Technical Field
[0001] The present invention relates generally to a reaction-type steam turbine and, more
particularly, to a reaction-type steam turbine capable of removing a vortex phenomenon
in a housing and maximizing energy output by reducing an initial load against a rotation
of a turbine shaft.
Background Art
[0002] As well known in the art, a reaction-type steam turbine is a machine suitable for
medium and small capacity prime movers because it obtains rotational energy from reaction
of steam energy being discharged and has a simple structure and high thermal efficiency.
[0004] FIG. 1 is a perspective view showing a part of a reaction-type steam turbine according
to the related art, and FIG. 2 is a front cross-sectional view showing the reaction-type
steam turbine.
[0005] As shown in FIGS. 1 and 2, the steam turbine includes a housing 10, a turbine shaft
20 rotatably supported by the housing 10 in the housing 10, and a plurality of disk
blades 30 installed in the housing 10 and integrally rotating with the turbine shaft
20, the disk blades being arranged in parallel along the lengthwise direction of the
turbine shaft 20.
[0006] Herein, the housing 10 is provided with a steam inlet tube 11 and a steam outlet
tube 12, and steam introduced through the steam inlet tube 11 rotates the plurality
of disk blades 30 while sequentially passing through the disk blades 30 to drive the
turbine shaft 20, and then is discharged through the steam outlet 12.
[0007] Here, as shown in FIG. 2, each of the disk blades 30 is provided with a nozzle hole
31 and an inlet hole 32, such that when steam introduced into the inlet hole 32 is
discharged to the nozzle hole 31, the disk blade 30 is rotated by reaction of the
discharged steam.
[0008] Here, in accordance with this principle, the steam discharged from the nozzle hole
31 of each disk blade 30 enters the inlet hole 32 of the adjacent disk blade 30, thereby
rotating the disk blade 30. Consequentially, all the disk blades 30 are rotated due
to reaction of the steam, thereby rotating the turbine shaft 20 connected to the plurality
of disk blades 30 to perform power generation.
[0009] On the other hand, the aforementioned conventional reaction-type steam turbine has
the following problems.
[0010] The steam introduced through the steam inlet tube 11 is introduced into a turbine
entrance 13 and then must be diverted toward the inlet hole 32 of the disk blade 30
(toward the right side in the drawing). However, the steam introduced through the
steam inlet tube 11 may fail to be diverted to the disk blades 30 from the turbine
entrance 13, and thus as shown in FIG. 3, a vortex phenomenon occurs due to steam
that swirls in the turbine entrance 13.
[0011] Thus, since steam may fail to efficiently flow into the disk blades 30, it is difficult
to maximize the rotational output of the turbine shaft 20.
[0012] Further, due to the vortex phenomenon, there is a problem that the friction loss
is large.
Documents of Related Art
(Patent Document)
Disclosure
Technical Problem
[0014] Accordingly, the present invention has been made keeping in mind the above problems
occurring in the related art, and an object of the present invention is to provide
a reaction-type steam turbine, in which a guide blade assembly is installed on a turbine
shaft at a position where a turbine entrance is provided such that steam introduced
through the turbine entrance is automatically guided to disk blades, thereby removing
a vortex phenomenon and maximizing the output of the turbine shaft.
Technical Solution
[0015] In order to accomplish the above object, the present invention provides a reaction-type
steam turbine, including: a housing provided at a first side thereof with a steam
inlet tube and at a second side thereof with a steam outlet tube, the housing having
a space formed therein; and a turbine shaft provided to pass through the space of
the housing, with a plurality of disk blades fitted over the turbine shaft, wherein
a guide blade assembly is coupled to the turbine shaft at a position between a duct
of the steam inlet tube and the disk blades, the guide blade assembly guiding steam
introduced through steam inlet tube into the space of the housing toward the disk
blades.
[0016] The guide blade assembly may be provided with a plurality of drag blades radially
arranged along a circumference of the turbine shaft, and facing the steam introduced
through the steam inlet tube.
[0017] Each of the drag blades of the guide blade assembly may be formed such that an end
of each drag blade is bent toward the steam inlet tube in a curved shape, such that
a flow of the steam is guided to flow only toward the disk blades.
[0018] The space of the housing may include: a turbine entrance directly connected to the
duct of the steam inlet; and turbine spaces provided at a side of the turbine entrance
and arranged such that the turbine shaft having the plurality of disk blades is placed
perpendicular to the steam inlet tube, and the guide blade assembly is coupled to
the turbine shaft at a position where the turbine entrance is provided.
Advantageous Effects
[0019] The reaction-type steam turbine according to the present invention has the following
effects.
[0020] First, since the guide blade assembly for guiding steam introduced through the steam
inlet tube to the disk blades is provided at a position where the turbine entrance
is provided in the housing, a vortex phenomenon is removed.
[0021] In other words, since the flowing direction of steam introduced into the turbine
entrance from the steam inlet tube can be directly diverted to the disk blades by
the guide blade assembly, the steam can be introduced into the disk blades without
staying in the turbine entrance. Accordingly, a vortex phenomenon occurring due to
a steam swirling can be removed.
[0022] Consequentially, it is possible to prevent friction loss caused by the vortex phenomenon,
and thereby it is possible to realize improved energy efficiency and to maximize rotational
output of the turbine shaft.
[0023] Second, since the turbine shaft can be rotated firstly by the rotation of the guide
blade assembly prior to rotation of the disk blades by the steam inflow, it is possible
to reduce the load required to initially start the turbine shaft.
[0024] In other words, since the turbine shaft can be rotated firstly by pressure applied
to the guide blade assembly due to the pressure-feeding force of steam initially introduced
straight from the steam inlet tube, it is possible to reduce the load required when
the turbine shaft is secondarily and earnestly rotated by the rotation of the disk
blades.
[0025] Third, as described above, since the rotational force of the turbine shaft is increased
by using the pressure-feeding force of the steam that rotates the guide blade assembly,
the rotational force of the turbine shaft can be doubled in comparison with the rotational
force of the turbine shaft that is rotated only by the reaction force of the disk
blades in the related art.
[0026] Consequentially, there is an effect that the output of the turbine can be maximized.
[0027] Fourth, since the guide blade assembly is provided with the drag blades that face
the direction in which steam is introduced, it is possible to increase the rotational
output of the turbine shaft.
[0028] In other words, since the guide blade assembly is structured to rotate through drag
of the steam, the rotational output of the turbine shaft can be maximized.
Description of Drawings
[0029]
FIG. 1 is a view showing an inside of a reaction-type steam turbine according to the
related art.
FIG. 2 is a partial cross-sectional view showing steam flow through disk blades of
the reaction-type steam turbine according to the related art.
FIG. 3 is a schematic view showing a state in which a vortex phenomenon occurs in
the reaction-type steam turbine according to the related art.
FIG. 4 is a view showing an inside of a reaction-type steam turbine according to a
preferred embodiment of the present invention.
FIG. 5 is an enlarged perspective view showing guide blade assembly of the reaction-type
steam turbine according to the preferred embodiment of the present invention.
FIG. 6 is a schematic view showing a state in which steam is introduced into the reaction-type
steam turbine according to the preferred embodiment of the present invention.
Best Mode
[0030] All terms or words used in the specification and claims have the same meaning as
commonly understood by one of ordinary skill in the art to which inventive concepts
belong. It will be further understood that terms, such as those defined in commonly
used dictionaries, should be interpreted as having a meaning that is consistent with
their meaning in the context of the relevant art and will not be interpreted in an
idealized or overly formal sense unless expressly so defined herein.
[0031] Hereinafter, a reaction-type steam turbine according to a preferred embodiment of
the present invention will be described with reference to FIGS. 4 to 6.
[0032] The reaction-type steam turbine has a technical feature wherein a turbine shaft is
provided with a guide blade assembly whereby a direction of steam being introduced
straight can be diverted to disk blades.
[0033] As shown in FIG. 4, the reaction-type steam turbine includes a housing 100, a turbine
shaft 200, disk blades 300, and a guide blade assembly 400.
[0034] The housing 100 provides a space in which the disk blades 300 are rotated by a reaction
force of steam and is provided at a first side thereof with a steam inlet tube 110
and at a second side thereof with a steam outlet tube 120.
[0035] The steam inlet tube 110 forms a duct through which steam is introduced into the
housing 100, and the steam outlet tube 120 forms a duct through which the steam introduced
into the housing 100 is discharged from the disk blades 300.
[0036] The housing 100 is provided therein with a space 130 in which the turbine shaft 200
and the disk blades 300 are installed.
[0037] The space 130 includes a turbine entrance 131 and turbine spaces 132.
[0038] The turbine entrance 131 defines an entrance space through which steam introduced
through the steam inlet tube 110 passes before it is transferred to the turbine spaces
132, thereby forming a space directly connected to the duct of the steam inlet tube
110 in a straight line.
[0039] Herein, the turbine spaces 132 provide spaces in which the disk blades 300 are installed
and the disk blades 300 are rotated and are provided at a side of the turbine entrance
131.
[0040] As shown in FIG. 4, the side of the turbine entrance 131 refers to a side perpendicular
to the duct of the steam inlet tube 110.
[0041] In addition, the turbine spaces 132 are structured to be connected to the duct of
the steam outlet tube 120.
[0042] Next, the turbine shaft 200 is rotated by the rotational force of both the disk blades
300 and the guide blade assembly 400 to provide a power output and is installed inside
the housing 100.
[0043] Herein, as shown in FIG. 4, the turbine shaft 200 is installed to pass through the
turbine entrance 131 and the turbine spaces 132 of the housing 100.
[0044] Next, the disk blades 300 serve to provide power for rotating the turbine shaft 200.
The disk blades are rotated by the reaction force generated when steam introduced
through the steam inlet tube 110 flows in and out of the disk blades 300, thereby
generating power for rotating the turbine shaft 200.
[0045] A plurality of disk blades 300 are fitted over the turbine shaft 200 along the axis
of the shaft, and the disk blades are placed in the respective turbine spaces 132
of the housing 100.
[0046] Herein, the disk blades 300 are formed in a circular shape, and each of the disk
blades is provided with an inlet hole through which steam is introduced and a nozzle
hole through which steam is discharged. This structure of the disk blades 300 remains
the same as that of the related art described above.
[0047] Next, the guide blade assembly 400 serve to divert a flowing direction of steam introduced
through the steam inlet tube 110 to the turbine spaces 132 and is placed in the turbine
entrance 131.
[0048] In other words, the guide blade assembly 400 serves to interfere with steam introduced
straight to the turbine entrance 131 through the steam inlet tube 110 and to transfer
the steam to the turbine spaces 132 placed at the side of the turbine entrance 131.
[0049] As shown in FIG. 4, the guide blade assembly 400 is coupled to the turbine shaft
200 at a position where the turbine entrance 131 is provided.
[0050] The configuration of the guide blade assembly 400 will be described in detail with
reference to FIG. 5.
[0051] The guide blade assembly 400 includes a blade hub 410 that is coupled to the turbine
shaft 200 and a plurality of drag blades 420 that are radially arranged along the
circumference of the blade hub 410.
[0052] The blade hub 410 is structured to be coupled to the turbine shaft 200, and has a
cylindrical shape having an inner diameter corresponding to a diameter of the turbine
shaft 200.
[0053] Further, the drag blades 420 are configured to face steam introduced into the turbine
entrance 131 through the steam inlet tube 110 and serve to guide the steam to the
turbine spaces 132.
[0054] In other words, the guide blade assembly 400 is structured such that the drag blades
420 face the flowing direction of steam, thereby maximizing the effect of rotating
the turbine shaft 200 due to the pressure of steam, and also serves to divert the
flowing direction of steam to the turbine spaces 132 where the disk blades 300 are
placed.
[0055] Herein, a rotation of the guide blade assembly 400 is generated by drag of steam,
so that a rotational output of the turbine shaft 200 can be maximized.
[0056] Here, the plurality of drag blades 420 is radially arranged along the circumference
of the blade hub 410.
[0057] Here, as shown in FIG. 5, each of the drag blades 420 includes a bent portion 421
and a straight portion 422.
[0058] The bent portion 421 serves to divert steam introduced into the turbine entrance
131 to the straight portion 422 and constitutes a first side of the drag blades 420.
[0059] Here, the first side of the drag blades 420 refers to a side opposite to the turbine
spaces 132 where the disk blades 300 are placed, and the bent portion 421 is bent
in a direction in which steam is introduced.
[0060] As such, since the first side of the drag blades 420 is bent in the direction in
which steam is introduced, steam introduced into the turbine entrance 131 is guided
by the bent portion 421, so that the steam can be always directed to the turbine spaces
132.
[0061] Here, the bent portion 421 of the drag blades 420 may be formed in a curved shape.
[0062] This is to flexibly divert the direction of steam introduced straight into the turbine
entrance 131.
[0063] The straight portion 422 serves to guide steam guided by the bent portion 421 directly
to the turbine spaces 132 and constitutes a second side of the drag blades 420.
[0064] Hereinafter, the operation of the reaction-type steam turbine having the above configuration
will be described.
[0065] Steam is supplied through the steam inlet tube 110, and then the steam is pressure-fed
to the turbine entrance 131 through the duct of the steam inlet tube 110.
[0066] Here, the steam hits the drag blades 420 of the guide blade assembly 400 and is then
guided along both the bent portion 421 and the straight portion 422 to the right side
(turbine spaces side) in the drawing (FIG. 4).
[0067] Here, the drag blades 420 of the guide blade assembly 400 guide the steam to the
turbine spaces 132 to divert the direction of the steam, and simultaneously rotate
by receiving pressure of the steam.
[0068] In other words, the steam introduced through the steam inlet tube 110 also serves
to firstly rotate the turbine shaft 200 by applying pressure to the guide blade assembly
400.
[0069] As such, by firstly rotating the turbine shaft 200 by using the steam pressure, the
load required to initially rotate the turbine shaft 200 can be reduced, thereby realizing
improved energy efficiency when rotating the turbine shaft 200.
[0070] Then, the steam introduced through the steam inlet tube 110 continuously pressurizes
the drag blades 420 of the guide blade assembly 400 to rotate the turbine shaft 200
and is simultaneously introduced into the inlet holes of the disk blades 300 provided
at the turbine spaces 132.
[0071] Thereafter, the steam rotates the disk blades 300 while flowing in and out of the
plurality of disk blades 300, thereby secondarily rotating the turbine shaft 200.
[0072] Through this series of processes, the output of the turbine shaft is achieved.
[0073] As described above, the reaction-type steam turbine according to the present invention
has a technical feature wherein the guide blade assembly 400 is coupled to the turbine
shaft 200 at a position where the turbine entrance 131 is provided.
[0074] Accordingly, the steam introduced straight into the housing can be naturally guided
toward the disk blades 300 after hitting the guide blade assembly 400, so that it
is possible to remove a vortex phenomenon occurring due to steam that swirls in the
turbine entrance 131 and thereby reduce the energy loss.
[0075] Also, due to the pressure of steam initially introduced into the housing, the turbine
shaft can be firstly rotated by the rotation of the guide blade assembly. Thus, it
is possible to reduce the load required when the turbine shaft is secondarily and
earnestly rotated by the rotation of the disk blades, thereby realizing improved energy
efficiency when rotating the turbine shaft.
[0076] Although a preferred embodiment of the present invention has been described for illustrative
purposes, those skilled in the art will appreciate that various modifications, additions
and substitutions are possible, without departing from the scope and spirit of the
invention as disclosed in the accompanying claims.
[0077]
<Description of the Reference Numerals in the Drawings>
| 100 |
: |
housing |
110 |
: |
steam inlet tube |
| 120 |
: |
steam outlet tube |
130 |
: |
space |
| 131 |
: |
turbine entrance |
132 |
: |
turbine spaces |
| 200 |
: |
turbine shaft |
300 |
: |
disk blades |
| 400 |
: |
guide blade assembly |
410 |
: |
blade hub |
| 420 |
: |
drag blades |
421 |
: |
bent portion |
| 422 |
: |
straight portion |
|
|
|