U.S. patent application number 11/862897 was filed with the patent office on 2008-04-03 for eddy current testing apparatus and eddy current testing method.
Invention is credited to Yuuji Adachi, Katsumi Isaka, Kojirou Kodaira, Masahiro Koike, Kenji Kumasaka, Tetsuya Matsui, Mitsuru Odakura, Kazuhiro Suzuki, Yutaka Suzuki, Kenji Tayama.
Application Number | 20080079426 11/862897 |
Document ID | / |
Family ID | 38754757 |
Filed Date | 2008-04-03 |
United States Patent
Application |
20080079426 |
Kind Code |
A1 |
Suzuki; Yutaka ; et
al. |
April 3, 2008 |
EDDY CURRENT TESTING APPARATUS AND EDDY CURRENT TESTING METHOD
Abstract
The eddy current testing apparatus includes a probe having an
eddy current testing sensor including a pair of eddy current
testing coils. The apparatus also includes an eddy current testing
flaw detector inputting detection signals from the eddy current
testing sensor. The diameter of a magnetic core used in each of the
pair of eddy current testing coils is within the range of 0.1 mm to
0.5 mm.
Inventors: |
Suzuki; Yutaka; (Hitachi,
JP) ; Koike; Masahiro; (Hitachi, JP) ; Matsui;
Tetsuya; (Hitachi, JP) ; Kodaira; Kojirou;
(Hitachinaka, JP) ; Isaka; Katsumi; (Mito, JP)
; Odakura; Mitsuru; (Hitachi, JP) ; Tayama;
Kenji; (Mito, JP) ; Suzuki; Kazuhiro;
(Hitachi, JP) ; Kumasaka; Kenji; (Hitachi, JP)
; Adachi; Yuuji; (Hitachi, JP) |
Correspondence
Address: |
MATTINGLY, STANGER, MALUR & BRUNDIDGE, P.C.
1800 DIAGONAL ROAD, SUITE 370
ALEXANDRIA
VA
22314
US
|
Family ID: |
38754757 |
Appl. No.: |
11/862897 |
Filed: |
September 27, 2007 |
Current U.S.
Class: |
324/238 |
Current CPC
Class: |
G01N 27/902
20130101 |
Class at
Publication: |
324/238 |
International
Class: |
G01N 27/90 20060101
G01N027/90 |
Foreign Application Data
Date |
Code |
Application Number |
Sep 29, 2006 |
JP |
2006-267571 |
Claims
1. An eddy current testing apparatus, comprising: a probe having an
eddy current testing sensor including a pair of eddy current
testing coils; and an eddy current testing flaw detector inputting
detection signals from said eddy current testing sensor, wherein
diameter of a magnetic core used in each of said pair of eddy
current testing coils is within the range of 0.1 mm to 0.5 mm.
2. The eddy current testing apparatus according to claim 1, wherein
said pair of eddy current testing coils are disposed in said probe
and each axial central line of said magnetic core crosses an
external surface of said probe.
3. The eddy current testing apparatus according to claim 1, further
comprising: a rotating apparatus for rotating said probe.
4. The eddy current testing apparatus according to claim 1, further
comprising: a supporting member for supporting said probe by being
inserted into a hole formed in a test object.
5. The eddy current testing apparatus according to claim 4, wherein
a probe holding member mounted on said probe is slidably attached
to said supporting member.
6. The eddy current testing apparatus according to claim 5, wherein
a rotating apparatus for rotating said probe is mounted on said
probe holding member.
7. An eddy current testing apparatus, comprising: a probe having an
eddy current testing sensor, and for performing eddy current
testing of a test object; an eddy current flaw detector for
inputting a detection signal from said eddy current testing sensor;
and a supporting member for supporting said probe by being inserted
into a hole formed in said test object.
8. The eddy current testing apparatus according to claim 7, wherein
a probe holding member mounted on said probe is slidably attached
to said supporting member.
9. The eddy current testing apparatus according to claim 8, wherein
a rotating apparatus for rotating said probe is mounted on said
probe holding member.
10. An eddy current testing method for a turbine rotor comprising a
disc, a plurality of turbine blades disposed along the periphery of
said disc, and a plurality of pins for joining a blade fork portion
formed on each of said plurality of turbine blades to a disc fork
portion formed on said disc, comprising the steps of: inserting a
probe having an eddy current testing sensor into a hole formed
through the disc fork and blade fork by pulling out one of the
plurality of pins in a state that said blade fork portion is still
inserted into said disc fork portion; and performing eddy current
testing for at least part of internal surface of said hole by using
said probe.
11. An eddy current testing method for a turbine rotor comprising a
disc, a plurality of turbine blades disposed along the periphery of
said disc, and a plurality of pins for joining a blade fork portion
formed on each of said plurality of turbine blades to a disc fork
portion formed on said disc, comprising the steps of: pulling some
of the plurality of pins out of said disc fork portion and said
blade fork portion; inserting a probe having an eddy current
testing sensor into a hole formed through the disc fork and blade
fork by pulling out one of the plurality of pins in a state that
said blade fork portion is still inserted into said disc fork
portion; and performing eddy current testing for at least part of
the internal surface of said hole by using said probe.
12. The eddy current testing method according to claim 10, wherein
said pin to be pulled out is disposed at the outermost position of
said plurality of pins disposed in a radial direction of said disc
and joining said blade fork portion to said disc fork portion.
13. An eddy current testing method for a turbine rotor comprising a
disc, a plurality of turbine blades disposed along the periphery of
said disc, and a plurality of pins for joining a blade fork portion
formed on each of said plurality of turbine blades to a disc fork
portion formed on said disc, comprising the steps of: inserting a
probe having an eddy current testing sensor into a first hole
formed through said disc fork portion and a first blade fork
portion of a first turbine blade of said plurality of turbine
blades by pulling out a first pin, which joins said first turbine
blade to said disc, of said plurality of pins; inserting a
supporting member for supporting said probe into a second hole
formed through said disc fork and a second blade fork portion of a
second turbine blade, which is different from said first turbine
blade and is positioned in said periphery, of said plurality of
turbine blades by pulling a second pin, which joins said second
turbine blade to said disc, of said plurality of pins; and
performing eddy current testing for at least part of the internal
surface of said first hole by using said probe.
14. The eddy current testing method according to claim 13, wherein
said first pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said first blade fork portion to said disc
fork portion.
15. The eddy current testing method according to claim 13, wherein
said second pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said second blade fork portion to said
disc fork portion.
16. The eddy current testing method according to claim 13, wherein
said probe is inserted into said first hole by guiding a probe
holding member attaching said probe along said supporting
member.
17. The eddy current testing method according to claim 13, wherein
said supporting member is inserted into said second hole, and after
insertion of said supporting member, said probe is inserted into
said first hole.
18. The eddy current testing method according to claim 13, wherein
another supporting member for supporting said probe is inserted
into a third hole formed through said disc fork portion and a third
blade fork portion of a third turbine blade of said plurality of
turbine blades by pulling out a third pin, which is positioned in
said periphery and joins said third turbine blade to said disc, of
said plurality of pins in a state that said first turbine blade is
placed between said second turbine blade and said third turbine
blade.
19. The eddy current testing method according to claim 18, wherein
said third pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said third blade fork portion to said disc
fork portion.
20. An eddy current testing method for a turbine rotor comprising a
disc, a plurality of turbine blades disposed along the periphery of
said disc, and a plurality of pins for joining a blade fork portion
formed on each of said plurality of turbine blades to a disc fork
portion formed on said disc, comprising the steps of: pulling a
first pin, which joins a first turbine blade of said plurality of
turbine blades to said disc, of said plurality of pins out of a
first blade fork portion of said first turbine blade; pulling a
second pin, which joins a second turbine blade of said plurality of
turbine blades to said disc, of the plurality of pins out of said
first blade fork portion a second blade fork portion of said second
turbine blade; inserting a probe having an eddy current testing
sensor into a first hole formed through said disc fork portion and
said first blade fork portion by pulling out said first pin;
inserting a supporting member for supporting said probe into a
second hole formed through said disc fork and said second blade
fork portion by pulling out said second pin; and performing eddy
current testing for at least part of the internal surface of said
first hole by using said probe, wherein said second turbine blade
is different from the first turbine blade.
21. The eddy current testing method according to claim 20, wherein
said first pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said first blade fork portion to said disc
fork portion.
22. The eddy current testing method according to claim 20, wherein
said second pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said second blade fork portion to said
disc fork portion.
23. The eddy current testing method according to claim 20, wherein
said probe is inserted into said first hole by guiding a probe
holding member attaching said probe along said supporting
member.
24. The eddy current testing method according to claim 20, wherein
said supporting member is inserted into said second hole, and after
insertion of said supporting member, said probe is inserted into
said first hole.
25. The eddy current testing method according to claim 20, wherein
another supporting member for supporting said probe is inserted
into a third hole formed through said disc fork portion and a third
blade fork portion of a third turbine blade of said plurality of
turbine blades by pulling out a third pin, which is positioned in
said periphery and joins said third turbine blade to said disc, of
said plurality of pins in a state that said first turbine blade is
placed between said second turbine blade and said third turbine
blade.
26. The eddy current testing method according to claim 25, wherein
said third pin being pulled out is disposed at the outermost
position of said plurality of pins disposed in a radial direction
of said disc and joining said third blade fork portion to said disc
fork portion.
27. An eddy current testing method for a turbine rotor comprising a
disc, a plurality of turbine blades disposed along the periphery of
said disc, and a plurality of pins for joining a blade fork portion
formed on each of said plurality of turbine blades to a disc fork
portion formed on said disc, said each turbine blade being joined
to the disc by said plurality of pins disposed in a radial
direction of said disc, comprising the steps of: pulling said pin
disposed at the outermost position of said plurality of pins
disposed in the radial direction for said each turbine blade, out
of said disc fork portion and each blade fork portion; inserting a
probe having an eddy current testing sensor into a plurality of
holes, which are formed through disc fork portion and corresponding
blade fork portions by pulling said plurality of pins disposed at
said outermost position, in succession in a state that said blade
fork portions is still inserted into said disc fork portion; and
performing eddy current testing for at least part of internal
surface of said hole by using said probe.
28. The eddy current testing method according to claim 27, further
comprising the steps of: pulling out another pin, which is disposed
inside said pin pulled out, of said plurality of pins disposed in
the radial direction and joining one of said blade fork portion to
said disc fork portion, when there is a crack on at least part of
internal surface of said hole formed through said one of said blade
fork portions; and inserting said probe into another hole formed
through said disc fork portion and said one of said blade fork
portions by pulling said another pin.
29. The eddy current testing method according to claim 10, wherein
said probe is a probe having said eddy current sensor including a
magnetic core with a diameter within the range of 0.1 mm to 0.5 mm.
Description
CLAIM OF PRIORITY
[0001] The present application claims priority from Japanese
application serial no. 2006-267571, filed on Sep. 29, 2006, the
content of which is hereby incorporated by reference into this
application.
BACKGROUND OF THE INVENTION
[0002] The present invention relates to an eddy current testing
apparatus and an eddy current testing method, and more
particularly, to an eddy current testing apparatus and an eddy
current testing method preferably applicable to inspect internal
surfaces of fork pin holes formed in blade forks for turbine blades
attached to the rotor of a steam turbine.
[0003] To facilitate the manufacturing and maintenance of a steam
turbine used in a power generating plant, its rotational axis and
turbine blades are manufactured separately and then assembled.
Specifically, blade fork portions formed at the roots of the
turbine blades are assembled to disc fork portions formed on a disc
provided on the rotational axis of the steam turbine, and the
turbine blades are fixed to the disc by inserting pins into fork
pin holes formed in these fork portions (see FIG. 2 in Japanese
Patent Laid-open No. 2001-12208). As the steam turbine rotates,
stress is applied to the structural material of the turbine blade
in the vicinity of the fork pin holes in the blade fork portion.
Accordingly, cracks may be generated in the vicinity of the fork
pin holes in the turbine blade.
[0004] Conventional inspection for cracks in the vicinity of the
fork pin holes in the turbine blade is performed by removing the
turbine blade from the disc and then applying magnetic particle
testing (hereinafter referred to as MT). The MT is a method for
detecting a leak of a magnetic flux from a defect in a test object
when a magnetic field is applied to the test object. This MT is
applied to the turbine blade, which is a test object, as described
below. While a magnetic field is applied to the blade fork portion
of the turbine blade, the surface of the blade fork portion is
coated with magnetic metal particles on which a fluorescent
material is applied, the fluorescent material being accumulated by
the magnetic flux leaking from a defect. Ultraviolet rays are then
irradiated to the blade fork portion. The magnetic metal particles
accumulate in, for example, a defect in a fork pin hole. Since
ultraviolet rays are irradiated, whether the magnetic metal
particles accumulate can be determined by observing whether there
is fluorescent light, and thus whether there is a defect can be
determined. In inspection for defects on the basis of the MT, it is
necessary not only to remove pins by which a disc fork portion of a
disc and a blade fork portion of a turbine blade are joined but
also to remove the turbine blade from the disc. When the turbine
blade is inspected for defects on the basis of the MT, therefore,
it takes much time. Upon the completion of the inspection, an
additional task is needed to fit the turbine blade into the disc
and combine them with pins.
[0005] Eddy current testing (ECT) is often used as a method of
inspecting the surface of a test object for cracks. Particularly,
the ECT is widely used to inspect the internal surfaces of tubular
objects such as heat transfer tubes because an ECT probe can be
moved quickly in the tube and thus advantages of functions suitable
for high-speed ECT inspection can be fully taken. An example of ECT
is described in Patent Laid-open No. Hei 8(1996)-145954. In the ECT
disclosed in Japanese Patent Laid-open No. Hei 8(1996)-145954, a
test probe including an ECT sensor is inserted into a tube to check
whether the thickness of the tube is thinned and the interior is
corroded.
SUMMARY OF THE INVENTION
[0006] However, ECT has not been used for inspection for cracks on
the internal surfaces of fork pin holes in the steam turbine. As
described later, the conventional ECT probe has not been sufficient
to precisely detect the above crack generated on the internal
surface of a fork pin hole.
[0007] An object of the present invention is to provide an eddy
current testing apparatus and eddy current testing method that can
further improve testing precision in eddy current testing.
[0008] A feature of the present invention for attaining the above
object is that the diameter of a magnetic core used as an eddy
current testing coil included in an eddy current testing sensor
falls within the range of 0.1 mm to 0.5 mm. According to the
present invention, in a structure in which blade fork portions
formed at the roots of a plurality of turbine blades disposed along
the periphery of the disc of a turbine rotor are joined with disc
fork portion formed on the disc by use of pins, a crack which is
generated on at least part of the internal surface of a hole formed
through the disc fork portion and blade fork portion by pulling out
the pin can be precisely detected. Particularly, in the present
invention, it is possible to detect a minute crack that is
generated near a juncture of two fork portions oppositely-disposed
in adjacent blade fork portions, the juncture being formed on an
internal surface of a groove formed by the facing surfaces of these
fork portions, the internal surface being at least part of the
internal surface of the hole.
[0009] To bring the diameter of the magnetic core within the range
of 0.1 mm to 0.5 mm is a new fining obtained by the inventors, as
described later.
[0010] Another feature of the present invention is to insert a
probe having an eddy current testing sensor into the hole, which is
formed through the disc fork portion and blade fork portion by
pulling out the above pin while the blade fork portion is still
inserted into the disc fork portion and to perform eddy current
testing for at least part of the internal surface of the hole. This
feature can extremely shorten a time taken for the eddy current
testing because it is not necessary to remove the turbine blade
from the disc.
[0011] According to the present invention, testing precision in
eddy current testing can be further improved.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] FIG. 1 is an explanatory drawing showing a state in which
supporting rods of the eddy current testing apparatus shown in FIG.
2 are aligned to fork pin holes formed in a disc.
[0013] FIG. 2 is a structural diagram showing an eddy current
testing apparatus according to a preferred embodiment of the
present invention.
[0014] FIGS. 3A to 3C are a structural diagram showing a probe
shown in FIG. 2; FIG. 3A is a side view of a probe having an ECT
sensor; FIG. 3B is a cross sectional view of the probe at a
position at which the ECT sensor is set; FIG. 3C is a perspective
view of a pair of ECT coils included in the ECT sensor.
[0015] FIG. 4 is an explanatory drawing showing junctures between a
fork of a blade fork portion 4a and a fork of a blade fork portion
4b, the blade fork portion 4a being adjacent to the blade fork
portion 4b in the peripheral direction of the disc, and also the
scanning by the probe.
[0016] FIG. 5 is a flowchart showing a procedure executed in ECT
inspection using the eddy current testing apparatus shown in FIG.
2.
[0017] FIG. 6 is an explanatory drawing showing exemplary ECT
signals output from the eddy current testing apparatus shown in
FIG. 2.
[0018] FIG. 7 is an enlarged perspective view showing the blade
fork portion of a turbine blade under ECT inspection.
[0019] FIG. 8 is a structural diagram showing a combination portion
of the blade fork portion and the disc fork portion.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0020] Embodiments of the present invention will be described
below.
Embodiment 1
[0021] An eddy current testing apparatus, which is a preferred
embodiment of the present invention, inspects a blade fork portion
formed at the root of a turbine blade provided on the rotor of a
steam turbine and a disc fork portion formed on a disc.
Specifically, the eddy current testing apparatus checks whether
there is a crack on the internal surfaces of fork pin holes formed
in a blade fork portion and a disc fork portion.
[0022] Before explaining the eddy current testing apparatus in
present embodiment, the structure of the rotor of the steam turbine
will be schematically explained with reference to FIGS. 1, 7, and
8, the rotor having turbine blades and a disc being test objects.
The rotor (not shown) in the steam turbine has turbine blades 3 at
a plurality of stages, and is rotatably mounted in a turbine casing
(not shown). The rotor forms the disc 1 on the rotary axis thereof.
Many turbine blades 3 disposed along the periphery of the disc 1
are removably attached to the disc 1. A plurality of turbine blades
3 included in a turbine blade array in a single stage are mutually
linked at their tops by a shroud 7.
[0023] How the disc 1 and turbine blades 3 are joined together will
be specifically explained. Disc fork portions 2 are formed along
the outer periphery of the disc 1, and blade fork portions 4 are
formed at the roots of the turbine blades 3. The blade fork portion
is a embedding portion of the blade 3. The shape of the disc fork
portion 2 is such that a plurality of disc grooves 22 are formed in
parallel in the axial direction of the rotor at fixed intervals.
The disc fork portion 2 forms forks (fork projections) 23, each of
which is between two adjacent disc grooves 22. For example, six
forks 23 are formed in the disc fork portion 2 for each turbine
blade 3. The blade fork portion 4 is stated by forming a plurality
of fork grooves 24 at the root of the turbine blade 3 at fixed
intervals. The blade fork portion 4 has forks (fork projections)
25, each of which is between two adjacent fork grooves 24. For
example, five forks 25 constitute a blade fork portion 4. The
number of forks 23 and the number of forks 25 vary with the turbine
blades at different stages.
[0024] In each fork 23 of the disc 1, many fork pin holes
(hereinafter simply referred to as pin holes) 5B are formed. The
pin hole 5B is a round penetrated hole. Pin holes 5B are formed in
each fork 23 for each of the turbine blades 3 disposed along the
periphery of the disc 1 at fixed intervals. A plurality of pin
holes 5B are also formed in a radial direction of the disc 1 at
equal intervals. In present embodiment, three pin holes 5B are
formed in a radial direction for each turbine blade 3. The pin
holes 5B formed in the radial directions are concentric.
[0025] Of the forks 25 of the blade fork portion 4 disposed on
single turbine blade 3, three forks located at the center are
denoted forks 25B. These forks 25B each have a plurality of pin
holes 5A, which are round penetrated holes. In present embodiment,
each fork 25B has three pin holes 5A at equal intervals in the
longitudinal direction of the fork 25B. The positions of the three
pin holes 5A in the longitudinal direction match the positions of
the three pin holes 5B formed in the forks 23 in the radial
direction. Of the forks 25 of the blade fork portion 4, forks at
both ends of the blade fork portion 4 are denoted forks 25A. These
forks 25A each have a plurality of grooves 5C which have a shape
resulting from cutting the pin hole 5A in half (the groove is
referred to below as the half-round groove) and which are
positioned at both ends facing in the peripheral direction of the
disc 1. Three half-round grooves 5C are formed at the both ends
each in the longitudinal direction of the fork 25A. The position of
the half-round groove 5C at one end matches the position of the pin
hole 5A formed in the fork 25B in the longitudinal direction of the
fork 25. The position of the half-round groove 5C at the other end
matches the position of the pin hole 5A formed in the fork 25B of
another turbine blade 3 adjacent to the turbine blade 3 in the
peripheral direction of the disc 1. The pin hole 5A, pin hole 5B,
and half-round groove 5C have the same radius.
[0026] Each fork 25 of the turbine blade 3 is inserted into the
disc grooves 22 respectively. In other words, each fork 23 of the
disc 1 is inserted into a fork groove 24 of the turbine blade 3. In
this state, a plurality of turbine blades 3 are lined up on the
periphery of the disc 1 in the peripheral direction. The turbine
blades 3 disposed like this are attached to the disc 1 by a
plurality of fork pins 6. These fork pins 6 are inserted into the
pin holes 5B formed in the forks 23, which are aligned in the axial
direction of the rotor, the pin holes 5A formed in the forks 25B,
and the half-round grooves 5C (see FIG. 8). Three fork pins 6 are
inserted into each fork 25 of a single turbine blade 3. These fork
pins 6 are an outer fork pin 6A, a middle fork pin 6B, and an inner
fork pin 6C. The three fork pins 6 are disposed in a radial
direction of the disc 1; the outer fork pin 6A is at the outermost
position, the inner fork pin 6C is at the innermost position, and
the middle fork pin 6B is at the middle position.
[0027] Suppose that a plurality of turbine blades 3 are disposed on
the disc 1 in the peripheral direction, as indicated by turbine
blades 3a, 3b, and 3c shown in FIG. 1. One pin hole similar to the
pin hole 5A is formed by half-round grooves 5C that are formed in
the oppositely-disposed end surfaces of the forks 25A of the
adjacent turbine blades 3a and 3b, the pin hole extending across
these forks 25A (see FIG. 4). Junctures X and Y are formed between
the oppositely-disposed forks 25A. The juncture Y is diametrically
opposite to the juncture X.
[0028] The eddy current testing apparatus in a preferred embodiment
of the present invention will be described below in detail with
reference to FIGS. 1 to 3. As shown in FIG. 2, the eddy current
testing apparatus 19 in present embodiment has a sensor unit 16, an
eddy current flaw detector 17, and a computer 18. The sensor unit
16 includes a probe 8, a pair of supporting rods 9, a flexible
shaft portion 10, a supporting member 13, and a positioning device
14. The pair of supporting rods 9 are fixed to the supporting
member 13. A linking member 36 links ends of the supporting rods 9.
The pair of supporting rods 9 pass through a casing 10A of the
flexible shaft portion 10. The flexible shaft portion 10 is movable
along the supporting rods 9 in the axial direction of the
supporting rods 9. The probe 8 is attached to the casing 10A and
disposed between the pair of supporting rods 9. The ends of the
probe 8 and supporting rods 9 are streamlined so that they can be
inserted smoothly into pin holes. The outer diameters of the probe
8 and supporting rods 9 are the same as the inner diameters of the
pin holes 5A and 5B. The end of the supporting rods 9 and the probe
8 may be replaceable according to the inner diameter of the pin
holes formed in the disc 1 etc. The positioning device 14 is
omitted in FIG. 1.
[0029] The probe 8 has an ECT sensor 12 is mounted in a main probe
body 8a, as shown in FIGS. 3A and 3B. The ECT sensor 12 including
ECT coils 12a and 12b is disposed at the end portion of the main
probe body 8a. The ECT coils 12a and 12b are disposed side by side
in the main probe body 8a, from the outer surface of the main probe
body 8a toward the axial center of the main probe body 8a. A space
is left between the ECT coils 12a and 12b in the peripheral
direction of the main probe body 8a (see FIG. 3B). The ECT coils
12a and 12b are each structured by forming a coil 29 around a
magnetic core 15 (see FIG. 3C). The magnetic core 15 is made of a
magnetic material such as ferrite. Both the ECT coils 12a and 12b
use a magnetic core 15 with diameter of 0.5 mm. The ECT sensor 12
is a self-induced ECT sensor based on a differential coil method.
Both the ECT coils 12a and 12b use current to perform excitation
and output detection signals. A feature of the self-induced ECT
sensor based on the differential coil method in present embodiment
is that when a metal member being the test object is made of a
magnetic material and produces magnetic noise, the effect by the
noise can be canceled with ease by detecting a difference between
the signals from the two ECT coils 12a and 12b. When the effect by
the noise is small, a cross correlation method, in which one of the
two ECT coils 12a and 12b is used for excitation and the other is
used for detection, or a self-inducing method, in which a single
coil used, may also be applied.
[0030] In addition to the casing 10A, the flexible shaft portion 10
has a handle 11 rotatably attached to the casing 10A and a
rotational force transmitting mechanism (not shown) disposed in the
casing 10A. The rotational force transmitting mechanism has a
rotational axis and a bevel gear and the like for transmitting the
rotational force of the handle 11 to the probe 8. When the handle
11 is rotated, the probe 8 rotates. An angle meter (not shown) is
attached at another end, which is in the casing 10A, of the main
probe body 8a. The angle meter detects the rotational angle of the
probe 8. Another handle and transmission mechanism (not shown) may
be disposed in the supporting member 13 so that the pair of
supporting rods 9 can be moved right and left with respect to the
probe 8. When the other handle is rotated, the supporting rods are
moved right or left and thereby the space between the supporting
rods 9 can be adjusted according to the space between the pin holes
5B, as described later. To allow the pair of supporting rods 9 to
move right and left, the penetrated holes formed in the casing 10A
through which the supporting rods 9 pass need to be elongated to
the right and left.
[0031] The positioning device 14 has a plate-like position setting
member 32 and a stopper member 34. One end of the position setting
member 32 is attached to the supporting member 13, and the other
end is attached to one of the supporting rods 9. The position
setting member 32 is disposed in parallel to the supporting rods 9
and outside the flexible shaft portion 10. When the flexible shaft
10 moves in the axial direction of the supporting rods 9, the
movement is not restricted by the position setting member 32. A
plurality of positioning holes 33 are formed in the position
setting member 32 according to the positional relationship among
the pin holes 5B, half-round grooves 5C, and pin holes 5A. The
stopper member 34 is disposed on a side of the casing 10A and
extends toward the position setting member 32. The stopper member
34 has a stopper portion 35 that can be inserted into and removed
from the positioning hole 33. The stopper part 35 is structured in
such a way that, for example, a metal ball movable in a cylindrical
member in its axial direction is pressed downward by a coil spring.
The metal ball does not come off the cylindrical member.
[0032] A power supply (not shown) for supplying excitation current
and the coils 29 of the ECT coils 12a and 12b are connected with
different wires. These wires are each provided with a switch (not
shown) disposed in the casing 10A. A first switch is connected to
the coil 29 of the ECT coil 12a, and a second switch is connected
to the coil 29 of the ECT coil 12b.
[0033] A multi-conductor cable 21 is connected to the eddy current
flaw detector 17 and extends up to the inside of the casing 10A of
the flexible shaft portion 10. For example, a conductor included in
the multi-conductor cable 21 is a signal line that is connected to
the coil 29 of the ECT coil 12a and transmits a signal detected by
the ECT coil 12a. Another conductor is a signal line that is
connected to the coil 29 of the ECT coil 12b and transmits a signal
detected by the ECT coil 12b. Another conductor transmits a
switching command output from the eddy current flaw detector 17 to
the first and second switches. Another conductor is connected to
the above-mentioned angle meter. The eddy current flaw detector 17
is connected to the computer 18 through a cable 28. The computer 18
has a function for outputting control commands, such as an
inspection start command and inspection termination command
described later, and also has a signal processing function for
processing ECT signals, which are output from the eddy current flaw
detector 17 according to the signals detected by the ECT coils 12a
and 12b. Accordingly, the computer 18 practically includes a
controller for outputting control commands and a signal processor
for processing its ECT signals.
[0034] As described above, the eddy current testing apparatus 19 is
used to perform ECT inspection of the disc fork portion 2 of the
rotor of the steam turbine and the blade fork portion 4. The ECT
inspection will be described below in detail according to the
flowchart, shown in FIG. 5, which comprises steps 40 to 45. First,
the turbine casing is disassembled, and the rotor, on which a
plurality of turbine blades 3 are disposed, is taken out from the
turbine casing. The taken out rotor is rotatably placed on a pair
of supporting bases mounted on the floor. Fork pins 6 are then
pulled out of the disc 1 (step 40). In the process of removing the
fork pins 6, the outer fork pins 6A, which are disposed at the
outermost positions for a turbine blade array in a single stage,
are all pulled out. Although all turbine blades 3 included in the
turbine blade array face downward, they do not come off because
they are joined with the disc 1 by the middle fork pins 6B and
inner fork pins 6C.
[0035] The sensor unit 16 is mounted in an inspection place (step
41). The supporting member 13 of the sensor unit 16 is mounted on a
supporting device (not shown) placed on the floor so as to be
slidable in the axial direction of the supporting rods 9. The
height of the supporting device can be adjusted according to the
position of the pin hole under inspection. The targets that undergo
ECT inspection are the internal surfaces of pin holes 5A and 5B and
half-round grooves 5C into which an outer fork pin 6A has been
inserted. Specifically, ECT inspection is performed for the
internal surface of a pin hole 5B into which a single outer fork
pin 6A has been inserted as well as the internal surfaces of a pin
hole 5A and half-round grooves 5C on a single turbine blade 3. Upon
the completion of the inspection, ECT inspection is performed for
the internal surface of a pin hole 5B into which another outer fork
pin 6A has been inserted, which is adjacent to the outer fork pin
6A in the peripheral direction of the disc 1 as well as the
internal surfaces of a pin hole 5A and half-round grooves 5C on
another turbine blade 3. For example, suppose that the internal
surfaces of first pin holes under ECT inspection are the internal
surface of the pin hole 5A, formed in the blade fork portion 4b of
the turbine blade 3b, into which the outer fork pin hole 6A has
been inserted, as well as the internal surfaces of the pin hole 5B
and half-round grooves 5C on an extending line of the axial center
of the pin hole 5A. The pin hole 5A, pin hole 5B, and half-round
grooves 5C are collectively referred to below as pin holes under
inspection. The probe 8 is inserted into the pin hole under
inspection, as described later. The pair of supporting rods 9 are
inserted into the pin holes 5A, into which the outer fork pin 6A
has been inserted, formed in the blade fork portions 4a and 4c of
the turbine blades 3a and 3c, each of which is adjacent to the
turbine blade 3b in the peripheral direction, as well as into the
pin holes 5B and half-round grooves 5C on extending lines of the
axial center of these pin holes 5A. These pin holes 5A and 5B and
the half-round grooves 5C, into which the supporting rods 9 are
inserted, are collectively referred to below as supporting pin
holes. In FIG. 1, the end portions of the pair of supporting rods 9
are aligned to two supporting holes, corresponding to the turbine
blades 3a and 3c, into which the end portions of the supporting
rods 9 will be inserted. When an operator manually slides the
supporting member 13 with respect to the supporting device, the
pair of supporting rods 9 are inserted into the corresponding
supporting pin holes. When the pair of supporting rods 9 are
inserted into the corresponding supporting pin holes, the sensor
unit 16 is set at the inspection place. While the ECT inspection is
in progress, the supporting rods 9 are held by the supporting
member 13 mounted on the supporting device and the supporting pin
holes. It is also possible to use an arrangement in which a motor
is mounted in the supporting device so as to move the supporting
member 13 toward the disc fork portion 2 by driving the motor.
[0036] Next, the probe 8 is inserted into the pin holes under
inspection (step 42). Specifically, the operator manually moves the
flexible shaft portion 10 toward the disc fork portion 2 by using
the supporting rods 9 as a guide. Due to this movement, the end
portion of the probe 8 is inserted into the pin holes, including
the pin hole 5A formed in the blade fork portion 4 of the turbine
blade 3b. The positioning device 14 positions the ECT sensor 12
attached to the probe 8 in the pin holes under inspection.
Specifically, the positioning is performed by inserting the stopper
portion 35 of the stopper member 34 into the positioning hole 33
formed in the position setting member 32 at a prescribed position.
When the flexible shaft portion 10 is moved, the metal ball pushes
the coil spring upward, so the stopper portion 35 easily comes off
the positioning hole 33, making the flexible shaft portion 10
movable. The ECT sensor 12 is then positioned at a prescribed
position, for example, an angular portion formed by two facing
half-around grooves 5C formed in the forks 25A of the adjacent
turbine blades 3b and 3a. The ECT sensor 12 is zero-adjusted at a
point on other than the junctures of forks of adjacent blade fork
portions (step 43). A signal detected by the angle meter is input
to the eddy current flaw detector 17 through the cable 21 and then
input to the computer 18 through the cable 28. The computer 18,
that is, the signal processing unit, outputs information about the
rotational angle of the probe 8, which is detected by the angle
meter, to a display unit 20. The operator determines whether the
ECT sensor 12 faces a normal portion, that is, other than the
junctures X and Y, with reference to the displayed information
about the rotational angle. If the ECT sensor 12 faces one (X or Y)
of the junctures, the operator rotates the handle 11 to turn the
probe 8 so that the ECT sensor 12 faces a portion (preferably, a
portion free from cracks) on the internal surfaces of the
half-round grooves 5C between the junctures X and Y. In this state,
the operator enters an inspection start signal from an input device
(for example, a keyboard) connected to the controller. The
controller (computer 18) outputs an inspection start command to the
eddy current flaw detector 17 in response to the inspection start
signal. Upon the input of the inspection start command, the eddy
current flaw detector 17 outputs a start command to the first
switch and second switch to close them. Excitation current is
supplied from a power supply to the coils 29 of the ECT coils 12a
and 12b. Eddy current is then generated on the surface of the
half-round grove 5C, and currents inducted by the eddy current are
generated in the coils 29. The currents generated in the coils 29
become signals detected by the ECT coils 12a and 12b and are input
to the eddy current flaw detector 17 through the cable 21. The eddy
current flaw detector 17 takes a difference between these detection
signals by a circuit provided therein, and outputs the resulting
ECT signal to the signal processing unit (computer 18). The ECT
signal is output from the signal processing unit to the display
unit 20 and displayed on the display unit 20. If the ECT signal is
0, it indicates that the ECT sensor 12 is zero-adjusted. If the ECT
signal is not 0, the balance of a bridge circuit (or an equivalent
circuit) provided in the eddy current flaw detector 17 is adjusted
so that the ECT signal becomes 0. This completes the zero
adjustment of the ECT sensor 12.
[0037] Upon the completion of the zero adjustment, the probe
undergoes rotary scanning (step 44). Specifically, the operator
operates the handle 11 to rotate the probe 8 one turn in the pin
hole under inspection. In this rotary operation, the ECT sensor 12
rotates along the internal surfaces of the pair of half-round
grooves 5C. ECT inspection is performed for the internal surfaces
of the pair of half-round grooves 5C, which are included in the pin
holes under inspection and face each other. Since exciting current
is supplied to the ECT coils 12a and 12b, a detection signal output
from the ECT coil 12a and another detection signal output from the
ECT coil 12b are both input to the eddy current flaw detector 17,
as described above. The eddy current flaw detector 17 outputs an
ECT signal, which is a differential signal obtained according to
both these detection signals. The ECT signal is input to the signal
processing unit, in which the signal is processed. The signal
processing unit creates image information that represents the
relation between the amplitude of the ECT signal and the rotational
angle by using, for example, the input ECT signal and the
information about the rotational angle of the probe 8, which is
input from the angle meter. This image information includes, for
example, image information showing the relation between the
X-direction component of the amplitude and the rotational angle and
another image information showing the relation between the
Y-direction component of the amplitude and the rotational angle.
The signal processing unit outputs these image information to the
display unit 20, and the display unit 20 displays these image
information. When the above angle meter is not attached to the
sensor unit 16, the signal processing unit creates image
information that represents the relation between the amplitude of
the ECT signal and time.
[0038] FIGS. 6A and 6B show exemplary ECT signals output from the
eddy current flaw detector 17 to which signals detected by the ECT
coils 12a and 12b are input in ECT inspection of the internal
surfaces of the pair of half-round grooves 5C described above. Even
in a normal state in which the internal surfaces of the pair of
half-round grooves 5C are free from cracks, ECT pulses C1 with a
large amplitude are generated at the junctures X and Y, in response
to the shapes of the mating planes at the junctures X and Y (see
FIG. 6A). At positions other than the junctures X and Y, the ECT
signal is zero. When the internal surface of a half-round groove 5C
has cracks 27, near the junctures, that extend the axial direction
of the pin hole under inspection (see FIG. 7), the ECT signal
output from the eddy current flaw detector 17 is, for example, as
shown in FIG. 6B. In addition to the ECT pulses C1 generated at the
X and Y junctures, the ECT signal includes ECT pulses with an
amplitude larger than zero, the ECT pulses being generated at the
positions at which the cracks are present. When the internal
surface of a half-round groove 5C on the blade fork portion 4a
includes a crack 27 near the juncture X, the ECT signal includes an
ECT pulse C2 with an amplitude larger than zero at the position at
which the crack 27 is present. When the internal surface of a
half-round groove 5C on the blade fork portion 4b includes a crack
27 near the juncture Y, the ECT signal includes an ECT pulse C3
with an amplitude larger than zero. The cracks 27 generated on the
internal surfaces of the half-round grooves 5C are small, so the
amplitudes of the ECT pulses C2 and C3 are extremely smaller than
the amplitude of the ECT pulse C1.
[0039] When a crack 27 is generated near the juncture X or Y, the
conventional ECT sensor is affected by the ECT pulse C1 generated
at the juncture, so the ECT pulse corresponding to an extremely
small crack 27 cannot be separated from the ECT pulse generated at
a juncture. Therefore, the conventional ECT sensor cannot detect a
crack 27 generated near the juncture. The inventors examined
various methods for detecting a crack 27 generated on the internal
surface of a half-round groove 5C near its juncture, without being
affected by the ECT pulse C1. The inventors then newly found
through experiments that when the diameter of the magnetic core of
the ECT sensor is 0.5 mm or less, the spatial resolution of the ECT
sensor can be improved and thereby an ECT pulse generated on the
internal surface of the half-round groove 5C near its juncture in
response to the crack 27 can be separated from the ECT pulse at the
juncture. However, when the diameter of the magnetic core is less
than 0.1 mm, fabrication of the ECT coils become difficult. When
the diameter of the magnetic core of the ECT sensor falls within
the range of 0.1 mm to 0.5 mm, a crack 27 generated on the internal
surface of a half-round groove 5C near its juncture can be
detected.
[0040] Since the diameter of the magnetic core 15 is 0.5 mm in
present embodiment, a crack 27 generated on the internal surface of
a half-round groove 5C near its X or Y juncture can be
detected.
[0041] Upon the completion of the ECT inspection for the above pair
of half-round grooves 5C, the operator manually moves the flexible
shaft portion 10 to move the probe 8 within the above pin holes
under inspection, which corresponds to the blade fork portion 4b,
so that the ECT sensor 12 is positioned at a position in other pin
holes 5B and 5A in succession. The probe 8 is rotated at each
position, and ECT inspection is performed at that position.
Detection signals output from the ECT sensor 12 in the ECT
inspection are input to the eddy current flaw detector 17 and
output as ECT signals. The ECT signals are input to the signal
processing unit and processed therein.
[0042] Whether there is a crack is determined (step 45).
Specifically, the operator determines whether there is a crack on
the internal surfaces of the half-round grooves 5C that have
undergone ECT inspection, based on the information, which is
displayed on the display unit 20, obtained in the ECT signal
processing by the signal processing unit.
[0043] When the internal surface of any of the pin holes 5A and 5B
and half-round grooves 5C, which are pin holes under inspection,
does not have a crack, the flexible shaft portion 10 is manually
moved to pull out the probe 8 from the pin holes under inspection.
The supporting member 13 is also manually moved to pull out the
pair of supporting rods 9 from the supporting pin holes. The next
pin holes under inspection are the pin holes 5A and 5B and
half-round grooves 5C into which an outer fork pin 6A, by which the
turbine blade 3c adjacent to the turbine blade 3b is joined with
the disc 1, has been inserted. The position of the sensor unit 16
is adjusted in the height direction so that the probe 8 faces the
front of the next pin holes under inspection. Specifically, as
described above, the supporting rods 9 are inserted into the
supporting pin holes adjacent to this pin hole under inspection,
and the probe 8 is then inserted into the pin holes under
inspection. ECT inspection is performed for the internal surfaces
of the pin holes and like under inspection. As described above, ECT
inspection is performed for all pin holes under inspection into
which all outer fork pins 6A have been inserted, the outer fork
pins joining a turbine blade array in a single stage to the disc
1.
[0044] If a crack is found in a pin hole under inspection into
which an outer fork pin 6A has been inserted, for example, in
half-round grooves 5C as part of the pin holes under inspection
including the outermost pin hole 5A in the blade fork portion 4b,
the middle fork pin 6B for the turbine blade 3b is pulled out of
the disc 1. Of the pin holes under inspection including the pin
holes in which the middle fork pin 6B has been inserted, ECT
inspection is performed, as described above, for the internal
surfaces of the half-round grooves 5C inside the half-round groove
5C in which the crack has been found. If a crack 27 is also found
in these half-round grooves 5C, the inner fork pin 6C disposed on
the inner side is also pulled out. ECT inspection is performed for
the internal surface of the half-round grooves 5C as part of the
pin holes under inspection into which the middle inner fork pin 6C
has been inserted. The middle fork pin 6B and inner fork pin 6C are
inserted into the appropriate pin holes after the ECT inspection
for their corresponding pin holes under inspection has been
completed. Accordingly, if height adjustment by the supporting
device is not possible, even when the rotor is rotated on a pair of
supporting tables for alignment with the probe 8 before ECT
inspection is performed for pin holes under inspection
corresponding to another outer fork pin 6A, the inserted middle
fork pin 6B and inner fork pin 6C prevent the turbine blade 3b from
coming off.
[0045] After ECT inspection is completed for all pin holes under
inspection corresponding to all the above outer fork pins 6A, new
outer fork pins 6A, which are prepared separately, are inserted
into appropriate pin holes formed in, for example, the disc 1,
etc.
[0046] Of the pin holes 5A and 5B and half-round grooves 5C formed
in each fork 25, which are included as pin holes under inspection,
ECT inspection may be performed only for the internal surfaces of a
pair of half-round grooves 5C that are located at the frontmost or
backmost position in the direction of the insertion of the probe
8.
[0047] The present embodiment can improve detection accuracy for
cracks because the ECT sensor 12 having the magnetic core 15 with a
diameter of 0.5 mm is used. Particularly, it is possible to detect
even a small crack 27 generated on internal surfaces of half-round
grooves 5C near a juncture X or Y of forks 25A of adjacent blade
fork portions 4a and 4b. In present embodiment, since the ECT coils
12a and 12b of the ECT sensor 12 are disposed so that their axial
centers face the outer surface of the main probe body 8a, it is
possible to easily detect a crack, on the internal surface of a pin
hole 5A or 5B or a half-round groove 5C, that extends in the axial
direction of the pin hole. Since the probe 8 is rotated, the entire
inner surface of a pin hole or the like can be checked for a
crack.
[0048] In present embodiment, the rotational angle of the probe 8
is also detected. When both the rotational angle and the ECT signal
are considered, the operator can recognize which of the adjacent
turbine blades 3a and 3b has a crack 27 on the internal surface of
the half-round groove 5C formed on the blade fork portion 4, as
illustrated in FIG. 6B. Furthermore, the operator can not only
recognize the presence of the above crack 27 but also know its
position in the peripheral direction by displaying rotational angle
information and the ECT signals.
[0049] In ECT inspection, if the distance (referred to below as the
liftoff) between the ECT sensor and the surface of the target under
inspection changes, a signal detected and output also changes. In
precise measurement of cracks, therefore, the change caused by a
liftoff in the detection signal needs to be eliminated. To achieve
this, the probe 8 must be firmly supported. However, the area
around a disc fork portion 2, which undergoes ECT inspection in
present embodiment, is narrow, so to find a way for supporting the
probe 8 was a problem that is difficult to achieve. The inventors
were insistent in studying solutions for eliminating liftoff
factors when ECT inspection was performed for the internal surfaces
of the pin holes under inspection in the disc fork portion 2 and
blade fork portion 4. The inventors then arrived at a new idea that
pin holes formed in the disc 1 etc. so as to accept fork pins 6 are
used to hold the supporting member that supports the probe 8. A
pair of supporting rods 9 were thus provided to the sensor unit 16
and inserted into two supporting pin holes formed in the disc 1
etc., near the pin hole under inspection (preferably, the
supporting pin holes adjacent to the pin hole under inspection) so
that the probe 8 is held by the pair of the supporting rods 9.
Since, in present embodiment, the probe 8 is held by the supporting
rods 9 that are inserted into supporting pin holes formed in the
disc 1, etc. to accept fork pins 6, as described above, the probe 8
is firmly held with high precision. Accordingly, changes in liftoff
can be substantially reduced and thereby liftoff-caused changes in
detection signals output from the ECT coils 12a and 12b can be
substantially reduced, improving crack detection precision. The
supporting rods 9 function as a holding member and guide member for
the probe 8 attached to the flexible shaft portion 10. It is also
possible to support the probe 8 by inserting a single supporting
rod into a supporting pin hole. However, when two supporting rods 9
are inserted into two supporting pin holes, as in this embodiment,
the probe 8 is supported more firmly and thereby changes in liftoff
can be made smaller.
[0050] In present embodiment, it suffices to remove only fork pins
6 that are present in an area to be subject to ECT inspection from
the disc 1, etc., so the ECT inspection can be performed for the
internal surface of a pin hole under inspection with the turbine
blade 3 attached to the disc 1. This eliminates the need to remove
the turbine blade 3 from the disc 1 when ECT inspection is
performed for the fork portions, substantially shortening a time
taken for ECT inspection to be performed for the disc fork 2 and
blade fork 4. Furthermore, since ECT inspection is performed for
the internal surface of a pin hole under inspection with the
turbine blade 3 attached to the disc 1, ECT inspection can be
performed for the internal surfaces of the pin holes formed in the
disc fork 2 and blade fork 4 and the internal surfaces of the
half-round grooves 5C formed in the blade fork 4 in succession with
the probe 8 left inserted into the pin hole under inspection. This
scheme also contributes to further shortening in ECT inspection
time. One factor of shortening of the above ECT inspection time is
an arrangement in which the supporting rods 9 are inserted into
supporting pin holes.
[0051] In present embodiment, the outer fork pin 6A, disposed at
the outermost position in a radial direction of the disc 1, is also
pulled out, and ECT inspection is performed for the pin hole under
inspection into which the outer fork pin 6A has been inserted. One
turbine blade 3 is joined to the disc 1 by a middle pin 6B and an
inner pin 6C, which are disposed in a radial direction of the disc
1. Due to this arrangement, even when all outer fork pins 6A
disposed in a radial direction of the disc 1 are pulled out of a
turbine blade array in a single stage during ECT inspection, the
turbine blades 3 do not fall off the disc 1. In present embodiment,
ECT inspection is first performed for the pin hole under inspection
into which an outer fork pin 6A has been inserted. If a crack is
found on the internal surface of the pin hole under inspection, ECT
inspection is performed for the pin hole under inspection into
which the middle fork pin 6B has been inserted, the middle fork pin
6B being positioned inside the outer fork pin 6A. In this
embodiment, in which ECT inspection is performed as described
above, the number of fork pins 6 pulled out of the disc 1 can be
substantially reduced, so time taken in ECT inspection can be
further shortened. The number of fork pins 6 to be attached to the
disc 1 after the completion of the ECT inspection is also reduced,
so working time taken to attach the fork pins 6 is also greatly
shortened. While the steam turbine is operated, stress is generated
in areas, in the fork, around the pin holes under inspection into
which the fork pin 6 has been inserted. The stress in the area
corresponding to the outer fork pin 6A is greater than the stress
in the areas corresponding to the middle fork pin 6B and inner fork
pin 6C. Accordingly, if there is no crack on the internal surface
of the pin hole under inspection into which the outer fork pin 6A
has been inserted, no cracks are generated on the internal surfaces
of the pin holes under inspection into which the middle fork pins
6B and inner 6C have been inserted.
[0052] In present embodiment, of a plurality of fork pins 6
attached to the disc 1, all outer fork pins 6A attached at
outermost positions are removed and ECT inspection is performed. It
is also possible to remove all outer fork pins 6A, middle fork pins
6B, and inner fork pins 6C attached to the disc 1 within the range
of, for example, a 120.degree. area extending upward from the axial
center of the disc 1 and then perform ECT inspection by using the
eddy current testing apparatus 19 for all the pin holes under
inspection into which these fork pins have been inserted. Upon the
completion of the ECT inspection in this range, the removed fork
pins 6 are attached to the disc 1, and the rotor is rotated so that
another 120.degree. area faces upward. All fork pins 6 are pulled
out of the disc 1 in the other 120.degree. area and ECT inspection
is then performed. This ECT inspection is repeatedly performed for
each 120.degree. area.
[0053] In the above ECT inspection as well, the turbine blades 3 do
not fall off the disc 1, eliminating the need to remove the turbine
blades 3 from the disc 1. That is, when ECT inspection is performed
by using the probe 8 for the internal surfaces of pin holes under
inspection, the blade fork portions 4 can be left inserted into the
disc fork portion 2. This ECT inspection takes a longer inspection
time than in the embodiment described earlier, but takes a shorter
inspection time than the conventional inspection in which the
turbine blades 3 are removed from the disc 1 to check the blade
fork portions for cracks.
* * * * *