US3661294A - Retaining wall for fluids and method for production - Google Patents

Abstract

A composite wall of reinforced synthetic resin, for retaining both gases and liquids, that is particularly adapted for underground use in gasoline storage tanks, which are resistant to external compression forces; such as, water flooded earth. The wall is characterized by a very high stiffness factor, produced by a combination of spaced ribs of filament wound material and that are hollow, retained on top of a chopped strand-resin wall, where the chopped strand bridges the spaces between the ribs. A process involving the steps of forming a tank end cap on a mandrel and thereafter supporting the end cap in space and laying up a resin-rich wall layer of chopped strand and resin in joined relation to the end cap, and curing the wall partially; then forming over the outer surface of the wall a hollow shell structure which comprises a combination of woven roving and filament wound layers superimposed and saturated with wet resin. Then completely curing the composite wall to produce a monolithic structure.

Description

nited States atent Pearson et al.

RETAINING WALL FOR FLUIDS AND METHOD FOR PRODUCTION Lee E. Pearson, Newark; Jeri 0. Clark, Granville, both of Ohio Owens-Corning Flberglas Corporation Aug. 10, 1970 Related US. Application Data Continuation of Ser. No. 62,678, Feb. 14, 1967, abandoned.

Inventors:

Assignee:

Filed:

Appl. No.:

US. Cl ..220/83, 220/3, 220/71 220/72 Int. Cl. ..B65d 7/46, 865d 1 H24 Field ofSearch ..220/3,5 R,5A,83,7l,72

References Cited UNITED STATESPATENTS 10/1952 Francis ..220/3 UX 9/1955 Noland ..220/3 UX 8/1967 Anderson ..220/83 8/1967 Anderson .....220/83 7/1968 Anderson .....220/7l 11/1968 Bastone ..220/83 firm/Ma FOREIGN PATENTS OR APPLICATIONS 1,456,663 9/1966 France ..220/5 R Primary Examiner-George E. Lowrance Attorney-StaeIin & Overman [57] ABSTRACT A composite wall of reinforced synthetic resin, for retaining both gases and liquids, that is particularly adapted for underground use in gasoline storage tanks, which are resistant to external compression forces; such as, water flooded earth. The wall is characterized by a very high stiffness factor, produced by a combination of spaced ribs of filament wound material and that are hollow, retained on top of a chopped strand-resin wall, where the chopped strand bridges the spaces between the ribs.

12 Claims, 11 Drawing Figures 6? 55 4 /a 4/4 I I PATENTEIJMAY 91972 3,661,294

sum 2 OF 3 L55 5 Puma/v & Jaw Q. CLZMK RETAINING WALL FOR FLUIDS AND METHOD FOR PRODUCTION This is a continuation of application Ser. No. 62,678, filed Feb. 14, 1967, now abandoned.

This invention relates to a novel alloy or composite wall of reinforced synthetic resin, for retaining fluids; and, more particularly, to a composite wall embodying an unusually high corrosion resistance factor; and, still further, that embodies an unusually high stiffness factor so that it is unexpectedly resistant to external compression forces. Thus, the invention is particularly adapted for manufacturing underground gasoline storage tanks for use under all earth conditions.

The invention also relates to a method for producing the novel composite wall.

THE PROBLEM Contamination of the soil, and water table beneath the surface of the soil in populated communities by gasoline and other petroleum products leaking from corroded underground iron storage tanks has risen to an alarming level. Though carbon steel tanks give reliable performance in many sections of the country, corrosive soil environments do present a serious problem in many other sections, particularly in the heavily populated eastern portion of the country. This is uniquely due to the fact that some of the most corrosive soils in the United States are found along the eastern seaboard and along the lower edge of the Great Lakes. These soil conditions seem to be particularly adverse to carbon steel tanks. The increasing human population naturally gives rise to an increasing automobile population. An increasing automobile population requires more service stations with more underground storage tanks.

When, in a highly populated area, several underground storage tanks leak substantially before being detected, it is obvious that more than the mere cost of replacing the tanks is at stake. Undetected "leakers" have been known to release 20,000 gallons or more of flammable fuel into the soil beneath a city. This is picked up and floated on the underground water table and is carried beneath the entire community. Two very substantial hazards are created as follows:

1. Fire Seepage of the floating fuel from crevices in the surface of the ground obviously presents a bad fire hazard. More particularly, the seepage of the fuel into the basement of a home or building presents an explosion hazard. Thus, a first threat arises against the safety and welfare of the population; and,

2. Contaminated Water Supply The contaminated water supply factor is self-explanatory. Hydrocarbon products are poisonous for human consumption and, therefore, the vital water supply of a community can become endangered by underground gasoline storage tank leakage.

A very important factor, which though not arising to the gravity of the two hazards discussed above, is nonetheless so interrelated to the two hazards as to absolutely require consideration along with them.

This is the factor of tank replacement caused by soil corrosion failure. This actually produces hazards (l) and (2). Therefore, if this third factor could be brought under control, hazards (l) and (2) could be eliminated and thus the vicious cycle of fire and health hazard and tank replacement could be stopped.

The key element in this cycle is corrosion which, when connected with underground stresses, causes tank failure.

Before explaining the manner in which these problems have been substantially eliminated by the present invention, however, a few further remarks about the tank replacement factor should be brought to light in order to illustrate the manner in which the tank owner will also benefit. Thus, in certain harsh soil conditions, carbon steel tanks have been known to require replacement in as little as 2 years.

Thus, the oil company not only faces the contingency of repeated tank replacement, but also the contingency of watered gasoline being pumped into cars.

The replacement costs of a 6,000-gallon capacity gasoline tank made of carbon steel make the original cost seem incidental. Thus, locating the leaker presents a first substantial cost. Then, once the leaker has been located, the station driveway has to be torn up so that the old tank can be excavated. This includes the cutting of connecting pipes and so forth, all involving substantial expense. Thereafter, either repairing or replacing the old tank involves cost, along with reburying the old tank, including the expense of a lift crane, making pipe connections and then repaving the apron.

Further, the replacement costs of the tank do not reflect the loss of product, the loss of business and the loss of prestige for the company by the community.

Whether corroded, leaking tanks let water in or gasoline out, they can disrupt a whole community and its residents, a contingency oil companies cannot afford from either an economic or public relations point of view.

It is, therefore, evident that a novel underground storage tank for liquid hydrocarbon fuels, that is substantially corrosion-proof; that is highly resistant to distortions by all earth loading conditions; that does not contaminate stored fuels, among others, would provide a substantial advancement to the 811.

Objects of the present invention are, therefore, to provide a novel fluid handling wall structure having the foregoing features.

A storage tank made by the present invention should prove substantially less expensive than steel tanks over the long term. The alloy design of the present invention forecasts a tank life of well over 20 years, even under adverse ground corrosion conditions. Thus, alleviation of the costs of replacement and the hazards enumerated above greatly favors the tank of the present invention.

As will become apparent from the following description, the wall of the present invention meets rigid tests for chemical inertness, abuse resistance, leakage, static and dynamic load bearing performance under flooded conditions, and fully meets standards of performance for an unequally supported tank as in faulty installation or wash-outs. These are all frequent causes of underground storage tank failure.

Other objects and advantages of the invention will appear in the following description and appended claims, reference being had to the accompanying drawings fonning a part of this specification, wherein FIG. 1 is a top-plan view of an underground gasoline storage tank using the novel composite wall of the present invention; and, made by the method of the present invention;

FIG. 2 is an enlarged sectional view, taken along the line 2-2 of FIG. 1;

FIG. 3 is a greatly enlarged sectional view, taken along the line 3-3 of FIG. 2, showing a valley or wall section between the stifiening ribs;

FIG. 4 is a perspective, sectional view of a rib area of the wall of the present invention, approximately actual size;

FIG. 5 is a schematic sectional view showing tank end cap formation or lay-up;

FIG. 6 is a schematic view, partly in section, illustrating the manner in which an end cap is placed against the end of amandrel 82, and is joined to an endless wall increment subsequently laid up on the outer surface of the mandrel;

FIG. 7 is a schematic view, partly in section, showing in greater detail the manner in which the side wall is laid up on the surface of a forming mandrel;

FIG. 8 is a schematic view, partly in section, showing the manner in which the ribs are applied to the wall and then covered with filament windings;

FIG. 9 is a fragmentary, side-elevational view of a rib;

FIG. 10 is a sectional view taken along the line l0l0 of FIG. 9; and,

FIG. 11 illustrates the manner in which two tank halves are welded at the center along the bracketedarea 24, to produce the tank of FIG. I.

By the present invention, a novel fluid handling wall is made from a glass-resin composite. Novelty resides particularly in the high stiffness factor imparted by the composite monolithic structure of the wall. Radial collapse forces, as in an earth buried condition, present a substantial challenge to the relatively low stifiness inherent in the usual glass reinforced resin laminate. By the present invention, unexpectedly high stiffness has been provided using a relatively low glass content, easily adequate, however, to surmount any tensile forces encountered.

It is unique in the method aspect of the present invention that a mobile chopped strand-resin system wall is autogenously set" so that a stiffening rib can be filament wound on the outside and be retained up on top of the surface of the chopped strand-resin wall.

THE INVENTION EMBODIED IN AN UNDERGROUND STORAGE TANK In FIG. 1, a tank is shown, which employs the wall structure of the present invention and which is made by the method of the invention. This is an ideal application of the invention for resisting external crushing forces, such as an earth and flooded water overburden as often encountered by a buried gasoline storage tank. Thetank 20 is made up of opposed frusto-conical tank halves 22, connected together by center joint 24. The novel composite"wall 26 includes a wall element in combination with arib 28. Actually, a plurality ofribs 28 are axially spaced along the length of thetank 20. The specific structure of the composite wall in the area of eachrib 28, will be described below. Theseribs 28 extend peripherally of thetank 20 and act in the nature of strong hoops against radially inwardly crushing forces. Since they are of high tensile strength, they also absorb tensile stresses to which thetank 20 may be subjected. It is important to note that theribs 28 unexpectedly add to the stiffness of thewall 25; also, they provide protective buffers during handling.

Theribs 28 are spaced apart a sufficient distance so that fill and vent fittings 30 and 32 can be installed between the ribs. Optional positions 34 for fittings are thus provided all along the length of thetank 20. In an actual 6,000-gallon capacity tank, of 8 feet nominal diameter, and approximately 20 feet length, a spacing of 16% inches between rib centers was employed and this provided adequate space for the installation of the fittings 30 and 32.

The specific cross-sectional profile of thecomposite wall 26 is shown in greater detail in FIG. 2. Thus, there arevalley sections 36 between each pair of spacedribs 28. It is particularly important to note that theribs 28 are of box-like cross section and are hollow forms. The rib profile includes a plateau 38 with slopingsides 40 extending down to thevalley sections 36 on each side.

In this particular embodiment of the invention, thesides 40 slope at an angle of about 45. However, this is not meant to be limiting and the broad scope of the invention is meant to encompass the hollow box form in the particular alloy or composite" wall as herein described.

THE WALL AND VALLEY STRUCTURE IN GREATER DETAIL, FIG. 3

A resin-rich surface 42 is indicated on the inside of thewall element 25; and, comprises a thin layer of substantially pure isophthalic polyester resin. This is used in a gasoline storage tank because it is so resistant to either corrosion by or contamination of hydrocarbon fuel products. Since the isophthalic polyester resins are produced from petroleum derivatives, they are inherently resistant to gasoline and gasoline additives. This resin-rich surface layer 42 is held in place by athin surfacing mat 44, made of lofted and bonded continuous glass fibers.

The centralsectional portion 46 of thewall 25 is made up of choppedcontinuous glass strands 48 andisophthalic polyester resin 50, thoroughly admixed and bonded to one another. This is a resin-rich layer, meaning having a greater content ofresin 50 than choppedstrand 48. The purpose of the higher resin content is to impart stiffness and, thus, thickness to thewall 25. The lower proportion of choppedstrand 48 is quite adequate, however, to impart necessary tensile strength to thewall 25, in combination with theribs 28. Thecomposite wall 26, therefore, readily withstands interior loading and other tensile stresses encountered in underground storage tank situations.

As is meant to be conveyed by FIG. 3, the choppedstrand segments 48 extend in random array and, thus, impart tensile strength in all directions. Thewall 25 is thus both stiff and strong.

A resin-rich surface 42 is also indicated on the outside, similarly being held in place by athin surface mat 44. Theouter surface mat 44 is optional. The resin-rich surface 42 is highly resistant to the most corrosive soil conditions.

The end caps 52, FIG. 1, are also of this general construction. According to the description of the method hereinafter, the end caps 52 are made by spray lay-up technique and are fitted on the end of a forming mandrel and joined to theside wall 25 as the side wall is similarly laid up.

An important feature of thecombination wall 25 of the present invention is that high stiffness is achieved with low glass content. This contributes substantially to a more economically competitive structure.

Stiffness increases at a rate 2.5 times thickness. Tensile modulus is not needed as much as stiffness in this construction. By comparison, stiffness bears only a 1:1 ratio to modulus. Therefore, an overlay of filament wound material, for example, is not nearly as efi'icient for stifiness increase.

THE RIB STRUCTURE As shown in FIG. 4, therib structure 28 is completely different from themain wall 25 and thevalley structure 36, shown in FIGS. 2 and 3. Thisrib structure 28 is formed or shaped over thewall 25, which is previously formed on the mandrel and is initially hardened. The twoelements 25 and 28 are then cured completely to produce a monolithic structure, wherein they are effectively welded together. Therib 28 is supported in its hollow shape by a simple three-sided cardboard shell 54. Trapezoidal wood blocks 56 are positioned at spaced points along the length of therib 28, to hold thecardboard shell 54 out from thewall 25. This preserves the hollow form of therib 28. This is important in order to preserve high strength in the rib, and in the rib in combination with thewall element 25.

Over thecardboard 54, there is a layer of woven roving 58. Glass cloth also can be used, though more expensive. Then, over the wovenroving layer 58, there is a layer of filament winding 60. This is made up of several thicknesses of continuousglass fiber strands 62 or rovings that are wound onto a tank half as it is rotated on a forming mandrel. This is explained in the method section of this specification.

Both the wovenroving layer 58 and thefilament wound layer 60 are saturated with thepolyester resin 50 used in forming theside wall 25. Note that thefilament wound layer 60 fans out somewhat from the lower edges of the ribs, and over theside wall 25 where theribs 28 join the side wall. The filament woundlayer 60 acts as a surfacing mat to hold aresinrich surface 42 in place over the top of theribs 28.

It will be noted that therib 28 andside wall 25 are welded together into a monolithic structure even though they are formed in quick succession. Thus, thewall 25 is first laid up and initially set or hardened by a self-contained catalyst; then, therib 28 is laid on over the top surface of the wall, and the filament winding 60 is applied. The initial set of thewall 25 keeps therib 28 up on the top surface of thewall 25 during the filament winding operation. The filament winding holds" the rib to the exterior of thewall 20. Theribs 28 are laid up with a heat-cure catalyst and are then thermally cured.

The thermal cure of the ribs produces a post-cure of theside wall 25 and welds the units into a composite, completely monolithic structure.

Thus, the chopped strand-resin wall 25 bridges the spaces between theribs 28, FIG. 1.

Therib 28 produces the action of a barrel hoop that is unexpectedly effective in resisting external crushing forces as encountered by the undergroundgasoline storage tank 20, as where a water-logged earth fill surrounds a buried tank. Tremendous crushing forces are present, and these are particularly severe when thetank 20 of FIG. 1 is empty and thewall 25 is thus not backed up by an incompressible liquid.

It is to be noted that the crush resistance of thecomposite wall 26 of the present invention is particularly resistant to oil canning. In order to hold a tank down under high water table conditions, steel straps are placed around each end and fastened to concrete piers. This prevents the tank from bursting out of the ground because of water pressure. High water conditions will tend to collapse the tank, if it is empty, by pushing up between the straps. Tanks made according to the present invention readily withstand such forces without rupture, and with very low distortion of the wall.

The composite wall of this invention, therefore, provides a substantial step forward in the art by using a chopped strand resin wall in combination with the filament wound and spaced hollow box ribs. Thus, the choppedstrand resin wall 25 bridges the spaces between theribs 28. Further, the choppedstrand wall 25 forms the base of each rib, providing a unique combination. Only the ribs are filament wound and, thus, costs are greatly reduced while stiffness and modulus are unexpectedly increased.

Corrosion resistance and long life are advantageously built into the wall structure of the present invention by means of the media which hold the thin layer of protective resin to the exposed surfaces of the total composite.

Important features of the tank shape of FIG. 1, with its slight taper from each end, growing larger at the center, in addition to the features just described are as follows. A natural sump area is provided at the center, bottom, for the accumulation of any moisture entrained in the fuel stored in the tank. This also provides a natural high loading point at the center of the tank. A natural high point is also provided at the center for venting the tank. Further, a high suction point is provided near each end, that is away from and above the level of the central sump so that fuel can be removed from the tank without withdrawing any moisture that collects in the sump area.

THE PROCESS The basic unit made by the present process is atank half 22. As shown in FIG. 1, this comprises anend cap 52 which is bonded to an endless frusto-conical wall segment 64 to form thetank half 22. The open ends of twotank halves 22 are welded at thearea 24, FIG. 1, to produce the completedtank 20.

The manner in which the end caps 52 are made and joined to the circularside wall increment 64 and the manner in which theribs 28 are put on theside wall 64 will now be described in detail.

END CAP MANUFACTURE, FIG.

Ametal mandrel 66 is utilized for laying up theend cap 52. Themandrel 66 has an appropriate contour to shape the end cap. In this instance, for producing the tank of FIG. 1, themandrel 66 is outwardly convex. A layer ofrelease agent 68 is first applied from a gun 70 to the outer surface of themandrel 66. Therelease agent 68 is suitable a wax or other to aid in removing the finished part from the polished surface of themandrel 66.

A layer of surfacingmat 44 is next applied to hold a resinrich surface on the inside of theend cap 52. Note FIG. 3 for this type of construction Next, there is applied by suitable means, alayer 74 of liquid resin and chopped strand reinforcement. One exemplary means for applying the chopped strand-resin layer 74 comprises agun 76 that chops continuous glass fiber strands and propels the choppedpieces 77 toward the exterior surface of themandrel 66. Simultaneously agun 78 applies a surrounding mist ofresin 50. Theresin 50 wets the choppedstrand 77 and together with the chopped strand, builds up thelayer 74 over thesurface mat 44 on themandrel 66.

Also, on the outside there can be applied an optional layer ofsurface mat 44 in order to hold a resin-rich surface on the outside. See FIG. 3 for this type of construction. Application of the surface mats is indicated schematically at the left, in order to keep FIG. 5 as clear as possible.

Theresin 50 applied by thegun 78 contains the catalyst. The resin is, therefore, self-curing.

Removal of the part from themandrel 66 is suitably affected by lifting off. If desired, an assist from a jet of air, introduced by a built-in conduit 80, can be used.

The process steps that arise from the prior description include the following:

1. Coating a forming mandrel with a release agent;

2. Applying surface mat and resin-rich coating;

3. Applying a chopped strand and resin lay-up of appropriate thickness;

4. Applying optional surface mat, and resin-rich coating;

5. Curing the resin to a solid, handleable condition; and,

6. Stripping the end cap from the mandrel.

This produces acap 52 that will fit onto the end of a formingmandrel 82, FIG. 6, used in making the endless frusto-conicalside wall increment 64 of FIG. 1.

THE SIDE WALL PROCESS, FIGS. 6 AND 7 As shown in FIG. 6, a rotatable mandrel is designated 82. This is a hollow, open-ended, frustoconical shell. The slight taper provides part release. Thus, the completed unit can be slid off the small end. Themandrel 82 is supported in a suitable manner for rotation on thecentral support shaft 84. Theshaft 84 is cantilevered so that the left end of themandrel 82 is exposed for application of theend cap 52, from FIG. 5.

As shown in FIG. 6, theend cap 52 is held in position at the end of themandrel 82 by means of a dead-center mechanism 86. The dead-center mechanism 86 is held in place by any suitable means. For example, aclamp 88 can be used to hold a leg of themechanism 86 to an angle iron 90 fastened to thefloor 92.

A dead-center mechanism 86 includes arotatable shaft 94 havingrubber pad 96 at one end, which abuts thetank end cap 52. Aspring 98 urges theshaft 94 in a direction to force therubber pad 96 against theend cap 52 and firmly holds the end cap in position on the end of themandrel 82.

As shown in FIG. 6, a layer ofwall 25, FIG 3, has been applied to cover the surface of themandrel 82 and is coupled with theend cap 52 during the process. The manner in which this is done is more specifically described by reference to FIG. 7.

Thus, as shown in FIG. 7, a layer ofrelease agent 100 is first applied to themandrel 82 by suitable means. This is shown schematically since release agents are known in the art. Theend cap 52, FIG. 6, is then pushed into position at the end of themandrel 82 as shown in FIG. 6. A layer of surfacingmat 44 is then applied, FIG. 7. Thereafter, alayer 74 of resin and chopped strand is built up on the outside of themandrel 82. This is of substantially the same thickness as that of theend cap 52. Then, a topsurfacing mat layer 44 is applied. The complete lay-up thus comprises the following components as shown in FIG. 3:

A resin-richinner surface 42, next to themandrel 82. applied after a suitable release agent has been applied to the mandrel;

Aninner surface mat 44;

Acentral zone 46, 74 in FIG. 7, of chopped strand and resin; thus, a resin-rich layer for stiffness;

An optionalouter surface mat 44; and,

A resin-richouter layer 42.

As shown by further reference to FIG. 7, theresin 50 is applied to the coated surface of themandrel 82 by thegun 78, as a layer of surfacingmat 44 is wound on from aroll 102, supported from the frame of the chopped strand andresin application apparatus 104. Appropriate tension is provided by abrake 106.

Theresin application apparatus 104 includes acarriage 108 supported byrollers 110 ontracks 112 that extend along the side of themandrel 82, parallel to the axis of the mandrel. The

to apply the various components.

Next, then, thestrand chopper 114 and theresin gun 78 apply thecentral zone 74 of choppedstrand 48 andresin 50. Theresin 50 contains catalyst and, thus, the resin system begins to cure as soon as it is applied; and, only enough catalyst is used to cause the resin to initially set to a firm or immobile condition.

After the layer of chopped strand andresin 74 is built up to a sufficient thickness, an optionalouter layer 44 of surfacing mat is applied and is saturated with appropriate resin to produce the resin-rich surface 42 as shown in FIG. 3.

Thebreak 116 in thesurface mat 44, shown in FIG. 7, indicates that the mat application may be discontinued between the inner and outer surfaces of theresin layer 74.

' APPLICATION OF THERIBS 28, FIG. 8

After thewall 25, FIG. 3, is built up in the manner shown in FIG. 7, it is permitted to cure to a sufficiently fin'n condition to support theribs 28, FIG. 8, without movement. Then, theribs 28 are applied as shown in FIG. 8. Each of theribs 28 is supplied to the machine operator as a long strip of material of the nature of the fragmentary showing of FIG. 9. Eachrib 28 is long enough to reach around thewall layer 74, previously formed as shown in FIG. 7, on themandrel 82, and the ends are abutted and temporarily secured.

As shown in FIGS. 9 and 10, arib 28 includes an elongated piece ofcardboard 54 that is slotted at 118 at spaced points to permit it to flex and wrap around themandrel 82. A long strip of woven roving 58 is tacked over the rib, through to the trapezoidal wood blocks 56, positioned underneath. This makes the rib strip a coherent unit for placing all the way around the tank.

The trapezoidal wood blocks 56, also shown in FIG. 4, establish and retain the appropriate cross-sectional form of theribs 28.

After theribs 28 are temporarily secured around thewall layer 25, afilament wound layer 60 is applied as shown in FIG. 8. A traversingcarriage 120 is movable back and forth parallel to the axis of themandrel 82. The carriage supports apan 122 containing a body ofliquid resin 124. Thecarriage 120 may include oneresin pan 122 for eachrib 28 applied. Referring to FIG. 1, this would amount to six resin pans for the six ribs on eachhalf 22 of thetank 20.

Therovings 62, made of continuous glass fibers, are fed from suitably locatedpackages 128 to aneye 130 and guideroll 132 and thence under adip roll 134 to be immersed inliquid resin 124. As thewet rovings 62 then pass between wiper bars 136, the amount of resin is reduced to a desirable level.

As themandrel 82, carrying the preformedribs 28 is turned, the traversingcarriage 120 is moved to and fro parallel to the axis of the mandrel. This is effective to lay the wettedrovings 62 on the outer surface of theribs 28 as shown in FIG. 4. Note the slight angular, or back and forth lay of therovings 62 in FIG. 4. Therovings 62 also lap over slightly onto thewall 25, FIG. 4, to provide a complete bond between therib 28 and the wall.

Due to the traverse of the wettedrovings 62 back and forth over theribs 28, the orientation of the rovings is both axial and peripheral. This imparts strength in both axial and peripheral directions to the tank. Additionally, the criss-cross lay of the rovings produces a very high strength shell structure, stress-resistance in all directions. Still further, the fabric layers 58, FIG. 4, positioned beneath thefilament wound rovings 62, provides high transverse strength to the ribs and this, in turn, is synergistically combined with the stiffness and strength of thewall 25 in a composite monolithic structure.

Additionally, the traverser of thecarriage 120 is adjusted to lay therovings 62 carefully along the slopingsides 40 of theribs 28 as shown in FIG. 4. Care is exercised in getting this orientation quite exact in order to provide a smooth contour over theribs 28. Control at this point is provided by the radiants 138, FIG. 8, which produce heat to gel the resin substantially as rapidly as thecontinuous strand rovings 62 are applied.

As therovings 62 are wound on, they compact the wovenroving layer 58, FIG. 4, gently down onto thecardboard shell 54, FIGS. 4, 9 and 10, and effectively drive out all gas. This renders the rib shell highly coherent.

It should be understood at this point, however, that therovings 62 for the filament winding operation shown in FIG. 8 are not in a condition that can actually be called "tension." The condition is more aptly described as oriented." Thus, thecontinuous rovings 62 are applied with just enough drag by the wiper bars 136 in theresin pan 124 to lay them on. This is sufficient to expel entrained gases and render the composite structure truly monolithic in character. Further, the rovings are ready to instantly assume load, but do not impart a prestressed condition to the composite body.

The combination of hollow form ribs is two-fold:

l. The peripheral orientation provides great radial strength;

and,

2. The axial traverse of therovings 62 provides great axial strength.

Therefore, the combination provides both radial and axial strengths; and, these include stiffness and tensile strength to meet all conditions encountered by the tank under consideration.

THE END CAP OVERLAY Referring back to FIG. 6, it will be understood that there is at least a hypothetical line joint between theend cap 52 and theside wall 25, because the wall is laid fresh against the previously partially cured end cap. Although the resins will theoretically cure together, added strength along the bend area is provided by adding a strip ofreinforcement 58. This is saturated with resin and cured. The result is a very strong monolithic structure with all of the resin cured together and strongly reinforced.

THE FINAL CURE This is now the point where the entire lay up is cured to a hard solid state to thereby produce a monolithic composite. This is effected by means of the radiants 138 in FIG. 8. When these are turned on they radiate heat against the lay-up; and, with themandrel 82 turning, the lay-up is heated evenly and uniformly. This post-cures theresin layer 25 and also fully cures the resin contained in theribs 28, and the resin applied to the area 140 in FIG. 6, at the joint between theend cap 52 and thewall portion 25.

THE MONOLITHIC RESULT It might be stated by way of comparison to prior processes known in the art, that is is known to first gel a chopped strand layer before covering directly with a filament wound layer. There has been some doubt that the two layers would weld into a monolithic structure. However, in the present invention, thewall 25 is catalytically set only to a sufficient hardness to hold or support therib 28 in position during the formation of the rib and keep the rib from being forced down into thewall 25 and displacing adjacent portions of the wall. Therib 28 is then wound on using wet resin which wets readily to thewall 25.

Thereafter, theribs 28 are cured by means of the radiants 138, shown in FIG. 8. This not only fully cures and post-cures the resin in the ribs, but also post-cures the resin of thewall 25. This very effectively produces a truly monolithic wall structure.

The final unit, therefore, is of monolithic character, yet displays a synergistic blend or combination of the unique stiffness and high tensile properties of the composite structure wherein the most far-reaching importance in the performance is the effeet produced by the inter-action of the properties of the constituents. The resin-rich wall 25 provides great stiffness in its own right. The box-like form of the ribs with filament winding over the top provides very high tensile and also imparts a high degree of stiffness. Thus, the rib overlay in combination with thestiff wall 25 beneath, provides a unique monolithic composite body that is light in weight yet of very high rigidity and strength. Note that there are dissimilar materials opposing each other in this structure.

By the present invention, the contribution of each eonstituent is independently acting relative to the other components. Thus, each constituent complements the other by contributing separate and distinct properties. Thus, the combination tank wall has radial crush resistance imparted by the rigid box ribs and also by the stiffness of thewall 25; further, the ribs impart high tensile strength. This brings out the fact that the properties of the constituents also supplement one another; the component properties are clearly higher than those of the constituent parts.

It is to be emphasized that the combination rib, in combination with the stiff wall, presents substantial novelty in accordance with this invention.

THE CENTER JOINT To assemble a complete tank as shown in FIG. 1, the open ends of the twotank halves 22, made as just described, are butted together and welded in the manner shown in FIG. 11. In one preferred method of center jointing in accordance with the invention, metal clips M2 are used. These include a U- shapedhalf 144 that fits over the open end edge of one of the tank halves. The other half comprises astrap 146 to slip inside the other tank half, thus holding it out to the contour of the first tank half.

With a plurality of these clips in place around the center, a layer ofmat 44 is placed over the joint, followed by alternate layers of woven roving 58 andmat 44, all being saturated with the catalyzedresin 50.

Since theclips 142 are buried in theresin 50, they are protected against corrosion.

The various layers of mat M and roving 58 are offset, to spread the weld or center joint 24 over a substantial area on each side of theabutment line 148. This is shown clearly by thebracket 24 in FIG. 1. This wide weld distributes stresses; and, further, thickness is sufficient to provide a fluid-proof seal.

SUMMARY OF THE SIDE WALL PROCESS The following method steps are inherent from the prior description, for the production of the composite wall of the present invention:

1. Laying up or forming a resin-rich wall layer of chopped strand and resin; the resin containing sufficient catalyst to set the layer whereby it will support the subsequent rib formation. Resin-rich surfaces are provided for the wall for corrosion resistance;

2. Forming over one surface of said wall layer, a hollow shell rib, using the wall layer as the base, for stiffness, and the rib shell comprising a combination of woven roving and filament wound layers, superimposed and saturated with set resin. Any suitable hollow shape or form, such as the cardboard illustrated, can be used to support the wet rib at this stage. It is important that the filament winding layer extend predominantly peripherally of the rib, with some axial traverse;

3. Completely curing the composite wall to produce a monolithic structure.

TANK PRODUCTION For the production of a tank, tank halves 22, FIG. 1, are formed by the steps of molding an end cap in the nature of the resin-rich wall 25 of FIG. 3, and joining this to a frusto-conical wall segment 64, made by Steps 1 and 2 above. Then, two tank halves are butt joined to complete the tank.

The effectiveness of storage tanks made by the present invention in withstanding actual use conditions include the following:

Four-inch pipe flanges were installed at the positions 30 and 32 in FIG. 1. These were carefully bonded to the wall. With the tank half buried, a torque of 3,300 pounds was applied without failure of the fitting or wall. Also, the fitting and wall withstood 400-pound load applied to the end of a 5-foot section of pipe installed in the fitting. The tank was checked for leakage before and after the test. There was none.

The tank was installed in a pit on a sand bed and covered with sand to a depth of 3 feet above the top. The sand was tamped in place. There was no damage to the tank.

In a very severe test, the tank was supported at each end and placed over a 3-foot void at the center. Thus, it was unequally supported at the bottom. Under buried conditions, and filled with water, there was no damage and maximum deflection was one-half inches in the side wall. When the test was reversed with the support in the center and the voids at each end, there was no damage and maximum deflection of the side wall was three thirty-seconds inch.

In an external hydrostatic pressure test, an empty tank was strapped down at the ends and buried in tamped sand, then flooded to 3 feet above the top. There was no failure and maximum deflection was twenty-five/thirty-seconds inch.

The tank that withstood the foregoing test was checked for leakage by using compressed air 5 psig., and soap solution around the fittings. There was no evidence of leakage.

In a drop test, an empty tank was dropped 2 feet onto a road surface. There was no protection. The only indication of the test was some whitening of the ribs at the point of impact, indicating slight delamination. However, there was no evidence of damage to the shell. Thus, the ribs provided an extremely high strength buffer, protecting the inner shell and retaining it fluid-proof.

The tank that was dropped was also tested, without repairing the rib damage, to 25 psig. gas pressure. This is five times the normal loading factor. The tank safely contained the pressure build up.

Immersion tests using cut sections of the tank wall were conducted using various acids, bases and fuels. These were extremely harsh tests conducted at F. At the end of six months there was more than 50 percent of original tensile, flexural and Izod impact strength retained in every instance. Test liquids included 5% NaOH, 20% l-l,S0,, 5% HNO;,, gasoline, toluene, benzene, etc., indicating the harshness of the tests.

Visual examination showed some discoloration, but there was no indication of fiber bloom or crazing.

The immersion and aging tests showed that the tank wall resisted the action of the stored product and surrounding soil conditions.

We claim:

1. In an underground storage tank for the retention of fluid contents and capable of withstanding the appreciable compression forces to be engendered by its below-ground location, the improvements of said tank being defined by a primary peripheral wall formed of randomly oriented, line-type reinforcement material and hardened resin bonded together into a sheet of substantially constant wall thickness throughout the length of the peripheral wall; and separate, axially spaced, annular, hollow stiffening ribs each superimposed upon said primary peripheral wall; and each rib being formed predominately of essentially the same randomly oriented, line-type reinforcement material and hardened resin as the primary peripheral wall, said ribs each having a peripheral outer wall joined to the primary peripheral wall by generally radially projecting side walls, and said ribs only each being circumscribed by a filament wound roving extending angularly to the rib to an extent such that the rib outer walls and side walls are enclosed thereby, the resin of (l) the primary peripheral wall, (2) the rib side walls, and (3) the rib peripheral walls being integrated into an integal monolithic mass, including the filament wound roving, by a common final curing.

2. In a storage vessel of the class described and having end caps closing the ends of an essentially cylindrical wall, the cylindrical wall consisting essentially of hardened matrix material containing discrete lengths of line-type reinforce ment material, the matrix being present in a predominate amount, a plurality of circumferentially extending, substantially hollow, ribs superimposed upon and spaced along the outer surface of said cylindrical wall, each rib being defined by a plateau surface spaced from said cylindrical wall and including sloping side walls extending between and integrally joined to said cylindrical wall and said plateau area, respectively, said ribs being of essentially the same matrix material as said wall plus superimposed continuous filament reinforcing material arranged in layer form and covering substantially the entire extent of each rib, said filament material being angularly disposed relative to each rib and being embedded in the hardened matrix of each rib, said cylindrical wall alone bridging the gap between said spaced ribs, and the matrix of said cylindrical wall and the matrix of said ribs being cured to an integral monolithic mass.

3. In a composite monolithic structure of the class described, a generally cylindrical primary wall comprising a layer of discrete randomly oriented lengths of line-type reinforcement material and hardened resin bonded together; a hollow rib superimposed upon and circumscribing a portion of the exterior surface of said primary wall and comprising axially spaced side portions projecting from said wall and joined by a peripheral wall spaced from said primary wall, said rib consisting essentially of the same discrete, randomly oriented lengths of line-type reinforcement material and hardened resin, as comprises the primary wall; and a layer of filament wound roving superimposed only on said hollow rib and extending angularly of the rib in a plurality of layers to circumferentially enclose the rib, the filament wound roving being saturated and bonded with the resin of the hollow rib, and the resin of the primary wall and of said rib being cured to an integral mass including the reinforcement material of said primary wall and of said rib and the filament wound roving.

4. In a composite monolithic structure for confining fluid contents underground and capable of withstanding the appreciable compression forces engendered by its below-ground location, the improvements of said structure being defined by a primary peripheral wall formed of randomly oriented, linetype reinforcement material and hardened resin bonded together into a sheet of substantially constant wall thickness throughout the length of the peripheral wall; and separate, axially spaced, annular, hollow stiffening ribs formed of reinforcement material and hardened resin and each superimposed upon said primary peripheral wall; said ribs only each being circumscribed by a filament wound roving extending angularly to the rib to an extent such that each such rib is enclosed thereby, the resin of l) the primary peripheral wall, and (2) the ribs being integrated into an integral monolithic mass, including the filament wound roving, by a common final curing.

5. In a composite monolithic structure of the class described and having an essentially cylindrical wall capable of confining fluid in an underground installation, said cylindrical wall consisting essentially of hardened matrix material containing discrete lengths of line-type reinforcement material, the matrix being present in a predominate amount, a plurality of circumferentially extending ribs superimposed upon and spaced along the outer surface of said cylindrical wall, said ribs being formed of essentially the same matrix material as said wall and each such rib being circumscribed by superimposed continuous filament reinforcing material arranged in layer form and covering substantially the entire extent of each rib, said filament material being angularly disposed relative to each rib and being embedded in the hardened matrix of each rib, said cylindrical wall along bridging the gap between said spaced ribs, and the matrix of said cylindrical wall and the matrix of said ribs being cured to an integral monolithic mass.

6. In a composite monolithic structure of the class described, a general? cylindrical grimaryl wall comprising a layer of discrete ran om y onente lengt s of line-type remforcement material and hardened resin bonded together; a rib superimposed upon and circumscribing a portion of the exterior surface of said primary wall and comprising axially spaced side portions projecting from said wall and joined by a peripheral wall spaced from said primary wall, said rib comprising a mixture of hardened resin and reinforcement material enclosing a hollow form, and said rib being circumscribed by a layer of filament wound roving superimposed only on said rib and extending angularly of the rib in a plurality of layers to circumferentially enclose the rib, the filament wound roving being saturated and bonded with the resin of the rib, and the resin of the primary wall and of said rib being cured to an in' tegral mass including the reinforcement material of said primary wall and of said rib and the filament wound roving.

7. In a composite monolithic structure of the class described, a layer of discrete lengths of line-type reinforcement material and hardened resin bonded together, a hollow shell form having sides joined to and bridged by a wall spaced from said layer, said hollow shell fonn being of generally trapezoidal shape and wherein the sides slope toward one another and away from said layer, and including a fiber layer as a shaping element, supported by spaced trapezoidal blocks to establish and retain form, and over the fiber layer shell is positioned a layer of woven roving and on top a layer of filament winding extending axially of the shell, the layers being saturated and bonded with synthetic resin and instantly ready to assume loading, and substantially without tension in the unstressed condition of the structure, and the resin of said composite being cured to an integral mass.

8. The invention according to claim 7, wherein said fiber layer comprises fiberboard and said trapezoidal block is wood.

9. The invention according to claim 2, wherein said hardened matrix is a synthetic resin and said discrete lengths of line-type reinforcement material are chopped glass strands, and said continuous filament reinforcement comprises continuous glass strands.

10. The invention according to claim 2, wherein said tank comprises opposed, aligned, and abutted endless wall elements of frusto-conical configuration, with the large ends abutted at the center of the vessel, and wherein said hardened matrix is a synthetic resin and said discrete lengths of line-type reinforcement material are chopped glass strands and said continuous filament reinforcement comprises continuous glass strands, and said wall elements being connected together at the center by alternate layers of mat and woven roving spanning the abutment line and being embedded in a hardened resin matrix.

11. The invention according toclaim 10, wherein said end caps consist essentially of layer of hardened matrix, in predominant amount, and containing discrete lengths of linetype reinforcement material, a layer of woven reinforcement extending over the end cap and the endless wall along the area where said end cap and endless wall join one another, and the woven reinforcement being embedded in hardened matrix.

12. The invention according to claim 11, wherein said discrete lengths are chopped glass strands and said woven reinforcement is made of continuous glass strands.

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Claims (11)

1. 2. In a storage vessel of the class described and having end caps closing the ends of an essentially cylindrical wall, the cylindrical wall consisting essentially of hardened matrix material containing discrete lengths of line-type reinforcement material, the matrix being present in a predominate amount, a plurality of circumferentially extending, substantially hollow, ribs superimposed upon and spaced along the outer surface of said cylindrical wall, each rib being defined by a plateau surface spaced from said cylindrical wall and including sloping side walls extending between and integrally joined to said cylindrical wall and said plateau area, respectively, said ribs being of essentially the same matrix material as said wall plus superimposed continuous filament reinforcing material arranged in layer form and covering substantially the entire extent of each rib, said filament material being angularly disposed relative to each rib and being embedded in the hardened matrix of each rib, said cylindrical wall alone bridging the gap between said spaced ribs, and the matrix of said cylindrical wall and the matrix of said ribs being cured to an integral monolithic mass.
2. 3. In a composite monolithic structure of the class described, a generally cylindrical primary wall comprising a layer of discrete randomly oriented lengths of line-type reinforcement material and hardened resin bonded together; a hollow rib superimposed upon and circumscribing a portion of the exterior surface of said primary wall and comprising axially spaced side portions projecting from said wall and joined by a peripheral wall spaced from said primary wall, said rib consisting essentially of the same discrete, randomly oriented leNgths of line-type reinforcement material and hardened resin, as comprises the primary wall; and a layer of filament wound roving superimposed only on said hollow rib and extending angularly of the rib in a plurality of layers to circumferentially enclose the rib, the filament wound roving being saturated and bonded with the resin of the hollow rib, and the resin of the primary wall and of said rib being cured to an integral mass including the reinforcement material of said primary wall and of said rib and the filament wound roving.
3. 4. In a composite monolithic structure for confining fluid contents underground and capable of withstanding the appreciable compression forces engendered by its below-ground location, the improvements of said structure being defined by a primary peripheral wall formed of randomly oriented, line-type reinforcement material and hardened resin bonded together into a sheet of substantially constant wall thickness throughout the length of the peripheral wall; and separate, axially spaced, annular, hollow stiffening ribs formed of reinforcement material and hardened resin and each superimposed upon said primary peripheral wall; said ribs only each being circumscribed by a filament wound roving extending angularly to the rib to an extent such that each such rib is enclosed thereby, the resin of (1) the primary peripheral wall, and (2) the ribs being integrated into an integral monolithic mass, including the filament wound roving, by a common final curing.
4. 5. In a composite monolithic structure of the class described and having an essentially cylindrical wall capable of confining fluid in an underground installation, said cylindrical wall consisting essentially of hardened matrix material containing discrete lengths of line-type reinforcement material, the matrix being present in a predominate amount, a plurality of circumferentially extending ribs superimposed upon and spaced along the outer surface of said cylindrical wall, said ribs being formed of essentially the same matrix material as said wall and each such rib being circumscribed by superimposed continuous filament reinforcing material arranged in layer form and covering substantially the entire extent of each rib, said filament material being angularly disposed relative to each rib and being embedded in the hardened matrix of each rib, said cylindrical wall along bridging the gap between said spaced ribs, and the matrix of said cylindrical wall and the matrix of said ribs being cured to an integral monolithic mass.
5. 6. In a composite monolithic structure of the class described, a generally cylindrical primary wall comprising a layer of discrete randomly oriented lengths of line-type reinforcement material and hardened resin bonded together; a rib superimposed upon and circumscribing a portion of the exterior surface of said primary wall and comprising axially spaced side portions projecting from said wall and joined by a peripheral wall spaced from said primary wall, said rib comprising a mixture of hardened resin and reinforcement material enclosing a hollow form, and said rib being circumscribed by a layer of filament wound roving superimposed only on said rib and extending angularly of the rib in a plurality of layers to circumferentially enclose the rib, the filament wound roving being saturated and bonded with the resin of the rib, and the resin of the primary wall and of said rib being cured to an integral mass including the reinforcement material of said primary wall and of said rib and the filament wound roving.
6. 7. In a composite monolithic structure of the class described, a layer of discrete lengths of line-type reinforcement material and hardened resin bonded together, a hollow shell form having sides joined to and bridged by a wall spaced from said layer, said hollow shell form being of generally trapezoidal shape and wherein the sides slope toward one another and away from said layer, and including a fiber layer as a shaping element, supported by spaced trapezoidal bLocks to establish and retain form, and over the fiber layer shell is positioned a layer of woven roving and on top a layer of filament winding extending axially of the shell, the layers being saturated and bonded with synthetic resin and instantly ready to assume loading, and substantially without tension in the unstressed condition of the structure, and the resin of said composite being cured to an integral mass.
7. 8. The invention according to claim 7, wherein said fiber layer comprises fiberboard and said trapezoidal block is wood.
8. 9. The invention according to claim 2, wherein said hardened matrix is a synthetic resin and said discrete lengths of line-type reinforcement material are chopped glass strands, and said continuous filament reinforcement comprises continuous glass strands.
9. 10. The invention according to claim 2, wherein said tank comprises opposed, aligned, and abutted endless wall elements of frusto-conical configuration, with the large ends abutted at the center of the vessel, and wherein said hardened matrix is a synthetic resin and said discrete lengths of line-type reinforcement material are chopped glass strands and said continuous filament reinforcement comprises continuous glass strands, and said wall elements being connected together at the center by alternate layers of mat and woven roving spanning the abutment line and being embedded in a hardened resin matrix.
10. 11. The invention according to claim 10, wherein said end caps consist essentially of layer of hardened matrix, in predominant amount, and containing discrete lengths of line-type reinforcement material, a layer of woven reinforcement extending over the end cap and the endless wall along the area where said end cap and endless wall join one another, and the woven reinforcement being embedded in hardened matrix.
11. 12. The invention according to claim 11, wherein said discrete lengths are chopped glass strands and said woven reinforcement is made of continuous glass strands.

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