US2461096A - Self-sealing gasoline tank - Google Patents
Self-sealing gasoline tank Download PDFInfo
- Publication number
- US2461096A US2461096A US500420A US50042043A US2461096A US 2461096 A US2461096 A US 2461096A US 500420 A US500420 A US 500420A US 50042043 A US50042043 A US 50042043A US 2461096 A US2461096 A US 2461096A
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- US
- United States
- Prior art keywords
- tank
- walls
- wall
- sealing
- sealant
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000007789 sealing Methods 0.000 title description 16
- 239000000565 sealant Substances 0.000 description 16
- 238000010276 construction Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 9
- 150000001875 compounds Chemical class 0.000 description 8
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 241000272525 Anas platyrhynchos Species 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 229920003051 synthetic elastomer Polymers 0.000 description 3
- 239000005061 synthetic rubber Substances 0.000 description 3
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 2
- 229920002472 Starch Polymers 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 229920001971 elastomer Polymers 0.000 description 2
- 239000012850 fabricated material Substances 0.000 description 2
- 238000009877 rendering Methods 0.000 description 2
- 239000005060 rubber Substances 0.000 description 2
- 235000019698 starch Nutrition 0.000 description 2
- 239000008107 starch Substances 0.000 description 2
- JIAARYAFYJHUJI-UHFFFAOYSA-L zinc dichloride Chemical compound [Cl-].[Cl-].[Zn+2] JIAARYAFYJHUJI-UHFFFAOYSA-L 0.000 description 2
- UAOUIVVJBYDFKD-XKCDOFEDSA-N (1R,9R,10S,11R,12R,15S,18S,21R)-10,11,21-trihydroxy-8,8-dimethyl-14-methylidene-4-(prop-2-enylamino)-20-oxa-5-thia-3-azahexacyclo[9.7.2.112,15.01,9.02,6.012,18]henicosa-2(6),3-dien-13-one Chemical compound C([C@@H]1[C@@H](O)[C@@]23C(C1=C)=O)C[C@H]2[C@]12C(N=C(NCC=C)S4)=C4CC(C)(C)[C@H]1[C@H](O)[C@]3(O)OC2 UAOUIVVJBYDFKD-XKCDOFEDSA-N 0.000 description 1
- WSLDOOZREJYCGB-UHFFFAOYSA-N 1,2-Dichloroethane Chemical compound ClCCCl WSLDOOZREJYCGB-UHFFFAOYSA-N 0.000 description 1
- DMYOHQBLOZMDLP-UHFFFAOYSA-N 1-[2-(2-hydroxy-3-piperidin-1-ylpropoxy)phenyl]-3-phenylpropan-1-one Chemical compound C1CCCCN1CC(O)COC1=CC=CC=C1C(=O)CCC1=CC=CC=C1 DMYOHQBLOZMDLP-UHFFFAOYSA-N 0.000 description 1
- 229920002261 Corn starch Polymers 0.000 description 1
- 240000003183 Manihot esculenta Species 0.000 description 1
- 235000016735 Manihot esculenta subsp esculenta Nutrition 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 229920001079 Thiokol (polymer) Polymers 0.000 description 1
- 229960000583 acetic acid Drugs 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000003490 calendering Methods 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000008120 corn starch Substances 0.000 description 1
- 230000000994 depressogenic effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000009969 flowable effect Effects 0.000 description 1
- 239000012362 glacial acetic acid Substances 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229920001021 polysulfide Polymers 0.000 description 1
- 239000005077 polysulfide Substances 0.000 description 1
- 150000008117 polysulfides Polymers 0.000 description 1
- 229920001592 potato starch Polymers 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 229910052979 sodium sulfide Inorganic materials 0.000 description 1
- GRVFOGOEDUUMBP-UHFFFAOYSA-N sodium sulfide (anhydrous) Chemical compound [Na+].[Na+].[S-2] GRVFOGOEDUUMBP-UHFFFAOYSA-N 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 235000005074 zinc chloride Nutrition 0.000 description 1
- 239000011592 zinc chloride Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/90—Rupture proof
Definitions
- This invention has reference generally tol that class of inventions known as metallic receptacles and more particularly relates to a self-sealing gasoline tank and method of constructing the same, the tank being adapted for use on combat tanks and for other purposes.
- the invention contemplates the provision of a double wall tank for receiving a sealing compound or sealant between the walls and including means for yieldably spacing the outer flexible wll from the inner rigid wall.
- the invention consists in a novel construction of an outer wall of i'lexible layers and a method of forming such wall.
- a further aim and object of the invention resides in the provision of a tank of the above character involving the use of a novel sealing compound provided between the walls which, upon rupturing of either of the walls of the container, the material of the sealing compound having previously been put under slight compression, immediately flows to close the rupture, the invention including the heating of the completed tank in a closed room to a temperature of approximately 150 F., then removing and allowing the same to stand and cool for 12 hours, the compound expanding approximately in volume on congealing while the ilexible outer wall, including the gum coating, actually shrinks on the slight heating.
- More speciflc objects of the invention consist in the provision of improved means for interlocking the ends of the resilient spacing members to each other when arranged about the Wall of the inner tank and for applying and spacing other fiexible members about the interlocked or chimed ends of the inner container, the members being constructed so as to allow the sealing compound not only to pass throughout the complete area between the inner and outer walls but, owing to their hollow construction, allow the sealing to completely fill the same.
- a still further object of the invention resides in the provision of a device of the above char acter which permits of the use as an inner tank or container of a conventional jettison type tank now in use in the armed forces and in employing in connection therewith nonmetallic synthetic materials for producing the outer wall and the completed tank thereby resulting in a saving oi' vital war materials.
- Figure 1 is a longitudinal vertical sectional view through the improved tank.
- Figure 2 is a fragmentary cross sectional view taken on line 2-2 of Figure 1.
- Figure 3 is a longitudinal sectional detail through a portion of the end of the tank on an enlarged scale.
- Figure 4 is an enlarged transverse sectional detail on line 4 4 of Figure 1.
- FIG. 5 is a perspective detail
- Figure 6 is a diagramatic view indicating generally the method of lling the tank with a sealant.
- Figure 7 is a sectional detail through the bung opening.
- the improved tank comprising generally a double wall structure including an inner wall I, an outer ilexible wall generally designated 2, the walls being spaced from each other by the improved resilient spacing means 3 and 4.
- any type of an inner metallic container may serve as the inner tank in the double wall construction
- a conventional jettison type tank which includes a cylindrical metallic wall with bent over ends 5 which are embraced by the crimped or .beaded edges 6 on the outer edges of dished-like end plates 1.
- One end plate is tted with a conventional bushing 8 for receiving an outlet pipe or bung, not shown, while the cylindrical wall is also depressed on one side as at 9 and fitted with a combined filling and filtering element generally designated l 0 and of a conventional construction.
- a sheet of flexible material II preferably composed of l-ply 18-ounce duck skim coated on both sides with Wagner gum (the reaction product of ethylene dichloride and a freshly prepared solution of sulfur in an aqueous sodium sulfide solution).
- Wagner gum the reaction product of ethylene dichloride and a freshly prepared solution of sulfur in an aqueous sodium sulfide solution.
- the end edges of this material are arranged in overlapping relation and are heated and pressed ilrmly together to form a homogeneous mass.
- a similar layer I2 is arranged on the outer surface of the ends of the inner container.
- the spacing elements In constructing the tank it is ilrst desired to arrange the spacing elements on the inner tank or container I and in reducing this feature of the invention to practice it has been found ex ⁇ pedient, though not absolutely essential, to arrange seven of such elements circumferentially about the wall of the tank I, said elements preferably being constructed from ⁇ hose also formed of Wagner gum.
- the hose before being applied is slotted as at I3 to a depth equal to one-half of the diameter thereof, each slot being approximately 2" long with a section I4 of of approximately 1" of uncut hose remaining between the ends of the slot in order that the sealingV compound of the type disclosed in my prior Patent 2,403,836 dated July 9, 1946, may readily flow through and between the slotted rings and the double wall.
- the ends of the hose-like elements 3 may be scarfed in any suitable manner such as. for instance, shown at I5 in Figure 4 at their meeting ends and said ends being further held together by a covering of tape i6.
- 'I'he elements 4 are also of a cylindrical hose-like structure, there being preferably provided fourteen pieces which are slotted longitudinally as at I'i for engagement about the chimed or interlocked ends 6 of the inner container in suitably spaced relation so that the compound may flow through and between and by the same.
- a further disc may be tted at the other end of the tank structure but this is not desired for a reason that will become apparent.
- of double skim coated duck ⁇ which are approximately larger in diameter than the effective area of the outside of the tank and these form covers for both end areas, being suitably scarfed or cut out at their outer edges where they are turned in to overlie and smoothly engage the inner duck layer I8, being drawn taut, heated and pressed to form a homogeneous mass therewith.
- the intermediate layer 22 which is preferably formed of synthetic rubber and consists, for instance, of 50% standard. Wagner gum and 50% of reclaimed rubber, or 50% of Wagner gum and 50% of Thiokol F. A. (a, polysulfide gum).
- This layer 22 extends to a point as shown at 23 beyond the hose pieces I1 and two disc-like pieces 24 of the same material are applied at the ends of the tank and over the duck pieces 2i constituting the innermost layer. The edges of these pieces 24 are heated so as to be homogeneously connected with the wrapping 22 at the point 23. It is to be noted that 'this synthetic rubber material is such that it will resist in brittleness down to minus F.
- two flange-like covers 25 preferably formed from disc-like pieces of double skim coated duck having an outside diameter 10" larger than the tank with the inturned flanged portions being suitably cut so that they are applied as at 26 to the' layer 22. These flanged portions after being drawn taut are heated and pressed so as to be homogeneously connected with said layer 22.
- a channeled plate 211 is fitted over the attaching flange of the combined filling and strainer element I0 and suitably fastened as at 281 to the inner tank. It is also to be noted that the channel sides are inclined and arched at the upper edges and .10 formed with curved lateral flanges 291 which acts to clamp against the adjacent portions of the outermost fabric layer.
- the tank is now ready to receive the sealing compound 28 and in this instance it may be said that the sealing compound is the same as that employed in my prior Patent 2,403,836 granted July 9, 1946 and preferably consists of 25 pounds of zinc chloride solution and l0 pounds of starch, consisting preferably of four parts of corn starch and six parts of a specially treated tapioca or potato starch which has been found to contain a large part of starch inhibitors.
- This mixture has added thereto approximately 50 cc. glacial acetic acid which is maintained at 50 F. for four to ve hours, at which time it becomes freely flowable.
- It is now ready for insertion into the tank through a standard processor which, as shown in Figure 6, includes a receptacle 29 for containing, for instance, about pounds.
- the tank be placed in an inverted condition on end, that is, with the bushing 8 at the top, the bottom resting on a suitable support 30 while a tongue 3
- a vent opening 35 has been arranged in the top end and air pressure applied to the sealant, the latter flows through the tube 3 3 and nozzle 32 into the void area in the bottom, displacing air and discharging it through the vent opening 35.
- Continued pressure causes the sealant to flow gradually upward with the air pressure being varied or adjusted to counterbalance the sealant.
- the sealant, ofcourse flows between the walls through, into and by the hose-
- the completed tank is now placed in a room,
- the tank herein described is of 25-gallon capacity and in this connection it may also be observed that the hose-like elements 3 are preferably of outside diameter while the hose-like pieces 4 are preferably of 1%, outside diameter, to insure the formation of a symmetrical tank.
- loop-like handles 31 are tted over thel end edges.
- an inner metallic tank including side and end. walls in interlocking engagement with each other, a flexible outer tank surrounding the inner tank, spaced hollow and slotted yieldable means arrranged between the walls of the tanks and about and between the interlocking edges of the inner tank and the adjacent parts of the flexible tank for maintaining the respective walls in suitable spaced relation, and a sealant under compression arranged between the inner and outer tank walls and movable in and between the resilient spacing means.
- the combination in a metallic tank having interlocked chimed ends, of a series of endless slotted resilient elements arranged in suitably spaced relation about the side walls of the tank, a series of slotted tubular elements of slightly larger diameter arranged in spaced relation about the chimed edges of the inner tank, an outer laminated flexible tank arranged about the inner tank and spaced therefrom by the resilient elements, and a sealing comannoso 6 pound arranged under compression between the inner and outer tanks.
- a method of rendering a metallic tank for gasoline self-sealing consisting in'wrapping reo silient tubular elements in suitably spaced relation about the outer surface of the metallic tank, applying other resilient elements in spaced relation about the end edges of the metallic tank, alternately wrapping pre-treated fabricated matively about the side and end walls of the tank and about the resilient elements thereon to form an outer laminated flexible tank, heating and pressing said layers of fabricated material and rubberlike material so as to homogeneously fasten them in position, and inserting a sealant between the outer surface of the metallic tank and the flexible tank.
- Y 4 A method of rendering a metallic tank for gasoline self-sealing, consisting in'wrapping reo silient tubular elements in suitably spaced relation about the outer surface of the metallic tank, applying other resilient elements in spaced relation about the end edges of the metallic tank, alternately wrapping pre-treated fabricated matively about the side and end walls of the tank and about the resilient elements thereon to form an outer laminated flexible tank, heating and pressing said
- a method of rendering a metallic tank for ⁇ 20 gasoline self-sealing consisting in wrapping resilient tubular elements in suitably spaced relation about the outer surface of the metallic tank, applying other resilient elements in spaced relation about the end edges of the metallic tank, alternately wrapping pre-treated fabricated material and sheeted rubber-like material respectively about the side and end walls of the tank and about the resilient elements thereon, heating and pressing said alternately wrapped layers so as to homogeneously fasten them in position, inserting a sealant between the outer surface of the metallic tank and the formed laminated structure arranged thereabout, heating the complete structure in a closed groom at a temperature of aD- proximately 150 F. for a period of approximately five minutes, then removing and allowing the tank to stand for approximately l2 hours, thereby placing the sealant under compression and causing the shrinkage of the pre-treated layers.
- sealant under compression arranged between the tanks and endless resilient tubular elements arranged between the tanks to maintain the tanks in spaced relation and provided with-slots forming passageways through which the sealant may Dass.
- an inner metallic tank a flexible outer tank surrounding the inner tank, spaced hollow resilient means arranged between the tanks and about and between the end edges of the inner tank and the adjacent parts of the flexible tank for maintaining the tanks in suitably spaced relation and including endless tubular members constructed of resilient material and provided at their outer portions with a series of suitably spaced slots and a sealant under compression arranged between the inner and outer tank walls and movable in and between the resilient spacing means.
- an inner metallic tank including side walls and end walls in interlocking engagement therewith, a, flexible outer tank surrounding the inner tank, spacing means arranged between the inner and outer side walls of the tanks and about and between the interlocking edges of the inner tank and the adjacent parts of the flexible tank for maintaining the respective walls in suitably spaced relation, said spacing means including a plurality of slotted tubular yieldable elements, the slotted portions of which engage the interlocked ends of the inner tank while the tubular elements are arranged in suitably spaced relation about the interlocked terial, and sheeted rubber-like material respec- 59.01118' meins.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Description
H. P. WAGNER SELF-SEALING GASOLINE TANK Feb. 8, 1949.
Filed Aug. 28. 1945 95%- H. Pdfczjzer awful; #Mm
Feb. 8, 1949.
y H. P. WAGNER SELF-SEALING GASOLINE TANK Filed Aug. 2s, 1943 3 Sheets-Sheet 2 1 6 3mm 5.3M@
Feb. 8, 1949. H. P. WAGNER SELF-SEALING GASOLINE TANK 3 Sheets-Sheet 3 Filed Aug. 28, 1945 I. 'Il
. gwwm li. PI/layzzez Patented Feb. 8, 1949 UNITED. sTATEs PATENT vol-FlcE 2,461,096 SELF-SEALING GAsoLlNE TANK Hans P. Wagner, Akron, Ohio Application August 28, 1943, Serial No. 500,420
This invention has reference generally tol that class of inventions known as metallic receptacles and more particularly relates to a self-sealing gasoline tank and method of constructing the same, the tank being adapted for use on combat tanks and for other purposes.
As its primary aim and object the invention contemplates the provision of a double wall tank for receiving a sealing compound or sealant between the walls and including means for yieldably spacing the outer flexible wll from the inner rigid wall.
As an additional and equally important object the invention consists in a novel construction of an outer wall of i'lexible layers and a method of forming such wall.
A further aim and object of the invention resides in the provision of a tank of the above character involving the use of a novel sealing compound provided between the walls which, upon rupturing of either of the walls of the container, the material of the sealing compound having previously been put under slight compression, immediately flows to close the rupture, the invention including the heating of the completed tank in a closed room to a temperature of approximately 150 F., then removing and allowing the same to stand and cool for 12 hours, the compound expanding approximately in volume on congealing while the ilexible outer wall, including the gum coating, actually shrinks on the slight heating.
More speciflc objects of the invention consist in the provision of improved means for interlocking the ends of the resilient spacing members to each other when arranged about the Wall of the inner tank and for applying and spacing other fiexible members about the interlocked or chimed ends of the inner container, the members being constructed so as to allow the sealing compound not only to pass throughout the complete area between the inner and outer walls but, owing to their hollow construction, allow the sealing to completely fill the same.
A still further object of the invention resides in the provision of a device of the above char acter which permits of the use as an inner tank or container of a conventional jettison type tank now in use in the armed forces and in employing in connection therewith nonmetallic synthetic materials for producing the outer wall and the completed tank thereby resulting in a saving oi' vital war materials.
Other objects, as well as the nature, characteristic features and scope of the invention will be more readily apparent from the following description taken in connection with the accompanying drawings and pointed out in the claims forming part of this specification.
The invention is clearly illustrated in the accompanying drawings in which:
Figure 1 is a longitudinal vertical sectional view through the improved tank.
Figure 2 is a fragmentary cross sectional view taken on line 2-2 of Figure 1.
Figure 3 is a longitudinal sectional detail through a portion of the end of the tank on an enlarged scale.
Figure 4 is an enlarged transverse sectional detail on line 4 4 of Figure 1.
Figure 5 is a perspective detail, and
Figure 6 is a diagramatic view indicating generally the method of lling the tank with a sealant.
Figure 7 is a sectional detail through the bung opening.
Referring now, more particularly, to the accompanying drawings in which similar reference numerals designate corresponding parts throughout the various views, there is provided the improved tank comprising generally a double wall structure including an inner wall I, an outer ilexible wall generally designated 2, the walls being spaced from each other by the improved resilient spacing means 3 and 4.
Although any type of an inner metallic container may serve as the inner tank in the double wall construction, it has been found expedient to employ a conventional jettison type tank which includes a cylindrical metallic wall with bent over ends 5 which are embraced by the crimped or .beaded edges 6 on the outer edges of dished-like end plates 1. One end plate is tted with a conventional bushing 8 for receiving an outlet pipe or bung, not shown, while the cylindrical wall is also depressed on one side as at 9 and fitted with a combined filling and filtering element generally designated l 0 and of a conventional construction.
In carrying out the invention it has been found desirable to apply about the outer surface of the cylindrical inner wall I a sheet of flexible material II preferably composed of l-ply 18-ounce duck skim coated on both sides with Wagner gum (the reaction product of ethylene dichloride and a freshly prepared solution of sulfur in an aqueous sodium sulfide solution). The end edges of this material are arranged in overlapping relation and are heated and pressed ilrmly together to form a homogeneous mass.
Likewise, a similar layer I2 is arranged on the outer surface of the ends of the inner container.
In constructing the tank it is ilrst desired to arrange the spacing elements on the inner tank or container I and in reducing this feature of the invention to practice it has been found ex` pedient, though not absolutely essential, to arrange seven of such elements circumferentially about the wall of the tank I, said elements preferably being constructed from` hose also formed of Wagner gum. The hose before being applied is slotted as at I3 to a depth equal to one-half of the diameter thereof, each slot being approximately 2" long with a section I4 of of approximately 1" of uncut hose remaining between the ends of the slot in order that the sealingV compound of the type disclosed in my prior Patent 2,403,836 dated July 9, 1946, may readily flow through and between the slotted rings and the double wall. The ends of the hose-like elements 3 may be scarfed in any suitable manner such as. for instance, shown at I5 in Figure 4 at their meeting ends and said ends being further held together by a covering of tape i6. 'I'he elements 4 are also of a cylindrical hose-like structure, there being preferably provided fourteen pieces which are slotted longitudinally as at I'i for engagement about the chimed or interlocked ends 6 of the inner container in suitably spaced relation so that the compound may flow through and between and by the same.
The parts are now in position to receive the laminated outer wall 2 and in reducing this fea.- ture of the invention to practice there is employed for the inner layer I8 another piece of 18- ounce duck provided with a double skimmed coating of Wagner gum, the same being wrapped around the hose assembly area, the ends being drawn tightly, arranged in overlapping relation and heated `at this point and pressed together to form a homogeneous mass. It has been found desirable to employ a disc-like member I9 preferably of fibrous material, the same being fitted to lie against the inner edge and adjacent the outer periphery of the inner circumference defined by the slotted hose-like elements I'I, said disc having a tubular extension 20 which seats about the edge of the bung bushing 8. If desired, a further disc may be tted at the other end of the tank structure but this is not desired for a reason that will become apparent. There are now employed two disc-like pieces 2| of double skim coated duck `which are approximately larger in diameter than the effective area of the outside of the tank and these form covers for both end areas, being suitably scarfed or cut out at their outer edges where they are turned in to overlie and smoothly engage the inner duck layer I8, being drawn taut, heated and pressed to form a homogeneous mass therewith. Next there is applied the intermediate layer 22 which is preferably formed of synthetic rubber and consists, for instance, of 50% standard. Wagner gum and 50% of reclaimed rubber, or 50% of Wagner gum and 50% of Thiokol F. A. (a, polysulfide gum). It is preferably in the form of a calendered sheet and is wrapped around the inner layer I3, drawn taut with the overlapped edges arranged to adhere to each other by the application of' heat. This layer 22 extends to a point as shown at 23 beyond the hose pieces I1 and two disc-like pieces 24 of the same material are applied at the ends of the tank and over the duck pieces 2i constituting the innermost layer. The edges of these pieces 24 are heated so as to be homogeneously connected with the wrapping 22 at the point 23. It is to be noted that 'this synthetic rubber material is such that it will resist in brittleness down to minus F.
In providing the outermost layer there are employed two flange-like covers 25 preferably formed from disc-like pieces of double skim coated duck having an outside diameter 10" larger than the tank with the inturned flanged portions being suitably cut so that they are applied as at 26 to the' layer 22. These flanged portions after being drawn taut are heated and pressed so as to be homogeneously connected with said layer 22. Finally, a further sheet of double skim coated duck 21 is wrapped about the intermediate synthetic rubber layer on the wall and over the flanged ends of the outer end covers 25 as shown clearly in Figure 3 and constitutes the outermost layer, the end edges being arranged in overlapping relation and after =being drawn taut are heated and pressed to form a homogeneous connection while the side edges, of course, are likewise similarly treated so as to be homogeneously connected to the flanged covers 25.
As shown in Figures 1, 3 and 5, a channeled plate 211 is fitted over the attaching flange of the combined filling and strainer element I0 and suitably fastened as at 281 to the inner tank. It is also to be noted that the channel sides are inclined and arched at the upper edges and .10 formed with curved lateral flanges 291 which acts to clamp against the adjacent portions of the outermost fabric layer.
The tank is now ready to receive the sealing compound 28 and in this instance it may be said that the sealing compound is the same as that employed in my prior Patent 2,403,836 granted July 9, 1946 and preferably consists of 25 pounds of zinc chloride solution and l0 pounds of starch, consisting preferably of four parts of corn starch and six parts of a specially treated tapioca or potato starch which has been found to contain a large part of starch inhibitors. This mixture has added thereto approximately 50 cc. glacial acetic acid which is maintained at 50 F. for four to ve hours, at which time it becomes freely flowable. It is now ready for insertion into the tank through a standard processor which, as shown in Figure 6, includes a receptacle 29 for containing, for instance, about pounds. In filling it is preferred that the tank be placed in an inverted condition on end, that is, with the bushing 8 at the top, the bottom resting on a suitable support 30 while a tongue 3| is cut on an angle as shown, to receive preferably a rubber nozzle 32 on the outer end of a hose connection 33 leading from the receptacle 29 the same having been previously placed under air pressure as at 34. After a vent opening 35 has been arranged in the top end and air pressure applied to the sealant, the latter flows through the tube 3 3 and nozzle 32 into the void area in the bottom, displacing air and discharging it through the vent opening 35. Continued pressure causes the sealant to flow gradually upward with the air pressure being varied or adjusted to counterbalance the sealant. The sealant, ofcourse, flows between the walls through, into and by the hose- The completed tank is now placed in a room,
which is heated to 150 F. and allowed to stand for approximately iive minutes. It is then removed and allowed to cool and let stand for a period of approximately twelve hours. The sealant expands approximately in volume on congealing while the flexible laminated layer actually shrinks on the said slight heating. As a result the sealant area is put under slight pressure between the double Walls so that in the event of a bullet passing through and rupturing the outer wall or both walls the sealant under compression immediately ilows to close the rupture.
In actual use the tank herein described is of 25-gallon capacity and in this connection it may also be observed that the hose-like elements 3 are preferably of outside diameter while the hose-like pieces 4 are preferably of 1%, outside diameter, to insure the formation of a symmetrical tank.
In order to facilitate quick manipulation of the tank, loop-like handles 31 are tted over thel end edges.
It is believed in view of the foregoing that a further and detailed description of the operation of the invention is entirely unnecessary. Likewise, it is believed that the advantages of the invention will be readily apparent. It is to be noted, however, that it is preferable to fasten the laminated layer about the inner surface of the tubular extension by means of -a fastening and clamping sleeve V3Ii1 having an internal annular flange seating against the bushing 8 and an external annular flange clamping against the outer flexible end wall as shown clearly in Figure 'l on the engagement of the sleeve in the position shown. y
Having thus fully described the invention, what is claimed as new and desired to be secured by Letters Patent is:
1. In a tank construction, an inner metallic tank including side and end. walls in interlocking engagement with each other, a flexible outer tank surrounding the inner tank, spaced hollow and slotted yieldable means arrranged between the walls of the tanks and about and between the interlocking edges of the inner tank and the adjacent parts of the flexible tank for maintaining the respective walls in suitable spaced relation, and a sealant under compression arranged between the inner and outer tank walls and movable in and between the resilient spacing means.
2. In atank construction, the combination, in a metallic tank having interlocked chimed ends, of a series of endless slotted resilient elements arranged in suitably spaced relation about the side walls of the tank, a series of slotted tubular elements of slightly larger diameter arranged in spaced relation about the chimed edges of the inner tank, an outer laminated flexible tank arranged about the inner tank and spaced therefrom by the resilient elements, and a sealing comannoso 6 pound arranged under compression between the inner and outer tanks.
3, A method of rendering a metallic tank for gasoline self-sealing, consisting in'wrapping reo silient tubular elements in suitably spaced relation about the outer surface of the metallic tank, applying other resilient elements in spaced relation about the end edges of the metallic tank, alternately wrapping pre-treated fabricated matively about the side and end walls of the tank and about the resilient elements thereon to form an outer laminated flexible tank, heating and pressing said layers of fabricated material and rubberlike material so as to homogeneously fasten them in position, and inserting a sealant between the outer surface of the metallic tank and the flexible tank. Y 4. A method of rendering a metallic tank for` 20 gasoline self-sealing, consisting in wrapping resilient tubular elements in suitably spaced relation about the outer surface of the metallic tank, applying other resilient elements in spaced relation about the end edges of the metallic tank, alternately wrapping pre-treated fabricated material and sheeted rubber-like material respectively about the side and end walls of the tank and about the resilient elements thereon, heating and pressing said alternately wrapped layers so as to homogeneously fasten them in position, inserting a sealant between the outer surface of the metallic tank and the formed laminated structure arranged thereabout, heating the complete structure in a closed groom at a temperature of aD- proximately 150 F. for a period of approximately five minutes, then removing and allowing the tank to stand for approximately l2 hours, thereby placing the sealant under compression and causing the shrinkage of the pre-treated layers.
5. In a tank construction an inner metallic tank, a flexible outer tank arranged in space surrounding relation with respect to the inner tank,
a sealant under compression arranged between the tanks and endless resilient tubular elements arranged between the tanks to maintain the tanks in spaced relation and provided with-slots forming passageways through which the sealant may Dass.
6. In a tank construction, an inner metallic tank, a flexible outer tank surrounding the inner tank, spaced hollow resilient means arranged between the tanks and about and between the end edges of the inner tank and the adjacent parts of the flexible tank for maintaining the tanks in suitably spaced relation and including endless tubular members constructed of resilient material and provided at their outer portions with a series of suitably spaced slots and a sealant under compression arranged between the inner and outer tank walls and movable in and between the resilient spacing means.
7. In a tank construction, an inner metallic tank including side walls and end walls in interlocking engagement therewith, a, flexible outer tank surrounding the inner tank, spacing means arranged between the inner and outer side walls of the tanks and about and between the interlocking edges of the inner tank and the adjacent parts of the flexible tank for maintaining the respective walls in suitably spaced relation, said spacing means including a plurality of slotted tubular yieldable elements, the slotted portions of which engage the interlocked ends of the inner tank while the tubular elements are arranged in suitably spaced relation about the interlocked terial, and sheeted rubber-like material respec- 59.01118' meins.
REFERENCES CITED The following references are of record 1n the me of this patent:
UNITED STATES PATENTS Nmber Name nm 582,285 num et aL my u, 1m
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'portionethe-innertmkandnseelmt under Nhmber compression snmedbetween theinnerand-outertnnkwlllsnndmovableinmdbehenthe HANS` P. WAGNIR Number
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US500420A US2461096A (en) | 1943-08-28 | 1943-08-28 | Self-sealing gasoline tank |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US500420A US2461096A (en) | 1943-08-28 | 1943-08-28 | Self-sealing gasoline tank |
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US2461096A true US2461096A (en) | 1949-02-08 |
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Application Number | Title | Priority Date | Filing Date |
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US500420A Expired - Lifetime US2461096A (en) | 1943-08-28 | 1943-08-28 | Self-sealing gasoline tank |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3632012A (en) * | 1970-01-20 | 1972-01-04 | Philips Corp | Refrigerator cabinets |
US3632011A (en) * | 1970-01-20 | 1972-01-04 | Philips Corp | Refrigerator cabinets |
US4393980A (en) * | 1980-06-17 | 1983-07-19 | The Minister Of Transport In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Liquid container arranged to limit undesirable drainage |
US4609004A (en) * | 1984-07-30 | 1986-09-02 | Greene Archibald L | Aircraft safety fuel tank |
US5398839A (en) * | 1992-10-06 | 1995-03-21 | Kleyn Die Engravers, Inc. | Compartmented fuel tank with fuel absorbent material |
US6293419B1 (en) * | 2000-10-06 | 2001-09-25 | Delphi Technologies, Inc. | Fuel tank cover assembly for fuel tank |
US20140283920A1 (en) * | 2013-03-22 | 2014-09-25 | Airbus Helicopters | Tank provided with an over-pressure valve |
US20190061947A1 (en) * | 2017-08-29 | 2019-02-28 | Goodrich Corporation | Conformable tank with sandwich structure walls |
US10816138B2 (en) | 2017-09-15 | 2020-10-27 | Goodrich Corporation | Manufacture of a conformable pressure vessel |
US11091266B2 (en) | 2017-08-29 | 2021-08-17 | Goodrich Corporation | Conformable tank fabricated using additive manufacturing |
US11939105B2 (en) | 2017-08-29 | 2024-03-26 | Goodrich Corporation | 3D woven conformable tank |
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US1422670A (en) * | 1918-12-26 | 1922-07-11 | Gayner Pneumatic Company Ltd | Receptacle, flexible conduit, gas mask, and the like |
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US582285A (en) * | 1897-05-11 | And frank c | ||
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Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3632012A (en) * | 1970-01-20 | 1972-01-04 | Philips Corp | Refrigerator cabinets |
US3632011A (en) * | 1970-01-20 | 1972-01-04 | Philips Corp | Refrigerator cabinets |
US4393980A (en) * | 1980-06-17 | 1983-07-19 | The Minister Of Transport In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Liquid container arranged to limit undesirable drainage |
US4609004A (en) * | 1984-07-30 | 1986-09-02 | Greene Archibald L | Aircraft safety fuel tank |
US5398839A (en) * | 1992-10-06 | 1995-03-21 | Kleyn Die Engravers, Inc. | Compartmented fuel tank with fuel absorbent material |
US6293419B1 (en) * | 2000-10-06 | 2001-09-25 | Delphi Technologies, Inc. | Fuel tank cover assembly for fuel tank |
US20140283920A1 (en) * | 2013-03-22 | 2014-09-25 | Airbus Helicopters | Tank provided with an over-pressure valve |
US9399395B2 (en) * | 2013-03-22 | 2016-07-26 | Airbus Helicopters | Tank provided with an over-pressure valve |
US20190061947A1 (en) * | 2017-08-29 | 2019-02-28 | Goodrich Corporation | Conformable tank with sandwich structure walls |
US10703481B2 (en) * | 2017-08-29 | 2020-07-07 | Goodrich Corporation | Conformable tank with sandwich structure walls |
US11091266B2 (en) | 2017-08-29 | 2021-08-17 | Goodrich Corporation | Conformable tank fabricated using additive manufacturing |
US11939105B2 (en) | 2017-08-29 | 2024-03-26 | Goodrich Corporation | 3D woven conformable tank |
US10816138B2 (en) | 2017-09-15 | 2020-10-27 | Goodrich Corporation | Manufacture of a conformable pressure vessel |
US11725779B2 (en) | 2017-09-15 | 2023-08-15 | Goodrich Corporation | Manufacture of a conformable pressure vessel |
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