US2461096A - Self-sealing gasoline tank - Google Patents

Self-sealing gasoline tank Download PDF

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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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tank
walls
wall
sealing
sealant
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Hans P Wagner
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/06Constructional adaptations thereof
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S220/00Receptacles
    • Y10S220/90Rupture proof

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  • 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
imm
'portionethe-innertmkandnseelmt under Nhmber compression snmedbetween theinnerand-outertnnkwlllsnndmovableinmdbehenthe HANS` P. WAGNIR Number
US500420A 1943-08-28 1943-08-28 Self-sealing gasoline tank Expired - Lifetime US2461096A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
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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

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US582285A (en) * 1897-05-11 And frank c
GB150173A (en) * 1919-08-28 1920-09-02 John Innes Improvements in fuel tanks for aircraft
US1386791A (en) * 1918-01-16 1921-08-09 George J Murdock Self-puncture-sealing covering for fuel-containers
US1422670A (en) * 1918-12-26 1922-07-11 Gayner Pneumatic Company Ltd Receptacle, flexible conduit, gas mask, and the like
US1453305A (en) * 1919-07-09 1923-05-01 Cleghorn Charles Angus Self-sealing petrol tank or other container
US1510133A (en) * 1922-10-26 1924-09-30 Aviation Louis Breguet Sa Protecting device for fuel tanks
US2063228A (en) * 1933-07-07 1936-12-08 Eugene Charmat Apparatus for the delivery of liquids
FR852133A (en) * 1938-03-26 1940-01-24 Colombes Goodrich S A Improvements to the protective coatings of tanks containing flammable liquids, in particular fuel tanks for automobiles or aircraft
US2326263A (en) * 1941-04-26 1943-08-10 Us Rubber Co Tank fitting
US2336885A (en) * 1942-07-18 1943-12-14 Glenn L Martin Co Fitting construction for tanks

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US582285A (en) * 1897-05-11 And frank c
US1386791A (en) * 1918-01-16 1921-08-09 George J Murdock Self-puncture-sealing covering for fuel-containers
US1422670A (en) * 1918-12-26 1922-07-11 Gayner Pneumatic Company Ltd Receptacle, flexible conduit, gas mask, and the like
US1453305A (en) * 1919-07-09 1923-05-01 Cleghorn Charles Angus Self-sealing petrol tank or other container
GB150173A (en) * 1919-08-28 1920-09-02 John Innes Improvements in fuel tanks for aircraft
US1510133A (en) * 1922-10-26 1924-09-30 Aviation Louis Breguet Sa Protecting device for fuel tanks
US2063228A (en) * 1933-07-07 1936-12-08 Eugene Charmat Apparatus for the delivery of liquids
FR852133A (en) * 1938-03-26 1940-01-24 Colombes Goodrich S A Improvements to the protective coatings of tanks containing flammable liquids, in particular fuel tanks for automobiles or aircraft
US2326263A (en) * 1941-04-26 1943-08-10 Us Rubber Co Tank fitting
US2336885A (en) * 1942-07-18 1943-12-14 Glenn L Martin Co Fitting construction for tanks

Cited By (14)

* Cited by examiner, † Cited by third party
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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