[0001] The present invention refers to a tank construction and may be used for the construction
of storage tanks for light ends of petroleum products and preferably for gasoline
storage.
[0002] In petroleum product storage tanks currently operated for storage of petroleum products
without a floating cover or pontoons, the intensive evaporation of petroleum products
occurs on a liquid surface, which results in the formation of explosive and flammable
vapor mixture in the gas space of a tank. Even with the use of modem lighting protection
systems, we cannot avoid lighting striking to the tank. If lighting strikes any tanks
filled with petroleum products, explosions and fires occur, which lead not only to
significant losses but also result in injuries and death of people.
[0003] There are known methods of production of single-disc floating covers with a circular
pontoon, radial and circular floats or a ring pontoon and point floats, in which a
central part of the floating covers is delivered to a construction site as individual
sheets, ring pontoon, radial, ring buoys are delivered as individual elements, respectively:
hermetically sealed units (compartments), profile or box girders, bottomless boxes.
Radial, circular, point floats are located evenly over the entire cover area /
RU2200120, B65D88/34, 10.03.2003;
GB1191461A, B65D88/34, 13.05.1970,
RU2127216 C1, B65D88/34, 10.03.1999,
RU2163559 C1, B65D88/34, 27.02.2001/. On the racks above the bottom, a frame and floating cover
pontoons are collected. By the frame layers of the central part are spread, welded
together. On the spreading central part of the floating cover, radial and circular
or point floats are welded. The finished central part of the floating cover is welded
to the pontoon ring.
[0004] The main disadvantages of such covers are significant labor intensity of the construction,
low portability and, moreover, large metal intensity. In tanks using such pontoons,
the problem of formation of explosive and flammable vapor mixture is significantly
reduced but also remains. In such tanks in the event of lighting or the discharge-load
of petroleum products, the pontoon may be skewed within the tank, and it stops to
perform its protective functions (so called rigid pontoons).
[0005] Invention /
EP 2530032 A1, B65D88/34, 01.06.2012/ includes a cover, which consists of independent flexible
compartments in which spherical bodies are located. The specified spherical bodies
may have a different diameter to overlap densely a liquid margin by evaporation to
the gas space of a tank. However, as practice shows spherical bodies with a lower
diameter due to gravity action, as well present vibrations, always drop below the
bodies with a large diameter and do not overlap the space between the bodies with
a big diameter. Moreover, by chaotic filling of compartments with the bodies of various
diameters, they would not form an ordered structure with the minimum size of an empty
cell formed by the surfaces of the spherical bodies. But perforated cover compartments
will decrease but not prevent liquid evaporation. Moreover, according to our studies,
not only overlapping of liquid surface by the cover, which is located in the plane
of a liquid surface, is of great importance, but also an overlap in the gas space
above the liquid surface plays its role. At that in case of any collapsing of constructions
into the liquid, for example, the elements of automatic fire extinguishing systems,
what most likely occurs in explosions in the gas space of the tank, for example, with
lighting strike, such cover will be submerged and stop playing protective role in
the reduction of evaporation to the tank gas space combusted.
[0006] There is known the invention /
US12533218, B65D88/34, 31.07.2008/ that represents a floating barrier to reduce evaporation
of liquid product, which contains floating elements, which have a cross-sectional
polyhedron form. This invention like the previously described one solves the problems
of reduced evaporation, but does not solve the problem of combustion processes phlegmatization
in the possible combustion of liquid and air mixture. In the specified invention,
the problem of liquid surface overlapping on the tank walls is not also solved. On
tank walls the increased evaporation of liquid product will occur, and hazardous liquid
and air mixture will be collected in the gas space of the tank. Moreover, by chaotic
filling of the tank with the floating elements specified in the invention, it is rather
highly probable that the correct order of dense element installation "brink to the
brink" will be impaired that inevitably will result in the increase of liquid evaporation
rate.
[0007] Invention /
US8616398 B2, B65D 90/22, 25.09.2012/ is the closest to the declared invention in which a floating
barrier for the prevention of liquid evaporation is made with the set of floating
bodies. But as in the invention /
EP 2530032 A1, B65D88/34, 01.06.2012/, spherical bodies with a lower diameter, due to gravity action
and vibrations, always drop below the bodies with a large diameter and do not overlap
space between the bodies with a large diameter. As well by chaotic tank filling with
the bodies of various diameters, they would not form an ordered structure with the
minimum size of an empty cell formed by the surfaces of spherical bodies. But perforated
cover compartments will decrease but not prevent liquid evaporation. Moreover, according
to our studies, not only overlapping of liquid surface by the cover, which is located
in the plane of a liquid surface, is of great importance but also an overlap in the
gas space above the liquid surface plays the role. At that in case of any collapsing
of constructions into the liquid, for example, the elements of automatic fire extinguishing
systems, which most likely occurs in explosions in the gas space of the tank, for
example, with lighting strike or static discharge, even preliminarily ordered installation
of spherical bodies of various diameters will be impaired. Besides, in liquid discharge
- loading to the tank, the spherical bodies will be shifted with respect to each other,
rotated in respect of geometrical axis, what results in the adherence of flammable
liquid to their surface and increased evaporation. Moreover, the wall multi-layemess
of the spheroid bodes declared in the invention /
US8616398 B2, B65D 90/22, 25.09.2012/, with the use of various plastics and resins even with the
applied antistatic coating may not completely prevent the accumulation of static electricity
and the occurrence of discharge, which may cause ignition or explosion of vapor-air
mixture. It is confirmed with the introduction of the appropriate amendments to the
regulatory documents concerning prohibition to use plastic and other polymeric products
for tanks and other tanks for petroleum products.
[0008] Therefore, the goal of the invention is to make the tank for the storage of petroleum
products devoid of the disadvantages. The technical result is the following:
- 1) decrease of vapor mixture volume, which is formed with the evaporation of petroleum
products, i.e. the decrease of liquid vapor concentration in the gas space of the
tank;
- 2) provision of combustion process phlegmatization in the event of fire, lighting
strike;
- 3) prevention of the possible accumulation of static discharge and occurrence of spark
discharge between the floating bodies.
[0009] To solve the assigned task, as well to achieve the declared technical result, the
petroleum product storage tank is offered, which consists of a body, a shell and a
floating protective coating from numerous floating elements. The floating elements
are made as rotation bodies of the same shape. Some part of the floating elements
in the tank is located below a liquid surface, and some of them - in the tank gas
space. The distinctive feature of the proposed invention is that the floating elements,
which differ from each other in size for more than 5%. And the floating elements from
which the floating protective coating is made have the flotation center offset from
their geometric centre. All elements of the protective coating are made of non-sparkling
metal.
[0010] It is also proposed to locate the floating elements in the gas space forming not
more than four layers.
[0011] It is also proposed to locate the floating elements within a liquid forming not less
than one and a half layers.
[0012] As well in the upper part of the tank, a grid with a cell less than the floating
element diameter may be installed.
[0013] In the upper part of the tank, internal collaring may be also made.
[0014] In the lower part of the tank above a liquid discharge-load level, a grid with a
cell smaller than the floating element diameter may be installed.
[0015] A floating element constituting a floating protective coating may be made of aluminum
or its alloy.
[0016] A floating element may be made with a ceramic coating of aluminum oxide or stainless
steel.
[0017] Hydrophobic coating may be applied to a floating element surface.
[0018] It is preferable that the ratio of a maximum diameter of a rotation body to its wall
thickness is at least 60.
[0019] It is also proposed to make a floating element with the minimum diameter not less
than 10 mm.
[0020] It is also proposed to make a floating element with the maximum diameter not more
than 60 mm.
[0021] It is also proposed to make a floating element in a spheroid, ellipsoid or egg-shaped
form.
[0022] The invention essence is clarified by drawings where
on fig.1, the general appearance of a covered tank is provided; where it is denoted:
1 - the tank, 2 - the tank cover, 3 - the floating protective coating consisting of
numerous floating elements 4, 5 - the liquid (petroleum products), 6 - the liquid
surface, 7 - the gas space, 8 - the grid, 9 - the collaring, 12 - the lower grid.
on fig.2 and fig.3 - section A of fig. 1;
on fig.4,5,6,7 - cross section of some possible forms of the floating elements; where
it is denoted: 10 - the flotation center of a floating element, 11 - the geometric
center of the floating element 4.
on fig.8- the flow charts of liquid evaporation rate in the tank are provided depending
on its configuration: 13 - a curve for a tank without floating elements, 14 - a curve
for a rigid pontoon tank, 15 - a curve for a tank with a floating protective coating
from numerous floating elements.
[0023] The petroleum product storage tank 1 contains a cover 2, a floating protective coating
3 consisting of numerous floating elements 4 some of which are located in liquid 5,
i.e. below liquid surface 6, and some of them above liquid surface 6, i.e. in gas
space 7 (fig.1). In the upper part of the tank, a grid 8 (fig.2) or a collaring 9
(fig.3) are installed. Flotation center 10 of the floating elements 4 is offset from
their geometric centre 11 (fig.4, 5, 6, 7). In the lower part of the tank above a
drainage-load level, the upper grid 12 is made with a perforation cell smaller than
the floating element diameter 4.
[0024] The tank 1 with the cover 2 and the floating protective coating 3 acts in the following
way.
[0025] When the floating elements 4 are filled in to the tank 1 with the liquid 5 (petroleum
products), as well when the liquid 5 is loaded and discharged, they, being chaotically
distributed in the tank, are placed in several layers forming the floating protective
coating 3 with dense packing.
[0026] In the event of oscillation of liquid surface 6 in loads and discharges or explosion,
the floating protective coating 3 consisting of the numerous floating elements 4 as
rotation bodies of the same shape functions by the principle of tank duckweed. In
the event of possible lighting strike or collapse of the cover constructions 2 within
the tank 1, the floating elements 4 may diverge, even fly apart within the tank 1.
But then chaotically returning, they are placed to the structure with dense packaging
(floating protective coating 3) thereby they extinguish evaporation and evolving fire
locus, as well significantly phlegmatize combustion process. To prevent the discharge
of the floating elements 4 beyond the tank 1 in the event of explosion, in its upper
part, the grid 8 or the collaring 9 are installed. The grid 8 has a cell smaller than
the floating element diameter 4. The collaring 9 is installed as it is shown on fig.3,
by the periphery of the upper part of the tank 1. It allows to localize and extinguish
fire quickly and with the lack of risk of new explosions. To reduce the risk of penetration
of the floating elements to drainage holes, in the lower part of the tank above liquid
discharge -load, the grid 5 is made with a perforation cell smaller than a floating
element diameter.
[0027] To reduce the concentration of liquid vapors in the gas space 7 of the tank 1 and
provide phlegmatization of combustion process as the protective coating 3, the floating
elements 4 are used which are made as rotation bodies, with the flotation center 10
offset from their geometric centre 11. E.g., as fig.4, 5, 6, 7 show, the floating
element 4 may have a spherical, ellipsoid or egg-shaped form. Further considerations
would be made in relation to the floating elements 4 having spherical form. However,
it should be understood that such considerations also cover other rotation bodies.
With the tank discharge and loading, the spherical floating elements 4 may touching
each other turn about its geometrical center and touching the liquid 5 have a liquid
film on its surface. The film may evaporate and vapors will penetrate to the gas space
of the tank 7. To prevent this the spherical floating elements 4 are made so that
their gravity center 10 is offset from their geometric centre 11 (fig.4-8). Hereby
the spherical floating elements 4 will be constantly oriented in relation to the liquid
surface 6 and in the event of the tank discharge-load may only fluctuate slightly
in relation to their position. So a dry surface of the spherical floating element
4 will not be immersed to the liquid 5, and, respectively, have a liquid film. Moreover,
hydrophobic coating may be applied to the surface of the floating element 4, which
prevents a capillary effect. It will significantly reduce evaporation.
[0028] To prevent static electricity and possible spark discharge in the mass of the spherical
floating elements 4, these elements should be made from non-sparkling metal, mainly
from aluminum or its alloys. In this case, the necessary buoyancy of the elements
4 of the floating protective coating 3 may be provided. The criterion for selection
of the floating element size 4 is the ratio:
where D - the external diameter of the spherical floating element 4,
t - wall width of the spherical floating element 4.
[0029] The ratio of the floating element diameter n D to its wall thickness t should be
at least 60. The preferred ratio is n=80...110. The larger ratio is undesirable as
the floating wall element 4 will be too thin and not resistant to mechanic exposures.
For the same reasons, the minimum diameter of the floating diameter D should be at
least 10 mm. The maximum diameter of the floating element D should be not more than
60 mm. In this case the size of a cell formed by the surfaces of the floating elements
4, densely located will be less than the critical value, i.e. sufficient to break
a chain reaction (explosion) of stoichiometric petroleum product and air mixture (see
Semenov N.N., Chain reactions, M., Nauka, 1986). In other words, vapor -air mixture within such a cell will not explode being exposed
to any ignition source (static electricity spark, lightning strike, open fire exposure,
etc.).
[0030] Our studies have shown that a minimum number of layers of the floating elements 4
located in gas space to reduce the dramatically flammable liquid evaporation 5 and,
respectively, entry of liquid vapors to the gas space 7 of the tank 1 should be at
least four. Hereby combustion in the gas space 7 of the tank 1, even if it occurs
for any reasons, would be phlegmatic. It is explained by the fact that the liquid
evaporation rate 5 would be minimized due to overlapping of the liquid surface 6 and
the gas space 7 above the surface 6 with several layers of the floating elements 4.
[0031] Our calculations and tests have shown that the number of layers of the floating elements
4 located in the liquid 5 is of the same importance. After possible explosion in the
gas space 7 and spread of the floating elements 4 located in the gas space 7, they
first, being emerged, overlap the liquid surface 6 and thereby phlegmatize combustion.
And as the tests have shown the floating elements 4 scattered in the tank 1 completely
recover the floating protective coating 3. The number of layers of the floating elements
4 in the liquid 5 should be at least one and a half.
[0032] Reduction of evaporation rate is well illustrated by the diagram of relationship
between the level of excessive pressure and achievement time in the tank 1 in which
pressure is released (fig. 8), where 13 - a curve for a tank without the floating
elements, 14 - a curve for a rigid pontoon, 15 - a curve for a tank with the floating
protective coating 3 from the numerous floating elements 4. The diagram on fig. 8
shows that with the presence of the floating protective coating 3 in which the floating
elements 4 are placed in several layers, an excessive pressure is achieved for a longer
time.
[0033] To prevent the surface corrosion of the floating elements 4, a layer of aluminum
or its alloys should be applied to their surface. The preferred coating composition
for the floating elements is Al
2O
3. Our studies have shown that the ceramic surface coating of the floating elements
4 makes effective corrosive protection of metallic surface for the overwhelming majority
of petroleum products both of original manufacture and having various types of additives.
The studies have shown high corrosive resistance of such coating in relation to a
variety of flammable liquids and for benzenes it fully protects the surface of the
floating aluminum elements 4 from corrosion.
[0034] So the assigned goal and the technical result are achieved.
1. A petroleum product storage tank, which consists of a body, a shell and a floating
protective coating consisting of numerous floating elements as rotation bodies of
the same shape, some part of which are located below a liquid surface in the tank
and some of them - in the tank gas space characterized in that the floating elements in size and shape differ from each other for not more than
5%, the floating elements have a center of flotation offset from their geometric centre,
and all floating elements are made of non-sparkling metal.
2. The tank according to claim 1 characterized in that the floating elements located in the gas space form not less than four layers.
3. The tank according to claim 1 characterized in that the floating elements located within the liquid form not less than one and a half
layers.
4. The tank according to claim 1 characterized in that in its upper part, a grid with a cell less than the floating element diameter is
installed.
5. The tank according to claim 1 characterized in that in its lower part above the liquid discharge-load level a grid with a cell smaller
than the floating element diameter is installed.
6. The tank according to claim 1 characterized in that in its upper part an internal collaring is also made.
7. The floating element for the tank according to claim 1 made as a rotation body characterized in that it is made of aluminum or its alloy.
8. The floating element according to claim 3 characterized in that it is made with the ceramic coating of aluminum oxide or stainless steel.
9. The floating element according to claim 3 characterized in that the ratio of maximum diameter of the rotation body to its wall thickness is at least
60.
10. The floating element according to claim 3 characterized in that it is made with the minimum diameter not less than 10 mm.
11. The floating element according to claim 3 characterized in that it is made with the maximum diameter not more than 60 mm.
12. The floating element according to claim 3 characterized in that it has a spheroid, ellipsoid or egg-shaped form.