electric motor is controlled by a variable frequency drive with a sinusoidal filter
and shielded cables to attenuate noise interference. The components of the agitator vessel
system and their specifications are summarized in Table 1.
Table 1. Components of the agitator vessel system and their attributes.
Feature Description
Vessel storage capacity 500 L
Vessel height 1450 mm
Vessel inner diameter 786 mm
Shaft diameter 50 mm
Agitator bearings 2×SKF 6309-2Z
Agitator type 3-blade propeller
Gear manufacturer Lenze (Hameln, Germany), type 12.410.10.1.0
Gear ratio 3.15
Motor manufacturer ATB (Nordenham, Germany), type: CD112M-4 Y2
Motor output power 4 kW
Motor nominal speed 1460 rpm
Belt drive pulley ratio 0.76
Furthermore, the mechanical seal of the agitator vessel system was equipped with a
thermosyphon-type barrier fluid system. Additionally, a pressurized vessel with variable
pressure between 0 and 10 bar was installed. White mineral oil and demineralized water
were used as barrier fluids. Figure 5shows the agitator vessel system assembly and
Figure 6the barrier fluid system.
Vibration 2021, 4 FOR PEER REVIEW 7
speed, the electric motor is controlled by a variable frequency drive with a sinusoidal filter
and shielded cables to attenuate noise interference. The components of the agitator vessel
system and their specifications are summarized in Table 1.
Table 1. Components of the agitator vessel system and their attributes.
Feature Description
Vessel storage capacity 500 L
Vessel height 1450 mm
Vessel inner diameter 786 mm
Shaft diameter 50 mm
Agitator bearings 2× SKF 6309-2Z
Agitator type 3-blade propeller
Gear manufacturer Lenze (Hameln, Germany), type 12.410.10.1.0
Gear ratio 3.15
Motor manufacturer ATB (Nordenham, Germany), type: CD112M-4
Y2
Motor output power 4 kW
Motor nominal speed 1460 rpm
Belt drive pulley ratio 0.76
Furthermore, the mechanical seal of the agitator vessel system was equipped with a
thermosyphon-type barrier fluid system. Additionally, a pressurized vessel with variable
pressure between 0 and 10 bar was installed. White mineral oil and demineralized water
were used as barrier fluids. Figure 5 shows the agitator vessel system assembly and Figure 6
the barrier fluid system.
Figure 5. Test rig showing the agitator vessel system and the components of the drive unit.
Figure 5. Test rig showing the agitator vessel system and the components of the drive unit.
Vibration 2021,4270
Vibration 2021, 4 FOR PEER REVIEW 8
Figure 6. Thermosyphon-type barrier fluid system with pressurized vessel.
Two double-acting mechanical seals in back-to-back arrangement with a hard/soft
seal ring pairing (designation: Cartex-DN/60-00) from EagleBurgmann were tested
consecutively in this work. The soft seal ring material consists of resin-impregnated
carbon graphite while a non-pressure sintered silicon carbide was used for the hard seal
ring material. The temperature was measured in a borehole located in the mechanical
seal’s housing near the upper seal ring pair.
The emitted AE were measured, processed and visualized with the acoustic emission
device AMSY-6 (Acoustic Measurement System 6th generation) from Vallen Systeme
GmbH. The AMSY-6 is a well-accepted measuring system in the field of non-destructive
testing and material science and is frequently used in scientific publications [15,16,22].
In this work, the “continuous mode” of the AMSY-6 was used. First, a threshold is
defined based on the results of previous experiments. If this threshold is exceeded, the
recording of the time signal begins and ends after a previously selected measurement
period. Consecutive measurements are recorded as long as the threshold is being
exceeded. In this work, the measurement period was set to 1000 µs, as this corresponds
approximately to the duration of the longer expected burst signals. From each one of these
measurements, some parameters of the time signal and frequency spectra are derived and
stored in the AMSY-6. In the present work, the maximum amplitude value and the
frequency spectrum of the measured AE were considered.
The WD sensor from the physical acoustics corporation (PAC) with an operating
frequency range from 125 kHz to 1 MHz was employed in a radial position to obtain the
AE signals. These were amplified by 34 dB
AE
with the AEP3N preamplifier from Vallen
Systeme GmbH. The sampling frequency was 2.5 MHz and the maximum number of
samples per set was 262.144. The Vallen VisualAE software from Vallen Systeme GmbH
was used to visualize the data. The Korasilon Paste M-S 2-200 from Kurt Obermeier
GmbH (Bad Berleburg, Germany) was used as a coupling agent for the sensor. For test rig
monitoring purposes, one additional AE sensor and one sensor from the classical
vibration analyses, which can be seen in Figure 7. AMSY-6 measuring system setup on the
double-acting mechanical seal, were also installed. The experimental setup is shown in
Figure 7.
Figure 6. Thermosyphon-type barrier fluid system with pressurized vessel.
Two double-acting mechanical seals in back-to-back arrangement with a hard/soft
seal ring pairing (designation: Cartex-DN/60-00) from EagleBurgmann were tested con-
secutively in this work. The soft seal ring material consists of resin-impregnated carbon
graphite while a non-pressure sintered silicon carbide was used for the hard seal ring
material. The temperature was measured in a borehole located in the mechanical seal’s
housing near the upper seal ring pair.
The emitted AE were measured, processed and visualized with the acoustic emission
device AMSY-6 (Acoustic Measurement System 6th generation) from Vallen Systeme GmbH.
The AMSY-6 is a well-accepted measuring system in the field of non-destructive testing
and material science and is frequently used in scientific publications [15,16,22].
In this work, the “continuous mode” of the AMSY-6 was used. First, a threshold is
defined based on the results of previous experiments. If this threshold is exceeded, the
recording of the time signal begins and ends after a previously selected measurement
period. Consecutive measurements are recorded as long as the threshold is being exceeded.
In this work, the measurement period was set to 1000
µ
s, as this corresponds approximately
to the duration of the longer expected burst signals. From each one of these measurements,
some parameters of the time signal and frequency spectra are derived and stored in the
AMSY-6. In the present work, the maximum amplitude value and the frequency spectrum
of the measured AE were considered.
The WD sensor from the physical acoustics corporation (PAC) with an operating
frequency range from 125 kHz to 1 MHz was employed in a radial position to obtain
the AE signals. These were amplified by 34 dB
AE
with the AEP3N preamplifier from
Vallen Systeme GmbH. The sampling frequency was 2.5 MHz and the maximum number of
samples per set was 262.144. The Vallen VisualAE software from Vallen Systeme GmbH was
used to visualize the data. The Korasilon Paste M-S 2-200 from Kurt Obermeier GmbH (Bad
Vibration 2021,4271
Berleburg, Germany) was used as a coupling agent for the sensor. For test rig monitoring
purposes, one additional AE sensor and one sensor from the classical vibration analyses,
which can be seen in Figure 7. AMSY-6 measuring system setup on the double-acting
mechanical seal, were also installed. The experimental setup is shown in Figure 7.
Vibration 2021, 4 FOR PEER REVIEW 9
Figure 7. AMSY-6 measuring system setup on the double-acting mechanical seal.
4. Experimental Procedure
In order to develop indicators for the early detection of increased leakage in
mechanical seals, various fault condition modes were induced in the barrier fluid system
to investigate their influence on the seals’ vibrational behavior. These are typical fault
conditions that can occur during the operation of an agitator vessel system. The agitator
speed was set to 615 rpm in all experiments. For the measurement of the AE signals in the
AMSY-6, the threshold was adjusted manually for each experiment in accordance with
previously collected experimental data. For the first two measurements, the selected
threshold was 60 dB
AE
and for the last two measurements it was 45 dB
AE
. The experimental
procedure was as follows:
• Measurement 1: Operation under normal conditions of the barrier fluid system with
white oil serving as barrier fluid. No fault condition modes were induced.
• Measurement 2: Dry-running operation of the mechanical seal. In order to investigate
the vibrational behavior of the mechanical seal without lubrication, the barrier fluid
system was emptied. Thus, the seal operated without barrier fluid.
• Measurement 3: Abrasive particles. As high abrasive friction is associated with the
onset of cracks, microscopic corundum particles were added to the barrier fluid
system in order to investigate their influence on the seals’ vibrations. The
agglomeration of the abrasive particles inside the barrier fluid system prevents them
arriving at the mechanical seal. To avoid this, demineralized water was used as the
barrier fluid because these particles tend to agglomerate in high-viscosity liquids
rather than in low-viscosity ones.
• Measurement 4: Cooling failure. High temperatures in the sealing gap can lead to a
partial or total evaporation of the barrier fluid, thus causing seal operation under BL
conditions. As BL is associated with high wear, a cooling failure in the mechanical
seal could lead to a high increase in the leakage rate. After reaching a steady-state
temperature in the mechanical seal, the supply of barrier fluid in the seal was
completely interrupted. The previously introduced corundum particles were not
removed to ensure an accelerated wear process.
5. Results
5.1. Normal Operation
The results of the first experiment with normal operating conditions of the barrier
fluid system are represented in Figure 8. Whenever the amplitude of the signal exceeds
Figure 7. AMSY-6 measuring system setup on the double-acting mechanical seal.
4. Experimental Procedure
In order to develop indicators for the early detection of increased leakage in mechanical
seals, various fault condition modes were induced in the barrier fluid system to investigate
their influence on the seals’ vibrational behavior. These are typical fault conditions that
can occur during the operation of an agitator vessel system. The agitator speed was set
to 615 rpm in all experiments. For the measurement of the AE signals in the AMSY-6,
the threshold was adjusted manually for each experiment in accordance with previously
collected experimental data. For the first two measurements, the selected threshold was
60 dB
AE
and for the last two measurements it was 45 dB
AE
. The experimental procedure
was as follows:
•
Measurement 1: Operation under normal conditions of the barrier fluid system with
white oil serving as barrier fluid. No fault condition modes were induced.
•
Measurement 2: Dry-running operation of the mechanical seal. In order to investigate
the vibrational behavior of the mechanical seal without lubrication, the barrier fluid
system was emptied. Thus, the seal operated without barrier fluid.
•
Measurement 3: Abrasive particles. As high abrasive friction is associated with the
onset of cracks, microscopic corundum particles were added to the barrier fluid system
in order to investigate their influence on the seals’ vibrations. The agglomeration of
the abrasive particles inside the barrier fluid system prevents them arriving at the
mechanical seal. To avoid this, demineralized water was used as the barrier fluid
because these particles tend to agglomerate in high-viscosity liquids rather than in
low-viscosity ones.
•
Measurement 4: Cooling failure. High temperatures in the sealing gap can lead
to a partial or total evaporation of the barrier fluid, thus causing seal operation
under BL conditions. As BL is associated with high wear, a cooling failure in the
mechanical seal could lead to a high increase in the leakage rate. After reaching a
steady-state temperature in the mechanical seal, the supply of barrier fluid in the seal
Vibration 2021,4272
was completely interrupted. The previously introduced corundum particles were not
removed to ensure an accelerated wear process.
5. Results
5.1. Normal Operation
The results of the first experiment with normal operating conditions of the barrier
fluid system are represented in Figure 8. Whenever the amplitude of the signal exceeds the
previously set threshold, a time signal with a duration of 1000
µ
s is measured and then its
frequency spectrum is calculated. The highest amplitude during the 1000
µ
s timespan of
each signal is represented in Figure 8with a green dot. This is called a hit. The y-axis on
the left-hand side is associated with the amplitudes of the hits. In this case, a band with a
higher distribution density of hits can be distinguished after 6000 s with amplitude values
under 65 dB
AE
. With the Vallen VisualAE software, the associated information of each hit
(e.g., its respective time signal and frequency spectrum) can be visualized. The red line
describes the temperature progression over time of the mechanical seal’s housing and is
represented in the right y-axis.
Vibration 2021, 4 FOR PEER REVIEW 10
the previously set threshold, a time signal with a duration of 1000 µs is measured and
then its frequency spectrum is calculated. The highest amplitude during the 1000 µs
timespan of each signal is represented in Figure 8 with a green dot. This is called a hit. The
y-axis on the left-hand side is associated with the amplitudes of the hits. In this case, a
band with a higher distribution density of hits can be distinguished after 6000 s with
amplitude values under 65 dB
AE
. With the Vallen VisualAE software, the associated
information of each hit (e.g., its respective time signal and frequency spectrum) can be
visualized. The red line describes the temperature progression over time of the mechanical
seal’s housing and is represented in the right y-axis.
Figure 8. Amplitude values of the hits over time during agitator vessel system operation under normal conditions of the
barrier fluid system.
5.2. Dry-Running Operation
The barrier fluid system was emptied to initiate dry-running operation. The results
are shown in Figure 9. During the first 6000 s of the experiment, no noticeable change in
AE was apparent although no barrier fluid was present in the pressurized vessel of the
barrier fluid system. This is probably due to the remaining barrier fluid in the sealing gap,
most likely between the asperities of the seal ring faces. Subsequently, an increase of the
hits exceeding the threshold can be observed. This can be assigned as the real start of dry-
running operation. The calculated frequency spectra of the hits recorded during dry
running showed the presence of the harmonics of a 33 kHz frequency. This behavior was
identical for each measurement. During dry-running operation, there was a strong
increase in AE intensity, causing the system to exceed its measurement range. As a result,
the maximum amplitudes could not be detected. However, a level increase of at least 35
dB
AE
compared to normal operation was found, which corresponds to an increase of the
linear amplitude by a factor of 56.
After approximately 30 min of dry-running operation, the measurement was paused
and the mechanical seal was filled with barrier fluid to verify whether the leakage rate
had increased. When the seal barrier fluid system was reestablished, the vibrational
behavior of the seal showed no deviations in comparison to normal operation. After 11
days of repeating the same procedure, a higher leakage rate was detected and the seal was
replaced.
Figure 8.
Amplitude values of the hits over time during agitator vessel system operation under normal conditions of the
barrier fluid system.
5.2. Dry-Running Operation
The barrier fluid system was emptied to initiate dry-running operation. The results
are shown in Figure 9. During the first 6000 s of the experiment, no noticeable change in
AE was apparent although no barrier fluid was present in the pressurized vessel of the
barrier fluid system. This is probably due to the remaining barrier fluid in the sealing
gap, most likely between the asperities of the seal ring faces. Subsequently, an increase
of the hits exceeding the threshold can be observed. This can be assigned as the real start
of dry-running operation. The calculated frequency spectra of the hits recorded during
dry running showed the presence of the harmonics of a 33 kHz frequency. This behavior
was identical for each measurement. During dry-running operation, there was a strong
increase in AE intensity, causing the system to exceed its measurement range. As a result,
the maximum amplitudes could not be detected. However, a level increase of at least
35 dB
AE
compared to normal operation was found, which corresponds to an increase of
the linear amplitude by a factor of 56.
Vibration 2021,4273
Vibration 2021, 4 FOR PEER REVIEW 11
Figure 9. Amplitude values of the hits over time and the frequency spectrum of a selected hit during dry-running operation
of the agitator vessel system.
5.3. Abrasive Particles
As addressed in the Introduction, abrasive particles can cause wear in the sealing
gap, especially on the surface of the seal ring made of carbon graphite. This can lead to
the formation of microcracks on the surface of the carbon graphite and spalling on the
surface of both sliding materials. Here, the continuous flow of the barrier fluid through
the mechanical seal plays an important role, since this is the only way to guarantee the
supply of particles to the sealing gap and, consequently, induce abrasive wear. The
friction heat generated in the sealing gap is transferred to the barrier fluid, which activates
the thermosyphon principle in the barrier fluid system. Due to their sedimentation
tendency, the corundum particles were occasionally manually stirred in the pressurized
vessel of the barrier fluid system during the experiments in order to bring the sedimented
particles back in motion. A lower threshold was set to allow a better understanding of the
vibrational behavior of the mechanical seal under this fault condition mode.
The results are shown in Figure 10. A more unstable vibrational behavior can be
observed, as the measured hits exhibited amplitude values between 45 and 87.5 dB
AE
, the
latter being the maximum amplitude detected during the experiment. A band with a
higher distribution density of hits can be distinguished between 45 and approximately 50
dB
AE
; this can be defined as the background noise of the measurement. The hits with
amplitudes greater than 50 dB
AE
are relevant to a further discussion of the AE activity at
a later part of this paper. For this reason, a digital filter was later used.
Figure 9.
Amplitude values of the hits over time and the frequency spectrum of a selected hit during dry-running operation
of the agitator vessel system.
After approximately 30 min of dry-running operation, the measurement was paused
and the mechanical seal was filled with barrier fluid to verify whether the leakage rate had
increased. When the seal barrier fluid system was reestablished, the vibrational behavior
of the seal showed no deviations in comparison to normal operation. After 11 days of
repeating the same procedure, a higher leakage rate was detected and the seal was replaced.
5.3. Abrasive Particles
As addressed in the Introduction, abrasive particles can cause wear in the sealing
gap, especially on the surface of the seal ring made of carbon graphite. This can lead to
the formation of microcracks on the surface of the carbon graphite and spalling on the
surface of both sliding materials. Here, the continuous flow of the barrier fluid through
the mechanical seal plays an important role, since this is the only way to guarantee the
supply of particles to the sealing gap and, consequently, induce abrasive wear. The friction
heat generated in the sealing gap is transferred to the barrier fluid, which activates the
thermosyphon principle in the barrier fluid system. Due to their sedimentation tendency,
the corundum particles were occasionally manually stirred in the pressurized vessel of the
barrier fluid system during the experiments in order to bring the sedimented particles back
Vibration 2021,4274
in motion. A lower threshold was set to allow a better understanding of the vibrational
behavior of the mechanical seal under this fault condition mode.
The results are shown in Figure 10. A more unstable vibrational behavior can be
observed, as the measured hits exhibited amplitude values between 45 and 87.5 dB
AE
,
the latter being the maximum amplitude detected during the experiment. A band with
a higher distribution density of hits can be distinguished between 45 and approximately
50 dB
AE
; this can be defined as the background noise of the measurement. The hits with
amplitudes greater than 50 dB
AE
are relevant to a further discussion of the AE activity at a
later part of this paper. For this reason, a digital filter was later used.
Vibration 2021, 4 FOR PEER REVIEW 12
Figure 10. Amplitude values of the hits over time during agitator vessel system operation with
abrasive particles in the barrier fluid system.
The upper diagram in Figure 11 shows the accumulation of the previously detected
hits, which is represented by the green line corresponding to the left y-axis. The height of
the green bars in the lower diagram represents the number of hits that occurred over the
course of the previous 30 s. In both diagrams, the red line corresponds to the temperature
measurement. Furthermore, all hits considered in Figure 11 had amplitude values greater
than 50 dB
AE
.
Figure 11. AE signals with an amplitude value greater than 50 dB
AE
during agitator vessel system operation with abrasive
particles in the barrier fluid system; (a) cumulative number of hits; (b) number of hits that occurred over the course of the
previous 30 s.
By comparing Figure 10 and the diagrams of Figure 11, the change in AE activity over
time becomes obvious. Peak-like AE activity increases were detected briefly after the
abrasive particles were stirred in the pressurized vessel of the barrier fluid system. These
instant accumulations of hits were followed by a noticeable rise of the temperature of the
mechanical seal housing. Due to proximity, this correlates with a greater generation of
heat inside the sealing gap. During the last 3000 s of the measurement, the number of hits
Figure 10.
Amplitude values of the hits over time during agitator vessel system operation with abrasive particles in the
barrier fluid system.
The upper diagram in Figure 11 shows the accumulation of the previously detected
hits, which is represented by the green line corresponding to the left y-axis. The height of
the green bars in the lower diagram represents the number of hits that occurred over the
course of the previous 30 s. In both diagrams, the red line corresponds to the temperature
measurement. Furthermore, all hits considered in Figure 11 had amplitude values greater
than 50 dBAE.
By comparing Figure 10 and the diagrams of Figure 11, the change in AE activity
over time becomes obvious. Peak-like AE activity increases were detected briefly after the
abrasive particles were stirred in the pressurized vessel of the barrier fluid system. These
instant accumulations of hits were followed by a noticeable rise of the temperature of the
mechanical seal housing. Due to proximity, this correlates with a greater generation of heat
inside the sealing gap. During the last 3000 s of the measurement, the number of hits with
amplitude values greater than 50 dB
AE
increased due to the increase by 1 bar of the pressure
inside the barrier fluid system. This corroborates the findings of Towsyfyan [
7
], who found
that for low speeds (below 1.200 rpm) the increase in pressure inside the mechanical seal
leads to an increase in the amplitudes of the detected AE.
A hit was randomly selected from the hits with a greater amplitude than 50 dB
AE
and
that occurred during the abrupt increases of AE activity. Its time signal and frequency
spectrum are shown in Figure 12. The frequency spectrum exhibits a general excitation of
the frequencies between 100 and 625 kHz. In particular, high amplitude peaks occurred at
approximately 105, 115, 195, 275 and 450 kHz. This frequency pattern was found in other
hits that occurred during the abrupt increases of AE activity.
Vibration 2021,4275
Vibration 2021, 4 FOR PEER REVIEW 12
Figure 10. Amplitude values of the hits over time during agitator vessel system operation with
abrasive particles in the barrier fluid system.
The upper diagram in Figure 11 shows the accumulation of the previously detected
hits, which is represented by the green line corresponding to the left y-axis. The height of
the green bars in the lower diagram represents the number of hits that occurred over the
course of the previous 30 s. In both diagrams, the red line corresponds to the temperature
measurement. Furthermore, all hits considered in Figure 11 had amplitude values greater
than 50 dB
AE
.
Figure 11. AE signals with an amplitude value greater than 50 dB
AE
during agitator vessel system operation with abrasive
particles in the barrier fluid system; (a) cumulative number of hits; (b) number of hits that occurred over the course of the
previous 30 s.
By comparing Figure 10 and the diagrams of Figure 11, the change in AE activity over
time becomes obvious. Peak-like AE activity increases were detected briefly after the
abrasive particles were stirred in the pressurized vessel of the barrier fluid system. These
instant accumulations of hits were followed by a noticeable rise of the temperature of the
mechanical seal housing. Due to proximity, this correlates with a greater generation of
heat inside the sealing gap. During the last 3000 s of the measurement, the number of hits
Figure 11.
AE signals with an amplitude value greater than 50 dB
AE
during agitator vessel system operation with abrasive
particles in the barrier fluid system; (
a
) cumulative number of hits; (
b
) number of hits that occurred over the course of the
previous 30 s.
Vibration 2021, 4 FOR PEER REVIEW 13
with amplitude values greater than 50 dB
AE
increased due to the increase by 1 bar of the
pressure inside the barrier fluid system. This corroborates the findings of Towsyfyan [7],
who found that for low speeds (below 1.200 rpm) the increase in pressure inside the
mechanical seal leads to an increase in the amplitudes of the detected AE.
A hit was randomly selected from the hits with a greater amplitude than 50 dB
AE
and
that occurred during the abrupt increases of AE activity. Its time signal and frequency
spectrum are shown in Figure 12. The frequency spectrum exhibits a general excitation of
the frequencies between 100 and 625 kHz. In particular, high amplitude peaks occurred
at approximately 105, 115, 195, 275 and 450 kHz. This frequency pattern was found in
other hits that occurred during the abrupt increases of AE activity.
Figure 12. AE properties of a hit during the abrupt increases of AE activity; (a) time signal; (b) frequency spectrum.
5.4. Cooling Failure
Almost 3000 s after the start of this experiment, a cooling failure was induced by
removing the barrier fluid supply from the mechanical seal. After approximately 3 h
without effective cooling of the seal, a leakage was detected by visual observation of the
drain hole. The barrier fluid supply and thus, also the cooling, was restored immediately
afterwards. Hereafter, a higher leakage rate was observed due to the recently
reestablished barrier fluid flow into the mechanical seal (see Figure 13). Despite the
leakage, the pressure in the barrier fluid system remained constant during the whole
experiment.
Figure 14 depicts the vibrational behavior of the experiment over time. In the first
3000 s, AE with greater amplitude values were measured. After the cooling was stopped,
the range of the amplitude values of the measured hits was narrower than before the
failure was induced. It can be observed that the minimum amplitude values of the
recorded hits were greater than the threshold.
Figure 12. AE properties of a hit during the abrupt increases of AE activity; (a) time signal; (b) frequency spectrum.
Vibration 2021,4276
5.4. Cooling Failure
Almost 3000 s after the start of this experiment, a cooling failure was induced by
removing the barrier fluid supply from the mechanical seal. After approximately 3 h
without effective cooling of the seal, a leakage was detected by visual observation of the
drain hole. The barrier fluid supply and thus, also the cooling, was restored immediately
afterwards. Hereafter, a higher leakage rate was observed due to the recently reestablished
barrier fluid flow into the mechanical seal (see Figure 13). Despite the leakage, the pressure
in the barrier fluid system remained constant during the whole experiment.
Vibration 2021, 4 FOR PEER REVIEW 14
Figure 13. Close-up of the mechanical seal with leakage in the drain hole of the seal housing; (a)
during the induced cooling failure; (b) after the reestablishment of the barrier fluid supply.
Figure 14. Amplitude values of the hits over time during agitator vessel system operation with two failures in the barrier
fluid system: presence of abrasive particles and cooling failure through the interruption of the barrier fluid supply.
After approximately 2 h of operation without cooling, the time signals and frequency
spectra of the hits changed significantly. Before this change was detected, the time signal
and the frequency spectra of the hits were similar to the ones obtained during AE
measurement under only the presence of abrasive particles. Although the operating
frequency range of the employed sensor starts at 125 kHz, the frequency spectra of the
newly detected hits show strong peaks around 66, 100, 135 and 165 kHz, which are integer
multiples of 33.33 kHz (see Figure 15). This 33.33 kHz frequency corresponds to a period
duration of 30 µs, which can be observed in the time signals of these hits.
Some hits presented such high amplitude values that the measuring system exceeded
its measurement range. Although the leakage was only visible one hour after the change
in the AE properties was noticed, this change in AE properties could be an indication of
damage in the mechanical seal rings.
Figure 13.
Close-up of the mechanical seal with leakage in the drain hole of the seal housing;
(a) during the induced cooling failure; (b) after the reestablishment of the barrier fluid supply.
Figure 14 depicts the vibrational behavior of the experiment over time. In the first
3000 s, AE with greater amplitude values were measured. After the cooling was stopped,
the range of the amplitude values of the measured hits was narrower than before the failure
was induced. It can be observed that the minimum amplitude values of the recorded hits
were greater than the threshold.
Vibration 2021, 4 FOR PEER REVIEW 14
Figure 13. Close-up of the mechanical seal with leakage in the drain hole of the seal housing; (a)
during the induced cooling failure; (b) after the reestablishment of the barrier fluid supply.
Figure 14. Amplitude values of the hits over time during agitator vessel system operation with two failures in the barrier
fluid system: presence of abrasive particles and cooling failure through the interruption of the barrier fluid supply.
After approximately 2 h of operation without cooling, the time signals and frequency
spectra of the hits changed significantly. Before this change was detected, the time signal
and the frequency spectra of the hits were similar to the ones obtained during AE
measurement under only the presence of abrasive particles. Although the operating
frequency range of the employed sensor starts at 125 kHz, the frequency spectra of the
newly detected hits show strong peaks around 66, 100, 135 and 165 kHz, which are integer
multiples of 33.33 kHz (see Figure 15). This 33.33 kHz frequency corresponds to a period
duration of 30 µs, which can be observed in the time signals of these hits.
Some hits presented such high amplitude values that the measuring system exceeded
its measurement range. Although the leakage was only visible one hour after the change
in the AE properties was noticed, this change in AE properties could be an indication of
damage in the mechanical seal rings.
Figure 14.
Amplitude values of the hits over time during agitator vessel system operation with two failures in the barrier
fluid system: presence of abrasive particles and cooling failure through the interruption of the barrier fluid supply.
After approximately 2 h of operation without cooling, the time signals and frequency
spectra of the hits changed significantly. Before this change was detected, the time signal
Vibration 2021,4277
and the frequency spectra of the hits were similar to the ones obtained during AE mea-
surement under only the presence of abrasive particles. Although the operating frequency
range of the employed sensor starts at 125 kHz, the frequency spectra of the newly detected
hits show strong peaks around 66, 100, 135 and 165 kHz, which are integer multiples of
33.33 kHz (see Figure 15). This 33.33 kHz frequency corresponds to a period duration of
30 µs, which can be observed in the time signals of these hits.
Vibration 2021, 4 FOR PEER REVIEW 15
Figure 15. AE properties of a hit during agitator vessel system operation with an induced failure in the barrier fluid system;
(a) time signal; (b) frequency spectrum.
After detecting the leakage, the barrier supply was restored and the frequencies
around 66, 100, 135 and 165 kHz disappeared, as shown in Figure 16. The signal pattern
then reverted to approximately its previous state, as shown in Figure 12.
Figure 16. AE properties of a hit after the barrier fluid supply was restored; (a) time signal; (b)
frequency spectrum.
6. Discussion
In the previous chapters, the AE signals of a liquid-buffered mechanical seal operated
in fault condition modes of the barrier fluid system were presented. A change in the
number of detected hits and the amplitudes of the hits between normal operation and the
operation mode under fault conditions was considered as an indicator for damage
development at an early stage. This is discussed for each fault operation mode in the
following.
Figure 15.
AE properties of a hit during agitator vessel system operation with an induced failure in the barrier fluid system;
(a) time signal; (b) frequency spectrum.
Some hits presented such high amplitude values that the measuring system exceeded
its measurement range. Although the leakage was only visible one hour after the change
in the AE properties was noticed, this change in AE properties could be an indication of
damage in the mechanical seal rings.
After detecting the leakage, the barrier supply was restored and the frequencies
around 66, 100, 135 and 165 kHz disappeared, as shown in Figure 16. The signal pattern
then reverted to approximately its previous state, as shown in Figure 12.
Vibration 2021, 4 FOR PEER REVIEW 15
Figure 15. AE properties of a hit during agitator vessel system operation with an induced failure in the barrier fluid system;
(a) time signal; (b) frequency spectrum.
After detecting the leakage, the barrier supply was restored and the frequencies
around 66, 100, 135 and 165 kHz disappeared, as shown in Figure 16. The signal pattern
then reverted to approximately its previous state, as shown in Figure 12.
Figure 16. AE properties of a hit after the barrier fluid supply was restored; (a) time signal; (b)
frequency spectrum.
6. Discussion
In the previous chapters, the AE signals of a liquid-buffered mechanical seal operated
in fault condition modes of the barrier fluid system were presented. A change in the
number of detected hits and the amplitudes of the hits between normal operation and the
operation mode under fault conditions was considered as an indicator for damage
development at an early stage. This is discussed for each fault operation mode in the
following.
Figure 16. AE properties of a hit after the barrier fluid supply was restored; (a) time signal; (b) frequency spectrum.
Vibration 2021,4278
6. Discussion
In the previous chapters, the AE signals of a liquid-buffered mechanical seal operated
in fault condition modes of the barrier fluid system were presented. A change in the number
of detected hits and the amplitudes of the hits between normal operation and the operation
mode under fault conditions was considered as an indicator for damage development at
an early stage. This is discussed for each fault operation mode in the following.
6.1. Dry-Running Operation
Hits with amplitude values greater than 65 dB
AE
were often detected during the
startup of the agitator vessel system, regardless of whether operation was being carried out
with or without the barrier fluid. This is a result of the missing lubrication film inside the
sealing gap when the agitator is switched on after standstill. During the startup process,
the lubrication film builds up with increasing relative velocity of both seal rings until,
depending on the operation conditions, boundary (BL) or mixed lubrication (ML) forms
and the initial wear decreases.
As depicted in Figure 9, operation of the mechanical seal without barrier fluid does
not lead to an immediate change in the acoustic behavior, most likely due to the remaining
lubricant between the sliding surfaces. This could indicate the presence of BL inside the
mechanical seal.
The beginning of dry running was always indicated by a sudden increase in the
maximum amplitude of the detected hits, which correlates with the expected drastic
change in wear rate during the transition between BL and dry running as described by
Hamrock et al. [
6
]. In addition, the frequency spectrum of the hits measured during
dry-running operation repeatedly showed a characteristic frequency distribution which
could clearly be distinguished from AE during operation with barrier fluid. This pattern is
characterized by several harmonics of a fundamental frequency of 33 kHz, which could be
measured up to the 500 kHz range. The first visible peak in the spectrum was at 66 kHz,
despite an operating frequency range of the sensor starting at 125 kHz, most likely due to
the high amplitude values of the AE. This pattern could represent the natural frequency of
the tribosystem composed by the seal rings and its harmonics.
6.2. Abrasive Particles
The amplitude values of the measured hits that are relevant to an examination of the
AE activity were approximately 10 dB
AE
lower (around 50 dB
AE
) than the threshold set
during the dry running measurement. This is due to the dismantling of the agitator vessel
system in order to change the mechanical seal that was damaged during dry-running
operation, which affects the attachment between various agitator components and thereby
the frequency response between the sensors and the mechanical seals.
The abrupt increases in AE activity shown in Figures 10 and 11 could be explained by
the presence of a large number of corundum particles that suddenly entered the sealing
gap after the pressurized vessel of the barrier fluid system was stirred, which caused a high
level of abrasive wear. These peak-like AE activity increases could indicate the transition
from normal friction inside the sealing gap to high wear, in this case to high abrasive wear.
As discussed, the different microscopic interaction between the asperities of all the
involved surfaces, as well as the microscopic changes due to wear, generate high-frequency
signals. Therefore, it is assumed that the excited high-frequency signals could have been
stimulated by the abrasive wear between the seal rings and the abrasive particles. The high
amplitude values could have resulted from resonances between the excited frequencies
and the natural frequency of some of the mechanical seal components.
According to Hase et al. [
10
], the AE caused by abrasive wear are characterized by
the excitation of a wide frequency range from 250 kHz to 1 MHz with strong peaks at
around 250, 450 and 850 kHz. The measured peaks at 275 and 450 kHz are very close to the
results of Hase et al. [
10
]. The difference between the excited frequencies is probably due
to the difference in the materials used and the geometry of the investigated tribosystem.
Vibration 2021,4279
Chung et al. [
17
] found a general excitation of frequencies between approximately 100 and
400 kHz with a large peak at 200 kHz for three-body wear. According to Ramadan et al. [
18
],
the growth and propagation of cracks are characterized by the excitation of a frequency
range between 100 and 600 kHz with a large peak at 200 kHz. Since different materials
were used in these studies [
17
,
18
], it can be assumed that three-body wear, as well as the
growth and propagation of cracks, was also present during the abrasive lubrication of the
mechanical seal used in this work. The overlap of the excited frequency ranges is explained
by the fact that the generation of acoustic emission signals during abrasive wear, either
between two or three bodies, is related to crack growth and propagation [10,17,18].
Since the diameter of the corundum particles is in the microscopic range, the particles
can settle everywhere in the mechanical seal: in the springs, between the housing and
the sliding pair, etc. In Figure 17, the accumulation of corundum particles throughout
the interior of the mechanical seal can be observed. As it is assumed that the measured
high frequencies are excited only when the corundum particles generate abrasive wear
in the sealing gap, its non-continuous excitation may be due to the fact that the particles
experience a centrifugal force when they enter the sealing gap, which directs them to the
other parts of the mechanical seal.
Vibration 2021, 4 FOR PEER REVIEW 17
three-body wear, as well as the growth and propagation of cracks, was also present during
the abrasive lubrication of the mechanical seal used in this work. The overlap of the
excited frequency ranges is explained by the fact that the generation of acoustic emission
signals during abrasive wear, either between two or three bodies, is related to crack
growth and propagation [10,17,18].
Since the diameter of the corundum particles is in the microscopic range, the particles
can settle everywhere in the mechanical seal: in the springs, between the housing and the
sliding pair, etc. In Figure 17, the accumulation of corundum particles throughout the
interior of the mechanical seal can be observed. As it is assumed that the measured high
frequencies are excited only when the corundum particles generate abrasive wear in the
sealing gap, its non-continuous excitation may be due to the fact that the particles
experience a centrifugal force when they enter the sealing gap, which directs them to the
other parts of the mechanical seal.
Figure 17. Accumulation of corundum particles inside the mechanical seal; (a) springs; (b) product
side seal ring pair; (c) seal housing; (d) atmospheric side seal ring pair.
6.3. Cooling Failure
At the beginning of the experiment, high amplitude values of the AE were measured.
This is an indication of the fatigue suffered by the seal rings due to the continuous abrasive
wear induced in the previous experiment. Furthermore, the time signals, as well as the
frequency spectra of these AE, showed similar patterns to the ones obtained in the
previous experiments with abrasive particles. This acoustic behavior continued during
the hole measurement, even after the barrier fluid supply was stopped and restored.
As the barrier fluid supply was interrupted, the heat could not be properly dissipated
and the thermosyphon principle was no longer effective. This probably caused the
evaporation of part of the remaining barrier fluid inside the sealing gap, which could have
caused BL between the seal rings and therefore more frictional heat. This process
continued until the barrier fluid supply was restored. The temperature then dropped
considerably as seen in Figure 14. As a drop of lubricant was present on the drain hole of
the seal housing (see Figure 13), it can be assumed that the barrier fluid did not evaporate
completely, meaning that lubricant was still present in the mechanical seal and thus
prevented dry-running operation. This confirms the presence of BL in the sealing gap.
Figure 17.
Accumulation of corundum particles inside the mechanical seal; (
a
) springs; (
b
) product
side seal ring pair; (c) seal housing; (d) atmospheric side seal ring pair.
6.3. Cooling Failure
At the beginning of the experiment, high amplitude values of the AE were measured.
This is an indication of the fatigue suffered by the seal rings due to the continuous abrasive
wear induced in the previous experiment. Furthermore, the time signals, as well as the
frequency spectra of these AE, showed similar patterns to the ones obtained in the previous
experiments with abrasive particles. This acoustic behavior continued during the hole
measurement, even after the barrier fluid supply was stopped and restored.
As the barrier fluid supply was interrupted, the heat could not be properly dissipated
and the thermosyphon principle was no longer effective. This probably caused the evapora-
tion of part of the remaining barrier fluid inside the sealing gap, which could have caused
BL between the seal rings and therefore more frictional heat. This process continued until
the barrier fluid supply was restored. The temperature then dropped considerably as seen
in Figure 14. As a drop of lubricant was present on the drain hole of the seal housing (see
Figure 13), it can be assumed that the barrier fluid did not evaporate completely, meaning
Vibration 2021,4280
that lubricant was still present in the mechanical seal and thus prevented dry-running
operation. This confirms the presence of BL in the sealing gap.
The damage in the mechanical seal and the time of its onset were determined by a
change in the maximum amplitude values of the hits and their respective frequency spectra.
As described in the previous chapter, the spectrum of these hits shows a characteristic
harmonic pattern with a fundamental frequency of 33 kHz and its harmonics (see
Figure 15
).
Thanks to the greater amplitude values of these hits, they could be distinguished from
those generated due to abrasive wear. This also indicates that the friction mechanism
due to prolonged operation under BL conditions caused by the interruption of the barrier
fluid supply is the dominant mechanism in this experiment. After the barrier supply was
restored, the spectra of the measured hits resembled those measured under the presence
of abrasive wear, as illustrated in Figure 18. The figure shows a comparison between the
frequency spectrum depicted in Figure 12 and the frequency spectrum of a hit measured
after the barrier fluid supply was restored.
Vibration 2021, 4 FOR PEER REVIEW 18
The damage in the mechanical seal and the time of its onset were determined by a change
in the maximum amplitude values of the hits and their respective frequency spectra. As
described in the previous chapter, the spectrum of these hits shows a characteristic
harmonic pattern with a fundamental frequency of 33 kHz and its harmonics (see Figure
15). Thanks to the greater amplitude values of these hits, they could be distinguished from
those generated due to abrasive wear. This also indicates that the friction mechanism due
to prolonged operation under BL conditions caused by the interruption of the barrier fluid
supply is the dominant mechanism in this experiment. After the barrier supply was re-
stored, the spectra of the measured hits resembled those measured under the presence of
abrasive wear, as illustrated in Figure 18. The figure shows a comparison between the
frequency spectrum depicted in Figure 12 and the frequency spectrum of a hit measured
after the barrier fluid supply was restored.
Figure 18. Comparison between two frequency spectra of different measurements; (a) frequency
spectrum of the hit depicted in Figure 12; (b) frequency spectrum of a detected hit after the barrier
fluid supply was restored when simulating a cooling failure.
The frequency pattern depicted in Figure 15 was very similar to the one observed
during the dry running experiments (see Figure 9), with the exception that in this experi-
ment the frequency spectra only presented harmonics up to 200 kHz. As this frequency
pattern disappeared in both experiments after the barrier fluid supply was restored, the
presence of a fundamental frequency of about 33 kHz with its respective harmonics could
be an indicator for inadequate friction mechanisms inside the sealing gap of a double-
acting mechanical seal with a hard/soft seal ring pairing due to deficient lubrication. This
could lead to an inadmissible increase in the leakage rate.
Further investigations can be carried out to determine the natural frequencies of the
components of a mechanical seal, as well as the natural frequency of the tribosystem. This
could provide a better identification of the frequencies excited during operation with fault
condition modes. Moreover, the influence of different geometries and material combina-
tions of mechanical seals on the vibrational behavior due to different fault condition
modes could be investigated.
Despite increased leakage, the overpressure in the locking system remained constant.
The increase of the leakage rate is usually monitored through the overpressure in the bar-
rier fluid system or the liquid level in the pressurized vessel. For this reason, it can be
concluded that the measuring systems used in these experiments have detected a defect
in the mechanical seal that would not be detected using conventional monitoring methods.
Figure 18.
Comparison between two frequency spectra of different measurements; (
a
) frequency spectrum of the hit
depicted in Figure 12; (
b
) frequency spectrum of a detected hit after the barrier fluid supply was restored when simulating a
cooling failure.
The frequency pattern depicted in Figure 15 was very similar to the one observed dur-
ing the dry running experiments (see Figure 9), with the exception that in this experiment
the frequency spectra only presented harmonics up to 200 kHz. As this frequency pattern
disappeared in both experiments after the barrier fluid supply was restored, the presence
of a fundamental frequency of about 33 kHz with its respective harmonics could be an
indicator for inadequate friction mechanisms inside the sealing gap of a double-acting
mechanical seal with a hard/soft seal ring pairing due to deficient lubrication. This could
lead to an inadmissible increase in the leakage rate.
Further investigations can be carried out to determine the natural frequencies of the
components of a mechanical seal, as well as the natural frequency of the tribosystem. This
could provide a better identification of the frequencies excited during operation with fault
condition modes. Moreover, the influence of different geometries and material combina-
tions of mechanical seals on the vibrational behavior due to different fault condition modes
could be investigated.
Vibration 2021,4281
Despite increased leakage, the overpressure in the locking system remained constant.
The increase of the leakage rate is usually monitored through the overpressure in the
barrier fluid system or the liquid level in the pressurized vessel. For this reason, it can be
concluded that the measuring systems used in these experiments have detected a defect in
the mechanical seal that would not be detected using conventional monitoring methods.
7. Conclusions
This work presents an experimental investigation of typical failure condition modes of
a face-end mechanical seal mounted on a test agitator vessel system. The AET was utilized
to measure the vibrational response of the friction processes between the seal rings during
the fault condition modes, with the aim of detecting the inadequate friction mechanisms
that could develop into an inadmissible increase of the leakage rate. The fault condition
modes “dry running”, “presence of abrasive particles in the barrier fluid” and “cooling
failure in the barrier fluid system” were induced separately and the emitted AE recorded.
These fault condition modes represent typical unfavorable conditions for the mechanical
seal of an agitator vessel system, which can occur suddenly during normal operation.
It was found that the high-frequency AE analysis is suitable for detecting inadequate
friction, as the measuring system was able to detect the induced fault condition modes
before leakage was visible at the drain hole.
Dry-running operation and cooling failure caused leaks on the mechanical seal: The
former because of the absence of lubrication and the latter due to the insufficient lubrication
state (BL), which led in both cases to inadequate friction mechanisms within the sealing
gap, causing irreversible damage in the mechanical seal over time, as evidenced by an
inadmissible increase in the leakage rate. Although the amplitudes of the measured AE
during the onset of the leakage could not be quantified because they exceeded the AMSY-
6 measurement range, the significant change in the time signal and frequency spectra
indicated the presence of inadequate friction. These signals showed a pattern in the high-
frequency range that consisted of the harmonics of a fundamental frequency of about
33 kHz. This pattern is not detectable with the classical vibration diagnostic methods.
Additionally, abrasive wear in the sealing gap could be detected independently from the
other fault conditions.
8. Outlook
The pressure in the lubrication system remained constant despite the presence of a
leakage. Since the mechanical seal is usually monitored through pressure changes in the
lubrication system, the leakage would not have been detected by traditional monitoring
methods. The basic requirement for a potential broader industrial application is a more eco-
nomical measuring system compared to the one used in this experiment. It can be assumed
that the price of a specialized system for pure industrial use can be significantly lower than
the widely applicable system used, with a predominantly scientific field of application.
The amount of data that need to be handled at high sampling frequencies can be
greatly reduced by choosing a suitable threshold, since measurements are only taken when
the amplitude exceeds this limit. In addition, it is also possible to derive only the AE data
from the measured time signals of the hits, but not to store the time signal itself.
The amount of data combined with the characteristics of each detected wear mech-
anism that can lead to seal failure can be used as a base for future works involving deep
learning techniques. The different geometries, material pairings and barriered/buffered
fluids or dry gas running mechanical seals will very likely have an influence on the signal
characteristics. Therefore, an appropriate machine learning algorithm and its suitable
parameters need to be identified and tested. These algorithms generally require suffi-
cient amounts of data, often labeled, whereas algorithms in the “unsupervised learning”
category should eliminate that requirement.
Vibration 2021,4282
Author Contributions:
Conceptualization, F.W., M.S., F.S., J.S. and M.M.-A.; methodology, M.M.-A.,
F.S. and F.W.; validation, M.M.-A., F.S., J.S. and R.K.; formal analysis, M.M.-A., F.W., J.S. and F.S.;
investigation, M.M.-A. and F.S.; resources, F.W., M.S., J.S., R.K., F.S.; data curation, M.M.-A. and F.S.;
writing—original draft preparation, M.M.-A.; writing—review and editing, M.M.-A., F.S., F.W., J.S.
and R.K.; visualization, M.M.-A. and F.S.; supervision, F.W., M.S., R.K. and J.S.; project administration,
F.W. and J.S. All authors have read and agreed to the published version of the manuscript.
Funding: This research received no external funding.
Institutional Review Board Statement: Not applicable.
Informed Consent Statement: Not applicable.
Data Availability Statement:
The raw data has not been approved by the approval office of BASF
SE. The raw data of individual test parts and measurements are available on request from the
corresponding author.
Acknowledgments:
The authors would like to acknowledge Rui de Oliveira from BASF SE for his
great support regarding the applied measurement equipment and for the fruitful discussions. Many
thanks go to the entire workshop crew of BASF’s Special Machinery Maintenance department in
Ludwigshafen under the leadership of Thorsten Reisser for their technical assistance during the
setting up of the agitator vessel test rig and mounting of the mechanical seals.
Conflicts of Interest: The authors declare no conflict of interest.
Abbreviations
The following abbreviations are used in this work:
AET Acoustic emission technique
AE Acoustic emissions
BL Boundary lubrication
ML Mixed lubrication
HL Hydrodynamic lubrication
dBAE Decibels of acoustic emissions
AMSY-6 Acoustic Measurement System 6th generation
PAC Physical Acoustics Corporation
RMS Root mean square
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