US20060096651A1 - Liquid tank puncture repair kit and method - Google Patents
Liquid tank puncture repair kit and method Download PDFInfo
- Publication number
- US20060096651A1 US20060096651A1 US11/067,565 US6756505A US2006096651A1 US 20060096651 A1 US20060096651 A1 US 20060096651A1 US 6756505 A US6756505 A US 6756505A US 2006096651 A1 US2006096651 A1 US 2006096651A1
- Authority
- US
- United States
- Prior art keywords
- container
- wound
- liquid
- cavity
- outside
- 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.)
- Granted
Links
- 239000007788 liquid Substances 0.000 title claims abstract description 41
- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000008439 repair process Effects 0.000 title description 3
- 206010052428 Wound Diseases 0.000 claims abstract description 57
- 208000027418 Wounds and injury Diseases 0.000 claims abstract description 38
- 238000007789 sealing Methods 0.000 claims abstract description 37
- 238000006243 chemical reaction Methods 0.000 claims abstract description 22
- 239000000126 substance Substances 0.000 claims abstract description 22
- 239000000701 coagulant Substances 0.000 claims abstract description 15
- 239000008188 pellet Substances 0.000 claims abstract description 12
- 239000000463 material Substances 0.000 claims description 24
- 230000002401 inhibitory effect Effects 0.000 claims description 6
- 238000004873 anchoring Methods 0.000 claims description 4
- 238000010079 rubber tapping Methods 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims description 2
- 238000003825 pressing Methods 0.000 claims 1
- 230000008961 swelling Effects 0.000 abstract description 4
- 239000011248 coating agent Substances 0.000 description 34
- 238000000576 coating method Methods 0.000 description 34
- 239000000446 fuel Substances 0.000 description 18
- 239000002828 fuel tank Substances 0.000 description 9
- 239000010410 layer Substances 0.000 description 9
- 239000011324 bead Substances 0.000 description 6
- 229920001971 elastomer Polymers 0.000 description 5
- 239000004215 Carbon black (E152) Substances 0.000 description 4
- 229930195733 hydrocarbon Natural products 0.000 description 4
- 150000002430 hydrocarbons Chemical class 0.000 description 4
- 230000001112 coagulating effect Effects 0.000 description 3
- 239000000806 elastomer Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000009970 fire resistant effect Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 238000006424 Flood reaction Methods 0.000 description 1
- 244000273618 Sphenoclea zeylanica Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 150000002825 nitriles Chemical class 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920001084 poly(chloroprene) Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000003566 sealing material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/16—Devices for covering leaks in pipes or hoses, e.g. hose-menders
- F16L55/168—Devices for covering leaks in pipes or hoses, e.g. hose-menders from outside the pipe
- F16L55/17—Devices for covering leaks in pipes or hoses, e.g. hose-menders from outside the pipe by means of rings, bands or sleeves pressed against the outside surface of the pipe or hose
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/16—Devices for covering leaks in pipes or hoses, e.g. hose-menders
- F16L55/168—Devices for covering leaks in pipes or hoses, e.g. hose-menders from outside the pipe
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/20—Patched hole or depression
Definitions
- This invention pertains to structure (a kit) and related methodology for patching a leak of liquid from a puncture wound in the wall of a liquid container.
- Two, different preferred embodiments of, and manners of practicing, the invention are described and illustrated herein in the setting of making an emergency, from-the-outside, repair of a ballistic (such as from a bullet) puncture wound in the container wall of a military vehicle fuel tank—a setting wherein the invention has been proven to offer significant defensive advantage in a combat zone.
- the two, herein-disclosed embodiments of the invention differ in component count, and in specific leak-sealing methodology.
- this just-above-mentioned component substance whether or not effective to create a coagulant mass, nevertheless preferably imbibes leakage liquid, swells in size, and, with the structure of the invention positioned adjacent a container puncture wound for use, is confined and stabilized in such a manner that, in its swelling and ultimately swollen conditions, it applies progressively increasing, and ultimately robust, sealing pressure to close the wound.
- a patch body has a perimeter portion which directly engages the effective outside surface of a container to seal thereagainst in the implementation of puncture-wound sealing.
- a unique, washer-like, resilient sealing gasket is employed intermediate the just-mentioned perimeter portion of the patch body and a container's outside surface. This gasket finctions to implement a somewhat different wound-sealing methodology.
- a unique hollow-stem, self-torque-limiting bolt is preferably utilized to make an attachment to the outside of a container of the type possessing a self-healing puncture-defeating coating which is there applied to the container.
- Another feature of the invention comes into play in a circumstance, described herein, where the container whose puncture wound is to be sealed is itself externally coated with an intended self-sealing coating which is formed with a liquid-reaction material (“substance”) which is compatible with that employed in the patch-kit structure and practice of the present invention.
- the sealing response behavior of the invention uniquely collaborates with the self-sealing capabilities of such a coating.
- FIG. 1 is a simplified, small-scale side view of a military vehicle which possesses an exposed, side-mounted fuel tank (liquid container). This illustrated tank is one which is coated with an intended self-sealing coating of the type mentioned above.
- FIG. 2 is an enlarged, fragmentary view of a portion of the fuel tank shown in FIG. 1 , wherein a penetrating bullet wound (puncture) has just occurred. Around this puncture, a small portion of a special, nominally self-sealing, tank coating has been broken away to provide a clearer view of the mentioned wound, and of the direct outside surface of the fuel tank.
- FIG. 3 is a further enlarged, fragmentary cross-sectional view of the mentioned fuel tank and its outer coating taken generally along the line 3 - 3 in FIG. 2 .
- FIG. 4 presents a view similar to that provided in FIG. 2 showing the mentioned puncture wound, and picturing (in dashed lines) the intended footprint of a wound patch sealing structure which will be employed in accordance with the present invention to seal the illustrated wound.
- FIG. 5 is a somewhat enlarged and exploded view which isolates and shows each of the several components of one embodiment of the patch sealing kit structure of the invention.
- FIG. 6 is a still further enlarged, isolated, isometric and fragmentary view showing the same embodiment of the patch sealing structure proposed by the present invention which is illustrated in FIG. 5 .
- all components in this kit embodiment are also shown, including a patch body with a perimetered cavity, an embedded washer in this body, what is referred to herein as a patch pellet which includes a special substance described in this document as being a liquid reaction substance, and a specially designed, hollow-shank, threaded patch-body anchoring bolt.
- FIG. 7 which is presented on about the same scale employed in FIG. 6 , shows a cross-sectional, isometric view of the patch kit of this invention, as illustrated in FIG. 6 , in an operative condition sealing a puncture (bullet) wound in a fuel tank.
- FIG. 8 is a transverse, cross-sectional view illustrating essentially the same information contained isometrically in FIG. 7 , and additionally illustrating what is referred to herein as a coagulant mass which develops during preferred practice of the invention to aid in the important wound-sealing behavior of the invention.
- FIG. 9 presents an enlarged detail, drawn from near the center of FIG. 8 , illustrating how a specially designed, hollow-shank bolt in the kit of this invention accommodates self-torque-limiting securement of other components in the invention to a punctured liquid container whose outside surface is coated, per se, with a certain kind of penetration-sealing material which is physically compatible (i.e., somewhat like) material employed in the structure of the invention.
- FIG. 10 is like FIG. 5 , except that it illustrates the above-mentioned, gasket-employing embodiment of the invention.
- FIG. 11 is a bottom isometric view of the embodiment of FIG. 10 , shown with all components assembled and ready for use.
- FIG. 12 is a larger-scale, top isometric view which is directly related to what is shown in FIG. 11 .
- FIG. 13 is a larger scale view, similar to that presented in FIG. 11 , but with the structure of FIG. 11 sliced open to reveal details of internal construction.
- FIG. 1 shown at 10 in FIG. 1 is a military vehicle which possesses an exposed, side-mounted hydrocarbon fuel tank 12 , also referred to herein as a liquid container.
- Fuel in this tank is typically under a residual, above-atmospheric pressure attributable principally to the vapor pressure of the contained fuel per se.
- This residual pressure might typically be as high as about 4- to about 5-psi above atmosphere pressure.
- Such a condition exacerbates fuel leakage if the tank is punctured, as by a bullet.
- container as employed herein is not confined to meaning only a vehicle's fuel tank. It may also apply, as examples, to a conduit, to a fuel-supply tanker, to holding tanks, to rail tanker cars, and to other kinds of liquid containers.
- tank 12 While it is not necessary that tank 12 be coated with a self-sealing protective jacket, or skin, 14 , tank 12 herein is so coated, and the illustrated and described preferred embodiment of the invention will be seen to have special “collaborative” utility in the presence of such a coating.
- FIG. 3 illustrates coating 14 in cross section.
- Layer 14 c (shown abutting layer 14 b at the location of a dash-dot line in FIG. 3 ) has a thickness herein of about 1 ⁇ 4- to about 3 ⁇ 8-inches, and is formed of the same elastomer material which is employed in layer 14 a .
- the outer side of layer 14 c defines the outside surface of coating 14 .
- reaction substances refers to the fact that when hydrocarbon leakage fuel from tank 12 contacts these materials, a chemical/mechanical reaction takes place which causes material-imbibing of such fuel, and volume-swelling of the imbibing material. Additionally, and preferably though not necessarily, a congealing/coagulating reaction occurs with respect to the interaction which occurs between leakage fuel and the imbiber beads, which reaction produces a sticky coagulant mass that, as will be seen, significantly contributes to the puncture-sealing capability of the present invention.
- FIGS. 2 and 4 shown at 16 is a bullet wound puncture in the wall of container 12 .
- coating 14 nominally is deemed to be capable of sealing this wound on its own, the structure and methodology of the present invention come into play when this does not happen.
- Structure 18 includes a patch body 20 possessing the shape, generally, of a cylindrical hockey puck, formed of a suitable rubber material, and including, on one of its circular sides, a domed patch cavity 20 a which is perimetered by downwardly facing, annularly ribbed perimeter structure 20 b which is seen to include ribs 20 c .
- An annular steel washer 22 is embedded in body 20 as shown (except in the exploded illustration of FIG. 5 ).
- Body 20 has an outside diameter preferably of about 3-inches, with the diameter of the edge rim of cavity 20 a being about 21 ⁇ 2-inches.
- Washer 22 and body 20 are centrally apertured, as can be seen, to provide operative clearance for the elongate, threaded shank 24 a of a hex bolt 24 which has a hex head 24 b and a central long axis 24 c (see FIGS. 4 and 5 ).
- FIGS. 6-8 inclusive, the upper portion of the central aperture in body 20 is exposed for ultimate bearing contact (as will be explained) between embedded washer 22 and the underside of bolt head 24 b .
- the end of shank 24 a which is opposite the end joined to bolt head 24 b has an elongate, hollow, cylindrical interior region 24 c , the inner (upper) end of which is closed at 24 d .
- Bolt 24 functions herein as an attaching device, or mechanism, especially suited for use with a container like tank 12 which is coated with a modest thickness (about 5 ⁇ 8-inches) self-sealing coating, like coating 14 .
- bolt 24 is also referred to herein as a self-tapping, self-torque-limiting bolt.
- a patch pellet Shown at 26 recessed within cavity 20 a in FIGS. 6-8 , inclusive, is what is referred to herein as a patch pellet which is flat-annular in configuration, and formed with a suitable wicking-fabric material 26 a (see FIG. 5 ) shaped as an annular bag, or outer envelope, which holds a fill of the same reaction-substance beads mentioned earlier herein. A few of such beads are shown generally and schematically at 26 b in FIGS. 6-8 , inclusive.
- FIG. 6 structure 18 is shown assembled for use before attachment to a punctured container.
- FIGS. 7 and 8 structure 18 has been attached effectively to tank 12 (via screw securement to coating 14 ) to seal against fuel leakage from previously mentioned bullet puncture wound 16 which has not been healed by coating 14 .
- body 20 is placed to seat perimeter structure 20 b against the exposed outside surface of coating 14 , with the “footprint” of the body generally relating to puncture wound 16 as illustrated by a dashed-line circle 28 in FIG. 4 .
- wound 16 is effectively located within the perimeter rim of cavity 20 a , and bolt 24 is sufficiently laterally offset, preferably about 1 ⁇ 2-inches, from the puncture wound so that it is “aimed”, so-to-speak, at an unpunctured portion of coating 14 .
- Bolt 24 is then pressed against coating 14 , and thereafter screwed in a self-tapping manner to tightness, as follows.
- the unique hollow end of the shank in the bolt screws self-tappingly into coating 14 —cutting an annular and deepening, threaded path into the coating until the inner “end” 24 d of the hollow interior region 24 c of bolt shank 24 a engages and begins to bear against the upper surface of the portion of coating 14 which now extends into this hollow interior.
- bolt head 24 b is already bearing sufficiently downwardly on washer 22 to begin to drive and compress body perimeter structure 20 b against coating 14 in an annular region surrounding wound 16 .
- Bolt tightening continues until sufficient compression exists in the coating material portion which bears against the inner end 24 d of the bolt-shank hollow automatically to establish an appropriate “tightness torque”.
- shank interior 24 c is shown with an exaggerated length, with end 24 d shown spaced somewhat upwardly from the portion, 14 a , of coating 14 which extends upwardly into this interior.
- end 24 d shown spaced somewhat upwardly from the portion, 14 a , of coating 14 which extends upwardly into this interior.
- interior end 24 d with the components of the invention positioned substantially as shown in FIGS. 7 and 8 , would be bearing firmly and tightly downwardly on coating portion 14 a . This condition is clearly pictured if FIG. 9 .
- This special bolt design thus, through appropriate “interior” length selection which is well within the skill in the relevant art, automatically establishes a proper final torque tightness (self-torque-limiting).
- This bolt tightening action attaches and binds (anchors) structure 18 firmly to tank 12 through the connection thus established with coating 14 so as to drive body 20 into secured sealing tightness around the perimeter of cavity 20 a.
- a ribbon of a suitable urethane caulking material may be applied around the outside perimeter of body 20 where that perimeter meets with coating 14 .
- FIG. 8 illustrates, in dark cross-hatching at 29 , a resulting coagulant mass.
- FIGS. 10-13 inclusive, here there is illustrated an important alternative embodiment of the invention.
- Those specific components of this embodiment which are essentially the same as like components included in the first-described embodiment, are given, in these four drawings figures, the same respective reference numbers.
- slits 30 b provide central passageways for the controlled, central symmetrical introduction of leakage liquid into the region containing pellet 26 .
- a very effective, “axially symmetric” (relative to axis 24 c ) seal develops against the outside of a container, like fuel tank 12 .
- a certain amount of liquid-reaction imbibing and swelling also occurs in the material (mentioned above) which forms gasket 30 , and this behavior contributes additionally to the sealing capability of this embodiment of the invention.
- this invention both with respect to its structure and its methodology, may be implemented and practiced in various ways which do not necessarily involve dealing with leakage from a container which is jacketed with a coating like coating 14 . Where such a coating is, however, involved as described herein, the “reaction substance” portion of the coating clearly collaborates with the patching/sealing structure and practice of the invention. Also the invention may readily be adapted and employed to deal with leaking liquids which are other than hydrocarbon fuel liquid by selecting and employing “reaction substances” which are appropriate to the particular liquid involved. The invention may also be implemented in a manner wherein “liquid reaction” does indeed involve material-swelling, but not necessarily the formation of a coagulant mass. Thus, effective sealing may readily be achieved simply with the use, in pellet 26 , of a reaction substance which merely imbibes leakage liquid, and swells appreciably in size as a result.
- the structure of this invention is quite clearly very simple in construction, is easily carried for emergency use when required, and is very easily installed quickly for rapid, effective leak stoppage.
- a method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container including the steps of (a) placing adjacent the outside of that wound a body of material including a reaction substance which reacts to contact with leakage liquid to form, with that liquid, a flow-inhibiting coagulant, and (b) effectively anchoring that material body to the outside of the container adjacent the wound.
- a method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container including the steps of (a) utilizing liquid leaking from the wound as a participating agent, forming a leakage-inhibiting coagulant immediately outside the wound, and (b) stabilizing the disposition of that coagulant adjacent the wound in a manner aimed at stopping liquid leakage through the wound.
- a method for sealing a perimetered puncture wound in a fuel tank from the outside of the tank including the steps of (a) creating against the outside of the tank a generally closed chamber encompassing the wound perimeter, (b) within that chamber, coagulating fuel leaking into the chamber, and (c) by that coagulating, sealing the wound against subsequent fuel leakage.
- a method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container including the steps of (a) placing adjacent the outside of that wound a body of material including a reaction substance which reacts to contact with leakage liquid to imbibe fuel and swell in size, and (b) effectively anchoring that material body to the outside of the container adjacent, and to apply sealing pressure to, the wound.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Details Of Rigid Or Semi-Rigid Containers (AREA)
- Gasket Seals (AREA)
Abstract
Description
- This application claims priority to currently pending U.S. Provisional Patent Application Ser. No. 60/627,628, filed Nov. 11, 2004, for “Fluid Tank Puncture Repair Kit and Method”. The entirety of the disclosure in that prior-filed application is hereby incorporated herein by reference.
- This invention pertains to structure (a kit) and related methodology for patching a leak of liquid from a puncture wound in the wall of a liquid container. Two, different preferred embodiments of, and manners of practicing, the invention are described and illustrated herein in the setting of making an emergency, from-the-outside, repair of a ballistic (such as from a bullet) puncture wound in the container wall of a military vehicle fuel tank—a setting wherein the invention has been proven to offer significant defensive advantage in a combat zone. As will be seen, the two, herein-disclosed embodiments of the invention differ in component count, and in specific leak-sealing methodology.
- While, as will become apparent, the invention has significant utility in other settings, it is illustrated and described herein in a military vehicle setting which serves to highlight the key features of the invention.
- A special characteristic of the invention in its preferred form is that it includes a wound-patching component which possesses a “substance” that reacts to leaking liquid, such as hydrocarbon fuel, to create a collaboration with such liquid thereby to produce a fluid-and-“substance” triggered coagulant that swells to seal a container puncture wound.
- Somewhat more broadly viewed, this just-above-mentioned component substance, whether or not effective to create a coagulant mass, nevertheless preferably imbibes leakage liquid, swells in size, and, with the structure of the invention positioned adjacent a container puncture wound for use, is confined and stabilized in such a manner that, in its swelling and ultimately swollen conditions, it applies progressively increasing, and ultimately robust, sealing pressure to close the wound.
- In one embodiment of the invention, what is referred to herein as a patch body has a perimeter portion which directly engages the effective outside surface of a container to seal thereagainst in the implementation of puncture-wound sealing. In another disclosed and illustrated embodiment of the invention, a unique, washer-like, resilient sealing gasket is employed intermediate the just-mentioned perimeter portion of the patch body and a container's outside surface. This gasket finctions to implement a somewhat different wound-sealing methodology. In both embodiments of the invention as illustrated herein, a unique hollow-stem, self-torque-limiting bolt is preferably utilized to make an attachment to the outside of a container of the type possessing a self-healing puncture-defeating coating which is there applied to the container.
- Another feature of the invention comes into play in a circumstance, described herein, where the container whose puncture wound is to be sealed is itself externally coated with an intended self-sealing coating which is formed with a liquid-reaction material (“substance”) which is compatible with that employed in the patch-kit structure and practice of the present invention. In this kind of setting, the sealing response behavior of the invention uniquely collaborates with the self-sealing capabilities of such a coating.
- All of the features and advantages of the invention will become more fully apparent as the description which now follows is read in conjunction with the accompanying drawings.
-
FIG. 1 is a simplified, small-scale side view of a military vehicle which possesses an exposed, side-mounted fuel tank (liquid container). This illustrated tank is one which is coated with an intended self-sealing coating of the type mentioned above. -
FIG. 2 is an enlarged, fragmentary view of a portion of the fuel tank shown inFIG. 1 , wherein a penetrating bullet wound (puncture) has just occurred. Around this puncture, a small portion of a special, nominally self-sealing, tank coating has been broken away to provide a clearer view of the mentioned wound, and of the direct outside surface of the fuel tank. -
FIG. 3 is a further enlarged, fragmentary cross-sectional view of the mentioned fuel tank and its outer coating taken generally along the line 3-3 inFIG. 2 . -
FIG. 4 presents a view similar to that provided inFIG. 2 showing the mentioned puncture wound, and picturing (in dashed lines) the intended footprint of a wound patch sealing structure which will be employed in accordance with the present invention to seal the illustrated wound. -
FIG. 5 is a somewhat enlarged and exploded view which isolates and shows each of the several components of one embodiment of the patch sealing kit structure of the invention. -
FIG. 6 is a still further enlarged, isolated, isometric and fragmentary view showing the same embodiment of the patch sealing structure proposed by the present invention which is illustrated inFIG. 5 . In this figure, all components in this kit embodiment are also shown, including a patch body with a perimetered cavity, an embedded washer in this body, what is referred to herein as a patch pellet which includes a special substance described in this document as being a liquid reaction substance, and a specially designed, hollow-shank, threaded patch-body anchoring bolt. -
FIG. 7 , which is presented on about the same scale employed inFIG. 6 , shows a cross-sectional, isometric view of the patch kit of this invention, as illustrated inFIG. 6 , in an operative condition sealing a puncture (bullet) wound in a fuel tank. -
FIG. 8 is a transverse, cross-sectional view illustrating essentially the same information contained isometrically inFIG. 7 , and additionally illustrating what is referred to herein as a coagulant mass which develops during preferred practice of the invention to aid in the important wound-sealing behavior of the invention. -
FIG. 9 presents an enlarged detail, drawn from near the center ofFIG. 8 , illustrating how a specially designed, hollow-shank bolt in the kit of this invention accommodates self-torque-limiting securement of other components in the invention to a punctured liquid container whose outside surface is coated, per se, with a certain kind of penetration-sealing material which is physically compatible (i.e., somewhat like) material employed in the structure of the invention. -
FIG. 10 is likeFIG. 5 , except that it illustrates the above-mentioned, gasket-employing embodiment of the invention. -
FIG. 11 is a bottom isometric view of the embodiment ofFIG. 10 , shown with all components assembled and ready for use. -
FIG. 12 is a larger-scale, top isometric view which is directly related to what is shown inFIG. 11 . -
FIG. 13 is a larger scale view, similar to that presented inFIG. 11 , but with the structure ofFIG. 11 sliced open to reveal details of internal construction. - Turning now to the drawings, and referring first to
FIGS. 1-4 , inclusive, shown at 10 inFIG. 1 is a military vehicle which possesses an exposed, side-mountedhydrocarbon fuel tank 12, also referred to herein as a liquid container. Fuel in this tank is typically under a residual, above-atmospheric pressure attributable principally to the vapor pressure of the contained fuel per se. This residual pressure might typically be as high as about 4- to about 5-psi above atmosphere pressure. Such a condition, of course, exacerbates fuel leakage if the tank is punctured, as by a bullet. - It should be understood that the word “container” as employed herein is not confined to meaning only a vehicle's fuel tank. It may also apply, as examples, to a conduit, to a fuel-supply tanker, to holding tanks, to rail tanker cars, and to other kinds of liquid containers.
- While it is not necessary that
tank 12 be coated with a self-sealing protective jacket, or skin, 14,tank 12 herein is so coated, and the illustrated and described preferred embodiment of the invention will be seen to have special “collaborative” utility in the presence of such a coating.FIG. 3 illustratescoating 14 in cross section. - Coating 14 herein includes, effectively, a stack of three
layers 14 a 14b 14 c.Layer 14 a lies directly against theoutside surface 12 a oftank 12, has a thickness herein of about ⅛-inches, and is formed of an elastomer, such as the product sold under the trademark TUFF STUFF® (FR (fire resistant) made by Rhino Linings USA, Inc. in San Diego, Calif.Layer 14 b (shown abuttinglayer 14 a at the location of a dashed line inFIG. 3 ) has a thickness herein of about ⅛- to about 3/16-inches, and is formed of a composite of the same elastomer material just mentioned forlayer 14 a, and entrained (about 20% by weight) fuel imbiber beads (not specifically shown inFIGS. 1-4 , inclusive) such as those bearing the product identifier IMB230300 made by Imbibitive Technologies America, Inc. in Midland, Mich.Layer 14 c (shown abuttinglayer 14 b at the location of a dash-dot line inFIG. 3 ) has a thickness herein of about ¼- to about ⅜-inches, and is formed of the same elastomer material which is employed inlayer 14 a. The outer side oflayer 14 c defines the outside surface ofcoating 14. - Both of the fundamental materials which are employed in coating 14 herein are referred to as being liquid reaction substances. The term “reaction substances” refers to the fact that when hydrocarbon leakage fuel from
tank 12 contacts these materials, a chemical/mechanical reaction takes place which causes material-imbibing of such fuel, and volume-swelling of the imbibing material. Additionally, and preferably though not necessarily, a congealing/coagulating reaction occurs with respect to the interaction which occurs between leakage fuel and the imbiber beads, which reaction produces a sticky coagulant mass that, as will be seen, significantly contributes to the puncture-sealing capability of the present invention. - In
FIGS. 2 and 4 , shown at 16 is a bullet wound puncture in the wall ofcontainer 12. And, while coating 14 nominally is deemed to be capable of sealing this wound on its own, the structure and methodology of the present invention come into play when this does not happen. - Adding attention now to
FIGS. 5-9 . inclusive, in the drawings, one embodiment of the patch kit structure of the present invention is shown generally at 18.Structure 18 includes apatch body 20 possessing the shape, generally, of a cylindrical hockey puck, formed of a suitable rubber material, and including, on one of its circular sides, adomed patch cavity 20 a which is perimetered by downwardly facing, annularly ribbedperimeter structure 20 b which is seen to includeribs 20 c. Anannular steel washer 22 is embedded inbody 20 as shown (except in the exploded illustration ofFIG. 5 ).Body 20 has an outside diameter preferably of about 3-inches, with the diameter of the edge rim ofcavity 20 a being about 2½-inches. -
Washer 22 andbody 20 are centrally apertured, as can be seen, to provide operative clearance for the elongate, threadedshank 24 a of ahex bolt 24 which has ahex head 24 b and a centrallong axis 24 c (seeFIGS. 4 and 5 ). As can be seen inFIGS. 6-8 , inclusive, the upper portion of the central aperture inbody 20 is exposed for ultimate bearing contact (as will be explained) between embeddedwasher 22 and the underside ofbolt head 24 b. The end ofshank 24 a which is opposite the end joined tobolt head 24 b has an elongate, hollow, cylindricalinterior region 24 c, the inner (upper) end of which is closed at 24 d.Bolt 24 functions herein as an attaching device, or mechanism, especially suited for use with a container liketank 12 which is coated with a modest thickness (about ⅝-inches) self-sealing coating, like coating 14. As will be further explained shortly,bolt 24 is also referred to herein as a self-tapping, self-torque-limiting bolt. - Shown at 26 recessed within
cavity 20 a inFIGS. 6-8 , inclusive, is what is referred to herein as a patch pellet which is flat-annular in configuration, and formed with a suitable wicking-fabric material 26 a (seeFIG. 5 ) shaped as an annular bag, or outer envelope, which holds a fill of the same reaction-substance beads mentioned earlier herein. A few of such beads are shown generally and schematically at 26 b inFIGS. 6-8 , inclusive. - In
FIG. 6 ,structure 18 is shown assembled for use before attachment to a punctured container. InFIGS. 7 and 8 ,structure 18 has been attached effectively to tank 12 (via screw securement to coating 14) to seal against fuel leakage from previously mentioned bullet puncture wound 16 which has not been healed by coating 14. - To seal against fuel leakage from
wound 16, withstructure 18 pre-assembled as shown inFIG. 6 ,body 20 is placed toseat perimeter structure 20 b against the exposed outside surface ofcoating 14, with the “footprint” of the body generally relating to puncture wound 16 as illustrated by a dashed-line circle 28 inFIG. 4 . With this disposition established, wound 16 is effectively located within the perimeter rim ofcavity 20 a, andbolt 24 is sufficiently laterally offset, preferably about ½-inches, from the puncture wound so that it is “aimed”, so-to-speak, at an unpunctured portion ofcoating 14. -
Bolt 24 is then pressed againstcoating 14, and thereafter screwed in a self-tapping manner to tightness, as follows. The unique hollow end of the shank in the bolt screws self-tappingly intocoating 14—cutting an annular and deepening, threaded path into the coating until the inner “end” 24 d of the hollowinterior region 24 c ofbolt shank 24 a engages and begins to bear against the upper surface of the portion ofcoating 14 which now extends into this hollow interior. By the time that this bearing contact has been established,bolt head 24 b is already bearing sufficiently downwardly onwasher 22 to begin to drive and compressbody perimeter structure 20 b againstcoating 14 in an annularregion surrounding wound 16. Bolt tightening continues until sufficient compression exists in the coating material portion which bears against theinner end 24 d of the bolt-shank hollow automatically to establish an appropriate “tightness torque”. - In
FIGS. 7 and 8 ,shank interior 24 c is shown with an exaggerated length, withend 24 d shown spaced somewhat upwardly from the portion, 14 a, of coating 14 which extends upwardly into this interior. This has been done in these two figures simply to provide a clearer illustration here of the inside ofshank 24 a. In reality,interior end 24 d, with the components of the invention positioned substantially as shown inFIGS. 7 and 8 , would be bearing firmly and tightly downwardly oncoating portion 14 a. This condition is clearly pictured ifFIG. 9 . This special bolt design thus, through appropriate “interior” length selection which is well within the skill in the relevant art, automatically establishes a proper final torque tightness (self-torque-limiting). - This bolt tightening action attaches and binds (anchors)
structure 18 firmly totank 12 through the connection thus established withcoating 14 so as to drivebody 20 into secured sealing tightness around the perimeter ofcavity 20 a. - Later on, if it is desired to add an extra measure of sealing “security” regarding this embodiment of the invention, a ribbon of a suitable urethane caulking material (not illustrated) may be applied around the outside perimeter of
body 20 where that perimeter meets withcoating 14. - Leaking
fuel floods cavity 20 a wherein it becomes trapped, and is quickly wicked intopellet 26 to contactbeads 26 b therein.Pellet 26 is trapped and positionally stabilized in the chamber defined betweencavity 20 a and the confronting outside surface ofcoating layer 14 c. The beads and fuel promptly react with one another to form, collaboratively, a swelling coagulant which, as it swells, becomes compressed within the small volume of stabilized space which is defined betweencavity 20 a and the confronting surface ofcoating 14. The result of this activity is an immediate, full, and secure compressive seal against fuel leakage fromtank 12 throughwound 16.FIG. 8 illustrates, in dark cross-hatching at 29, a resulting coagulant mass. - An additional matter to note is that, aiding in the leakage-sealing process which is implemented by the behavior of the present invention, is enhanced compression in the zone of the puncture wound, introduced by reactive pressure which develops between
coating 14 andexternal structure body 20 due to tightening ofbolt 24, and associated tensing inshank 24 a. This tensing condition is referred to herein as a “tension reaction force”. - Turning attention now to
FIGS. 10-13 , inclusive, here there is illustrated an important alternative embodiment of the invention. Those specific components of this embodiment which are essentially the same as like components included in the first-described embodiment, are given, in these four drawings figures, the same respective reference numbers. - This alternative embodiment of the invention includes one additional component in the form of a uniquely configured, annular,
resilient gasket 30.Gasket 30 herein has an outside diameter which is slightly greater than that ofpatch body 20, a thickness of about ⅛-inches, and is formed of a PVC/Nitrile/Neoprene polymer sold under the trademark Duraform™. Specifically, this material is referred to by its manufacturer, Monmouth Rubber & Plastics Corp. of Long Branch, N.J., with an inventory number IVN41. - As can be seen especially well in
FIGS. 11 and 13 ,gasket 30 possesses acentral throughbore 30 a which accommodates the shank ofbolt 24.Gasket 30 is unique in its design, in that plural (four herein), generally T-shaped through-slits 30 b are formed at orthogonally related locations distributed circumferentially about throughbore 30 a, as can been seen best inFIGS. 10, 11 and 13. Throughbore 30 a and through-slits 30 b are referred to collectively herein as central passage structure. - Significantly, with the structure of
FIGS. 10-13 , inclusive, installed for use, slits 30 b provide central passageways for the controlled, central symmetrical introduction of leakage liquid into theregion containing pellet 26. As the material located centrally inpellet 26 swells in response to contact with this liquid, a very effective, “axially symmetric” (relative toaxis 24 c) seal develops against the outside of a container, likefuel tank 12. A certain amount of liquid-reaction imbibing and swelling also occurs in the material (mentioned above) which formsgasket 30, and this behavior contributes additionally to the sealing capability of this embodiment of the invention. - It will be understood that this invention, both with respect to its structure and its methodology, may be implemented and practiced in various ways which do not necessarily involve dealing with leakage from a container which is jacketed with a coating like
coating 14. Where such a coating is, however, involved as described herein, the “reaction substance” portion of the coating clearly collaborates with the patching/sealing structure and practice of the invention. Also the invention may readily be adapted and employed to deal with leaking liquids which are other than hydrocarbon fuel liquid by selecting and employing “reaction substances” which are appropriate to the particular liquid involved. The invention may also be implemented in a manner wherein “liquid reaction” does indeed involve material-swelling, but not necessarily the formation of a coagulant mass. Thus, effective sealing may readily be achieved simply with the use, inpellet 26, of a reaction substance which merely imbibes leakage liquid, and swells appreciably in size as a result. - The structure of this invention is quite clearly very simple in construction, is easily carried for emergency use when required, and is very easily installed quickly for rapid, effective leak stoppage.
- From a methodologic perspective, the invention can be expressed in a number of different ways. A few of these ways are set forth immediately below in several, letter-identified paragraph statements, as follows:
- A. A method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container, including the steps of (a) placing adjacent the outside of that wound a body of material including a reaction substance which reacts to contact with leakage liquid to form, with that liquid, a flow-inhibiting coagulant, and (b) effectively anchoring that material body to the outside of the container adjacent the wound.
- B. A method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container, including the steps of (a) utilizing liquid leaking from the wound as a participating agent, forming a leakage-inhibiting coagulant immediately outside the wound, and (b) stabilizing the disposition of that coagulant adjacent the wound in a manner aimed at stopping liquid leakage through the wound.
- C. A method for sealing a perimetered puncture wound in a fuel tank from the outside of the tank, including the steps of (a) creating against the outside of the tank a generally closed chamber encompassing the wound perimeter, (b) within that chamber, coagulating fuel leaking into the chamber, and (c) by that coagulating, sealing the wound against subsequent fuel leakage.
- D. A method for sealing, from the outside, a leaking puncture wound in the wall of a liquid-holding container, including the steps of (a) placing adjacent the outside of that wound a body of material including a reaction substance which reacts to contact with leakage liquid to imbibe fuel and swell in size, and (b) effectively anchoring that material body to the outside of the container adjacent, and to apply sealing pressure to, the wound.
- Accordingly, while a preferred embodiment of, and manner of practicing, the invention, with certain variations described, have been expressed and illustrated herein, it is appreciated that other variations and modifications may be made without departing from the spirit of the invention.
Claims (8)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/067,565 US7044166B1 (en) | 2004-11-11 | 2005-02-25 | Liquid tank puncture repair kit and method |
CA2697572A CA2697572A1 (en) | 2004-11-11 | 2005-05-18 | Liquid tank puncture repair kit and method |
CA2584620A CA2584620C (en) | 2004-11-11 | 2005-05-18 | Liquid tank puncture repair kit and method |
PCT/US2005/017819 WO2006052287A1 (en) | 2004-11-11 | 2005-05-18 | Liquid tank puncture repair kit and method |
EP05750610A EP1800050A4 (en) | 2004-11-11 | 2005-05-18 | Liquid tank puncture repair kit and method |
US11/346,931 US7409969B2 (en) | 2004-11-11 | 2006-02-04 | Liquid tank puncture repair kit |
US12/148,213 US7624760B2 (en) | 2004-11-11 | 2008-04-16 | Liquid tank puncture-repair method |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US62762804P | 2004-11-11 | 2004-11-11 | |
US11/067,565 US7044166B1 (en) | 2004-11-11 | 2005-02-25 | Liquid tank puncture repair kit and method |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/346,931 Continuation US7409969B2 (en) | 2004-11-11 | 2006-02-04 | Liquid tank puncture repair kit |
Publications (2)
Publication Number | Publication Date |
---|---|
US20060096651A1 true US20060096651A1 (en) | 2006-05-11 |
US7044166B1 US7044166B1 (en) | 2006-05-16 |
Family
ID=36315095
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/067,565 Expired - Fee Related US7044166B1 (en) | 2004-11-11 | 2005-02-25 | Liquid tank puncture repair kit and method |
US11/346,931 Expired - Lifetime US7409969B2 (en) | 2004-11-11 | 2006-02-04 | Liquid tank puncture repair kit |
US12/148,213 Expired - Lifetime US7624760B2 (en) | 2004-11-11 | 2008-04-16 | Liquid tank puncture-repair method |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/346,931 Expired - Lifetime US7409969B2 (en) | 2004-11-11 | 2006-02-04 | Liquid tank puncture repair kit |
US12/148,213 Expired - Lifetime US7624760B2 (en) | 2004-11-11 | 2008-04-16 | Liquid tank puncture-repair method |
Country Status (4)
Country | Link |
---|---|
US (3) | US7044166B1 (en) |
EP (1) | EP1800050A4 (en) |
CA (2) | CA2697572A1 (en) |
WO (1) | WO2006052287A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010032127A3 (en) * | 2008-09-18 | 2010-07-29 | Marchesini, Franco | System for making watertight a fabric covering a cavity which, by way of microvalves consisting of fibres produced during the chemical reaction of a polymer that comes into contact with a fluid which expands and builds up within the cavity, creates a high barrier effect |
US20230047757A1 (en) * | 2021-08-11 | 2023-02-16 | Wally Jarrett | Repair patch for pipes |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7314164B2 (en) | 2004-07-01 | 2008-01-01 | American Express Travel Related Services Company, Inc. | System for biometric security using a smartcard |
US7169452B1 (en) * | 2004-10-20 | 2007-01-30 | Russell Allen Monk | Projectile barrier and method |
US7044166B1 (en) * | 2004-11-11 | 2006-05-16 | High Impact Technology Llc | Liquid tank puncture repair kit and method |
US20100307373A1 (en) * | 2009-06-03 | 2010-12-09 | Robert Joseph Kinsella | Containment Systems for Use With Railcars |
SG10201604290TA (en) * | 2011-05-27 | 2016-07-28 | Hutchinson Sa | Self-sealing liquid containment system and method of installing same |
US10124448B2 (en) * | 2011-12-31 | 2018-11-13 | Forge Tech, Inc. | Apparatus for repairing and improving structural integrity of storage tanks |
US9174313B2 (en) * | 2011-12-31 | 2015-11-03 | Forge Tech, Inc. | Method for repairing and improving structural integrity of storage tanks |
US8685513B1 (en) | 2012-02-29 | 2014-04-01 | Carolyn M. Dry | Inflatable articles comprising a self-repairing laminate |
US9694629B1 (en) | 2012-02-29 | 2017-07-04 | Carolyn Dry | Self-repairing inflatable articles incorporating an integrated self-repair system |
CN103170794A (en) * | 2013-03-21 | 2013-06-26 | 安徽淮河化工股份有限公司 | Method of mending damage on non-clamping sleeve portion of enamel reaction kettle |
US9625599B2 (en) | 2013-12-17 | 2017-04-18 | Schlumberger Technology Corporation | Downhole elastic anisotropy measurements |
US9933103B1 (en) * | 2016-09-28 | 2018-04-03 | Technofink Llc | Apparatus and method for sealing a leak from a tubular member |
KR102038297B1 (en) | 2018-01-29 | 2019-10-30 | 국방과학연구소 | Repair method of the integral composite fuel tank |
US10436373B2 (en) * | 2018-03-12 | 2019-10-08 | Frank Seth Gaunce | Copper plumbing pinhole prevention; pinhole repair and protection for long life of copper plumbing |
US12188513B2 (en) | 2022-04-29 | 2025-01-07 | Sustant, LLC | Fastener seals |
Citations (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1285210A (en) * | 1918-07-26 | 1918-11-19 | William Ross Jones | Quick-repair device for holes in metallic hollow ware. |
US3509016A (en) * | 1966-02-16 | 1970-04-28 | Goodyear Tire & Rubber | Self-sealing fuel cell wall |
US3698587A (en) * | 1970-06-18 | 1972-10-17 | Goodyear Aerospace Corp | Self sealing composite |
US3801425A (en) * | 1971-03-22 | 1974-04-02 | Goodyear Aerospace Corp | Self-sealing container |
US4025677A (en) * | 1975-12-08 | 1977-05-24 | Belke Manufacturing Company, Inc. | Temporary patch for a crack in the wall of a container |
US4115616A (en) * | 1978-02-09 | 1978-09-19 | The United States Of America As Represented By The Secretary Of The Air Force | Self-sealing fuel line assembly |
US4216803A (en) * | 1976-06-15 | 1980-08-12 | Martin Marietta Corporation | Self-sealing fuel lines |
US4345698A (en) * | 1980-03-25 | 1982-08-24 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft self-sealing fuel tank |
US4352851A (en) * | 1980-12-16 | 1982-10-05 | The United States Of America As Represented By The Secretary Of The Navy | Void filler foam fire suppression system |
US4422561A (en) * | 1981-05-18 | 1983-12-27 | Imi Marston Limited | Fuel tank component |
US4728711A (en) * | 1986-01-06 | 1988-03-01 | Mobay Corporation | Swellable coating compositions |
US4743468A (en) * | 1987-02-04 | 1988-05-10 | Renbec International Corp. | Method for repairing a rupture in a metal or plastic surface |
US4859491A (en) * | 1987-10-13 | 1989-08-22 | Mobil Oil Corporation | Process for repairing a cryogenic heat exchanger |
US5166007A (en) * | 1991-09-11 | 1992-11-24 | Smith W Novis | Repair compositions and structure |
US5301983A (en) * | 1992-03-23 | 1994-04-12 | Porowski Jan S | Pipe component seal assembly |
US6386236B1 (en) * | 2000-05-31 | 2002-05-14 | Air Logistics Corporation | Method of prestressing and reinforcing damaged cylindrical structures |
US6860297B2 (en) * | 2001-03-16 | 2005-03-01 | Paul Stephen Manzon | Local degraded area repair and restoration component for pressure retaining items |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3236407A (en) * | 1964-01-30 | 1966-02-22 | Gen Aniline & Film Corp | Repair patch assembly |
US3583593A (en) * | 1969-09-23 | 1971-06-08 | Us Army | Variable level coagulant reservoir for self-sealing fuel tanks |
US4088240A (en) * | 1976-09-13 | 1978-05-09 | The United States Of America As Represented By The Secretary Of The Navy | Fuel tank leakage fiber flow sealant |
US4529656A (en) * | 1983-04-22 | 1985-07-16 | The Dow Chemical Company | Oil imbibing polymer particles which are block resistant |
US7169452B1 (en) * | 2004-10-20 | 2007-01-30 | Russell Allen Monk | Projectile barrier and method |
US7044166B1 (en) * | 2004-11-11 | 2006-05-16 | High Impact Technology Llc | Liquid tank puncture repair kit and method |
-
2005
- 2005-02-25 US US11/067,565 patent/US7044166B1/en not_active Expired - Fee Related
- 2005-05-18 CA CA2697572A patent/CA2697572A1/en not_active Abandoned
- 2005-05-18 CA CA2584620A patent/CA2584620C/en not_active Expired - Fee Related
- 2005-05-18 WO PCT/US2005/017819 patent/WO2006052287A1/en active Application Filing
- 2005-05-18 EP EP05750610A patent/EP1800050A4/en not_active Withdrawn
-
2006
- 2006-02-04 US US11/346,931 patent/US7409969B2/en not_active Expired - Lifetime
-
2008
- 2008-04-16 US US12/148,213 patent/US7624760B2/en not_active Expired - Lifetime
Patent Citations (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1285210A (en) * | 1918-07-26 | 1918-11-19 | William Ross Jones | Quick-repair device for holes in metallic hollow ware. |
US3509016A (en) * | 1966-02-16 | 1970-04-28 | Goodyear Tire & Rubber | Self-sealing fuel cell wall |
US3698587A (en) * | 1970-06-18 | 1972-10-17 | Goodyear Aerospace Corp | Self sealing composite |
US3801425A (en) * | 1971-03-22 | 1974-04-02 | Goodyear Aerospace Corp | Self-sealing container |
US4025677A (en) * | 1975-12-08 | 1977-05-24 | Belke Manufacturing Company, Inc. | Temporary patch for a crack in the wall of a container |
US4216803A (en) * | 1976-06-15 | 1980-08-12 | Martin Marietta Corporation | Self-sealing fuel lines |
US4115616A (en) * | 1978-02-09 | 1978-09-19 | The United States Of America As Represented By The Secretary Of The Air Force | Self-sealing fuel line assembly |
US4345698A (en) * | 1980-03-25 | 1982-08-24 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft self-sealing fuel tank |
US4352851A (en) * | 1980-12-16 | 1982-10-05 | The United States Of America As Represented By The Secretary Of The Navy | Void filler foam fire suppression system |
US4422561A (en) * | 1981-05-18 | 1983-12-27 | Imi Marston Limited | Fuel tank component |
US4728711A (en) * | 1986-01-06 | 1988-03-01 | Mobay Corporation | Swellable coating compositions |
US4743468A (en) * | 1987-02-04 | 1988-05-10 | Renbec International Corp. | Method for repairing a rupture in a metal or plastic surface |
US4859491A (en) * | 1987-10-13 | 1989-08-22 | Mobil Oil Corporation | Process for repairing a cryogenic heat exchanger |
US5166007A (en) * | 1991-09-11 | 1992-11-24 | Smith W Novis | Repair compositions and structure |
US5301983A (en) * | 1992-03-23 | 1994-04-12 | Porowski Jan S | Pipe component seal assembly |
US6386236B1 (en) * | 2000-05-31 | 2002-05-14 | Air Logistics Corporation | Method of prestressing and reinforcing damaged cylindrical structures |
US6860297B2 (en) * | 2001-03-16 | 2005-03-01 | Paul Stephen Manzon | Local degraded area repair and restoration component for pressure retaining items |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010032127A3 (en) * | 2008-09-18 | 2010-07-29 | Marchesini, Franco | System for making watertight a fabric covering a cavity which, by way of microvalves consisting of fibres produced during the chemical reaction of a polymer that comes into contact with a fluid which expands and builds up within the cavity, creates a high barrier effect |
US20230047757A1 (en) * | 2021-08-11 | 2023-02-16 | Wally Jarrett | Repair patch for pipes |
US11953140B2 (en) * | 2021-08-11 | 2024-04-09 | Wally Jarrett | Repair patch for pipes |
Also Published As
Publication number | Publication date |
---|---|
US20080190546A1 (en) | 2008-08-14 |
CA2584620A1 (en) | 2006-05-18 |
CA2584620C (en) | 2010-11-16 |
US7409969B2 (en) | 2008-08-12 |
US20060272723A1 (en) | 2006-12-07 |
US7044166B1 (en) | 2006-05-16 |
CA2697572A1 (en) | 2006-05-18 |
US7624760B2 (en) | 2009-12-01 |
WO2006052287A1 (en) | 2006-05-18 |
EP1800050A4 (en) | 2011-03-30 |
EP1800050A1 (en) | 2007-06-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7409969B2 (en) | Liquid tank puncture repair kit | |
US7229673B1 (en) | Projectile barrier method for sealing liquid container | |
RU2466329C2 (en) | Protruding end element and combined high-pressure capacity | |
US9103499B2 (en) | Gas storage tank comprising a liquid sealant | |
CA2792155C (en) | Rock bolt sealing system | |
JP2000220752A (en) | Water-cut-off method using waterproof seal member | |
CA3004341A1 (en) | Method and apparatus for repairing a pipe junction | |
US8220130B2 (en) | Method for manufacturing an underground storage tank for flammable and combustible liquids | |
CA2486194A1 (en) | Apparatus and method for containing and regulating the pressure in a pressure vessel | |
US3496969A (en) | Valve for pressurizing a container | |
US11994258B2 (en) | Methods of preventing failure of corrugated tube in type IV pressure vessels | |
EP0690816A1 (en) | A storage vessel | |
US4626133A (en) | Waterstop for monolith joints | |
US10005253B1 (en) | Fuel containment autonomous self-sealing system | |
US20090026212A1 (en) | Underground storage tank for flammable liquids | |
US20120001393A1 (en) | Deformable composite plug | |
JPH11230461A (en) | Aseismatic saddle snap tap | |
CA2584694C (en) | Projectile barrier and method | |
JP2005233414A (en) | Hose coupling structure | |
US20240353061A1 (en) | Pressure vessel end fitting retention | |
CN220416361U (en) | Side leakage prevention sealing valve for semiconductor manufacturing | |
JPH09156627A (en) | Molding and manufacture thereof | |
JPH09156689A (en) | Container, and manufacturing method therefor | |
JPH0557472B2 (en) | ||
JPH0638238Y2 (en) | Fluid transport pipe |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: HIGH IMPACT TECHNOLOGY, LLC, OREGON Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MONK, RUSELL A.;OHNSTAD, THOMAS S.;REEL/FRAME:017700/0807 Effective date: 20051105 |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
AS | Assignment |
Owner name: HIGH IMPACT TECHNOLOGY, LLC, OREGON Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MONK, RUSSELL A.;OHNSTAD, THOMAS S.;REEL/FRAME:025346/0018 Effective date: 20051101 |
|
REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20140516 |