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Fiber Optic Sensors for Predictive Health
Monitoring
Jason W. Borinski, Clark D.
Boyd, Jason
A.
Dietz
Luna Innovations, Blacksburg, VA
24062-
1704
John
C. Duke, Michael R. Horne
Virginia Tech, Blacksburg,
VA 2406 1-02
19
Abstract
The ability to
predict the onset of failure in mechanical systems
is key to the reduction in
maintenance
costs, downtime, and health hazards in industrial
environments. Vibration
monitoring can
be used to spot mechanical problems, trigger
preventative maintenance
and diagnose
the health of rotating machinery. Accelerometers
are used in this role
to
detect defects in rotating components
through analysis of harmonics in the
power-frequency distribution. Further,
high frequency acoustic emission sensors can be
used to determine crack growth in metal
components or failures in composite structures.
Currently, a variety of
MEMS
accelerometers and piezoelectric
acoustic emission sensors
are used in
health monitoring that are limited by their size,
cost, and performance. Optical
fiber
sensors are rapidly emerging as viable
alternatives to these devices as effective
means of health monitoring in harsh
environments. These sensors are tolerant to
extreme
temperature, EMI, shock and
vibration, and offer reduced weight and increased
accuracy
over conventional
instrumentation.
As
a
result, these sensors have begun to replace
conventional sensors in harsh
environment applications. Optical fiber sensors
offer much
smaller size, reduced
weight, ability to operate at temperatures
up
to
2000
,
immunity
to
electromagnetic
interference, resistance to corrosive
environments, inherent safety within
flammable environments, and the ability
to multiplex multiple sensors on
a
single optical
fiber. This
paper presents the research and development of
both low-profile fiber
optic-based
acoustic emissions sensors for use in
nor
destructive evaluation
systems and
fiber optic accelerometers
for harsh environment health monitoring
applications.
Keywords
:
optical fiber sensors, Fabry-Perot,
interferometer, nondestructive evaluation,
health monitoring, acoustic emission,
accelerometer
1
Introduction
Fiber optic sensors have
been established as one of
the best available technologies for
acquiring
measurements
in
harsh
environments.
These
sensors
are
tolerant
to
extreme
temperature, EMI,
shock and vibration, and offer reduced weight and
increased accuracy
over
conventional
instrumentation.
As
a
result,
these
sensors
have
begun
to
replace
conventional electrical sensors in many
applications, and have been proposed for use in
health
monitoring
aboard
high
performance
aircraft.
For
example,
the
immunity
to
electromagnetic
interference
is
especially
advantageous
in
environments
where
electromagnetic interference is
unavoidable, such as near radar emitters or on the
skin of
spacecraft
and
re-entry
vehicles.
Further,
a
single
optical
fiber
can
support
multiple
sensors, reducing the weight and
increasing aircraft efficiency and performance.
Fiber
optic
strain
and
temperature
technology
has
already
found
acceptance
among
commercial users. However, more
advanced sensors, such as accelerometers and
acoustic
emission
sensors,
are
still
used
primarily
in
R&D
applications
in
the
aerospace
community. The authors developed the
fiber optic acceleration sensors discussed here
for
use
in
severe
flight
environments,
specifically
for
airborne
measurements
on
board
the
NASA
F-18
Systems
Research
Aircraft
(SRA).
The
performance
of
the
fiber
optic
accelerometer
compares
well
with
that
of
conventional
accelerometers,
with
the
added
gain of
reduced weight, increased temperature tolerance
and EM1 immunity. The flight
testing
and qualification of these sensors on board the
SRA
will validate the all-
optical
instrumentation
concept.
The
transition
of
the
technology
to
general
industrial
health
monitoring
will
depend
on
the
system
cost,
usability,
and
performance
gains
of
over
conventional sensing methods.
In addition, this paper
reviews the development of both broadband and
resonant optical
fiber
sensors
for
monitoring
acoustic
emission
for
NDE
of
composite
and
aluminum
structures.
High
frequency
acoustic
emission
sensors
can
be
used
to
determine
crack
growth in metal
components or various damage events in composite
structures, such
as
fiber
breaks,
matrix
cracking,
or
delaminations.
Currently,
a
variety
of
piezoelectric
acoustic
emission sensors are used in health monitoring
that are limited by their tolerance
of
extreme
temperature,
their
size,
cost,
and
performance.
Optical
fiber
sensors
are
rapidly
emerging
as
viable
alternatives
to
these
devices
as
effective
means
of
health
monitoring.
As
a
result,
these
sensors
have
begun
to
replace
conventional
electrical
sensors in many applications, and have
been proposed for
use in nondestructive
(NDE)
health monitoring in extreme
harsh environment conditions. This paper also
discusses the
research and development
of low-profile fiber optic-based AE sensors for
non destructive
evaluation (NDE)
systems.
2 Fiber optic accelerometer
development
The design of the fiber
optic accelerometer (FOA) is focused on creating a
thermally
stable, ultra-miniature, low
profile sensor through the use of silicon
micromachining
technology. This
technology obtains exceptional quality, high
yields, dimensional
accuracy, and
sensor head stability, all of which are required
for a reliable low cost
accelerometer.
The accelerometer design is based on a suspended
silicon mass that is
excited
proportionately by acceleration. The design
concept is shown in Figure 1.
Acceleration is measured by monitoring
an extrinsic Fabry-Perot interferometer (EFPI)
formed by the endface of a fiber and
the surface of a moving micromachined silicon
diaphragm. Movement in the mass is then
monitored by measuring the distance between
the mass and fiber using
interferometric techniques. The device is a
version of an offthe-
shelf
accelerometer made by a commercial accelerometer
manufacturer, modified to
incorporate
an optical fiber and the interferometric
monitoring techniques. In this manner,
the fiber optic accelerometer retained
the performance characteristics of the
conventional
sensor while demonstrating
increased resolution and temperature
tolerance
due to the
optical measurement technique.
Additional accelerometer models can be retrofitted
similarly with this technique.
A
picture of the
FOA
used in testing is shown
in Figure
2.
A
high frequency dual-
wavelength demodulation system' was used to test
the
FOA.
The
scope trace in Figure
3
demonstrates the operation of the
optical demodulation system
and the
FOA
compared with a
piezoelectric accelerometer. Figure
3
shows the two
channel
outputs of the photodetectors before demodulation
(channels 1 and 2), the output
of the
signals after demodulation representing the
movements of the mass measured by
the
EFPI technique (channel 3), and the output of a
conventional reference accelerometer
(channel
A).
This
figure demonstrates the correlation between the
output of the fiber optic
system and
the conventional reference accelerometer. The 10-g
low profile accelerometer
was evaluated
for frequency response and to determine its
transfer function. The high
frequency
dual wavelength prototype system was used for
demodulation of the optical
signal, and
a TrigTek signal conditioner and a model 6810
calibration accelerometer
provided
absolute data for comparison, as shown in Figure
4.
The transfer function, or
system input/output response,
is
shown in Figure
5.
The response is linear
with a system
constant of 40.8 [ d g ,
gap movement per g acceleration], giving a minimum
detectable
level of 0.025g using the
current demodulation system. The frequency
response of the
sensor is shown
in
Figure
6.
The response curve showed less than 0.4
dE3 of variation in
response from DC to
1.6
kHz.
The sensor is
slightly underdamped with a resonant
frequency of 2
kHz
and a high order roll-off.
The final
sensor specifications for the FOA are shown in
Figure
7
and a packaged,
flightqualified sensor is shown in the
photograph of Figure 8. This sensor, currently
available off-the-shelf, offers
increased temperature tolerance, EM1 immunity,
reduced
weight, and greater durability
over the conventional sensor performance.
3
Fiber optic acoustic emission sensor
development
This section
reports the results of the development of fiber
optic-based acoustic emission
(AE)
sensors for non-destructive evaluation
(NDE)
systems. The authors
have employed
the extrinsic Fabry-Perot
interferometer (EFPI) sensing technology to
measure both
in-plane and out-of-plane
acoustic stress waves with both resonant and
broadband sensor
designs. The sensors
have been evaluated for sensitivity and
performance compared to
existing
conventional technologies such as piezoelectric
transducers. Further, feasibility
experiments were conducted,
demonstrating EFPI AE sensors in applications such
as leak
detection, crack propagation
detection and health monitoring of composite
pressure
vessels and bridge decks. The
authors continue to demonstrate the inherent
advantages of
fiber optic AE sensors
(over conventional AE sensors) through multiple
development
programs both government
and commercial.
3.1 EFPI Sensor Design
3.1.1
EFPI AE Broadband In-
plane Sensor
The broadband-type optical
fiber acoustic emission sensor is based on the
extrinsic
Fabry-Perot interferometric
(EFPI) displacement sensor. With the appropriate
design, the
EFPI sensor can be
configured to monitor strain, pressure,
temperature, chemical
concentration,
acceleration and acoustic waves. The following
sections give a background
of the EFPI
sensor and proposed modifications to obtain a
resonant type AE sensor. The
conventional extrinsic Fabry-Perot
interferometric (EFPI) sensor geometry is shown in
Figure 9. Here, a 1300 nm singlemode
fiber transmits light from a laser diode to the
sensor element. An interferometric
cavity is formed between a signal fiber and
reflector
fiber aligned within a silica
capillary tube. The entire sensor is attached to
the surface
under study with an epoxy
or other appropriate adhesive. The surface
displacement
caused by the impinging
stress wave changes the length
of
the interferometric cavity,
which can be measured extremely
accurately through the optical demodulation
system.
Figure 9.
Conventional EFPI strain sensor element.
Inherent in this broadband sensor
design is the primary sensitivity to displacement
along
the axis of the sensor. This
causes the sensor to be selectively sensitive to
in-plane
acoustic energy. This differs
from conventional piezoelectric sensors, which are
primarily
sensitive to out-of-plane
energy. The uniaxial sensitivity can be used to
characterize the
nature of the
AE
event using multiple
sensors oriented in orthogonal planes. Further,
the
sensor can be oriented in the
direction of the grain of the material under
study, such as in
a unidirectional
composite material, to achieve the best
sensitivity to failures in the
material, such as fiber breakage or
debonding. Finally, the extreme low profile of the
sensor enables placement within layered
materials, monitoring
AE
events within each
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