Technical Field
[0001] The present disclosure relates to a cargo tank unit and a ship.
Background Art
[0003] A ship carrying liquefied gas such as natural gas is equipped with a cargo tank accommodating
the liquefied gas. For example, Patent Document 1 discloses a configuration in which
a cargo tank is supported by a hull via a cylindrical skirt. The upper end portion
of the skirt described in Patent Document 1 is disposed at the equatorial position
of the cargo tank. The upper end portion of this skirt is fixed by welding to the
equatorial part of the cargo tank.
[0004] Such cargo tanks are designed in accordance with the International Maritime Organization
(IMO) Tank Type B requirements specified in the International Gas Carrier (IGC) Code,
which is the IMO safety rules for liquefied gas ships.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0006] An IMO Tank Type B cargo tank is one in which the stress of each part of the structure
is precisely grasped using, for example, a model test and a detailed analysis method,
and fatigue analysis and fracture mechanism analysis are accurately performed. Accordingly,
the welded portion between the cargo tank and a skirt needs to meet the same fatigue
strength requirements as the tank. For this reason, a ring-shaped member formed by
machining is generally used for the welded portion between the equatorial part of
the cargo tank and the skirt. This ring-shaped member is joined between the upper
half portion and the lower half portion of the cargo tank. The upper end of the lower
half portion of the cargo tank and the upper end portion of the skirt disposed on
the radially outer side of the cargo tank are welded to the lower end portion of the
ring-shaped member. Accordingly, the thickness of the lower end portion of the ring-shaped
member is the sum of the wall thickness of the lower half portion of the cargo tank
and the wall thickness of the upper end portion of the skirt.
[0007] In the IMO Tank Type B cargo tank, the upper limit of the wall thickness of each
part including the ring-shaped member is 40 mm unless the material is an aluminum
alloy. The wall thickness of the lower half portion of the cargo tank is the thickness
of the welded ring-shaped member (up to 40 mm) minus the wall thickness of the upper
end portion of the skirt. In other words, at least in the lower half portion of the
cargo tank, an increase in wall thickness is limited to a certain level. This hinders
an increase in the size of the cargo tank required to have pressure resistance.
[0008] The present disclosure has been made in view of the above, and an object of the present
disclosure is to provide a cargo tank unit and a ship enabling an increase in the
wall thickness of a cargo tank and, by extension, an increase in the size of the cargo
tank.
Solution to Problem
[0009] In order to achieve the above object, the cargo tank unit according to the present
disclosure includes a cargo tank, a skirt, and a welded portion. The cargo tank is
of IMO IGC Code Tank Type C. The skirt has an upper end connected to a lower half
portion of the cargo tank over a circumferential direction. The skirt extends downward
to be fixed to a hull. The welded portion fixes the upper end of the skirt to the
cargo tank over the circumferential direction.
Advantageous Effects of Invention
[0010] According to the ship of the present disclosure, it is possible to increase the wall
thickness of a cargo tank and, by extension, increase the size of the cargo tank.
Brief Description of Drawings
[0011]
Fig. 1 is a plan view illustrating an overall configuration of a ship according to
an embodiment of the present disclosure.
Fig. 2 is a half cross-sectional view in which a cargo tank provided on the ship according
to the embodiment of the present disclosure is viewed from the ship stern direction.
Fig. 3 is an enlarged cross-sectional view illustrating the configuration of a cargo
tank-skirt joint according to the embodiment of the present disclosure. Description
of Embodiments
[0012] Fig. 1 is a plan view illustrating an overall configuration of a ship according to
an embodiment of the present disclosure. Fig. 2 is a half cross-sectional view in
which a cargo tank provided on the ship is viewed from the ship stern direction.
[0013] As illustrated in Figs. 1 and 2, a ship 1 of the embodiment of the present disclosure,
for example, stores and carries liquefied gas such as liquefied natural gas. The ship
1 includes at least a hull 2, a cargo tank 20, a skirt 30, and a welded portion 40.
[0014] For convenience, the cargo tank 20, the skirt 30, and the welded portion 40 are collectively
referred to as a cargo tank unit.
[0015] The hull 2 has a pair of broadsides 3A and 3B, a ship bottom 4, and an upper deck
5, which form the outer shell of the hull 2. The broadsides 3A and 3B are provided
with a pair of broadside skins respectively forming the left and right broadsides.
The ship bottom 4 is provided with a ship bottom skin connecting the broadsides 3A
and 3B. By the pair of broadsides 3A and 3B and the ship bottom 4, the outer shell
of the hull 2 has a U shape in a cross section orthogonal to a ship stern direction
Da. The upper deck 5 is a whole deck exposed to the outside. In the hull 2, an upper
structure 7 having a living quarter is formed on the upper deck 5 on a stern 2b side.
[0016] In the hull 2, a cargo loading section (hold) 8 is formed closer to a bow 2a side
than the upper structure 7. The cargo loading section 8 is recessed toward the ship
bottom 4 below the upper deck 5 and is open upward.
[0017] A plurality of the cargo tanks 20 are provided in the cargo loading section 8. The
plurality of cargo tanks 20 are disposed side by side in the ship stern direction
Da. An upper portion 20a of each cargo tank 20 protrudes upward beyond the upper deck
5 of the hull 2. The upper portions 20a of the plurality of cargo tanks 20 are covered
with tank covers 25 provided on the upper deck 5. A heat insulating material (not
illustrated) that suppresses heat input from the outside is provided on the outer
surface of each of the plurality of cargo tanks 20.
[0018] The cargo tank 20 has a spherical shape. Liquefied gas to be carried is accommodated
in the cargo tank 20. In the embodiment of the present disclosure, the liquefied gas
accommodated in the cargo tank 20 is, for example, a highpressure low-temperature
gas of approximately 9 to 20 (BarG). The cargo tank 20 is an IMO Tank Type C tank
specified in the IMO IGC Code.
[0019] Each cargo tank 20 includes a lower half portion 21 and an upper half portion 22.
[0020] The lower half portion 21 is hemispherical in the lower portion of the cargo tank
20. The diameter dimension of the lower half portion 21 gradually increases upward
from below. The lower half portion 21 may, for example, have a semi-true sphere shape
having a constant radius of curvature or be formed so as to have a radius of curvature
increasing in stages upward from below in the cross section illustrated in Fig. 2.
[0021] The upper half portion 22 is provided above the lower half portion 21. The upper
half portion 22 is hemispherical in the upper portion of the cargo tank 20. The diameter
dimension of the upper half portion 22 gradually decreases upward from below. In the
embodiment of the present disclosure, the upper half portion 22 may have a semi-true
sphere shape having a constant radius of curvature or be formed so as to have a radius
of curvature increasing in stages upward from below.
[0022] The cargo tank 20 is not limited to the above shape. The cargo tank 20 may be configured
to include a cylindrical portion (not illustrated) or the like between the upper half
portion 22 and the lower half portion 21.
[0023] Each cargo tank 20 is supported on the hull 2 by the skirt 30. Each cargo tank 20
has a tank structure independent of the hull 2. The cargo tank 20 has a liquid-tight
structure and self-supports the load of the liquefied gas accommodated in the cargo
tank 20.
[0024] Fig. 3 is an enlarged cross-sectional view illustrating the configuration of the
joint between the cargo tank and the skirt.
[0025] The skirt 30 supports the cargo tank 20. The skirt 30 has a cylindrical shape extending
in an up-down direction Dv as a whole. The lower end portion of the skirt 30 is fixed
on a foundation deck portion 9 provided in the bottom portion of the cargo loading
section 8. An upper end 30t of the skirt 30 is connected to an outer peripheral surface
21f of the lower half portion 21 of the cargo tank 20.
[0026] The skirt 30 includes a tubular portion 31 and a tank support portion 32.
[0027] The tubular portion 31 has a cylindrical shape extending in the up-down direction
Dv and has a constant diameter dimension over the up-down direction Dv. The tubular
portion 31 in this embodiment has a cylindrical shape centered on an axis a passing
through the center of the cargo tank 20 in the ship width direction.
[0028] The tank support portion 32 is provided in the upper end portion of the skirt 30.
The tank support portion 32 is continuously provided on the upper portion of the tubular
portion 31. The tank support portion 32 extends upward and toward the inside in a
radial direction Dr. In other words, the tank support portion 32 extends toward the
outside in the radial direction Dr and downward from a tip 32t. In this embodiment,
the tank support portion 32 includes a curved portion 32w that curves upward and to
the inside in the radial direction Dr. The curved portion 32w is formed such that
the angle formed by the curved portion 32w and the central axis of the tubular portion
31 gradually increases upward. In this embodiment, the tip 32t of the curved portion
32w on the inside in the radial direction Dr is the upper end 30t of the skirt 30.
The tip 32t of the curved portion 32w abuts against the outer peripheral surface 21f
of the lower half portion 21 of the cargo tank 20. Here, the radial direction Dr means
the radial direction centered on the axis a described above. In addition, the circumferential
direction in the following description means the circumferential direction centered
on the axis a.
[0029] A crossing angle θ of the tip 32t of the curved portion 32w with respect to the outer
peripheral surface of the cargo tank 20 can be, for example, approximately 30 degrees
to 90 degrees. Here, the crossing angle θ is the angle that is formed by the innermost
part of an inner surface 30f of the upper end 30t in the radial direction Dr (that
is, the tip 32t) and a tangent ta1 of the outer peripheral surface 21f (circular arc
shape in Fig. 3) of the cargo tank 20 at the position intersecting the inner surface
30f in a cross section including the axis a (see Fig. 3). In this embodiment, the
curved portion 32w is provided and the tip 32t of the inner surface 30f is also curved.
Accordingly, the crossing angle θ is the angle that is formed by a tangent ta2 at
the tip 32t of the inner surface 30f (curved in Fig. 3) and the tangent ta1 on the
outer peripheral surface 21f in a cross-sectional view including the axis a.
[0030] As illustrated in Fig. 2, an inner diameter D1 of the upper end 30t of the skirt
30 (the tip 32t of the curved portion 32w) is smaller than an outer diameter D2 at
the equatorial part of the cargo tank 20. In Fig. 2, the inner diameter D1 and the
outer diameter D2 are illustrated in half for convenience.
[0031] As a result, the cargo tank 20 is supported from below by the upper end 30t of the
skirt 30.
[0032] As illustrated in Fig. 3, the cargo tank 20 and the skirt 30 are joined by welding.
As a result, the welded portion 40 is formed at the joint between the cargo tank 20
and the skirt 30. A high-strength welding material such as 9% Ni steel can be used
as the welding material that is used in welding the cargo tank 20 and the skirt 30.
By using such a high-strength welding material, the strength of the welded portion
40 can be enhanced, and thus the reliability of the welded portion 40 can be improved.
[0033] The welded portion 40 fixes the upper end 30t of the skirt 30 to the cargo tank 20.
In the welded portion 40 exemplified in this embodiment, the upper end 30t of the
skirt 30 is continuously fixed to the outer peripheral surface 21f of the cargo tank
20 over the entire circumference in the circumferential direction. Although a case
where the welded portion 40 is continuously formed over the entire circumference in
the circumferential direction has been described, the present disclosure is not limited
to this configuration. For example, the welded portion 40 may be formed at a part
in the circumferential direction. In this case, the upper end 30t of the skirt 30
is fixed to the cargo tank 20 at a part in the circumferential direction. In this
case, the welded portion 40 may be intermittently provided in the circumferential
direction of the cargo tank 20, that is, at a plurality of locations.
[0034] A joining member 50 is provided between the outer peripheral surface 21f of the lower
half portion 21 of the cargo tank 20 and the inner surface 30f of the skirt 30 facing
the inside in the radial direction Dr. The joining member 50 is provided at a plurality
of locations at intervals in the circumferential direction of the lower half portion
21 of the cargo tank 20. The joining member 50 exemplified in this embodiment is formed
in a flat plate shape along a vertical plane orthogonal to the circumferential direction
(that is, a virtual plane including the axis a). The joining member 50 has an inside
edge portion 50a welded along the outer peripheral surface 21f of the lower half portion
21 of the cargo tank 20 on the inside in the radial direction Dr and an outside edge
portion 50b welded along the inner surface 30f of the skirt 30 on the outside in the
radial direction Dr. Welding may be performed on only one of the inside edge portion
50a and the outside edge portion 50b. A lower edge portion 50c of the joining member
50 exemplified in this embodiment is formed in a circular arc shape that is recessed
upward in the central portion in radial direction Dr. The shape of the lower edge
portion 50c is not limited to the circular arc shape in which the central portion
in the radial direction Dr is recessed upward.
[0035] The ship of the above embodiment further includes the joining member 50 provided
at a plurality of locations at intervals in the circumferential direction of the lower
half portion 21 of the cargo tank 20 and joining the lower half portion 21 of the
cargo tank 20 and the inner surface of the skirt 30.
[0036] Accordingly, the spherical lower half portion 21 and the inner surface 30f of the
skirt 30 can be more firmly joined by the plurality of joining members 50 provided
in the circumferential direction. As a result, it is possible to further enhance the
strength with which the skirt 30 supports the cargo tank 20.
[0037] In the ship of the above embodiment, the upper end portion of the skirt 30 extends
downward and toward the outside in the radial direction Dr of the cargo tank 20. The
upper end 30t of the skirt 30 supporting the cargo tank 20 is connected to the lower
half portion 21 of the cargo tank 20. In addition, the upper end 30t of the skirt
30 is connected by the welded portion 40 to the outer peripheral surface 21f of the
lower half portion 21 of the cargo tank 20 so as to abut from the outside in the radial
direction Dr.
[0038] Accordingly, the upper end 30t of the skirt 30 and the outer peripheral surface 21f
of the lower half portion 21 of the cargo tank 20 are reliably welded, and the joining
strength of the welded portion 40 can be effectively enhanced.
[0039] In the ship of the above embodiment, the upper end portion of the skirt 30 has the
curved portion 32w that curves upward and to the inside in the radial direction Dr,
and the tip 32t of the curved portion 32w is welded to the outer peripheral surface
21f of the cargo tank 20.
[0040] By forming the curved portion 32w in the upper end portion of the skirt 30 in this
manner, the lower end of the curved portion 32w and the upper end of the tubular portion
31 can be formed smoothly and continuously. Accordingly, in the skirt 30 where the
tip 32t of the curved portion 32w is welded to the outer peripheral surface 21f of
the cargo tank 20, stress attributable to the load of the cargo tank 20 being locally
concentrated is suppressed.
[0041] Although an embodiment of the present disclosure has been described in detail with
reference to the drawings, the specific configuration is not limited to this embodiment
and also includes, for example, design changes within the gist of the present disclosure.
[0042] Although the curved portion 32w is provided in the upper end portion of the skirt
30 in the above embodiment, the present disclosure is not limited thereto. The upper
end portion of the skirt 30 may extend downward and toward the outside in the radial
direction Dr of the cargo tank 20 and may have a conical tube shape as an example.
In this case, a corner portion is formed at the joint part between the lower end of
the conical tube-shaped part and the upper end of the tubular portion 31 in the upper
end portion of the skirt 30. Accordingly, in a case where stress attributable to the
load of the cargo tank 20 may be locally concentrated on the corner portion between
the lower end of the conical tube-shaped part and the tubular portion 31, the corner
portion may be reinforced or the like so that sufficient strength is ensured.
[0043] In addition, although the upper end portion of the skirt 30 in the above embodiment
is provided so as to extend downward and toward the outside in the radial direction
Dr of the cargo tank 20, the present disclosure is not limited thereto. For example,
the upper end portion of the skirt 30 may have a cylindrical shape having a constant
diameter along the up-down direction Dv.
[0044] Although the joining member 50 is provided in the above embodiment, the shape of
the joining member 50 is not limited at all. The joining member 50 may have another
shape as appropriate insofar as the joining member 50 joins the lower half portion
21 of the cargo tank 20 and the inner surface 30f of the skirt 30. In addition, the
circumferential installation interval, count, and the like of the joining member 50
can be appropriately changed. Further, a configuration without the joining member
50 is also possible.
[0045] Although the cargo tank 20 and the skirt 30 in the above embodiment are provided
in the cargo loading section 8 formed in the hull 2, the present disclosure is not
limited thereto. For example, the cargo tank 20 and the skirt 30 may be provided on,
for example, the upper deck 5.
[0046] In addition, although the above embodiment assumes installation on the hull 2, the
present disclosure is not limited thereto. For example, providing on a floating body
(not illustrated) may be performed instead.
<Additional Notes>
[0047] The ship 1 described in the embodiment is, for example, grasped as follows.
[0048]
- (1) A cargo tank unit according to a first aspect includes: a cargo tank 20 of IMO
IGC Code Tank Type C; a skirt 30 having an upper end 30t connected to a lower half
portion 21 of the cargo tank 20 over a circumferential direction and extending downward
to be fixed to a hull 2; and a welded portion 40 fixing the upper end 30t of the skirt
30 to the cargo tank 20 over the circumferential direction.
The IMO Tank Type C cargo tank 20 is designed based on pressure vessel standards to
be capable of withstanding the temperature and pressure of the liquefied gas accommodated
therein. In the IMO IGC Code Tank Type C, fatigue strength requirements are not required
up to the joint with the skirt 30 as in the IMO IGC Code Tank Type B. Accordingly,
the cargo tank 20 has excellent strength characteristics because it is spherical,
it can be designed to be increased in wall thickness, and an increase in diameter
and an increase in capacity can be achieved with strength ensured.
- (2) The cargo tank unit according to a second aspect, which is the cargo tank unit
of (1), further includes a joining member 50 provided at a plurality of locations
of the lower half portion 21 of the cargo tank 20 at intervals in the circumferential
direction and joining the lower half portion 21 of the cargo tank 20 and an inner
surface 30f of the skirt 30.
As a result, the spherical lower half portion 21 and the inner surface 30f of the
skirt 30 can be more firmly joined by the plurality of joining members 50 provided
in the circumferential direction. As a result, it is possible to further enhance the
strength with which the skirt 30 supports the cargo tank 20.
- (3) In the cargo tank unit according to a third aspect, which is the cargo tank unit
of (1) or (2), the skirt 30 includes a tubular portion 31 and a tank support portion
32, the tubular portion 31 has a cylindrical shape extending in an up-down direction,
and the tank support portion 32 is continuously provided on an upper portion of the
tubular portion 31 and extends downward and outward in a radial direction Dr of the
cargo tank 20.
As a result, the tank support portion 32 is connected to the outer peripheral surface
21f of the lower half portion 21 of the cargo tank 20 so as to abut from the outside
in the radial direction Dr. As a result, the tank support portion 32 and the outer
peripheral surface 21f of the lower half portion 21 of the cargo tank 20 are reliably
welded, and the joining strength of the welded portion 40 is effectively enhanced.
- (4) In the cargo tank unit according to a fourth aspect, which is the cargo tank unit
of (3), an angle formed by the tank support portion 32 and a central axis of the tubular
portion 31 is formed so as to gradually increase upward.
In this manner, corner portion formation at the joint part between the tank support
portion 32 and the tubular portion 31 is suppressed. As a result, in the skirt 30
welded to the outer peripheral surface 21f of the cargo tank 20, stress attributable
to the load of the cargo tank 20 being locally concentrated is suppressed.
- (5) A ship according to a fifth aspect includes the cargo tank unit according to
any one of (1) to (4).
[0049] On condition that the capacity of the cargo tank 20 is increased, the number of the
cargo tanks 20 on the hull 2 can be reduced and the manufacturing cost of the ship
1 can be reduced.
Industrial Applicability
[0050] According to the present disclosure, it is possible to increase the wall thickness
of a cargo tank and, by extension, increase the size of the cargo tank.
Reference Signs List
[0051]
1: ship
2: hull
2a: bow
2b: stern
3A, 3B: broadside
4: ship bottom
5: upper deck
7: upper structure
8: cargo loading section
9: foundation deck portion
20: cargo tank
20a: upper portion
21: lower half portion
21f: outer peripheral surface
22: upper half portion
25: tank cover
30: skirt
30f: inner surface
30t: upper end
31: tubular portion
32: tank support portion
32t: tip
32w: curved portion
40: welded portion
50: joining member
50a: inside edge portion
50b: outside edge portion
50c: lower edge portion
D1: inner diameter
D2: outer diameter
Da: ship stern direction
Dr: radial direction
Dv: up-down direction
θ: crossing angle