Abstract
In the early 1990’s work was initiated to develop a testing technique for
identifying fatigue cracks in aircraft airframes. Initial efforts focused
on the measurement of corrosion fatigue. The initial effort revealed that
a technique based upon electrochemical principles could measure corrosion current
with unusual precision. With this fundamental basis and a basic understanding
of the fatigue cracking process, the initial developmental work focused on a
crack detection technique that was actually based on the detection of the growth
of corrosion products. The resulting technology has a remarkable capability
at detecting very small fatigue cracks that are actively growing and is known
as the Electrochemical Fatigue Sensor (EFS).
This paper describes the EFS system including a detailed discussion of the fundamentals. In
addition, usage of the EFS system is presented through a case study. Additionally,
commentary is provided on the cost-effectiveness of the use of the EFS system
in an active bridge management approach.
INTRODUCTION
Fatigue crack detection is a very difficult task. In fact,
a study conducted at the Federal Highway Administration NDE Validation
Center in which 49 State Department of Transportation bridge
inspectors were asked to inspect two steel girder bridges with
fatigue crack indications revealed just how difficult crack identification
can be. This study indicated that fatigue cracks are only
likely to be correctly identified less than ten percent of the
time with current inspection techniques.
In the early 1990’s work was initiated to develop a testing
technique for identifying fatigue cracks in aircraft airframes. Initial
efforts focused on the measurement of corrosion fatigue. The
initial research on a testing technique based upon electrochemical
principles quickly revealed that corrosion current could be measured
with unusual precision. With this fundamental basis and
a basic understanding of the fatigue cracking process, the initial
developmental work focused on a crack detection technique that
was actually based on the detection of the growth of corrosion
products. The resulting technology has a remarkable capability
at detecting very small fatigue cracks that are actively growing
and is known as the Electrochemical Fatigue Sensor (EFS) system.
THE EFS SYSTEM
The EFS system is a nondestructive fatigue crack testing system. Specifically,
EFS is a method for determining if a previously unidentified
actively growing fatigue crack is present in the inspection area
or if known fatigue cracks are actively growing. During
an EFS test, an EFS sensor is applied to each location of interest
and crack detection occurs for areas under, or in the immediate
vicinity of, the sensor. The EFS system consists of an
electrolyte filled sensor, a potentiostat that applies a constant
polarizing voltage between the structure and the sensor, and
data collection and analysis software.
The EFS system works on fundamental electrochemical principles. During
testing, the inspection area is anodically polarized to create
a passive film on the area of interest. The polarizing
voltage produces a DC base current in the electrochemical cell. When
the structure being tested undergoes a cyclic stress, the current
flowing within the cell fluctuates in a complex relation to the
variation of the mechanical stress. As a result, an AC
current is superimposed on the base DC current. Dependent
upon the structural material, the loading conditions, as well
as the state of the fatigue damage in the structure, the transient
current within the cell provides information on any fatigue crack
activity.
The electrochemical conditions imposed during an EFS test are
designed to induce a stable, passive oxide film on the surface
of the material. During cyclic loading, the fatigue process
causes micro-plasticity and strain localization on a very fine
scale. The interaction of the cyclic slip and the passivating
process causes temporary and repeated alterations to the passive
films. These alterations, including both dissolution and repassivating
processes, give rise to transient currents. The resulting
EFS transient currents are complex and result from cyclic changes
in the electrical double layer at the interface of the metal
and the EFS electrolyte. The transient currents generally
possess the same frequency as that of the mechanical stress,
but also have a complex phase relationship. In addition,
the disruption of the surface oxide film by the cyclic slip causes
an additional component of the transient current which has double
the frequency of the elastic current. This occurs because
plasticity effects occur during both the tensile and compressive
portions of the loading cycle. As fatigue damage develops,
the cracks induce localized plasticity at different parts of
the fatigue cycle from those in which the background micro-plasticity
occurs and in locations where cracks have not yet formed. The
crack-induced plasticity, thus, introduces higher harmonic components
into the transient EFS current. It is the analysis of these
various current components that allows determination of whether
a growing crack is present or not. The EFS technique offers
several distinct advantages over other methods of nondestructive
evaluation because of the inherent ability to detect active fatigue
crack growth and because of the very small detectable crack size.
To enhance
the sensitivity of the EFS system, a configuration known as differential EFS
is employed. Differential EFS uses two sensors, one as the reference
(R) and one as the crack measurement (CM) sensor. The two sensors are
both installed near the location of interest. The CM sensor is specifically
located over the area to be inspected while the R sensor is located near the
CM sensor – but in a location where a crack is not probable. Using
signal processing, the two signals are compared to determine if a crack is
present. In this configuration and in the presence of a growing crack
the CM measurement sensor provides a larger frequency content magnitude than
the R sensor data and also contains extra frequency content. Several
proprietary data analysis techniques have been developed and are contained
within the EFS system software.
The EFS hardware system consists of three major components: the
EFS sensor, the EFS electrolyte, and the EFS potentiostat. The
following sections briefly discuss each of these components.
EFS Sensor
The basic EFS sensor consists of several parts as shown in Figure
1. Each sensor has a convenient contact adhesive on one
side for attachment to the structure. The open area in
the middle of the sensor holds the subsequently described EFS
electrolyte. The sensor is filled with electrolyte through
the lower filler tube while air escapes out of the upper bleeder
tube. The EFS sensor electrode – a stainless steel
mesh – is sandwiched between the upper and lower sensor
sections. When the sensor is filled with electrolyte,
the electrode is completely covered. Depending on the
area to be tested, EFS sensors can be custom-made to fit any
three-dimensional geometric requirements (including size, shape,
orientation, etc.).
EFS Electrolyte
The EFS electrolyte is a proprietary, water-based solution that
has been tested on multiple materials including aluminum, titanium,
copper, and steel. The EFS electrolyte has been found,
in all cases, to be benign to metals. The U.S. Air Force,
in fact, has conducted extended fatigue tests with EFS installed
on steel, aluminum, and titanium components and has found that
EFS did not cause premature failure or impact the fatigue life. The
EFS electrolyte is chemically inert and environmentally safe.

Figure 1 Basic schematic of an EFS sensor.
EFS Potentiostat
The EFS potentiostat is an electronic device that controls the
voltage difference between the working electrode and a reference
electrode. In the case of use during an EFS inspection,
both electrodes are contained within the previously mentioned
electrochemical cell. The specific variable controlled
by the EFS potentiostat is the cell potential and the measured
variable is the cell current. The EFS potentiostat has been
custom-designed to not only control the voltage but to also
measure the current flow between the working and reference
electrodes. During testing, the working electrode is
the structure and the reference electrode is the previously
mentioned EFS sensor electrode which is sandwiched within the
EFS sensor (i.e., the stainless steel mesh).
The battery-powered, wireless MATECH potentiostat, shown in Figure
2, provides all of the features necessary to collect data in
the field. The potentiostat is compact, lightweight, and
provides isolated channels for the R sensor and the CM sensor.
The MATECH potentiostat features onboard A/D conversion, data
collection to a removable MMC card, wireless data streaming,
and an easy to use wireless setup for bias, gain, and sample
rate.
APPLICATION CASE STUDY
MATECH was retained by the Pennsylvania Department of Transportation
(PENNDOT) to test three steel girder bridges using its EFS system. The
three structures were located on the following major highways:
I-476 over the Schuylkill River, PA; I-81 over the Susquehanna
River; and I-80 over Canoe Creek. Each structure has documented
cracks at fatigue sensitive details. PENNDOT was interested
in utilizing the EFS system to determine whether the documented
fatigue cracks were continuing to grow and to determine the effectiveness
of previously implemented repairs. The following briefly
describes the tested bridges and the testing that was conducted. A
brief discussion of the results of the testing then follows. Additional,
more detailed information on this application can be obtained
from the author.

Figure 2 The EFS Potentiostat.
Test Details
The dual 15-span steel bridges running north-south on I-476 over
the Schuylkill River in West Conshohocken, PA was inspected
by MATECH preliminarily on May 1, 2006 and with the EFS system
on October 5, 2006 and is shown in Figure 3. The
structure was constructed in the early 1970’s and cracking
was reported at the toes of the welds above the bearing locations
on the northbound and southbound spans at Pier 11 and within
the girder webs at the same locations. The following
locations were evaluated with the EFS system:
NORTHBOUND SPAN
- Girder 1, Pier 11, Span 12 at a transverse weld toe crack
on the outer side of thegirder
at the floorbeam at Pier 11
- Girder 7, Pier 11, Span 12
One
location is at a vertical weld toe crack which has propagated
into the
base metal of the floorbeam web. One
location is a weld toe crack at the same weld several inches
above the first location.
SOUTHBOUND SPAN
Girder 1, Pier 11, Span 12 Four
crack locations along the toe of weld at the girder to floorbeam
connection on both sides of the girder. One
location adjacent to a stop drill in the web of the Girder
1.

Figure 3. The I-476 bridge.
The second tested bridge was the southbound span of a dual 23-span
bridge system located on I-81 over the Susquehanna River just
north of Harrisburg, shown in Figure 4. A preliminary inspection
was performed on May 2nd with the EFS inspection performed on
October 10 and 12, 2006. The structure was built in 1972
with the first full year of traffic in 1976. Fatigue cracking
was reported during a biennial inspection. The cracking is the
result of out-of-plane bending in the girders and high stress
range levels. The following locations were tested on the southbound
span:
- Span 9, Girder 5, Floorbeam 1 - cracked
- Span 9, Girder 5, Floorbeam 3 – cracked
- Span 9, Girder 5, Floorbeam 4 - cracked
- Span 10 Girder 5 Floorbeam 1 – cracked
- Span 19, Girder 1, Floorbeam 7 - cracked
- Span 20, Girder 1, Floorbeam 4 – cracked

Figure 4. The I-81 bridge.
The third bridge inspected is the I-80 eastbound 6-span bridge
located west of Clarion, PA in Clarion County over the Canoe
Creek shown in Figure 5. A preliminary inspection was performed
on May 4 with the EFS inspection performed on October 2 and 3,
2006. The following locations were inspected with the EFS
system:
- Two crack locations at Girder 1, Floorbeam 22.
- Two locations beyond stop drills at Girder 2, Floorbeam 26
from the outside.
- Three locations beyond stop drills at Girder 1, Floorbeam
21 from the outside.
Four locations where cracks have propagated
beyond the stop drill holes at Girder
2, Floorbeam 19.

Figure 5. Bridge I-80
Results
Specific results of the tests are summarized in Tables 1 through
3. Note that crack location refers to the sequential inspection
location followed by a potentiostat identifier. For reference,
the term X in Tables 1 through 3 describes the ratio of the CM
output to the R output. This is one, but not the only,
factor used in determining the activity of a given crack.
The results summarized in Tables 1 through 3 lead to some important
findings. First, on the I-476 Bridge, the stop drill holes
appear to be of a large enough diameter to have arrested crack
growth. However, cracks along the toes of the welds are
continuing to grow at a fairly accelerated pace.
At the I-81 Harrisburg Bridge, it should be noted that the MATECH
team detected a crack not previously reported at Girder 5, Span
10, Floorbeam 1. This location contained a connection detail
similar to those which exhibited crack growth elsewhere on the
bridge. Results indicate that microplasticity is already
occurring in this area and that there is a good chance of crack
initiation.
The I-80 Canoe Creek bridge cracks have, in general, been stabilized. The
numerous drill stops and retrofits seem to have slowed the crack
growth. Additionally, it is possible that the cracks had
gotten so long that the stress field around the area of the crack
tip is now below critical levels. It should be noted that
testing at one location, the connection of Girder 2 to Floorbeam
26, revealed that there is microplasticity in the area of the
crack and that future crack growth is likely in this area.
Table 1. Inspection results, Bridge I-476
| Crack Location |
Crack Visually Detected? |
X, (X=CM/Ref) |
Activity |
1-53 |
Yes |
5.5 |
Active Growth |
2-60 |
Yes |
2.8 |
Active Growth |
3-56 |
No |
1.5 |
Growth not observed |
4-57 |
Yes |
2.3 |
Little growth |
5-63 |
Yes |
3.4 |
Active Growth |
6-52 |
Yes |
3.5 |
Active Growth |
7-54 |
Yes |
3.5 |
Active Growth |
8-62 |
No |
1.5 |
Growth not observed |
Table 2. Inspection results, Bridge I-81
Crack Location |
Crack Visually Detected? |
X, (X=CM/Ref) |
Activity |
1-52 |
Yes |
16.0 |
Active Growth |
2-53 |
Yes |
11.0 |
Active Growth |
3-54 |
Yes |
5.0 |
Active Growth |
4-63 |
No |
1.8 |
Little to no
growth |
5-57 |
Yes |
8.4 |
Active Growth |
6-62 |
Yes |
5.6 |
Active Growth |
Table 3. Inspection results, Bridge I-80
Crack Location |
Crack Visually Detected? |
X, (X=CM/Ref) |
Activity |
1-58 |
No |
<1.3 |
Growth not observed |
2-53 |
No |
1.9 |
Little to no
growth |
3-57 |
No |
<1.3 |
Growth not observed |
4-59 |
No |
<1.3 |
Growth not observed |
5-62 |
No |
<1.3 |
Growth not observed |
6-60 |
No |
<1.3 |
Growth not observed |
7-63 |
No |
<1.3 |
Growth not observed |
8-52 |
No |
<1.3 |
Growth not observed |
9-56 |
No |
<1.3 |
Growth not observed |
10-56 |
No |
<1.3 |
Growth not observed |
11-52 |
No |
<1.3 |
Growth not observed |
COST EFFECTIVENESS OF EFS INSPECTIONS
The overriding purpose for utilizing EFS as a condition assessment
tool for the above described testing was to help PENNDOT meet
one of the objectives set forth in a report recently released
by the Pennsylvania Transportation Funding and Reform Commission. This
report states that one reform that will significantly contribute
to PENNDOT’s goal of saving $120M per year is “…taking
the right maintenance steps at optimum intervals to extend the
life of highways and bridges…” by identifying growing
cracks in highway bridges. Using the EFS system, it was
determined that some of the inspected areas had growing cracks
(both at previously repaired and at unrepaired locations) and
that in other areas repairs had been successful. The inspection
results at the known cracks allowed PENNDOT to prioritize repairs
dollars to those most in need, to eliminate planned repairs to
areas that do not need repair, and to avoid very costly bridge
closures/load restrictions/failures. In addition, because
actively growing cracks that had not previously been documented
were identified by the EFS system, the agency could make minor
repairs before they become more expensive problems. All
together this resulted in a more efficient deployment of funds.
To illustrate the cost-effectiveness of conducting an EFS inspection,
the three bridges inspected for PENNDOT can be used as a case-study. Working
with PENNDOT data and following PENNDOT advice, policy, and practice,
the following savings were estimated and realized:
I-80 Canoe Creek Bridge (Total savings = $67,420)
Cause of savings – Elimination of planned cross-girder
repairs
Savings:
Repair mobilization $10,000
Maintenance
and protection of traffic $22,920
Repair $34,500
Total $67,420
I-476 in West Conshohocken (Total savings = $81,800)
Cause of savings – Elimination of planned stop drill repairs
Savings:
Repair mobilization $1,800
Repair $5,000
Total $6,800
Additional cause of savings – Cost of needing to restrict
traffic due to ineffective repairs
Savings: Estimated to be $75,000 for disruption
to commerce and the traveling public
I-81 over the Susquehanna River (Total savings =
$100,000)
Cause of Savings – Prioritization of repairs to avoid bridge
load restriction
Savings: Estimated to be $100,000 for
disruption to commerce and the traveling public
In total, these tests saved over $200,000 and cost just a fraction
of that to conduct. As a result of these savings and the
increase in safety resulting from the EFS inspections, PENNDOT
has initiated an on-call contract with MATECH to provide these
tests statewide.
CONCLUDING REMARKS
The EFS system is a novel NDE technique capable of detecting
active fatigue cracks that are smaller than those detectable
by other currently available techniques. Further, the fact
that EFS can detect whether a crack is actively growing gives
bridge owners never before available information that allows
for active prioritization of bridge repair/rehabilitation funds. The
ability to know which cracks require attention and which cracks
can conceivably be left as-is without structural impact has the
potential of allowing significant dollars to be more efficiently
allocated to fixing problems that could continue escalating in
scale.
EFS has been examined in side-by-side comparisons with currently
available NDE techniques during several field bridge inspections. These
comparisons have revealed that EFS consistently identifies all
cracks identified by other technologies and is able to detect
cracks that others can’t (even once their presence and
location is known). Additionally, EFS has been shown to
give owners information that no other technology can. Combined,
it is clear that EFS is an effective and cost-saving tool within
any active bridge management system.
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