U.S. patent number 3,859,805 [Application Number 05/440,785] was granted by the patent office on 1975-01-14 for flat bottom ship tank for transport of liquefied gas.
This patent grant is currently assigned to Chicago Bridge and Iron Company. Invention is credited to Paul Richard Johnson, Willis James Kircik, Kenneth Wilson Lange, Elmer Weyman Rothrock, Jamshid Teymourian.
United States Patent |
3,859,805 |
Johnson , et al. |
January 14, 1975 |
**Please see images for:
( Certificate of Correction ) ** |
FLAT BOTTOM SHIP TANK FOR TRANSPORT OF LIQUEFIED GAS
Abstract
A combination of a ship having a hold with a bottom and walls,
and a tank, which is circular in horizontal section, for
transporting a liquefied gas; said tank having a metal shell having
(1) a substantially flat metal bottom (2) a spheroidal section
constituting most of the upper part of the tank and (3) a toroidal
knuckle portion tangentially joined to the periphery of the metal
bottom and tangentially joined to the spheroidal section; load
bearing insulation between the ship hold bottom and the tank metal
bottom; and a skirt, circular in horizontal section, extending from
the tank above the toroidal knuckle portion downwardly to a
supporting base in the ship hold.
Inventors: |
Johnson; Paul Richard (Oak
Lawn, IL), Teymourian; Jamshid (Hinsdale, IL), Rothrock;
Elmer Weyman (Hinsdale, IL), Kircik; Willis James
(Hinsdale, IL), Lange; Kenneth Wilson (Burr Ridge, IL) |
Assignee: |
Chicago Bridge and Iron Company
(Oak Brook, IL)
|
Family
ID: |
23750178 |
Appl.
No.: |
05/440,785 |
Filed: |
February 8, 1974 |
Current U.S.
Class: |
62/45.1; 62/240;
220/560.09; 114/74A; 220/901; 220/560.12; 220/560.08;
220/560.03 |
Current CPC
Class: |
B63B
25/12 (20130101); B63B 25/16 (20130101); F17C
3/025 (20130101); F17C 2203/0631 (20130101); F17C
2223/033 (20130101); F17C 2203/0639 (20130101); F17C
2201/052 (20130101); F17C 2221/017 (20130101); F17C
2221/033 (20130101); F17C 2270/0105 (20130101); F17C
2203/013 (20130101); F17C 2203/0354 (20130101); F17C
2223/0161 (20130101); F17C 2221/012 (20130101); Y10S
220/901 (20130101); F17C 2201/0142 (20130101); F17C
2201/0119 (20130101); F17C 2201/035 (20130101); F17C
2201/0109 (20130101); F17C 2201/0166 (20130101); Y02E
60/32 (20130101) |
Current International
Class: |
F17C
3/02 (20060101); B63B 25/00 (20060101); B63B
25/16 (20060101); F17C 3/00 (20060101); B63B
25/12 (20060101); F17c 007/02 () |
Field of
Search: |
;62/45,240 ;114/74A
;220/9LG |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Perlin; Meyer
Assistant Examiner: Capossela; Ronald C.
Attorney, Agent or Firm: Merriam, Marshall, Shapiro &
Klose
Claims
What is claimed is:
1. In combination:
a ship having a hold with a bottom and walls;
a tank, which is circular in horizontal section, for transporting a
liquefied gas;
said tank comprising a metal shell having (1l ) a substantially
flat metal bottom (2) a spheroidal section constituting most of the
upper part of the tank and (3) a toroidal knuckle portion
tangentially joined to the periphry of the metal button and
tangentially joined to the spheroidal section;
load bearing insulation between the ship hold bottom and the tank
metal bottom; and
a skirt, circular in hoirzontal section, extending from the tank
downwardly to a supporting base in the ship hold.
2. A combination according to claim 1 in which the skirt is
conical.
3. A combination according to claim 1 in which the skirt is
cylindrical.
4. A combination according to claim 1 in which the tank shell above
the skirt is externally insulated, the skirt is insulated
externally for its full height and the skirt is insulated
internally over at least its lower portion.
5. A combination according to claim 1 in which the toroidal
knuckle, in vertical radial section, is tapered and has its
thinnest edge joined to the periphery of the tank bottom.
6. A combination according to claim 1 in which a membrane is
between he ship hold bottom and the tank bottom.
7. A combination according to claim 1 in which a drip sheet is
between the ship hold bottom and the tank bottom.
8. A combination according to claim 7 in which the drip sheet
extends upwardly against insulation on the inside of the skirt.
Description
This invention relates to ships used for transporting cryogenic
liquefied gases. More particularly, this invention is concerned
with improvements in ship tanks for transporting cryogenic
liquefied gases and which tanks are separate, independent,
structures supported by and anchored to the ship bottom and not
necessarily otherwise dependent on the ship hull or hold structure
for support.
Many useful gases are available or are produced at geographical
locations far removed from the locations where they are used or
needed. Although some such gases can be economically transported
under pressure in the form of a gas, it is generally more desirable
to liquefy the gas and transport it in that state because of the
increased volume of gas which can be transported in liquid state
rather than in the gaseous state.
Some gases can be liquefied at moderate pressures and shipped in
tanks capable of maintaining the gas under such pressure to keep it
in the liquefied state. Because the pressure needed to liquefy some
gases at atmospheric temperature is not unduly great, the pressure
vessel required for storage of the so-liquefied gas can be built of
a relatively large size economically. Other gases, however, cannot
be readily liquefied even at fairly high pressures unless the
temperature of the gas is also reduced substantially below
atmospheric temperature. Because it is difficult and expensive to
construct a pressure vessel capable of storing a cryogenic
liquefied gas at high pressure in large volume, it has been found
more practical and less expensive to cool the liquefied gas to a
temperature at which it can be stored in a tank designed to
withstand a minimum internal pressure plus of course the expected
dynamic loads due to ship motions. For example, it has been found
convenient to store liquefied natural gas, which is essentially
methane, at about -260.degree.F. and at about 15 psia or just
slightly above atmospheric pressure. Other cryogenic liquefied
gases such as hydrogen, helium and ethylene can be similarly stored
at about atmospheric pressure following their refrigeration to a
temperature below the boiling point of the gas at such
pressure.
Tanks for transporting cryogenic liquefied gases at about
atmospheric pressure in a ship are of two main types. One type of
tank is a membrane tank in which the tank walls and bottom are
substantially continuously supported by the ship hull structure.
Such a tank relies upon the structure of the ship for the strength
and support needed to contain the liquid being stored. Another type
of tank is a structurally self-supporting or free-standing vessel
or tank which is spaced or separated from the ship hold bottom and
walls. Such a vessel or tank does not rely on the strength of the
hold walls for necessary reinforcement because it is structurally
independent of the ship hold walls insofar as its ability to
effectively contain the stored liquid is concerned.
One of the structurally independent types of pressure vessel tanks
is spherical. Spherical tanks have been mounted in the ship hold on
a metal cylindrical skirt with the tank bottom located above the
ship hold bottom. See U.S. Pat. Nos. 3,677,021 and 3,680,323. While
such tanks are suitable for liquefied gas transport by ship, they
do not occupy as much of the total hold space as would be desired
for maximum capacity. The amount of nonusable space between the
tank and the ship hold is unduly large and for efficient, more
economical transport this space should be reduced and the tank
occupy a higher percentage of the hold space. Also, such tanks
required all liquid load to go to the perimeter of the tank and to
then be redistributed to the ship bottom. This is not efficient or
economical. Furthermore, the spherical pressure vessel tank as
mounted in a ship hold according to the prior art extends
considerably above the ship deck and this causes the center of
gravity of the ship to be higher than desired when the tanks are
full of a liquefied gas. There is accordingly a need for a ship
tank which occupies more of the hold space, is largely free
standing and which results in a ship having a lower center of
gravity when loaded.
According to the present invention there is provided, in
combination, a ship having a hold with a bottom and walls, and a
tank, which is circular in horizontal section, positioned in the
hold for transporting a liquefied gas. The tank is characterized by
a metal shell which has the following three main shell sections or
portions: (1) a substantially flat metal bottom, (2) a spheroidal
section constituting most of the upper part of the tank, and (3) a
toroidal knuckle portion tangentially joined to the periphery of
the metal bottom and tangentially joined to the spheroidal section.
Located between the ship hold bottom and the tank metal bottom is
load bearing insulation upon which the tank bottom rests. A skirt,
circular in horizontal section, extends from the tank above the
toroidal knuckle portion downwardly to a supporting base in the
ship hold.
The described tank of this invention permits most of the
hydrostatic load from liquid in the tank to be transferred directly
and substantially uniformly through the insulation to the ship hold
bottom. Only part of the load must go thru the skirt and be
redistributed to the hold bottom. The tank bottom, since it is
supported by load bearing insulation, need not be made as thick as
the major spheroidal shell portion of the tank which, to meet code
and safety requirements, is built to pressure vessel standards. A
tank with such a relatively thin bottom is a hybrid tank in that
the thin bottom is in the nature of a semi-membrane while most if
not all of the remaining tank shell is of independent free standing
vessel construction which must contain the internal pressure by
stress in the shell. The bottom is, however, to some extent in
tension when the tank is loaded because of the forces applied
against the toroidal knuckle. The internal pressure due to liquid
cargo is primarily applied downwardly on the tank bottom and
thereby is transferred to the ship hold bottom.
The toroidal knuckle extending upwardly and outwardly in a curved
manner from the tank flat bottom is generally at least as thick as
the tank bottom. It can be thicker however; for example, it can
have a thickness up to or greater than the thickness of the
spheroidal shell portion of the tank. It is furthermore considered
most suitable for the toroidal knuckle when viewed in vertical
cross-section to be tapered from a thin thickness, which can be
about the same as the thickness of the tank bottom where it joins
the tank flat bottom, to a greater thickness where it joins the
spheroidal part of the tank.
That part of the tank shell located upwardly from the toroidal
knuckle and extending to the top of the tank constitutes the
spheroidal section or portion of the tank shell. The spheroidal
section can be spherical, elipsoidal or conispherical in which a
conical portion joins the toroidal knuckle to an upper spherical
section. Regardless of the particular shape, it joins the toroidal
knuckle tangentially in a smooth curve.
Even though a major part of any hydrostatic load in the tank is
transferred directly to the ship hold bottom, the supporting
circular skirt is an essential part of the tank support system. The
skirt supports some of the hydrostatic load when the tank is full.
Thus, the skirt supports much of the load from the periphery of the
tank flat bottom outwardly to the width of the tank. More
importantly, however, the skirt supports the tank stably during the
various motions which the ship may encounter. The skirt transmits
reactions resulting from horizontal loads and overturning movements
to the ship structure. The skirt is essential in resisting the
forces encountered at sea.
The skirt can be joined to the tank at its equator or widest part,
or at some location below the equator. Regardless of where the
skirt joins the tank it is structurally desirable for the joint to
be tangential. The lower end of the skirt can be joined to the ship
hold bottom or some other supporting base in the hold.
The skirt can be a vertically positioned circular cylindrical
shell, or a conical section shell generally with the largest end at
the top.
Since the tank is intended to transport a cryogenic liquefied gas,
it is insulated to reduce heat leak into the tank. The insulation
is advisably extended down the skirt to the skirt-supporting base.
The internal lower part of the skirt is also advisably insulated to
effect development of a suitable thermal gradient from the very low
temperature where the skirt joins the tank to the much higher, more
or less ambient temperature of the skirt-supporting base. A
suitable spray shield is placed around the tank, inside or over the
insulation, to entrap any liquid escaping in the event a crack
develops in the tank shell, and to direct the escaped liquid to a
drip pan below the tank.
To prevent any leaking liquefied gas from contacting the ship hull
bottom, a drip pan of suitable sheet material is placed beneath the
entire tank flat bottom but above the ship hold bottom. The drip
pan collects the cold liquid and prevents it from contacting and
cooling the ship hull to a temperature which might lead to failure
of the carbon steel from which a ship hull is normally made.
The described flat bottom, self-supporting tank occupies a larger
amount of the space in a ship hold than a spherical tank and as a
result can carry a larger volume of liquid. The invention reduces
the cost of a suitable storage tank, as well as the cost of a ship
hull, by directly transferring much of the product load to the ship
bottom. The required capacity of the inerting system is also
reduced by reduction of the empty space between the tank and ship
hold. The inherently lower profile of the tank lowers the center of
gravity of the ship when both empty and loaded compared to a ship
having a spherical tank in the same size hold. The lower profile
allows improved visability over that allowed by a spherical tank,
thus improving ship operation. The top of a flat bottom tank of
this invention can be made as much as twenty feet lower in
elevation than a spherical tank of equal capacity.
The invention will be described further in conjunction with the
attached drawings, in which:
FIG. 1 is a vertical sectional view through the width of a ship
containing a conispherical tank with a flat bottom according to the
invention;
FIG. 2 is an enlarged view of the lower part of the tank and ship
hold shown in FIG. 1;
FIG. 3 is a vertical sectional view through the width of a ship
containing a spherical tank with a flat bottom according to the
invention;
FIG. 4 is an enlarged view of the lower part of the tank and ship
hold shown in FIG. 3; and
FIG. 5 is an enlarged view of the lower part of a tank in a ship
hold and illustrates a tank with a tapered toroidal knuckle
portion.
So far as is practical, the same or similar elements in the
drawings will be identified by the same numbers.
With reference to FIGS. 1 and 2, ship 10 has a hold 11 defined by
hold bottom 12 and hold walls 14. Inside of the ship hold is
positioned conispherical tank 20.
Tank 20, circular in horizontal section, has a substantially flat
relatively thin bottom 21 of metal plate which slidably rests on a
layer of support material 22 placed over liquid impermeable
flexible membrane 23 supported on top of load bearing insulation
24. Tank bottom 21 is essentially circular. It is joined
tangentially at its periphery, such as by welding, to metal
toroidal knuckle portion 25 which is joined at its upper peripheral
edge, such as by welding, to ring 26. The tank bottom 21 generally
can be made thinner than the maximum thickness of the toroidal
knuckle portion since the hydrostatic load is applied against the
tank bottom and it, in turn, is transferred through the support
material 22, which can be balsa wood, and load bearing insulation
24 to the ship hold bottom 12.
A conical section 27 is joined, such as by welding, at its lower
edge to ring 26 and at its upper edge to spherical section 28 which
completes the tank major structural elements. The conical section
27, the spherical section 28 and the ring 26 together are
encompassed within the term "spheroidal-section" as that term is
used herein in describing the invention. Equipment well 29 extends
inside the tank for its full height and is used for piping, pump
and monitoring equipment associated with the tank.
Projecting downwardly from the lower outer edge of ring 26 is
conical skirt 30. The lower edge of conical skirt 30 is joined to
plate 31 which is bolted to plate 32 supported by upright metal
plate 33, thereby forming a bolted transition connection which
permits the tank to be secured in position to the ship hold bottom
even though the skirt and ship hold bottom are made of dissimilar
metals which are not directly weldable. The means used to join the
lower edge of the skirt to the ship hold bottom is, however, not a
critical part of the invention and other suitable means can be
used.
A series of weep holes 34 (FIG. 2) extend through skirt 30 for
delivery of escaped liquid to drip accumulating space 35.
Insulation 36 is placed over the inner lower portion of conical
skirt 30 and the membrane 23 is extended upwardly on the surface of
that insulation to angle shield 37.
The external surface of tank 20, and the external surface of
conical skirt 30, are covered by insulation 38 and over the
insulation is placed spray shield 39. The lower edge of the spray
shield 39 terminates in angle gutter 40 which directs accumulated
liquid through weep holes 34. The lower part of the insulation 38
on conical skirt 30 is covered with a vapor barrier coating 41,
such as of butyl rubber. Weather shield 42 is placed over the
entire tank part which extends above the ship deck.
In the described tank 10, vertical loads due to cargo weight and
vertical ship acceleration are transmitted to the ship structure
primarily through the tank flat bottom 21. Loads resulting from
overturning moment, horizontal shear and uplift loadings are
transmitted to the ship structure primarily through the skirt 30.
The tank bottom is supported by loadbearing insulation 24 having
adequate compressive strength to transmit vertical loadings from
the tank to the ship structure. The support material 22 functions
as a slide pad or means of accommodating differential movement due
to thermal displacement of the tank bottom when cycled from
atmospheric temperature to a very low temperature, such as
-260.degree.F. when used for tranporting liquefied natural gas, and
back to atmospheric temperature.
Insulation of the conical skirt in the manner previously described
leads to development of a uniform thermal gradient through the
skirt height, from very cold product temperatures in the skirt
upper part to about ambient (i.e. ship hull temperature) or
atmospheric temperature in the skirt lower part, which results in
thermal stresses within allowable design limits. The skirt base is
at approximately ambient temperature so that carbon steel can be
used in the ship hold construction.
The tank described with reference to FIGS. 1 and 2 has better
utilization of ship hold space than a spherical tank. As a result,
such a tank will have less overall height than a spherical tank,
permitting a lower center of gravity and lower profile in the ship
thereby increasing visability from the ship deck. Furthermore, by
better utilizing the ship hold space there is less residual space
which must be inerted. This thereby minimizes the capacity of the
inerting system and results in a significant savings in initial
cost and operation.
The volume tank of FIGS. 1 and 2 can be increased or decreased by
adjusting the length of the conical portion, the conical angle, or
the radius of the spherical portion of the conispherical tank. This
can have the advantage of permitting an increase in tank volume
without changing the ship breadth. A spherical tank can only be
adjusted by changing its radius so that a larger tank will require
a larger ship breadth.
A further embodiment of the invention is shown in FIGS. 3 and 4.
Ship 50, shown in partial lateral cross-section through its width,
has a hold 51 defined by a bottom 52 and hold walls 53. Loadbearing
insulation 54 is placed on hold bottom 52 and secondary barrier 55
is positioned on top of the insulation. A layer of support material
56 is placed on top of the secondary barrier 55.
Tank flat bottom 57, having a circular periphery, rests on layer
56. The tank bottom 57 is made of thin metal plate. Toroidal
knuckle 58 is welded at its lower edge to the peripheral edge of
the tank bottom and at its upper edge 59 to spherical section 60.
The upper edge of spherical section 60 is welded to metal ring 61.
Spherical section 62, which is an approximately hemispherical
section, is joined at its lower edge, by welding, to the top edge
of ring 61.
Vertically positioned cylindrical metal skirt 63 is joined to ring
61 by welding the upper edge of the skirt to the lower outer edge
of the ring. The bottom edge of skirt 63 is joined to plate 64 and
it is bolted to plate 65 supported by base plate 66. Base plate 66
is welded to a horizontal ledge in the lower part of the hold. Such
a transition joint is not always necessary to join the lower edge
of a skirt to the ship hold bottom. A skirt made of 9% nickel could
be welded directly to a carbon steel ship hold bottom.
Insulation 67 is positioned over the internal lower portion of
skirt 63 and barrier or membrane 55 is extended upwardly over the
insulation to angle shield 68. Insulation 69 is located on the
external surface of the tank, above ring 61, and on the external
surface of the skirt 63. Spray shield 70 covers the insulation on
the outside of the tank down to angle gutter 71. Vapor barrier
coating 72 is positioned over the outside of the insulation on the
external surface of the skirt from below the angle gutter 71 down
to the bottom edge of the skirt. Weather shield 73 covers the top
of the tank and extends to the hold top or ship deck to protect the
hold interior. Equipment well 74 extends for the full height of the
tank.
T
T The tank described with reference to FIGS. 3 and 4 has the same
advantages as the tank shown and described in FIGS. 1 and 2.
FIG. 5 illustrates another embodiment of the invention but one
which is very similar to the one shown in FIG. 2. The embodiment
shown in FIG. 5 however employs a toroidal knuckle 255 which is
made of tapered metal plate when viewed in vertical radial section.
The bottom peripheral edge 256 has the same thickness as the tank
bottom 21 and the upper peripheral edge 257 has the same thickness
as spherical section 260 extending between the toroidal knuckel and
ring 26. By employing a toroidal knuckle which is tapered as
described, or in an equivalent manner, increased flexibility of the
metal can be achieved and stresses thus better distributed.
The foregoing detailed description has been given for clearness of
understanding only, and no unnecessary limitations should be
understood therefrom, as modifications will be obvious to those
skilled in the art.
* * * * *