ties) among the tie spans between the measurement sites
vary, ranging from 0.23 to 0.3 m (9 to 12 in.). Approximately at
the midpoint between the two measurement locations, a rail
de-stressing procedure (rail cut) was applied. The rail cut was
applied on the fourth tie span toward the west direction from
the East location, as shown in Figure 1.
At both testing locations, the rail web was instrumented
with two sets of strain gauge modules (active set and spare
set) and temperature sensors, as shown in Figure 2. At each
location, the strain measurement system uses a four-leg full-
bridge gauge comprising two axial and two transverse (vertical)
strain gauges, the output of which is modified to account for
transverse strains owing to temperature and the Poisson effect
when a value of Poisson ratio (0.285 was used to represent rail
steel here) is input to the system, the output value from the
gauges is an equivalent axial strain value ​​ x​​​ This approach has
been well established in practice (Samavedam et al. 1986), and
values of ​​ x​​​ obtained with such systems have been shown to
well represent the axial stress state in the rail owing to confined
thermal expansion (Liu et al. 2018). For the remainder of this
paper, the compensated equivalent strain output ​​ x​​​ will simply
be referred to as axial strain or microstrain. Alongside the
strain gauge modules, one resistance temperature detector
(RTD) on each side of the rail at each location was installed for
monitoring the rail temperature. Together these sensors enable
the rail RNT to be calculated using the formula:
(2)​ RNT =T ε​x​​
α
where
ε​x​​​ is the equivalent axial strain,
α​ is the presumed linear thermal expansion coefficient 1.169
× 10–5/°C (6.5 × 10–6/°F), and
T is the rail temperature.
The rail temperature, axial strain, and RNT readings are
transmitted to a track-side solar-powered, stand-alone data
logging system. The entire measurement system was installed
and tested one day before the rail-cutting procedure. The
logging system has continuously reported the temperature,
strain, and RNT data every 15 min since it was installed.
The rail-cutting procedure was conducted on the morning
of 31 July 2019. The cutting process released the rail stress
(tension) around the cut region and then the rail was pulled
and connected with a thermite weld to set the RNT to a
desired value. Because the strain and temperature measur-
ing system was deployed and operating before the rail cut
occurred, the equivalent axial strain and RNT of the system at
the two measurement locations can be accurately measured
moving forward. All reported strain and RNT are referenced by
the original cutting procedure, and no subsequent rail-cutting
procedure or other gauge calibration processes were carried
out. Although sensor systems are known to exhibit errors,
such as value drift, over the long term, in this case it is reason-
able to presume that the overall drift of the multisensor full-
bridge strain system will likely provide insignificant changes
with respect to the stress-state changes the system measures,
because the random drift of individual sensors within the
combined full-bridge system are likely to cancel each other out
over the two-year measurement period. To check for possible
drift problems, we switched from active to spare strain sensor
sets mounted nearby after over one year of measurement and
found no significant change in the strain readings.
The rail vibration responses are generated by mechanical
impulse events, which are initiated using a small steel sphere
with a diameter of 12 mm (0.47 in.). The impulse is applied by
hand to the center top of the railhead at the midspan location
between the ties. The vibration responses are sensed by a
polarized condenser microphone pointing to the side of the
railhead at the same location where the impulse is applied,
as illustrated by Figure 3. The microphone has a sensitivity
of ±3 dB across a frequency range of 4 to 100 000 Hz. The
response signals measured by the microphone are ampli-
fied through a sensor signal conditioner using a gain of
10, and then transmitted to a multifunction I/O device for
data acquisition. Each collected time signal set up by the
mechanical impulse is 0.3 s in duration with a sampling rate
of 500 kHz with a total of 150 001 sample points including
10 000 pre-trigger samples.
Vibration tests were carried out on 1, 5, 15, and 29 August,
19 September, and 18 October in 2019 29 May and 8 October
in 2020 and finally 16 June in 2021. Vibration data from both
the East and West locations were measured, although the West
location was not tested on 29 May 2020. A wide range of the
RNT and strain conditions are represented during these test
days. All vibration test days started at approximately 9:00 a.m.
and ended around 3:00 p.m. or when the rail temperature
started to decrease because of reduced sun exposure. The
vibration measurements started at one test location and then
switched to the other location every 40 to 60 min during the
ME
|
RAILROADS
RTD
Strain gauge modules
Figure 2. Sensors attached to the rail web: resistance temperature
detectors (RTD) and the two sets of strain gauges. Each set consists of
two strain gauge modules that contain two strain gauges, oriented in
the axial and transverse direction, each attached on both sides of the
rail web.
62
M A T E R I A L S E V A L U A T I O N J A N U A R Y 2 0 2 4
2401 ME January.indd 62 12/20/23 8:01 AM
testing day. Each vibration test at a given location comprised
10 or more repeated impulse-driven vibration responses, which
represents one set of responses. Five to 13 sets of responses
were collected at each test location on each test day, and con-
sequently a total of 73 sets at the East location and 65 sets
at the West were collected across all the test days. Because
this impulse-based vibration measurement does not require
any mounted sensors or rail surface and track structure
pre-preparation, application of the technique does not damage
the rail structure or disrupt rail service in any way.
Analysis
The collected vibration time signals are zero-padded to a
duration of 1 s and transformed into spectral responses using
a discrete Fourier transform routine. The frequency resolu-
tion of the spectral responses is 1 Hz. The spectra of each set
(~10 repeated signals) are averaged across frequency to provide
one averaged spectrum. A typical averaged spectrum is shown
in Figure 4. Vibration resonances are identified as peaks or
maxima in the averaged spectrum. Although several resonance
peaks are observed in the low frequency range under 20 kHz,
we focus our attention on four prominent higher frequency
resonances around 31, 37, 39, and 76 kHz because we expect
these modes to not be affected by support and boundary
condition effects such as tie span length variation. These four
modes are consistently present and visually trackable at both
locations across all testing days, as illustrated in more detail in
Figure 5. The frequency values at the peak of these four reso-
nances are tracked across the nine testing days, and the fre-
quency values of each of the monitored vibration modes are
correlated with measured strain values that occur at the corre-
sponding vibration measurement times.
Condenser microphone
Steel impactor
Figure 3. Illustration of (a) the
vibration testing configuration
and (b) application of the test at
the field site. The rail vibration
is initiated by the impulse
from a steel ball impactor at
the center-top of the railhead,
and the response is collected
by the condenser microphone
pointing toward the side of the
railhead.
20 000 0
0.0000
0.0002
0.0004
0.0006
40 000 60 000
Frequency (Hz)
80 000 100 000 120 000
Figure 4. A typical amplitude spectrum averaged over 10 repeated
signals. The red arrows indicate the four prominent resonances around
31 kHz, 37 kHz, 39 kHz, and 76 kHz, which will be investigated.
5 August
15 August
29 August
5 August
15 August
29 August
5 Augustu
15 Augustu
29 Augustu
5
15
29
30 800 31 000 31 200 31 400 31 600
Frequency (Hz)
36 800 37 000 37 200 37 400
Frequency (Hz)
39 000 39 200 39 400 39 600 39 800
Frequency (Hz)
76 200 76 400 76 600 76 800
Frequency (Hz)
77 000
s
s
s
AAugust
AAugust
AAugust
Figure 5. The four prominent spectral resonances around (a) 31 kHz
(b) 39 kHz (c) 37 kHz and (d) 76 kHz (indicated by arrows in cases of the
presence of multiple peaks nearby) are consistently identified on 5, 15,
and 29 August 2019.
J A N U A R Y 2 0 2 4 M A T E R I A L S E V A L U A T I O N 63
2401 ME January.indd 63 12/20/23 8:01 AM
Amplitude
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