Technical
Bulletin
Evolution
and Current Status of Nondestructive Evaluation of
Steam Turbines and Generators
Nondestructive
inspections of steam turbines and generators have been
performed for over a half-century. The early inspections
were performed during the manufacturing process by the
OEM and were typically limited to the large rotating forgings,
initially just the rotor forging. By current standards,
these early inspections were not very sophisticated and
the detection and flaw characterization capabilities were
correspondingly limited. Surface inspections that included
visual and magnetic particle techniques were the norm,
supplemented eventually with ultrasonic inspections performed
at relatively low test frequencies. Early ultrasonic practitioners
did not recognize certain physical characteristics of
the approach that are well established today, yet which
nonetheless limited the capabilities of the inspections.
For example, early inspections were conducted without
any consideration for the natural decay in beam intensity
with increasing propagation distance due to beam spread
and the effects of this on detection of deep-seated flaws.
Consequently, detection capabilities were very limited.
Starting
in the early 1950s, however, extensive research began
to promote a better understanding of the underlying fundamental
principles of the ultrasonic inspection technology. Once
the beam characteristics were understood, procedures began
to recognize the importance of corrections for a number
of factors affecting the sensitivity and accuracy of various
techniques, including compensation for the effects of
propagation distance on response strength, corrections
for surface curvature, compensation for the effects of
attenuation, and so on. Still, even with this improved
understanding of the physical parameters involved, the
inspections were performed manually, with heavy reliance
on observations made by an operator to detect, characterize,
classify, and size indications.
Beginning
with the advent of digital data acquisition capabilities
in the mid-1970s, a second evolution began to emerge,
this time involving the means of acquiring, processing,
and presenting the data for interpretation. The early
manual inspections have given way to the completely automated
inspections that are routinely performed today. Ultrasonic
imaging systems are standard. With these, the operator
can present different orthogonal views of the inspection
volume, with flaws presented within the volume at the
correct locations and relatively accurately relative to
size, shape, and orientation. Annular array systems provide
focused beam interrogation with electronically variable
focal depth, and linear array systems provide electronic
beam angulation or beam sweeping. Crack tip diffraction
techniques are used routinely to define flaw boundaries
and thereby provide greatly improved accuracy over early
amplitude-based sizing techniques. And digital filters
and processing algorithms are used to enhance data, extract
useful information, filter for specific features of interest,
and even perform automated processing and classification.
Processing steps have even been developed to look further
than the conventional distance/amplitude features of the
ultrasonic response, into frequency domain characteristics
that may indicate specific flaw characteristics, including
reflector type.
A
shift has also occurred in the types of inspections that
occur annually. Where components were once typically inspected
only during manufacture, today the predominant role of
inspection is to assess the condition of the component
after it has seen a period of service. Forging practices
have evolved to the point that an initial inspection for
life-limiting flaws is almost unnecessary because the
presence of such flaws in a modern forging is low probability.
Consequently, the role of the factory inspection is more
to establish a baseline for later comparison that to identify
conditions that are initially problematic in and of themselves.
In addition, inspections are no longer performed exclusively
by the OEM, permitting independent analysis that tends
to be less conservative and less expensive than with the
former. Non-OEM vendors, such as Structural Integrity
Associates (SI), now conduct large numbers of service
inspections and we are now even being requested to perform
pre-service inspections to establish the data baseline.
In
the past, most large turbine and generator rotor forgings
were bored from one end to the other as a means of removing
remnant ingot flaws that tend to consolidate to the center
of the ingot during solidification, and which are further
consolidated toward the center during the forging process.
This bore surface provides a convenient surface from which
an inspection can be conducted, and ultrasonic inspection
from the bore surface (boresonic) has become a standard
for pre-service inspection (PSI) and in-service inspection
(ISI) of such rotors. Most large turbine and generator
rotors currently in operation have central bores and undergo
periodic boresonic inspections as a means of assessing
present condition and possible flaw growth between inspections.
However, the presence of a bore, in and of itself, represents
a stress concentration and reduces tolerable flaw sizes
in the immediate vicinity of the bore. Therefore there
are certain advantages to be gained by eliminating the
bore. Under the improved steel-making practices now in
place, the reduction in potential flaw conditions near
the rotor centerline has over-ridden the stress effect
of the presence of a bore, and new or replacement rotors
often have no central bores.
Without
a bore, the standard for which rotor acceptance criteria
have been established no longer exists. One of the real
quandaries the NDE practitioner often finds himself in
involves inspection of components after some period of
operation but without benefit of any record of the initial
condition that existed prior to service. If no indications
are detected during the inspection, that is all well and
good and the initial ISI can serve as the baseline to
which subsequent inspections can be compared. However,
when indications are detected in the initial ISI without
benefit of a valid PSI baseline inspection, the NDE practitioner
is faced with the additional burden of attempting to characterize
the source of the indications as original discontinuities
or service-induced flaws, which is often a very difficult
distinction to make. Unless some positive evidence can
be produced to support a conclusion that the indications
were pre-existing, a conservative approach typically dictates
that the indications must be treated as service-induced
flaws, to be dealt with accordingly. In some cases, it
may be possible to perform additional inspections and/or
in-place metallography to help define the nature and source
of the indications. In other cases, it may even be possible
to remove material samples for detailed metallurgical
analysis to define the nature of the indication sources.
However, in turbine rotors this is typically not the case,
or at least not a desirable option. For indications arising
within the body of the forging, there is no known way
to obtain additional information on indications without
destroying the rotor. Even for blade attachments, where
service induced damage normally initiates at free surfaces,
the blades must be removed to access the surfaces. This
process is undesirable because it is very expensive and
provides an opportunity for damaging blades, disks, and
other components. Consequently, PSI becomes a vital step
in preparing such components for service.
SI’s
first introduction into rotor inspection began in the
1990s with the development of techniques to inspect nonmagnetic
retaining rings on generator rotors. Nearly all domestically-manufactured
rings were made of the same material, which has been found
to be susceptible to stress corrosion cracking (SCC) when
operated in a moist environment. Within the past twenty
years, a suitable replacement material has been introduced.
Many utilities, however, have elected to control the rings’
operating environment, i. e., keep the rings dry at all
times, and to conduct periodic inspection to assess the
effectiveness of their moisture mitigation programs. SI
developed an inspection program that has been very effective
and is routinely used today. This program follows the
recommended inspection protocol derived through an extensive
R&D effort conducted at the ERPI NDE Center. The program
features a multiple-inspection approach through which
the overall reliability of the inspection can be maximized.
For
many years now, SI has provided utilities with third party
analyses as alternatives to the conservative approaches
that OEMs typically follow relative to remaining life.
SI has developed a number of remaining life assessment
codes, including RRing-Life, developed under EPRI sponsor
for probabilistic assessment of generator retaining rings.
Similarly, SI has been an industry leader in probabilistic
assessment of rotors based upon boresonic inspection results.
More recently, SI has introduced our own boresonic inspection
capabilities for ISI. The boresonic system uses the latest
automation techniques and incorporates NDE techniques
to detect and size both pre-service indications and service-induced
flaws. The system has also been evaluated by demonstrating
its capability in the EPRI boresonic demonstration program,
and is the only system evaluated to date that has provided
100% detection in these trials.
To
complement rotor inspection, SI is currently participating
in an EPRI program to demonstrate our new ultrasonic linear
phased array technology for the inspection of disk blade
attachments. A linear array probe contains a series of
small, individual ultrasonic transducer elements arranged
in a row. Each element is supported by its own pulser/receiver
and is acoustically isolated from the other elements.
By controlling the timing of the pulse and reception for
each element, the angle, mode, and focus of the resulting
beam(s) can be accurately controlled electronically. For
straddle-mount disk rim dovetails, such as those typically
found on GE turbines, the linear array approach has been
proven effective through EPRI research. In fact, this
approach is rapidly becoming the state-of-the-art for
disk dovetail inspection. In the conventional approach,
a limited number of angles are used to test each hook
in the dovetail independently. There can be some error
in the selected angle relative to the optimum angle because
of uncertainty associated with the exact dovetail geometry
(i.e., choosing the correct angle), due to refracted angle
error (i.e., wedge angle tolerances, velocity variances,
etc.), and due to transducer position errors. The inspection
is also relatively time-intensive because each different
angle must be calibrated and implemented independently.
The use of the phased array technology provides a more
comprehensive inspection than can be accomplished with
the fixed-angle inspection. By electronically varying
the test angle, which is extremely rapid, all angles can
be conducted in a single scan rather than in multiple
scans, one per angle. In addition, prior knowledge of
the attachment geometry is not needed because the attachment
is reconstructed during the inspection process. Consequently,
the array inspection is not only much less time-intensive,
but also much more effective, accurate, and reliable.
As
of December 5, 2003, SI became the first company to complete
the data acquisition portion of the EPRI disk blade attachment
inspection demonstration program mentioned in the associated
article, “Evolution and Current Status of Nondestructive
Evaluation of Steam Turbines and Generators.” Refer
to that article for a technical description of the inspection
process. The data is currently being evaluated and initial
results look excellent. A report of this activity will
be completed by year end and submitted to EPRI for comparison
with the actual flaw sizes along with the results of the
other participants. EPRI expects to publish their final
report in 2004.
SI
will also make a report detailing our findings during
the inspection of the EPRI blade attachment demonstration
blocks available to our clients by early 2004.
Linear
phased array technology is also being developed for the
inspection of solid rotors, i.e., those not having a central
bore, as presented earlier. In the past, procedures for
inspecting unbored rotors have varied from using a single
transducer with a large beam spread to inspect the centerline
region, to using a number of different beam angles to
collectively cover the desired inspection volume at angles
appropriate for detection of the flaw orientations of
interest. Linear phased array offers an effective means
of implementing multiple angle inspections for all of
the inspections defined above. For the cylindrical sections
of the rotor body, electronic beam angulation can be used
to steer the beam from a purely radial path to interrogate
away from the rotor center for radial-axial discontinuities.
A much superior result is achieved because of the relatively
fine angulation index, say ½-degree or 1 degree,
over the range of angles needed rather than at a single
angle or limited number of selected angles.
SI
continues to provide innovative, state-of-the-art inspection
and condition assessment technologies for critical power
plant inspection applications. For additional information
on our turbine and generator condition assessment capabilities,
contact Larry Nottingham lnotting@structint.com at our
Charlotte, North Carolina office (704-573-1369), Ron O’Hara
rohara@structint.com at the Rockville, Maryland office
(301-231-7746), Harold Queen hqueen@structint.com in our
Florida office (954-572-2902), or Paul Sabourin psabourin@structint.com
(704-957-5243) out and about in his motor home.
Boresonic
system inspection of an in-service rotor.

Development
of phased array inspection for straddle-mount disk blade
attachment.

Phased array sector scan image overlaid on straddle-mount
disk blade attachment geometry with flaws shown at points
1, 2, and 3. Actual field TOFD Image of a fatigue crack
in a weldment.

