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| United States Patent Application |
20120001426
|
| Kind Code
|
A1
|
|
Yamashita; Shoki
;   et al.
|
January 5, 2012
|
HYDRAULIC DETACHABLE COUPLING
Abstract
A hydraulic detachable coupling, which can transmit rated torque in a
manner stable to vibrations, and can fully withstand abnormal torque. For
this purpose, in a hydraulic detachable coupling (4) mounted detachably
on a rotor (1) of a steam or gas turbine or other machine, a coupling
sleeve (4b), which is fitted on a shaft end portion of a casing
penetrating shaft (2) in the rotor (1), includes a taper hole portion
(4b-a) which is interference-fitted on a taper shaft portion (2a) of the
shaft end portion by a hydraulic pressure, and a straight hole portion
(4b-b) having teeth (13) engaging a plurality of teeth (12) formed in a
straight shaft portion (2b) of the shaft end portion, the taper hole
portion (4b-a) and the straight hole portion (4b-b) being located
adjacent to each other.
| Inventors: |
Yamashita; Shoki; (Takasago-shi, JP)
; Yashiki; Tadao; (Takasago-shi, JP)
; Ichiryu; Taku; (Akashi-shi, JP)
|
| Assignee: |
MITSUBISHI HEAVY INDUSTRIES, LTD.
Tokyo
JP
|
| Serial No.:
|
231071 |
| Series Code:
|
13
|
| Filed:
|
September 13, 2011 |
| Current U.S. Class: |
285/417 |
| Class at Publication: |
285/417 |
| International Class: |
F16L 21/00 20060101 F16L021/00 |
Foreign Application Data
| Date | Code | Application Number |
| Jul 18, 2006 | JP | 2006-195204 |
Claims
1-4. (canceled)
5. A hydraulic detachable coupling mounted detachably on a rotating shaft
of a rotating machine, comprising: a coupling sleeve which is fitted on a
shaft end portion of the rotating shaft, the coupling sleeve including an
interference fit portion which is interference-fitted on an outer
peripheral surface of the shaft end portion by a hydraulic pressure, and
an engagement portion which engages the outer peripheral surface of the
shaft end portion at a plurality of locations in a circumferential
direction, the interference fit portion and the engagement portion being
located adjacent to each other, wherein the engagement portion is a
straight hole portion having keyways formed therein, the keyways
corresponding to a plurality of keyways formed in a straight shaft
portion of the shaft end portion.
6. The hydraulic detachable coupling according to claim 5, wherein one of
the corresponding keyways is a groove of a rectangular cross section into
which a square key is inserted, and other of the corresponding keyways
are taper grooves of a semicircular cross section into which round taper
keys are inserted.
7. (canceled)
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a continuation application of U.S.
Non-Provisional application Ser. No. 12/304,844, filed Apr. 7, 2009,
which claims the benefit of PCT application PCT/JP2007/053133, filed Feb.
21, 2007 and Japanese Application No. 2006-195204, filed Jul. 18, 2006,
which are hereby incorporated by reference.
TECHNICAL FIELD
[0002] This invention relates to a hydraulic detachable coupling preferred
for use in a rotor of a rotating machine such as an electric generator, a
steam turbine, a gas turbine, or a compressor.
BACKGROUND ART
[0003] Generally, rotors of an electric generator, a steam turbine, a gas
turbine, or a compressor, for example, are coupled coaxially by a rotor
coupling (see Patent Document 1).
[0004] In the steam or gas turbine, gas seals (called mechanical seals)
101 may be installed at portions of a rotor 100 which penetrate a turbine
casing, as shown in FIG. 15. These are 360.degree. circular (endless)
components fitted from the shaft ends of the rotor 100. The gas seal 101
needs to be periodically detached and attached for maintenance and
checkup.
[0005] To enable the gas seal 101 to be detached and attached, therefore,
a rotor coupling 102A, which is installed at the shaft end of the rotor
100, is also designed to be capable of easy removal and reassembly. In
the illustrated example, for instance, a coupling sleeve 102a of the
rotor coupling 102A is increased in diameter by application of a
hydraulic pressure (see hydraulic paths 103 in the drawing), and then the
hydraulic pressure is released, whereby the coupling sleeve 102a is
interference-fitted (hydraulically fitted) to the shaft end of the rotor
100. From this state, on the other hand, a hydraulic pressure is applied
again to increase the diameter of the coupling sleeve 102a, whereby the
rotor coupling 102A can be removed from the shaft end of the rotor 100.
[0006] As shown in FIG. 16, moreover, there is a case in which an involute
spline tooth portion 104a cut in the outer periphery of the shaft end of
a rotor 100, and an involute spline groove portion 104b cut in the inner
periphery of a coupling sleeve 102b of a rotor coupling 102B are brought
into splined engagement with each other, and prevented by a press nut 105
from disengagement. [0007] Patent Document 1: JP-A-2003-65006
DISCLOSURE OF THE INVENTION
Problems to be Solved by the Invention
[0008] With the rotor coupling 102A as shown in FIG. 15, rated torque in a
shafting for driving the electric generator can be stably transmitted by
a frictional force attributed to the interference fit. However, there has
been the problem that the rotor coupling 102A cannot withstand abnormal
torque (usually, 5 to 10 times the rated torque) occurring in a
short-circuit accident or asynchronous input which is a special accident
of the electric circuit of the electric generator. That is, during the
occurrence of abnormal torque, slip occurs at the surface of pressure
contact between the outer peripheral surface of the shaft end of the
rotor 100 and the inner peripheral surface of the coupling sleeve 102a,
thereby inducing excessive vibration or damage.
[0009] The rotor coupling 102B as shown in FIG. 16, on the other hand, can
withstand abnormal torque because of its splined engagement, and can be
easily attached and detached. However, if the rotor 100 has a shaft with
a very large overall length (for example, exceeding 7 meters), as in an
upsized steam or gas turbine or compressor, the rotor coupling 102B has
presented the problem that cutting of a spline, such as the spline tooth
portion 104a or the spline groove portion 104b (by a gear cutting
machine), in the shaft end is difficult from the viewpoint of equipment.
[0010] The present invention has been accomplished in the light of the
above-described situations. It is an object of the invention to provide a
hydraulic detachable coupling which can transmit rated torque in a manner
stable to vibrations, and can fully withstand abnormal torque.
Means for Solving the Problems
[0011] A hydraulic detachable coupling according to the present invention,
intended for attaining the above object, is a hydraulic detachable
coupling mounted detachably on a rotating shaft of a rotating machine,
comprising: a coupling sleeve which is fitted on a shaft end portion of
the rotating shaft, the coupling sleeve including an interference fit
portion which is interference-fitted on an outer peripheral surface of
the shaft end portion by a hydraulic pressure, and an engagement portion
which engages the outer peripheral surface of the shaft end portion at a
plurality of locations in a circumferential direction, the interference
fit portion and the engagement portion being located adjacent to each
other.
[0012] The hydraulic detachable coupling is characterized in that the
interference fit portion is a taper hole portion corresponding to a
tapering-off taper shaft portion of the shaft end portion.
[0013] The hydraulic detachable coupling is also characterized in that the
engagement portion is a straight hole portion having teeth formed
therein, the teeth engaging teeth formed in a straight shaft portion of
the shaft end portion.
[0014] The hydraulic detachable coupling is also characterized in that the
teeth of the engagement portion, except for one of the teeth of the
engagement portion making high accuracy engagement without clearance,
engage a plurality of the teeth of the shaft end portion via taper
spacers disposed on both sides of other of the teeth of the engagement
portion.
[0015] The hydraulic detachable coupling is also characterized in that the
engagement portion is a straight hole portion having keyways formed
therein, the keyways corresponding to a plurality of keyways formed in a
straight shaft portion of the shaft end portion.
[0016] The hydraulic detachable coupling is also characterized in that one
of the corresponding keyways is a groove of a rectangular cross section
into which a square key is inserted, and other of the corresponding
keyways are taper grooves of a semicircular cross section into which
round taper keys are inserted.
[0017] The hydraulic detachable coupling is also characterized in that the
coupling sleeve is prevented from slipping off the rotating shaft, by
slipping-off preventing means secured to the shaft end portion.
Effects of the Invention
[0018] According to the features of the present invention, the
interference fit portion by the hydraulic pressure can stably transmit
rated torque while maintaining satisfactory shaft vibration
characteristics, whereas the engagement portion can sufficiently deal
with abnormal torque. As a result, a hydraulic detachable coupling having
high durability and involving low vibration can be realized.
BRIEF DESCRIPTION OF THE DRAWINGS
[0019] FIG. 1 is a side view of a rotor and a coupling showing Embodiment
1 of the present invention.
[0020] FIG. 2 is an enlarged sectional view of a coupling portion in FIG.
1.
[0021] FIG. 3 is a sectional view taken on line A-A in FIG. 2.
[0022] FIG. 4 is a sectional view taken on line B-B in FIG. 3.
[0023] FIG. 5 is a sectional view of a coupling portion showing Embodiment
2 of the present invention.
[0024] FIG. 6 is a sectional view taken on line C-C in FIG. 5.
[0025] FIG. 7 is a sectional view taken on line D-D in FIG. 6.
[0026] FIG. 8 is a sectional view of a coupling portion showing Embodiment
3 of the present invention.
[0027] FIG. 9 is a sectional view taken on line E-E in FIG. 8.
[0028] FIG. 10 is a sectional view of a coupling portion showing
Embodiment 4 of the present invention.
[0029] FIG. 11 is a view taken in the direction of an arrowed line G in
FIG. 10.
[0030] FIG. 12 is a sectional view taken on line H-H in FIG. 11.
[0031] FIG. 13 is a sectional view taken on line I-I in FIG. 12.
[0032] FIG. 14 is a sectional view taken on line J-J in FIG. 13.
[0033] FIG. 15 is a side view of a rotor and a coupling which represent a
conventional example.
[0034] FIG. 16 is a sectional view of another coupling according to the
conventional example.
DESCRIPTION OF THE NUMERALS
[0035] 1 Rotor [0036] 2 Casing penetrating shaft [0037] 2a Taper shaft
portion [0038] 2b Straight shaft portion [0039] 3 Gas seal [0040] 4 Rotor
coupling [0041] 4a Coupling flange [0042] 4b Coupling sleeve [0043] 4b-a
Taper hole portion [0044] 4b-b Straight hole portion [0045] 5 Rotor
[0046] 6 Spacer [0047] 7 bolt [0048] 8 Spiral groove [0049] 9a, 9b
Hydraulic path [0050] 10a, 10b O ring [0051] 11 Residual oil blowing hole
[0052] 12, 12A, 12B Tooth [0053] 13, 13A, 13B Tooth [0054] 14 Taper
spacer [0055] 15 Press plate [0056] 16 Clamping bolt [0057] 17 Spacer
hold-down screw [0058] 18 Press nut [0059] 19 Whirl-stop washer [0060] 20
Bolt [0061] 21 Coned disk spring [0062] 22 Liner [0063] 23 Square key
[0064] 24 Round taper key [0065] 25, 26 Groove of rectangular cross
section [0066] 28a, 28b Taper groove of semicircular cross section [0067]
29 Key hold-down screw [0068] 30 Screw hole
BEST MODE FOR CARRYING OUT THE INVENTION
[0069] A hydraulic detachable coupling according to the present invention
will now be described in detail by embodiments using the accompanying
drawings.
Embodiment 1
[0070] FIG. 1 is a sectional view of a rotor and a coupling showing
Embodiment 1 of the present invention. FIG. 2 is an enlarged sectional
view of a coupling portion in FIG. 1. FIG. 3 is a sectional view taken on
line A-A in FIG. 2. FIG. 4 is a sectional view taken online B-B in FIG.
3.
[0071] As shown in FIG. 1, 360.degree. circular (endless) gas seals
(called mechanical seals) 3 are detachably (removably) installed at
casing penetrating shafts 2 in right and left portions of a rotor
(rotating shaft) 1.
[0072] A rotor coupling 4 is mounted at the shaft end of one of the casing
penetrating shafts 2. One end of a rotor 5 (see FIG. 2) is coupled to the
same shaft by a bolt 7 via a spacer 6 (not absolutely necessary) through
the intermediary of a coupling flange 4a of the rotor coupling 4. The
rotor couplings 4 may be provided on both of the casing penetrating
shafts 2 (i.e., at opposite end portions of the rotor 1).
[0073] The rotor coupling 4 is composed of a hydraulic detachable
coupling. That is, as shown in FIG. 2, the shaft end of the casing
penetrating shaft 2 is constituted of a taper shaft portion 2a of a
tapered form having a slightly smaller diameter than that of the casing
penetrating shaft 2, and a straight shaft portion 2b connected to the
leading end of the taper shaft portion 2a. A taper hole portion
(interference fit portion) 4b-a, which is formed on the inner peripheral
surface of a coupling sleeve 4b of the rotor coupling 4 in correspondence
with the taper shaft portion 2a, is detachably mounted on the outer
peripheral surface of the taper shaft portion 2a by an interference fit
attributed to a hydraulic pressure.
[0074] In detail, a spiral groove 8 is formed on the outer peripheral
surface of the taper shaft portion 2a, and the spiral groove 8 is
supplied with a pressure oil from the end surface side of the straight
shaft portion 2b via hydraulic paths 9a, 9b during mounting and removal
of the rotor coupling 4. In FIGS. 2, 10a and 10b denote O rings which are
located on both sides of the spiral groove 8 and are provided on the
outer peripheral surface of the taper shaft portion 2a and on the
circumferential surface of the taper hole portion 4b-a. The numeral 11
denotes a residual oil blowing hole formed in the coupling sleeve 4b in
order to recover the pressure oil after mounting or removal of the rotor
coupling 4.
[0075] In the present embodiment, the straight shaft portion 2b, and a
straight hole portion (engagement portion) 4b-b of the coupling sleeve 4b
formed in correspondence therewith establish a structure in which teeth
12 and 13 formed therein engage each other.
[0076] As shown in FIGS. 3 and 4, the teeth 12 formed in the straight
shaft portion 2b are formed with a fanning cross section, and the teeth
13 formed in the straight hole portion 4b-b are formed with a rectangular
cross section. In each portion of their engagement, taper spacers 14
having a cone angle close to the angle of friction are interposed on both
sides of each tooth, except at one location where the straight shaft
portion 2b and the straight hole portion 4b-b mesh with high precision
without clearance for phase alignment during mounting of the rotor
coupling 4. For this purpose, both side surfaces of the tooth 12 formed
in the straight shaft portion 2b are formed as taper surfaces
corresponding to the taper spacers 14.
[0077] In FIG. 2, the numeral 15 denotes an annular press plate
(slipping-off preventing means) which is secured by a clamping bolt 16 to
the end surface of the straight shaft portion 2b of the casing
penetrating shaft 2 in order to prevent the rotor coupling 4 from
slipping off after the rotor coupling 4 is mounted. The numeral 17
denotes a spacer hold-down screw which is screwed into the press plate 15
in order to push in the taper spacer 14.
[0078] Because of the above configuration, when a pressure oil is supplied
from a hydraulic pressure supply source (not shown) to the spiral groove
8 of the taper shaft portion 2a via the hydraulic paths 9a, 9b, with most
of the coupling sleeve 4b of the rotor coupling 4 being loosely fitted on
the taper shaft portion 2a and the straight shaft portion 2b of the
casing penetrating shaft 2, the diameter of the coupling sleeve 4b (taper
hole portion 4b-a) is increased by the hydraulic pressure.
[0079] When, in this state, the rotor coupling 4 is pushed in by a
suitable means, the coupling sleeve 4b (taper hole portion 4b-a) is
fitted deeply (to a maximum) on the taper shaft portion 2a. Then, the
supply of the pressure oil is stopped and, at the same time, the
hydraulic paths 9a, 9b are switched to a drain side to discharge the
pressure oil. By so doing, the coupling sleeve 4b (taper hole portion
4b-a) is interference-fitted on the taper shaft portion 2a. At the time
of discharge of the pressure oil, pressurized air is blown in through the
residual oil blowing hole 11 to discharge the residual oil.
[0080] On this occasion, at the straight shaft portion 2b of the casing
penetrating shaft 2 and the straight hole portion 4b-b of the coupling
sleeve 4b, their teeth 12 and 13 engage in the circumferential direction,
with the taper spacers 14 being interposed therebetween. For this
engagement, phase alignment is carried out at the one location, i.e., an
engagement portion F where high accuracy engagement takes place without
clearance.
[0081] After the rotor coupling 4 is interference-fitted, the press plate
15, which engages the rotor coupling 4 in a slipping-off preventing
direction, is clamped by the bolt 16 onto the end surface of the straight
shaft portion 2b of the casing penetrating shaft 2. By so doing, the
interference-fitted state of the rotor coupling 4 is maintained.
Moreover, the taper spacer 14 is pushed in deeply by the spacer hold-down
screw 16 which is screwed into the press plate 15. Then, one end of the
rotor 5 is coupled to the coupling flange 4a of the rotor coupling 4 by
the bolt 7 via the spacer 6.
[0082] On the other hand, with the press plate 15 being detached along
with the spacer hold-down screw 16, the pressure oil is supplied again
from the hydraulic pressure supply source (not shown) to the spiral
groove 8 of the taper shaft portion 2a via the hydraulic paths 9a, 9b. As
a result, the diameter of the coupling sleeve 4b (taper hole portion
4b-a) is increased by the hydraulic pressure, whereby the
interference-fitted state of the coupling sleeve 4b (taper hole portion
4b-a) is released.
[0083] Then, simply upon supply of the hydraulic pressure, the rotor
coupling 4 is easily disengaged, together with the taper spacers 14, from
the casing penetrating shaft 2, for example, by pulling the rotor
coupling 4. Thus, the gas seals 3 can be disengaged from the casing
penetrating shaft 2 for replacement and maintenance.
[0084] In the present embodiment, while the rotor 1 is rotating, the rotor
coupling 4 deals with rated torque (normal torque) by use of frictional
torque at the interference fit portion between the taper shaft portion 2a
of the casing penetrating shaft 2 and the coupling sleeve 4b (taper hole
portion 4b-a) under the hydraulic pressure, and deals with abnormal
torque, such as one during short-circuiting of the electrical generator,
by utilizing the portion of engagement between the teeth 12 and 13 of the
straight shaft portion 2b of the casing penetrating shaft 2 and the
straight hole portion 4b-b of the coupling sleeve 4b.
[0085] Thus, in the rotor coupling 4, the interference fit portion due to
the hydraulic pressure has an interference margin sufficient for the
rotor 1 and the rotor coupling 4 to act as a single elastic body in
response to the lateral vibration of the shaft, so that stable shaft
vibration characteristics are obtained. A steam turbine and a gas turbine
generally rotate at a high speed and, in order for them to be kept with
minimal vibration, their axes have to be held in position relative to
each other at the portion of coupling between the adjacent rotors, and
this state has to be stably maintained. In the present embodiment, the
interference fit portion is subject to fitting of the taper surfaces, and
thus functions effectively.
[0086] In response to abnormal torque, such as that in the
short-circuiting accident of an electric generator, which is considered
to occur several times or less frequently during the total life of the
steam or gas turbine, the portion of engagement between the teeth 12 and
13 resists the marked slip of the rotor coupling 4, and this is capable
of preventing damage which makes the continued use of the rotor 1
difficult. On this occasion, the portion of engagement between the teeth
12 and 13 is brought into engagement by the taper spacers 14 without
play. Thus, all the teeth can be simultaneously resistant during abnormal
torque.
[0087] Furthermore, of the portions of engagement between the teeth 12 and
13, only one engagement portion F undergoes high accuracy engagement
without clearance. Therefore, an indexing mechanism as in a gear cutting
machine is not required. Even if the rotor 1 has a considerably long
shaft, it can be processed easily by an ordinary processing machine. In
other words, the introduction of equipment, which is expensive, but is
used with a low frequency, can be avoided. This is very advantageous in
the cost of production.
[0088] The reasons why the taper spacers 14 are disposed at positions on
both sides of the tooth at the portion of engagement between the teeth 12
and 13 are as follows: Abnormal torque in a short circuit of the
electrical generator as an accident appears as a positive-negative
alternate load, which has to be coped with by such disposition. Also,
accidental detachment has to be prevented under an abnormally heavy load.
Moreover, when the taper spacers 14 are mounted, their thickness
adjustment is easy to make because no play is present. When the taper
spacers 14 are dismounted, they are easy to withdraw. To fulfill all of
these requirements, it is preferred to adopt an angle close to the angle
of friction as the inclination of the spacer.
Embodiment 2
[0089] FIG. 5 is a sectional view of a coupling portion showing Embodiment
2 of the present invention. FIG. 6 is a sectional view taken on line C-C
in FIG. 5. FIG. 7 is a sectional view taken on line D-D in FIG. 6.
[0090] This is an embodiment in which at the portions of engagement
between the teeth 12A and 13A in Embodiment 1, the teeth 12A formed in
the straight shaft portion 2b are changed from a fanning cross sectional
shape to a rectangular cross sectional shape. Other features are the same
as those in Embodiment 1. Thus, the same members as those in FIGS. 2 to 4
are assigned the same numerals as in these drawings, and duplicate
explanations are omitted.
[0091] According to this embodiment, the advantage that the strength of
the teeth 12A formed in the straight shaft portion 2b can be enhanced is
obtained, in addition to the same actions and effects as those in
Embodiment 1.
Embodiment 3
[0092] FIG. 8 is a sectional view of a coupling portion showing Embodiment
3 of the present invention. FIG. 9 is a sectional view taken on line E-E
in FIG. 8.
[0093] This is an embodiment in which at the portions of engagement
between the teeth 12B and 13B in Embodiment 1, the teeth 12B formed in
the straight shaft portion 2b and the teeth 13B formed in the straight
hole portion 4b-b are engaged with each other, without using the taper
spacers 14, after processing by an ordinary processing machine such as a
lathe, and then performing polishing. In this case, it cannot be expected
for all the teeth to resist abnormal torque simultaneously. However,
because of the ductility of the rotor 1 and the rotor coupling 4
comprising an alloy steel, the load is borne, first of all, by the tooth
having a little play, sequentially by the tooth having more play, and
finally by all the teeth. Thus, no problem is posed.
[0094] In this embodiment, moreover, slipping-off of the rotor coupling 4
is prevented by a press nut (slipping-off preventing means) 18 which is
screwed to the shaft end of the straight shaft portion 2b, rather than by
the press plate 15. In FIG. 8, the numeral 19 denotes a whirl-stop washer
which engages the rotor coupling 4 to carry out whirl-stopping of the
press nut 18. The whirl-stop washer 19 is secured to the press nut 18 by
a bolt 20. The numeral 21 denotes a coned disk spring, and the numeral 22
denotes a liner.
[0095] In this embodiment as well, the same actions and effects as those
in Embodiment 1 are obtained.
Embodiment 4
[0096] FIG. 10 is a sectional view of a coupling portion showing
Embodiment 4 of the present invention. FIG. 11 is a view taken in the
direction of an arrowed line G in FIG. 10. FIG. 12 is a sectional view
taken on line H-H in FIG. 11. FIG. 13 is a sectional view taken on line
I-I in FIG. 12. FIG. 14 is a sectional view taken on line J-J in FIG. 13.
[0097] This is an embodiment in which the engagement structure by the
teeth 12 and the teeth 13 at the straight shaft portion 2b and the
straight hole portion 4b-b in Embodiment 1 is changed to an engagement
structure by a square key 23 and round taper keys 24.
[0098] That is, at the straight shaft portion 2b and the straight hole
portion 4b-b, one of keyways corresponding to each other is formed into
grooves 26, 25 of a rectangular cross section into which the square key
23 is inserted, while the other seven keyways corresponding to each other
are formed into taper grooves 28a, 28b of a semicircular cross section
into which the round taper keys 24 are inserted (see FIGS. 10 and 13).
[0099] Here, the grooves 26 and 25 of a rectangular cross section are
machined before the rotor coupling 4 (strictly, the taper hole portion
4b-a of the coupling sleeve 4b) is mounted on the casing penetrating
shaft 2 (strictly, the taper shaft portion 2a) by interference fit under
the hydraulic pressure. After the square key 23 is mounted in the groove
26 of the rectangular cross section on the side of the casing penetrating
shaft 2 (strictly, straight shaft portion 2b) by bolts 27, the rotor
coupling 4 is axially plunged and pressed in, with the square key 23
serving as a guide for phase alignment. On the other hand, after the
rotor coupling 4 is mounted on the casing penetrating shaft 2 by the
interference fit under the hydraulic pressure, the taper grooves 28a, 28b
of the semicircular cross section are formed by co-machining of the rotor
coupling 4 and the casing penetrating shaft 2. Then, the round taper keys
24 are inserted into taper grooves of a circular cross section which are
formed from the taper grooves 28a and 28b of the semicircular cross
section.
[0100] In FIG. 10, the numeral 29 denotes a round taper key hold-down
screw which is screwed into the press plate 15 to hold down the round
taper key 24, and the numeral 9a denotes a screw hole for connection of a
pressure oil supply pipe. In FIG. 14, the numeral 24a denotes an air vent
passage for use during insertion of the round taper key 24. The screw
hole 30 is used also in separately screwing a bolt into it and pulling
out the bolt when the round taper key 24 is to be detached. Other
features are the same as those in Embodiment 1. Thus, the same members as
those in FIG. 2 are assigned the same numerals as in this drawing, and
duplicate explanations are omitted.
[0101] According to the present embodiment, while the rotor is rotating,
the rotor coupling 4 can deal with rated (normal) torque by use of
frictional torque at the interference fit portion between the taper shaft
portion 2a of the casing penetrating shaft 2 and the coupling sleeve 4b
(taper hole portion 4b-a) under the hydraulic pressure, and can deal with
abnormal torque, such as one during short-circuiting of the electrical
generator, by utilizing the engagement structure attributed to the square
key 23 and the round taper keys 24 at the straight shaft portion 2b of
the casing penetrating shaft 2 and the straight hole portion 4b-b of the
coupling sleeve 4b. The same actions and effects as those in Embodiment 1
are obtained.
INDUSTRIAL APPLICABILITY
[0102] The hydraulic detachable coupling according to the present
invention is preferred for use in coupling the rotors of a rotating
machine coaxially.
* * * * *