U.S. patent number 3,903,824 [Application Number 05/422,533] was granted by the patent office on 1975-09-09 for liquefied gas ship tank insulation system.
This patent grant is currently assigned to Chicago Bridge & Iron Company. Invention is credited to Robert Newton Davis, Ivan Vallier La Fave, Royce Jay Laverman.
United States Patent |
3,903,824 |
Laverman , et al. |
September 9, 1975 |
Liquefied gas ship tank insulation system
Abstract
A ship having a hold containing a tank, for transporting a
cryogenic liquefied gas, which is structurally free-standing and is
spaced or separated from the ship hold walls, insulation secured to
the ship hold walls and hold bottom, a ship hold cover extending
over the tank top portion and joined to the ship, and a layer of
loose fill insulation and a resilient blanket layer between the
tank top portion and the ship hold cover.
Inventors: |
Laverman; Royce Jay (South
Holland, IL), Davis; Robert Newton (Bolingbrook, IL), La
Fave; Ivan Vallier (Naperville, IL) |
Assignee: |
Chicago Bridge & Iron
Company (Oak Brook, IL)
|
Family
ID: |
23675311 |
Appl.
No.: |
05/422,533 |
Filed: |
December 6, 1973 |
Current U.S.
Class: |
114/74A;
220/560.09; 220/901; 220/560.15 |
Current CPC
Class: |
F17C
3/025 (20130101); B63B 25/16 (20130101); F17C
2201/052 (20130101); F17C 2203/0631 (20130101); F17C
2203/0333 (20130101); Y10S 220/901 (20130101); F17C
2270/0105 (20130101); F17C 2221/033 (20130101); F17C
2221/012 (20130101); F17C 2201/0128 (20130101); F17C
2203/032 (20130101); F17C 2203/035 (20130101); F17C
2205/013 (20130101); F17C 2260/037 (20130101); F17C
2270/011 (20130101); F17C 2221/017 (20130101); F17C
2223/0161 (20130101); F17C 2203/0341 (20130101); Y02E
60/32 (20130101); F17C 2223/033 (20130101); F17C
2203/0636 (20130101); F17C 2260/038 (20130101) |
Current International
Class: |
F17C
3/02 (20060101); B63B 25/00 (20060101); B63B
25/16 (20060101); F17C 3/00 (20060101); B63B
025/16 () |
Field of
Search: |
;114/74A
;220/9LG,9B,9M |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Other References
"The Methane Tanker `Jules Verne`," The Motor Ship, Oct., 1964, p.
276t..
|
Primary Examiner: Blix; Trygve M.
Assistant Examiner: O'Connor; Gregory W.
Attorney, Agent or Firm: Merriam, Marshall, Shapiro &
Klase
Claims
What is claimed is:
1. In a ship having a hold containing at least one tank, for
transporting a cryogenic liquefied gas, which is structurally
free-standing and is spaced or separated from the ship hold walls,
the improvement comprising:
insulation secured to the ship hold walls and hold bottom,
a ship hold cover extending over the tank top portion and joined to
the ship,
a layer of loose fill insulation and a resilient blanket layer
between the tank top portion and the ship hold cover,
said resilient blanket and the loose fill insulation terminating at
a lower edge adjacent to the insulation on the ship hold walls,
and
said loose fill insulation is supported at the bottom against
downward flow by an expansion joint between the tank and ship hold
walls which permits horizontal and vertical displacements of the
tank relative to the ship hold walls.
2. In a ship having a hold containing at least one tank, for
transporting a cryogenic liquefied gas, which is structurally
free-standing and is spaced or separated from the ship hold walls,
the improvement comprising:
insulation secured to the ship hold walls and hold bottom,
a ship hold cover extending over the tank top portion and joined to
the ship,
a layer of loose fill insulation and a resilient blanket layer
between the tank top portion and the ship hold cover,
said resilient blanket and the loose fill insulation terminating at
a lower edge adjacent to the insulation on the ship hold walls,
and
the tank is a metal spherical shell and that part of the shell
which is in the insulated ship hold is uninsulated below the
resilient blanket, and the hold contains no other insulation.
3. The improvement according to claim 1 which the tank top portion
and the ship hold cover are both domed.
4. The improvement according to claim 1 in which a splash shield
separates the tank top portion from the loose fill insulation.
5. The improvement according to claim 3 in which the splash shield
is between the resilient blanket and the loose fill insulation.
6. The improvement according to claim 1 in which the tank is a
metal spherical shell and that part of the shell which is in the
insulated ship hold is uninsulated below the resilient blanket.
7. The improvement according to claim 1 in which the loose fill
insulation is expanded perlite or vermiculite.
8. The improvement according to claim 5 in which the splash shield
is fabricated from bonded sheets of polymeric material and aluminum
sheet.
Description
This invention relates to ships used for transporting cryogenic
liquefied gases. More particularly, this invention is concerned
with improvements in insulation systems used on ships which contain
tanks for transporting cryogenic liquefied gases and which tanks
are separate, independent, free-standing structures resting on
supports attached to the ship hull or hold structure.
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 form because of the
increased volume of gas which can be transported in liquid form
rather than in the form of a gas.
Some gases can be liquefied at moderate pressures and shipped in
tanks capable of maintaining the gas under such pressure to keep it
in liquid form. Propane and butane are representative of such
gases. Because the pressure needed to liquefy such gases at
atmospheric temperature is not unduly great, the pressure vessel
required for storage of the so liquefied gas can be built
economically and of a relatively large size. Cryogenic gases
however cannot be readily liquefied even at fairly high pressures
unless the temperature of the liquefied 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
cryogenic liquefied gas to a temperature at which it can be stored
in a tank designed to withstand a minimum internal pressure plus
the hydrostatic and dynamic loads of the liquid. 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 similarly
be stored at about atmospheric pressure following their
refrigeration to a temperature at which they boil at such
pressure.
Tanks for transporting cryogenic liquefied gases at about
atmospheric pressure in a ship or barge are of two main types. The
first type of tank is one in which the tank walls and bottom are
contoured to be in essentially continuous contact with, and be
supported by, the walls and bottom of a ship hold. Such a tank
relies upon this continuous contact with the walls of the hold of
the ship for its strength and support. The second type of tank is a
structurally free-standing tank which is spaced or separated from
the ship hold wall. Such a tank does not rely upon continuous
contact with the hold walls for necessary structural strength or
support. Such tanks have a support system which transmits the loads
of the storage tank to the ship structure through localized support
areas, such as would be the case, for example, when using columns
or a skirt to support a spherical tank. Such tanks are considered
to be safer than the first type of tank because they can maintain
their integral strength even if there is a failure of, or damage
to, portions of the ship's hull.
Suitable means must be used in ships or barges having cargo tanks
for transporting cryogenic liquefied gases to reduce or retard heat
leak so that the amount of liquefied gas which is vaporized is
minimized or limited to an acceptable value. Not only must the tank
be insulated to retard heat leak into the liquefied gas but, in
addition, it is necessary that insulation prevent the refrigerated
contents of the tank from cooling the ship structure to a
temperature low enough to cause structural failure of metal parts
not made of metal suitable for low temperature use.
Suitably insulating a cryogenic liquefied storage tank on a ship or
barge is not a simple matter. One type of tank suitable for this
use has double-curved surfaces which do not lend themselves to
ready insulation by the application of insulation boards or sheets
because of the cost and expense of fitting the insulation in
contact with the tank surface. Furthermore, such tanks often have a
top portion which extends partially above the ship deck. The tank
top portion furthermore is often domed and usually will have a
spherical or ellipsoidal shape. Not only must the tank top portion
having such a shape be suitably insulated but also the insulation
must be protected against the adverse weather conditions which the
ship will meet in service. A hold cover is generally installed for
this purpose.
According to the present invention there is provided an improved
system for insulating a ship tank for transporting a cryogenic
liquefied gas and which tank is structurally free-standing and is
spaced or separated from the ship hold wall. As used herein and in
the claims, "ship" includes all types of ships as well as barges
and boats. The improved insulation system comprises non-granular
insulation secured to the ship hold walls and hold bottom, a ship
hold cover extending over the tank top portion and joined to the
ship, and a layer of loose fill insulation plus a resilient blanket
layer between the tank top portion and the ship hold cover. The
insulating system of this invention is particularly useful when the
tank top portion extends partially above the ship deck and also
when the ship hold cover are both domed and are advisably also
approximately equally spaced apart over a substantial part of their
areas.
A further important feature of the invention is the inclusion of a
splash shield which separates the tank top portion from the loose
fill insulation so that in case there is a leak in the tank shell
the escaping liquid or vapor will be prevented from penetrating the
loose fill insulation and cooling the adjacent portion of the ship
hold cover or hold wall.
It is important that the tank be completely surrounded by an
insulating system. To do this, the resilient blanket and the loose
fill insulation can be terminated adjacent to the non-granular
insulation on the ship hold walls. In this way the tank is
positioned within a totally insulated space even though only the
upper portion of the tank has insulation directly, or essentially,
in contact with the outer surface of the tank shell. Thus, since
the tank shell lower part is located inside of the insulated ship
hold, it is suitable to leave the tank shell non-insulated over
that surface area which projects downwardly from the lower edge of
the resilient blanket.
The invention will now be described further in conjunction with the
attached drawings, in which:
FIG. 1 is an isometric view of a ship containing five spherical
storage tanks for cryogenic liquefied gas;
FIG. 2 is a sectional view taken along the line 2--2 of FIG. 1;
FIG. 3 is an enlarged sectional view of the insulation structure
used in the top portion of the tank shown in FIG. 2;
FIG. 4 is a vertical sectional view of an expansion joint
arrangement which separates the loose fill insulation from the
insulation applied to the ship hold walls;
FIG. 5 is a view similar to that shown in FIG. 2 but with a
somewhat different splash shield arrangement over the upper part of
the tank and with the tank supported by a cylindrical skirt rather
than a series of columns; and
FIG. 6 is an enlarged view of the insulation structure used in the
top portion of the tank of FIG. 5.
So far as is practical the same numbers will be used in the
different views of the drawings to identify the same or identical
parts or elements.
With reference to FIGS. 1, 2 and 3, the ship 10 is shown with five
spherical tanks 11 for storing cryogenic liquefied gas at a very
low temperature and at about atmospheric pressure or at such other
pressure as is considered appropriate and suitable for practical
transportation of the liquefied gas. Each tank 11 comprises a
spherical metal shell 12 positioned in the ship hold 13 so that the
major part of the shell is located below the main deck 14 of the
ship but with an upper top portion of the tank shell protruding
above the deck. As shown in FIG. 2, metal rings 15 and 16 extend
around shell 12 in a horizontal manner and the vertical stiffeners
17 extend between the rings. A plurality of spaced apart columns 18
around shell 12 extend from a supporting ledge in the ship hold to
ring 16 to support the metal shell 12 securely in position. The
lower portion of columns 18 can be insulated (not shown) to prevent
the adjacent ship hold at the base of the column from becoming too
cold.
The lower portion of the inside surface of the hold 13 is covered
by non-granular insulation 19 which extends over the entire ship
hold bottom and side walls up to the expansion joint 20. Insulation
19 can be of the foamed-in-place type of insulation or it can be
composed of insulation board or sheet stock firmly secured to the
hold surfaces. Sheet 21 is positioned over the insulation 19 in the
ship hold bottom and functions as a drip pan to collect all
liquefied gas which may leak from the spherical shell 12. The drip
pan 21 is made of a material which can withstand the low
temperature of the liquefied gas without structural failure. The
drip pan prevents liquefied gas from penetrating the insulation on
the ship hold bottom and thereby keeps it from contacting the metal
plates used in the construction of the ship hold. By keeping the
cold liquefied gas out of contact with the metal used for the ship
hold there is avoided any necessity to construct that part of the
ship proper of a metal or other material capable of withstanding
the cold temperature of the liquefied gas without failing.
As shown in FIGS. 2 and 3, resilient blanket 25 is placed in
contact with the outer surface of spherical shell 12 over that
surface of the shell extending above the expansion joint 20. A
liquefied gas and vapor impermeable sheet or covering splash shield
26 is placed over the outer surface of resilient blanket 25 to
prevent any liquefied gas which leaks therefrom from penetrating
into the loose fill insulation 27 which is placed over the
resilient blanket. Rigid metal hold cover 28 is placed over the
loose fill insulation and extends to the ship, such as to the ship
deck. The top of shell 12 is provided with a cupola 29 in which
supporting utility pipes, pumps and various operating control
systems can be positioned. The cupola is also shown covered both on
its sides and top with the resilient blanket 25, splash shield 26,
and loose fill insulation 27. In some instances it is desirable to
terminate the resilient blanket 25, splash shield 26, and loose
fill insulation at some position along the side wall of the cupola.
The upper remaining surface of the cupola can then be covered with
another insulation, such as foamed-in-place polyurethane foam.
Conduit 30 can be used to withdraw vapor from the shell 12 or to
fill it with a liquefied gas. Furthermore, conduit 31, which can
extend to the bottom of the tank shell, can be used to remove
liquefied gas from the tank.
FIG. 4 shows the expansion joint 20 in greater detail. Vertical
plate 32 constitutes the ship hold wall on which non-granular
insulation 19 equipped externally with a spray shield (not shown)
is secured. Metal plate 33 extends inwardly in a horizontal
direction from hold wall 32. Near the inner edge of plate 33 is
positioned upwardly extending metal plate 34 which supports an
inwardly directed horizontal plate 35. On the inner edge of plate
35 there is positioned a downwardly directed plate 36. Metal plate
38 is horizontally joined to the outer surface of tank shell 12.
Drain holes 37 are placed in metal plate 38 to permit drainage of
any leaking liquefied gas into the drip pan 21. Joined to the outer
edge of metal plate 38 is metal plate 39 which projects vertically
upwardly towards plate 35. Vertically extending plate 39 is
positioned approximately midway between the plates 34 and 36.
Resilient blanket 40 is doubled over twice to form a W-shape in the
space between the plates 34 and 36 with the fold between the two
v's of the W locked over the upwardly extending vertical plate 39.
The described expansion joint prevents the loose fill insulation 27
from falling downwardly into the ship hold yet it permits the tank
shell 12 to expand and contact with temperature change without
displacement of the loose fill insulation 27.
The described insulation system accommodates temperature expansion
and contraction of the tank shell 12 without displacement of the
loose fill insulation 27. When the vessel shell 12 expands the
dimensional enlargement of the shell is acccommodated through
compression of the resilient blanket 25. When the tank shell 12
cools and contracts, such as when it is filled with liquefied
natural gas, the dimensional shrinkage or reduction of tank shell
12 is accompanied by expansion of the resilient blanket 25 without
any significant displacement of loose fill insulation 27.
Any suitable resilient blanket can be used in the insulating system
of this invention. A particularly useful resilient blanket is one
made of fine glass fibers bonded together by a thin film of a
phenol-formaldehyde resin. The glass fibers can have a nominal
diameter less than 0.00015 inch and the blanket can have a density
of about 1-2 pounds per cubic foot. A commercially available
resilient blanket of glass fibers which can be used in practicing
this invention is marketed under the trade names Ultralite and
Textrafine. The thickness of the blanket employed will, of course,
depend on the size of the tank shell, the metal of which it is made
and the temperature cycle to which the shell will be subjected
during use. Further details concerning the qualities desired in a
suitable resilient blanket are set forth in Wissmiller U.S. Pat.
No. 3,147,878.
Any suitable loose fill insulation can be employed in the
insulating system of this invention. It is presently considered
advisable however to employ expanded perlite or vermiculite for
this purpose since it can withstand the pressures applied against
it by the resilient blanket during warm-up and expansion of the
tank shell.
Insulation of the ship hold is readily achieved because the bottom
of the hold and the hold walls generally are plane surfaces or no
more than single-curved surfaces so that they can be readily
covered with a minimum of fitting and cutting by use of insulation
board or sheet stock. Insulation board stock, however, is not
readily adaptable to insulating the surfaces of tank shell 12
because the surface of the shell is double-curved. The system of
this invention, however, employing the resilient blanket and loose
fill insulation combination is readily adaptable to double-curved
surfaces and involves no problem in fitting the insulation to the
contour of the tank shell.
The use of the resilient blanket-loose fill insulation combination
employed on the top portion of the tank shell surface does not lend
itself to use on the lower part of the tank shell surface because
the loose fill insulation complicates the provision of adequate
drain means for conveying spillage of liquefied gas into a drip
pan. Furthermore, the application of the insulation to the lower
portion of the tank shell would complicate visual inspection of the
vertical support system of the storage tank. By insulating the
surface of the ship hold below essentially the equator level of the
tank shell, instead of insulating the surface of the shell itself
over this area, easy access for visual inspection of the majority
of the tank support system is achieved.
The resilient blanket-loose fill insulation system also provides an
advantage in that no seams or gaps can develop in the insulation
over the top portion of the tank shell even during thermal movement
of the storage tank or through movement of the tank caused by
motion of the ship. If an insulating board system was used over the
top portion of the tank, gaps or seams could develop through such
movement and this would lead to a decrease in insulating capacity
because of the discontinuity in the insulation and the flow of air
through the gaps.
Any suitable material can be used for the splash shield 26. One
suitable material is made of a sheet of a polymeric material bonded
to an aluminum sheet. The polymeric material can be Mylar or some
equivalent material which can withstand the low temperatures to
which it will be subjected. A commercially available laminate of
Mylar and aluminum foil is available under the trade name Zero
perm.
FIGS. 5 and 6 illustrate a second embodiment of the invention;
however, the features, except those which will be subsequently
described, are the same as those illustrated in FIGS. 1 to 4. The
tank shell 12 in FIGS. 5 and 6 is supported by a cylindrical metal
skirt 50 which is mounted on its lower edge on a ledge of the ship
hold 13. Ring 51 is mounted on the shell 12 and extends around the
spherical shell. The ring is joined to the top edge of cylindrical
skirt 50. The top portion of the shell 12 shown in FIGS. 5 and 6
has a splash shield 55 made of metal, such as aluminum sheet,
spaced outwardly from the surface of shell 12 but joined thereto by
metal tabs 56. The space between the splash shield 55 and shell 12
provides clearance for any liquefied gas which leaks from the tank
to flow downwardly and to thereby avoid penetrating into any of the
adjacent insulation. The space also provides an accessible space
for leak detection by the passage of a carrier gas which can then
be analyzed for the presence of hydrocarbons. The illustrated
splash shield configuration does not depend on the use of columns
or a skirt support system. Of course, suitable drain holes 37 are
positioned in the expansion joint 20 to provide conduit means for
escaped liquefied gas to flow downwardly along the tank into the
drip pan 21.
Although the tank shown in the drawings is spherical, it should be
understood that the invention is not limited to a tank of this
shape or to the illustrated systems used to secure the tank to the
ship.
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.
* * * * *