BACKGROUND OF THE INVENTION
1. Field of the Invention
[0001] The present invention relates to a thrust generating apparatus for a side thruster
that can be installed at the bow end or the stern end of displacement ships, and a
rotating door that automatically opens and closes the opening of shell plating in
response to the movement of such a thrust generating apparatus.
2. Description of Related Art
[0002] A side thruster refers to an apparatus installed at the bow or the stern of ships
for maneuvering the ships sideways. Such a side thruster is often provided in large
ships, especially, ferries or the like that are docked and undocked a large number
of times. On the other hand, it is rare that small ships are provided with a side
thruster since they are relatively easy to maneuver, and can be moved with less labor.
[0003] However, with the recent labor shortage and aging of crew members, there is an increasing
necessity also for small ships to have a side thruster function. For this reason,
JP H05-016594U proposes a side thruster that generates a thrust force by jetting seawater from a
seawater pump that is used for a clear water cooling apparatus.
SUMMARY OF THE INVENTION
[0004] With the development of the declining of the birthrate and the aging of the population,
environment preservation and energy savings are serious challenges that are inevitable
when operating various ships. In the course of the aging of crew members, labor saving,
and globalization, simplification and safety ensuring for various operations performed
inside ships are becoming increasingly important. In particular, energy saving and
enhanced performance for ships themselves based mainly on motorization of the main
engine are becoming important challenges. Under such circumstances, the apparatus
of the present invention provides a side thruster that technically facilitates the
simplification and the streamlining of docking and undocking operations.
[0005] In view of the above-described challenges, a method is provided in which a thrust
is achieved by using jets of an on-board seawater pump, which puts little pressure
on the ship price. However, a large-capacity pump generally has a high pump head.
Therefore, randomly releasing high-speed jets into the sea would result in a vortex,
and a desired thrust as a reaction force cannot be achieved. The water column of the
pump has a viscosity higher than that of the surrounding seawater and will only be
diffused and annihilated, while sliding, into infinite seawater under hydrostatic
pressure, so that it is not possible to provide an effective thrust.
[0006] Under this phenomenon, the difficulty of the initial motion for turning increases
with an increase in resistance of drainage water that is to be moved. Therefore, the
proposed method has not been put to practical use.
[0007] Furthermore, a side thruster for displacement ships is required to achieve a slow-speed
thrust with high effectiveness, rather than a high-speed thrust. One problem solved
by the present invention is to convert a small-diameter spouting water flow of a seawater
pump into a larger-diameter water flow. That is, it is an object of the invention
to efficiently discharge a water flow having a practical diameter that is similar
to a water flow discharged by a commonly used thruster, under a constant output.
[0008] An ordinary side thruster generates a thrust using a propeller having a reversible
thrust generating function and disposed within a duct penetrating through the port
side and the starboard side, and it is essentially advantageous to provide a side
thruster at the tip of a bow where possible in order to achieve thrust for turning
the bow and the stern.
[0009] However, due to the overall size of the apparatus, or in other words, the constraints
on the arrangement in a ship, such as the complexity of shafting for rotating a propeller,
a side thruster is inevitably disposed at a location near a parallel portion of the
hull. Consequently, the duct length is increased more than necessary, which leads
to a reduction in thrust. If the opening position of the duct entrance of the side
thruster is moved forward to a portion having an incidence angle with the waterline
for this reason, the hull resistance increases, which will also lead to inflow of
foreign objects. Providing a guard at the openings at both ends of the entrance for
this reason will lead to an increase in the resistance of the duct itself. The stern
portion is no exception for this, and these constraints make it difficult to install
a side thruster at an optimum position.
[0010] Furthermore, a thrust that is equal in both the positive and negative directions
for the thrust generating direction can only be achieved by rotating the propeller
body, and performing this will result in a complex mechanism.
[0011] It should be noted that wakes of a propeller-type thruster provide a rotational flow,
which is less efficient than a straight water flow provided by jets of a general-purpose
pump.
[0012] Therefore, the present invention was made in order to solve the above-described various
problems. The underlying idea of the invention is to provide a thrust generating mechanism
inside a nozzle having a bell-shaped outer casing to achieve a thrust while increasing
a spouting water column of a seawater pump and performs flow straightening, thereby
achieving a strait flow having a thrust comparative to that achieved by a thruster
of an equivalent output, or a Kort nozzle thruster, in a similar diameter
[0013] Furthermore, it is an object of the invention to achieve a more effective thrust
for turning the bow and the stern by installing the thrust generating apparatus at
the tip of the bow or the stern such that the apparatus is pivotable toward the port
side and the starboard side, making use of the compactness of the apparatus, and to
realize a side thruster that prevents the increase of the hull resistance and the
inflow of foreign objects such as driftwood and drift ice during navigation by disposing,
at a shell plating opening at the operative position, a door that automatically opens
and closes in response to the movement of the nozzle position
[0014] It is another object of the invention to provide an omnidirectional thrust generating
apparatus having excellent maneuverability at a harbor or the like.
[0015] In order to solve the above-described problems, a thrust generating apparatus according
to the present invention is configured as follows.
[0016] According to a first aspect of the present invention, a bell-shaped nozzle is coupled
to an ejection port of a pump water flow, a ring having a blade-shaped cross section
is disposed inside the nozzle, and an artillery shell-shaped (referred to as "shell-shaped"
in the following) cone is disposed inside the ring on the center line of a water flow.
[0017] A thrust generating apparatus according to a second aspect of the invention is the
thrust generating apparatus of the first aspect, wherein the bottom of the cone is
open, and a slit is further provided at a shoulder portion of the cone upstream from
the ring.
[0018] According to a third aspect of the invention, a rotating door is further provided
that enables the nozzle located in a bow tip or a stern tip to pivot toward a shell
plating opening on a port side or a starboard side, and that closes or opens the shell
plating opening in accordance with the position of the nozzle.
According to a fourth aspect of the invention, an illuminant is provided above the
rotating door, and near the waterline at a hull end.
[0019] According to a fifth aspect of the invention, in an omnidirectional thrust generating
apparatus, a bell-shaped nozzle is coupled to an ejection port of a pump water flow,
a ring having a blade-shaped cross section is disposed inside the nozzle, and a shell-shaped
cone is disposed inside the ring on the center line of a water flow, the nozzle is
further provided inside a half spindle-shaped housing suspended from the bottom of
a ship, and the housing and the nozzle located inside the housing are pivotable in
the horizontal direction in accordance with pivoting of the ejection pipe of the pump
water flow.
[0020] An omnidirectional thrust generating apparatus according to a sixth aspect of the
invention is the omnidirectional thrust generating apparatus of the fifth aspect,
wherein the bottom of the cone is open, and a slit is further provided at a shoulder
portion of the cone upstream from the ring.
[0021] Since the present invention utilizes jets of a seawater pump, it is not necessary
to provide a side thruster apparatus itself with a motor unlike a propeller-type side
thruster. The present invention therefore makes it possible to realize the size reduction
of a side thruster and its related apparatuses. Accordingly, it is possible to house
the side thruster within a hold at the bow or the stern, or within the engine room,
and to select an optimum position of the side thruster. That is, due to its compactness,
the side thruster can be installed near the bow end or the stern end, making it possible
to perform turning efficiently.
[0022] The side thruster of the invention has a simple structure, and therefore can be made
of high performance plastics instead of steel, thereby facilitating the size reduction
and the standardization of its products.
[0023] With the thrust generating apparatus according to the first aspect, an exhaust flow
from the nozzle is changed to a straight flow that has been leveled in the radial
direction, so that it is possible to achieve a thrust efficiently. That is, a bell-shaped
nozzle is coupled to an ejection port of a pump water flow, a ring having a blade-shaped
cross section is disposed inside the nozzle, and a shell-shaped cone is disposed inside
the ring on the center line of a water flow, and therefore, it is possible to expand
and straighten the ejection flow. That is to say, the exhaust flow is changed to a
straight flow that has been leveled in the radial direction. Accordingly, it is possible
to achieve an exhaust flow having a thrust comparable to that achieved by a thruster
of an equivalent output or a Kort nozzle thruster, in a similar diameter.
[0024] The thrust generating apparatus according to the second aspect has a configuration
in which a slit is provided at a shoulder portion of the cone, and backwater in a
wake region that is produced at the rear end of the cone is in communication with
the interior of the nozzle through the interior of the cone. The water flow that is
in communication with the interior of the nozzle exerts the effect of suppressing
the turbulence of flow generating from this area due to the change in the internal
structure of the nozzle.
[0025] With the thrust generating apparatus according to the third aspect, the increase
in resistance of the duct opening and the entry of foreign objects such as driftwood
and drift ice can be prevented using the rotating door that automatically opens and
closes.
[0026] Since the side thruster room is a non-watertight compartment, it is possible to perform
maintenance work on a light load waterline.
[0027] With the thrust generating apparatus according to the fourth aspect, an illuminant
is provided above the rotating door and near the waterline at the end of the ship,
and therefore, it is possible to increase the safety in the area near the bow end
or the stern end that includes a side thruster where it is difficult to distinguish
between the rotating door and the shell plating.
[0028] According to the fifth and sixth aspects of the present invention, the nozzle, ring,
cone or the like according to the first and second aspects is provided inside a half
spindle-shaped housing pivotably suspended from the bottom of a ship. Since the housing
is pivotable, it is possible to discharge a water flow from the nozzle in any direction,
thereby improving the maneuverability at a harbor or the like.
[0029] The structure according to the second aspect, or in other words, a flow straightening
structure, can be also used for a propeller thruster. More specifically, as shown
in FIG. 20, a cylindrical outer casing 56 (low-strength member) is fixed to a blade
stump portion 74 with a spacing provided between the outer cylinder 56 and the outer
surface of a propeller hub 55, the rear end surface 57 of the outer casing 56 is opened,
and a slit 58 is formed forward of the blade stump portion 74 of the propeller. That
is, with the structure according to the second aspect, backwater in a wake region
that is produced at the rear end of the outer casing 56 is in communication with the
forward portion of the blade 75 through the interior of the outer casing 56. Accordingly,
the water flow that is in communication with the forward portion of the blade 75 exerts
the effect of suppressing a vortex that could have been produced near the blade 75.
BRIEF DESCRIPTION OF THE DRAWINGS
[0030]
FIG. 1 is a longitudinal cross-sectional view of a bow portion in which an apparatus
according to the present invention is provided.
FIG. 2 is a plan view on a floor surface on which the apparatus is installed.
FIG. 3 is a transverse sectional view at the bow end where the apparatus is located.
FIG. 4 is a longitudinal cross-sectional view of a nozzle of a thrust generating apparatus
of the apparatus of the present invention.
FIG. 5 is a front view showing a configuration of the nozzle.
FIG. 6 is a plan view showing operating positions of the nozzle and a rotating door
inside a thrust generating apparatus room.
FIG. 7 is a plan view showing operating positions of the nozzle and a rotating door
inside a thrust generating apparatus room.
FIG. 8 is a plan view showing operating positions of the nozzle and a rotating door
inside a thrust generating apparatus room.
FIG. 9 is a detail view of a pivot center of the rotating door.
FIG. 10 is a detail view of a pivot center of the rotating door.
FIG. 11 is a view taken along the arrow A-A in FIG. 6.
FIG. 12 is a view taken along the arrow C-C in FIG. 11.
FIG. 13 is a view taken along the arrow D-D in FIG. 11.
FIG. 14 is a view taken along the arrow B-B in FIG. 6.
FIG. 15 is a detail view of a rotating door closing mechanism of the thrust generating
apparatus.
FIG. 16 is a diagram showing the arrangement at a lower end portion of the nozzle
and a locking device for the rotating door.
FIG. 17 is a detail view of the same apparatus at a locked position.
FIG. 18 is a detail view of the same apparatus at a released position.
FIG. 19 is a simplified illustration showing rotating door supports and elbow plates.
FIG. 20 is an illustration in the case where a part of a nozzle configuration of the
present invention is applied to a general-purpose propeller thruster.
FIG. 21 is a configuration diagram of the case where a nozzle of the present invention
is applied to a flat bottom of a ship.
FIG. 22 is a simplified configuration diagram of the case where a nozzle of the present
invention is installed at a stern end.
DETAILED DESCRIPTION OF THE INVENTION
[0031] Hereinafter, the configuration of the present invention will be described by way
of examples with reference to the accompanying drawings.
FIG. 1 is a longitudinal cross-sectional view of a bow portion in which an apparatus
according to the present invention is provided; FIG. 2 is a plan view on a floor surface
on which the apparatus is installed; FIG. 3 is a transverse sectional view at the
bow end where the apparatus is located; FIG. 4 is a longitudinal cross-sectional view
of a nozzle of a thrust generating apparatus of the apparatus of the present invention;
FIG. 5 is a front view showing a configuration of the nozzle; FIGS. 6, 7 and 8 are
plan views showing operating positions of the nozzle and a rotating door inside a
thrust generating apparatus room; FIGS. 9 and 10 are detail views of a pivot center
of the rotating door; FIG. 11 is a view taken along the arrow A-A in FIG. 6; FIG.
12 is a view taken along the arrow C-C in FIG. 11; FIG. 13 is a view taken along the
arrow D-D in FIG. 11; FIG. 14 is a view taken along the arrow B-B in FIG. 6 (for convenience
in drawing the figures the rotating door and the nozzle are assumed to be located
on the hull center line); FIG. 15 is a detail view of a rotating door closing mechanism
of the thrust generating apparatus; FIG. 16 is a diagram showing the arrangement at
a lower end portion of the nozzle and a locking device for the rotating door; FIG.
17 is a detail view of the same apparatus at a locked position; FIG. 18 is a detail
view of the same apparatus at a released position; FIG. 19 is a simplified illustration
showing rotating door supports and elbow plates; FIG. 20 is an illustration of the
case where a part of a nozzle configuration of the present invention is applied to
a general-purpose propeller thruster; FIG. 21 is a configuration diagram of the case
where a nozzle of the present invention is applied to a flat bottom of a ship; and
FIG. 22 is a simplified configuration diagram of the case where a nozzle of the present
invention is installed at the stern.
[0032] While the present invention can be applied to ships of various sizes, ranging from
small ships to large ships, the maximum hull form is restricted by the ability of
available seawater pumps and the cost efficiency. The following embodiment corresponds
to a thrust of approximately two tons, which is required for a side thruster used
for a ship having a gross tonnage of less than 500 tons.
[0033] In this case, the required side thruster output is usually 180 to 200 PS (132 to
147 kilowatts), which corresponds to 1.0 ton to 1.1 tons for a bollard pull of 100
PS (73 kilowatts) of a commonly used tugboat. The diameter of a duct that contains
the propeller as a thrust generating apparatus is approximately 750 millimeters.
[0034] Therefore, the following embodiment is also aimed at achieving a low-speed, direct
ejection flow having a diameter of 750 millimeters and whose speed is leveled in the
radial direction with a seawater pump having an output of 180 PS (132 kilowatts).
In this case, the corresponding seawater pump ordinarily has an output of 180 PS (132
kilowatts) and the ejection pipe has a diameter of approximately 250 millimeters.
Therefore, with a configuration according to this embodiment, the diameter of an ejection
flow of the seawater pump is increased by three times to reduce the speed so that
an exhaust flow similar to that of a commonly used thruster having a duct diameter
of 750 millimeters can be used as a low-speed thrust for turning.
[0035] First, a configuration of the present invention will be described.
[0036] A side thruster according to the present invention includes a thrust generating apparatus,
an apparatus for opening and closing a shell plating opening, and operating devices
for these apparatuses. A side thruster 1 as shown in FIGS. 1 to 3 is simple and compact,
and therefore can be installed in a side thruster room 3 in a watertight compartment
at a tip portion of a bow hold 2.
[0037] A seawater pump 4, which powers the thrust generating apparatus, is installed inside
a pump room 7 in a watertight compartment accessible from an upper deck 6 located
approximately below a chain locker 5 at the back of the bow hold 2. The seawater sucked
through a suction pipe 8 passes through an ejection pipe 9, as well as a vertical
upper pipe portion 10 and a rotatable vertical lower pipe portion 11 of the ejection
pipe 9, and is ejected into a nozzle 12 having a bell-shaped outer casing, and thereby,
the water flow is expanded and straightened. Thereafter, the water flow passes through
an extension ring 13 at the end of the nozzle, and is discharged from a shell plating
opening 14.
[0038] A non-watertight rotating door 15 that pivots about a vertical stationary pipe portion
10 of the ejection pipe 9 and a rotatable pipe portion 11 of the ejection pipe 9 is
provided at the opening 14. Accordingly, the side thruster room 3 is configured to
be non-watertight to the outside.
[0039] At a mooring deck 16, a handle 19 for operating a side thruster operation rod 18
that is guided via a gear 17 attached to the vertical portions 10 and 11 of the ejection
pipe 9. Accordingly, the vertical portion 11 can be rotated by rotating the handle
19. Since the vertical portion 11 is connected to the nozzle 12 via an elbow pipe
20, rotating the handle 19 causes the nozzle 12 to rotate about a center line 63 (see
FIG. 4) of the vertical portion 11.
[0040] Next, the internal configuration and the action of a thrust generating apparatus
of a side thruster according to the present invention will be described.
[0041] In FIG. 4, the nozzle 12 having a bell-shaped outer casing is coupled to the end
of the elbow pipe 20 connected to the vertical portion 11 of the ejection pipe 9.
Inside the nozzle 12, a ring 21 having a blade-shaped cross section is fixed as an
inner casing via flow straightening plates 23 along with a shell-shaped cone 22 located
on the center line, as shown in FIGS. 4 and 5. The interior of the cone 22 is hollow,
and the bottom of the cone 22 is open. The ring 21 and the cone 22 are fixed to each
other with the flow straightening plates 23, and are also fixed to the nozzle outer
casing (FIG. 5 shows a state of the nozzle 12 as viewed from the ejection side).
[0042] It should be noted that "bell-shaped" as used herein refers to a shape whose diameter
gradually increases in the form of an arc, and takes the form of a linear cylinder
at its peripheral portion after the maximum diameter is reached. "Blade-shaped cross
section" refers to a form that has a round leading edge, a maximum thickness at a
portion located approximately at one third from the leading edge, a trailing edge
with an elongated teardrop shape, wherein the line connecting the top, bottom and
middle of the cross section is in an arch shape. "Shell-shaped" refers to a form whose
diameter increases more gradually than that of the bell shape.
[0043] Accordingly, jets ejected from the elbow pipe 20 are expanded in the radial direction
by the cone 22 at the position where the internal cross-sectional area of the nozzle
12 starts to increase, thereby equalizing the flow velocity in the radial direction
within the nozzle 12. At the same time, the jets flow into the ring 21 with an angle
of attack (θ) to generate a lift (L), thereby achieving a component of force in the
thrust direction (T). Furthermore, the cross-sectional area between the nozzle 12
serving as the outer casing and the ring 21 serving as the inner casing is set such
that the outlet of water flow is smaller than the inlet, thereby making the flow velocity
higher than on the inner surface of the ring 21 and achieving a lift. However, it
is also possible to achieve a larger effect by applying a coating for reducing the
frictional resistance or a lining of metal-clad steel such as titanium onto the outer
surface ring 21 and the inner surface of the nozzle 12.
[0044] Further, a slit 24 is formed in a shoulder portion of the cone 22, and backwater
60 in a wake region that is generated at the rear end of the cone 22 is in communication
with the interior of the nozzle 12 through the interior of the cone 22, thereby providing
an effect of suppressing the turbulence of flow generated at this area due to the
change in the internal structure of the nozzle 12 (the arrow in FIG. 4 indicates the
water flow).
[0045] It should be noted that for the apparatus for suppressing a vortex generated on the
outer surface of the cone 22 it is also possible to apply the flow straightening of
a hub vortex of a commonly used propeller. That is, in FIG. 20, by fixing a cylindrical
outer casing 56 (low-strength member) to a blade stump portion with a spacing between
the outer casing 56 and the outer surface of the propeller hub 55, opening the rear
end surface 57 of the outer casing 56, and forming a slit 58 forward of the propeller
blade stump portion, it is possible to realize the same function as described above,
and to achieve the effect of slowing a rotational flow at the blade stump portion
on the outer surface of the outer casing so that the flow becomes similar to a straight
flow, thereby further reducing the hum vortex.
[0046] Next, the configuration of the rotating door 15, which is a feature of the side thruster
according to the present invention, at the shell plating opening will be described.
[0047] As shown in FIGS. 1, 6, 7, 8, 9, 11, 12 and 13, the non-watertight rotating doors
15 are made up of an outer plate 27 and an inner plate 28. For the outer plate 27,
a "cut-out plate" from the shell plating at the relevant portion is used to ensure
precision, and the outer plate 27 is configured so as to be rotatable. In addition,
an internal space 29 is secured between the outer plate 27 and the inner plate 28
to reduce the apparent weight in water by the buoyancy of the inner space so that
the sliding of the rotating doors 15 can be performed easily.
[0048] The pivot center of the rotating doors 15 at the port side and the starboard side
is located on the center line 63 of the vertical portions 10 and 11 of the ejection
pipe. Supports 30 that are part of the rotating doors 15 are attached via elbow plates
45a and 45b to freely movable plate rings 25 and 26 surrounding the vertical portion
11 of the ejection pipe 9 (see FIG. 19). Here, the elbow plates 45a and 45b are L-shaped
plates. One side of the L-shaped plates is fixed to the support, and an aperture 50
and a cut-out portion 51 are formed in the other side. Further, the elbow plates 45a
and 45b are cut out to form arc-shaped portions, where the elbow plates 45a and 45b
are fixed to the freely movable rings 25 and 26.
[0049] The elbow plate 45a is fixed to an upper portion of the support 30 of the rotating
door 15 located at one of the port side and the starboard side, and the elbow plate
45a is fixed to the freely movable plate ring 25. The elbow plate 45b is fixed to
a lower portion of the support 30 of the rotating door 15 located at the other of
the port side and the starboard side, and the elbow plate 45b is fixed to the freely
movable plate ring 26. Thus, the pivoting and sliding of each of the supports 30 of
the right rotating door and the left rotating door can be performed on the same plane.
[0050] It should be noted that the supports 30 have a box-shaped cross section as shown
in FIG. 13, and enclose a space for achieving buoyancy that is balanced with the rotating
doors 15.
[0051] At the lower end of the rotating door 15, a skid 31 is provided to facilitate sliding,
and a skid 32 is further provided at the top in order to suppress floating in water.
A guide plate 64 that comes into slide contact with the skid 32 is provided inside
the thruster room 3.
[0052] Furthermore, for the purpose of suppressing floating or sinking of the plate rings
25 and 26, as well as the elbow plates 45a and 45b fixed to the plate rings 25 and
26, plate rings 33 fixed to the vertical pipe 11 are also attached above and below
the plate rings 25 and 26.
[0053] Although the length of the supports 30 is set so that the outer plates 27 are contained
inside the hull in order to prevent the outer plate 27 from becoming flush with the
shell plating of the hull, there will be an area 34 where the front end of the outer
plate slightly protrudes from the shell plating when the rotating door 15 is opened
or closed (see FIG. 6). However, this happens only for a short time when the rotating
door 15 is being pivoted, and therefore, will not cause a problem. In the case of
shell plating on the ship side where the incident angle of the waterline is large,
the size of such a protruding area 34 is small.
[0054] Next, operating devices and fixing devices of the side thruster will be described.
[0055] To generate a thrust toward either the port side or the starboard side, it is required
for a side thruster of the present invention to pivot the nozzle 12 itself, and the
rotating door 15 is moved in response to that pivoting. Therefore, the following mechanism
is provided.
[0056] As shown in FIG. 14, the vertical portion 11 of the ejection pipe can be pivoted
by means of a watertight washer 35 and a bearing 36 at the lower end of its vertical
axis, and supports the thrust generated in the nozzle 12 as well as its own weight.
The pivoting force of the vertical portion 11 is conducted by means of the gear 17
via the vertical rod 18 using the handle 19 on the mooring deck 16. The vertical portion
11 at the end of the fixed ejection pipe retains water tightness with a seal 37 on
the inner side of the gear 17.
[0057] Next, the nozzle 12 and the opening and closing operations of the rotating door 15,
which moves in response to the movement of the nozzle 12, using the above-described
devices will be described.
[0058] FIG. 6 shows the situation when the rotating door 15 is in a closing position for
the opening 14 on the port side when the nozzle 12 is in an operating position on
the starboard side, that is, in a mooring operation, i.e., in a state in which an
ejection flow is discharged from the nozzle 12. FIG. 7 shows the situation when the
rotating door 15 is in a closing position for the opening 14 on the starboard side
when the nozzle 12 is in an operating position on the port side, that is, in a mooring
operation, i.e., in a state in which an ejection flow is discharged from the nozzle
12. FIG. 8 shows that when the nozzle 12 is not in operation (during navigation),
i.e., is in a state in which no ejection flow is discharged from the nozzle 12, the
nozzle 12 is fixed at a position 38 on the hull center line, and the rotating door
15 is at the closing position on both the port side and the starboard side. That is
to say, when the nozzle 12 is pivoted from the navigation position to the mooring
operation position, the rotating door 15 is pushed by the nozzle 12, and stopped by
a stopper 39.
[0059] Furthermore, when the nozzle 12 moves from the operating position to the fixed position
or to the opposite side of the ship, the rotating door 15 is automatically restored
to the closing position by a torsion coil spring 42 that surrounds the vertical portion
11 of the ejection pipe and is disposed between a round bar 40 attached to its support
30 and a round bar 41 attached to the undersurface of the top plating of the thruster
room, and then is stopped at the fixed position by a stopper 44, as shown in FIGS.
9 and 10. The motive energy is given via the gear 17 by the rotating operation of
the handle 19 when the nozzle 12 moves to the operative position. Here, the stopper
39 and the stopper 44 are provided on the floor surface of the side thruster room
3.
[0060] The range of movement of the supports 30 of the rotating doors is limited to an area
between the stopper 39 and the stopper 44 of each of the port and starboard sides.
On the other hand, the nozzle 12 moves via a position 38 on the hull center, and the
supports 30 are stopped by the stoppers 39, and therefore, the range of movement of
the nozzle 12 is limited between the stoppers 39 of the port and starboard sides.
[0061] In addition, the fixing devices will be now described. In FIGS. 1, 6, 9, 14 and 16,
the operation rod 18 is located on the hull center line forward of the vertical portion
11 of the ejection pipe, and is configured to be vertically slidable together with
the gear 17. The rotating doors 15 on the port side and the starboard side are attached
to the freely movable plate rings 25 and 26 via the elbow plates 45a and 45b. An elbow
plate 46 is fixed to the vertical portion 11. The elbow plate 45a, elbow plate 45b,
and elbow plate 46 are penetrated by the rod 18. In the drawings, the rod 18 is located
at a position 47 that is pressed most downward (see FIG. 17), and each of the elbow
plates 45a, 45b and 46 is pierced by the rod 18, and thereby, the rotating doors 15
are fixed at the closing positions, and the nozzle 12 is fixed to the storage position
38 on the hull center line.
[0062] When a mooring operation is performed from such a condition (in the navigation position),
the rod 18 is lifted up to a position 48 shown in FIG. 18. Then, the elbow plate 46
fixed to the vertical portion 11 of the ejection pipe becomes laterally pivotable,
while the elbow plates 45a and 45b located at the position of a small diameter portion
49 provided in the rod 18 becomes pivotable in the direction opposite to the opening
side of the cut-out portion 51 formed at its aperture 50. Consequently, the rotating
doors 15 become rotatable toward their respective sides of the ship. Therefore, the
rotating door 15 at either the port or the starboard side on which the nozzle 12 rotates
is pushed by that nozzle 12, and is thereby pivoted. By depressing the rod 18 after
the pivoting, the rotating door 15 at the opposite side of the ship can be fixed with
a large diameter portion 52 of the rod.
[0063] It should be noted that the relationship between the large diameter portion 52 and
the small diameter portion 49 of the rod 18, and the aperture 50 and the cut-out portion
51 of the elbow plates 45a and 45b is as follows. That is, the diameter of the large
diameter portion 52 is smaller than the diameter of the aperture 50, but is larger
than a width H of the cut-out portion 51 (FIG. 10). The diameter of the small diameter
portion 49 is smaller than the width H.
[0064] Furthermore, since the rotating doors 15 are integrated via the elbow plates 45a
and 45b and the rod 18 by the above-described operation, the simultaneous fixation
of the nozzle 12 and the rotating doors 15 at both the port side and the starboard
side is completed by stopping lateral pivoting of the rotating doors 15 at both the
port side and the starboard side by the respective stoppers 44. However, it is also
possible to provide a safeguard by performing the above-described fixation, for example,
by using a barrel bolt (not shown) at the handle 19 on a worker's deck.
[0065] For large ships having a size larger than the ship in the above-described embodiment,
it is necessary to realize a light pivoting maneuver. In this respect, since the nozzle
has no movable parts, the nozzle can be easily made partly or entirely of plastic.
Furthermore, the realization of a light pivoting maneuver can be facilitated, for
example, by forming the rotating doors in the shape of a regular square and arranging
seawater resistant casters facing upward and downward at the four corners of the rotating
doors, or by injecting foamed plastics into the buoyancy tank of the rotating doors
in order to increase the rigidity of the rotating doors.
[0066] In order to realize a larger apparatus, it is necessary to increase the pump capacity,
which leads to an increase in the ship price. However, as shown in FIG. 1, by using
stop valves as the check valve 53a on the suction pipe side and the check valve 53b
on the ejection pipe side, and cleaning the seawater pump 4 by connecting the clear
water pipe 54 to the pump side of these valves, the ship service life will not be
reduced by the use of a general purpose clear water pump, making it possible to keep
the cost low.
[0067] The width of the thruster room increases with an increase in the size of a hull form.
Such a situation can be addressed, for example, by extending the extension ring 13
of the nozzle 12, and extending the length of the nozzle 12 itself. In the case of
a hull form whose bow cross section has a U shape 61 or a V shape 62 as shown in FIG.
3, the above-described situation can also be addressed in the same manner.
[0068] In order to avoid contact with the area near the rotating door of small crafts that
handle a mooring line at the bow and the stern in a mooring operation or the like,
in particular, in order to visually recognize the area near the waterline in clouded
water at night, for example, it is possible to increase the safety in the area near
the bow end or the stern end that includes a side thruster where it is difficult to
distinguish between the rotating door and the shell plating, by attaching a white
colored hemisphere-type, tempered glass reflection sphere that uses a lamplight as
the light source, such as a working light on the worker's deck near the bow end or
the stern end, or covering an illuminant 59 that requires no power wiring with a watertight
cover made of tempered glass, and attaching the illuminant directly above the rotating
door and near the waterline at the hull end.
[0069] Although the embodiment of the present invention has been described mainly as a bow
thruster, the invention can often be directly applied to a stern portion 72 by utilizing
the seawater pump in an engine room 73 as shown in FIG. 22.
[0070] In the case of a ship with a flat bottom, such as a shallow draft ship or a wide
width ship, it is also possible to suspend the nozzle 12 from the bottom of the ship
by applying the fifth and sixth aspects of the present invention.
[0071] In the following, this will be described in detail. In FIG. 21, a half spindle-shaped
housing 65 is provided for the purpose of straightening the water flow outside the
bell-shaped nozzle 12 and the ejection pipe 11 used as a pintle. A fin 66 having a
streamlined horizontal cross section and serving as a control surface is provided
at above and below the housing 65, and the area proportions are set such that the
whole structure functions as a balance rudder.
[0072] The vertical portion 11 of the ejection pipe is adapted to a horizontal thrust and
heaving, by using a bearing 68 at the bottom of a steering gear room 67. Furthermore,
a steering engine 69 capable of pivoting 360 degrees is installed above the bearing
68. It should be noted that existing techniques that have been put into practical
use can be used for these devices.
[0073] Furthermore, an ejection pipe 10, which forms fixed piping together with the seawater
pump 4, is provided above the vertical portion 11 of the ejection pipe used as a pintle,
and their connection portion is kept watertight by a seal case 70.
[0074] As shown in FIG. 22, the apparatus of the present invention can function as a side
thruster at the stern portion. Alternatively, the apparatus can be used as a propeller.
In that case, in order to achieve a further thrust by expanding the exhaust flow and
utilizing a wake gain resulting from the forward movement of the hull, a ring 71 having
a blade-shaped cross section is additionally provided at the rear end.
[0075] It should be noted that depending on the hull form, a thrust can be easily increased,
for example, by providing a plurality of the apparatus including a seawater pump,
and further increasing the pumping capability by driving an inverter-controlled electric
motor.