US3661683A - Patch press - Google Patents

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US3661683A
US3661683A US86437A US3661683DA US3661683A US 3661683 A US3661683 A US 3661683A US 86437 A US86437 A US 86437A US 3661683D A US3661683D A US 3661683DA US 3661683 A US3661683 A US 3661683A
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Prior art keywords
patch
frame
diaphragm
press
cover member
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US86437A
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Harry C Engel
Edward J Ardolino
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AIRLINE SYSTEMS Inc
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AIRLINE SYSTEMS Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/24Apparatus or accessories not otherwise provided for
    • B29C73/30Apparatus or accessories not otherwise provided for for local pressing or local heating
    • B29C73/32Apparatus or accessories not otherwise provided for for local pressing or local heating using an elastic element, e.g. inflatable bag
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • B29C73/10Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using patches sealing on the surface of the article
    • B29C73/12Apparatus therefor, e.g. for applying
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B43/00Improving safety of vessels, e.g. damage control, not otherwise provided for
    • B63B43/02Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking
    • B63B43/10Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy
    • B63B43/16Temporary equipment for stopping leaks, e.g. collision mats
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40Maintaining or repairing aircraft

Definitions

  • ABSTRACT The present invention relates to a patch press, particularly but not exclusively adapted to use in repairing airplane surfaces by adhesively patching a double plate over the damaged area.
  • the patch press itself involves a longitudinally split rectangular frame that has clamped therein a cover member which may be heavy duty fabric such as canvas that extends across the framed area and beyond and which serves to carry a plurality of suction cups at the periphery thereof so that the press may be mounted on and adhered to the undamaged surface around the region to be patched with the patch inside the frame.
  • a cover member which may be heavy duty fabric such as canvas that extends across the framed area and beyond and which serves to carry a plurality of suction cups at the periphery thereof so that the press may be mounted on and adhered to the undamaged surface around the region to be patched with the patch inside the frame.
  • That portion of the cover member inside the framed area acts as an outside reinforcement for the inflatable diaphragm, so that the forces generated when inflatable diaphragm is inflated and beats against the patch are transmitted directly to the suction cups.
  • the patch press is a portable, essentially self-contained unit which can be employed to hold a patch onto an airplane surface and to maintain the patch there under pressure long enough for the adhesive bond to cure.
  • the present invention relates to an apparatus adapted for use in quick fix, bonded repair systems wherein a patch is adhesively bonded over a damaged region of some surface.
  • the apparatus is adapted for use in time-limited, field type, bonded repair of aluminum aircraft assemblies.
  • Modern day airplanes are now constructed with wing and other surface regions of structurally bonded honeycomb panels that can easily be dented, even ruptured locally as, for example, by a dropped wrench, a thrown rock, impact with a bird. Overall, the airplane remains operable and safe, yet, obviously, the damage must be repaired as soon as possible. Needed is a patch which will hold permanently, or, failing that, at least until a convenient time comes to make permanent repair of the damaged region.
  • a typical repair sequence involves cleaning up the damaged region and removing all dirt and finish from the sound area immediately around the damaged region.
  • the dented and broken damaged region is filled with an adhesive or other filler material so that the surface of the damaged area is flush with that of the sound metal around the damage.
  • a doubler or patch piece is then adhesively bonded to the damaged area with enough of an overlap onto sound metal to obtain an adhesive metal-to-metal bond adequate to hold the doubler in place.
  • the doubler may overlap the damaged area from about 1%. to 4 inches in all directions.
  • the present invention provides a portable, essentially selfcontained apparatus, i.e., a patch press, capable of applying compliant uniform pressure to the doubler plate being adhered over a damaged surface region, and maintaining such pressure until the adhesive has cured.
  • FIG. 1 is a top plan view of the patch press
  • FIG. 2 is a side view of the patch press
  • FIG. 3 is a section taken along line 3-3 ofFIG. 1;
  • FIG. 4 is an enlarged partial section taken along the line 4- 4 of FIG. 1;
  • FIG. 5 is an enlarged partial section taken along line 5-5 of FIG. 1;
  • FIG. 6 is an enlarged partial section taken along line 6-6 of FIG. 1;
  • FIG. 7 is an exploded section taken along line 7-7 of FIG.
  • FIG. 8 is a top plan view of a modified form of the invention.
  • FIG. 9 is a bottom plan view of the device in FIG. 8.
  • FIG. 10 is a side elevation of FIG. 8 with parts broken away.
  • the present patch press 10 is adapted to seat on a damaged panel 12 through means of a plurality of suction cup assemblies 14 disposed peripherally around the patch press 10.
  • the damaged region 15, shadow illustrated in FIG. 1, is centered under patch press 10.
  • FIG. 3 shows how patch press 10 is seated over a doubler patch 16 and uniformly applies pneumatic pressure thereto by a lower fluid tight elastic diaphragm 18 which form s'a portion of patch press 10.
  • FIG. 2 shows the diaphragm 18 in a flaccid non-inflated state.
  • Patch press 10 further comprises a square (or rectangular) longitudinally split metallic frame 20 normally fabricated of aluminum.
  • the upper frame member 22 and lower frame member 24 (FIGS. 4 and 5) are secured together by machine screws 26 or other conventional fastening elements (e.g., rivet, nut and bolt, etc.). Locked together between the split halves 22 and 24, are the several layers of sheet material which form part of the present patch press.
  • FIG. 7 is an exploded view illustrating frame members and the several sheet layers in FIG. 7.
  • the cover member is a heavy duty inelastic sheet 28, film or fabric, e.g., heavy canvas, which extends across the open area inside frame 20 and beyond frame 20, as is shown in FIG. 1.
  • the heavy duty sheet 28 serves to carry suction cup assemblies 14 at the peripheral edges thereof.
  • upper elastic diaphragm 30 which desirably may be a rubber sheet (synthetic, natural, or even an elastic resin).
  • adhesive layer 32 between diaphragm 30 and sheet 28, disposed either on the underside of sheet 28 or on the top side of diaphragm 30 to adhere the two layers together.
  • the lower elastic diaphragm 18 previously alluded to is the bottom layer.
  • lower frame member 24 Therebeneath is lower frame member 24. Normally, the same (rubber or rubber-like) material would be employed for both diaphragms.
  • a soft sealing ring 34 whose area is generally co-extensive with that of frame 20 and whose purpose is to provide an airtight seal between upper diaphragm 28 and lower diaphragm 18 so that the space therebetween can serve as a sealed off region into which pressurizing fluid may be added and removed as desired by way of air valve 36.
  • Such valves are standard articles of commerce, e.g., an ordinary tire valve will sufiice, and the details thereof need not be described further.
  • a pressure gauge 38 may be present.
  • the suction cup assemblies 14 disposed at the periphery of the heavy duty sheet 28 each'comprise (FIG. 6) a suction cup 40 which seats on panel 12 and a threaded shank 42 to which cup 40 is secured.
  • the shank 42 passes up through a grommet 44 which provides a suitable opening in the sheet 28.
  • a knurled internally threaded adjusting nut 46 mounted on grommet 44 is threaded to shank 42. By rotation of adjusting nut 46, the relative position of the grommet 44 and with it the sheet 28 can be adjusted with regard to suction cup 40.
  • a groove 48 or some equivalent structure is provided as part of adjusting nut 46 to retain grommet and nut together and permit nut 46 to rotate freely.
  • patch press 10 is virtually self-apparent. Once the patching procedure has reachedthe point where a patch 16, e.g., a doubler plate, has been positioned over the damaged region 15 on panel 12, the patch press 10 may be.
  • each suction cup assembly 14 is raised or lowered by rotation of adjusting nut 46 so that the various suction cups 40 conform to whatever local curvature exists on panel 12 and suspend the inelastic sheet 28 and frame 20 generally parallel to panel 12 spaced away from panel 12 so that frame 20 clears the highest point on panel 12.
  • the lower diaphragm 18 will then rest on and around the patch 16 in a flaccid state as is illustrated in FIG. 2. However, when a fluid such as air or other gas is pumped into the space between lower diaphragm l8 and upper diaphragm 30, both diaphragms distend.
  • the upper diaphragm 30 also distends, but only to the limits set by inelastic sheet 28 against which it bears. All the forces set up by pressurizing the space between diaphragms l8 and 30 are transmitted to the plurality of vacuum cup assemblies 14, tending to unseat vacuum cups 40.
  • moderate pressures e.g., up to 20 psig, applied between diaphragms l8 and 30 can be withstood by a 12 inch frame patch press 10 constructed with eight standard suction cups 40 (3 inch diameter).
  • Standard materials of construction may be utilized for patch press 10.
  • lower diaphragm 18 should be of an elastic extensible air tight material such asrubber sheeting and frame 20 should be a relatively rigid material, such as aluminum bar or sheet stock, but substitute materials are widely available and may be employed.
  • upper diaphragm 30 any air tight sheet material maybe employed. Rubber sheeting is convenient, mostly because the two diaphragms may then be identical, and the material of inelastic sheet 28 may then be selected without regard for air permeability. Heavy duty canvas sheeting is preferred for sheet 28.
  • a less preferred altemative is to use a gas tight sheet material that can serve simultaneously for inelastic support sheet 28 and upper diaphragm
  • An alternative more rigid mode of patch press is illustrated in FIGS. 8, 9 and 10.
  • the patch press cover member 128 is a rigid sheet (e.g., aluminum) withthe vacuum cups 40 secured directly at the peripheral edges thereof, being attached to depending skirts l30j'lhe patch press mode illustrated in FIGS. 8 and 9 is particularly adapted for smaller patches and, advantageously, requires fewer members than the previously described patch press mode. Only lower diaphragm l8 and a single frame member 120 are required. Frame 120 is bolted or riveted directly to cover member 128 by fasteners 126. The metallic sheet material of cover 128 is air tight and rigid, so that the space between diaphragm l8 and cover 128 may be sealed off adequately by the sealing ring 34. Air valve 36 and pressure gauge 38 can be readily mounted in cover 128.
  • Air valve 36 and pressure gauge 38 can be readily mounted in cover 128.
  • the mode of patch press illustrated in FIGS. 8, 9 and 10 can be made with as little as two suction cups 40, one at each end of the center line, so that parts as narrow as the suction cups can be repaired.
  • the patch press mode of FIGS. 8, 9 and 10 is more rigid than the mode of FIGS. 1-7, the relatively thin, strong aluminum alloys employed for cover 128 are flexible enough to allow for attachment of the patch press to moderately curved surfaces.
  • thepatch press of the present invention may include provision for heating patch 16.
  • steam might be introduced into the space above I diaphragm 18 to provide both heat and pressure.
  • electric resistance wires. may be molded into lower diaphragm l8.
  • the patch press is capable of use on curved surfaces. lt is'not sensitive to altitude, and can be employed on vertical surfaces, top surfaces, even on upside down surfaces. This versatility is quite advantageous, since damages rarely occur on the most convenient to patch top horizontal surfaces. Essentially, therefore, thepatch press may be used almost anywhere on modern-day airplanes, allowing high quality patching to be done remote from central maintenance stations.
  • a patch press comprising:
  • suction cups peripherally mounted adjacent the outer edges of said cover member, said suction cups serving as the support elements for the patch press with said frame being supported thereby generally parallel to and in s aced apart relation to the surface being patched; a fluid Ug lt diap ragm extending acrossthe framed area beneath said cover member, said diaphragm being clamped gas tight by said frame and being of a flaccid elastic material; and
  • valve means for adding and removing fluid from the space 3.
  • a patch press as in claim 1 wherein a sealing ring coextensive with said frame and disposed between the diaphragm and cover member is clamped by said frame to provide the gas tight sealed space between said diaphragm and cover member.
  • a patch press comprising:
  • suction cup assemblies mounted adjacent the outer edges of said inextensible sheet around 'the periphery thereof, said suction cup assemblies serving as the support elements for the patch press with said frame being supported thereby generally parallel to and in spaced apart relation to the surface being patched;
  • valve means for adding and removing fluid from the space between said diaphragms;
  • the patch press may be mounted over a patched surface with the patch element positioned inside the framed area and said suction cups seated on undamaged portions of the surface so that when the space between the said diaphragm is filled with fluid under pressure, the lower diaphragm distends into full contact with the patch element applying pressure uniformlythereto.
  • each suction cup assembly comprises:

Abstract

The present invention relates to a patch press, particularly but not exclusively adapted to use in repairing airplane surfaces by adhesively patching a double plate over the damaged area. The patch press itself involves a longitudinally split rectangular frame that has clamped therein a cover member which may be heavy duty fabric such as canvas that extends across the framed area and beyond and which serves to carry a plurality of suction cups at the periphery thereof so that the press may be mounted on and adhered to the undamaged surface around the region to be patched with the patch inside the frame. Sealed inside the frame and secured thereto is an inflatable, suitably valved diaphragm into which air or other gas can be pumped. That portion of the cover member inside the framed area acts as an outside reinforcement for the inflatable diaphragm, so that the forces generated when inflatable diaphragm is inflated and beats against the patch are transmitted directly to the suction cups. The patch press is a portable, essentially self-contained unit which can be employed to hold a patch onto an airplane surface and to maintain the patch there under pressure long enough for the adhesive bond to cure.

Description

United States Patent Engelet al.
[4 1 May 9, 1972 [54] PATCH PRESS [72] Inventors: Harry C. Engel; Edward J. Ardolino, both of Harve de Grace, Md.
[73] Assignee: Airline Systems, Inc., Harve de Grace,
[22] Filed: Nov. 3, 1970 [21] Appl.No.: 86,437
[52] US. Cl 156/580, 156/94, 100/211, 269/21, 269/22 [51] int. Cl. ..B30b 9/22, 1329b 19/00 [58] Field of Search ..l56/94, 580; 100/211; 144/281; 269/21, 22
[56] References Cited UNITED STATES PATENTS 2,960,147 11/1960 Ferrell 100/211 2,987,098 6/1961 Daniel ..l56/94 Primary Examiner-Douglas J. Drummond Attorney-Fidelman, Wolffe & Leitner [5 7] ABSTRACT The present invention relates to a patch press, particularly but not exclusively adapted to use in repairing airplane surfaces by adhesively patching a double plate over the damaged area.
The patch press itself involves a longitudinally split rectangular frame that has clamped therein a cover member which may be heavy duty fabric such as canvas that extends across the framed area and beyond and which serves to carry a plurality of suction cups at the periphery thereof so that the press may be mounted on and adhered to the undamaged surface around the region to be patched with the patch inside the frame.
Sealed inside the frame and secured thereto is an inflatable,
suitably valved diaphragm into which air or other gas can be pumped. That portion of the cover member inside the framed area acts as an outside reinforcement for the inflatable diaphragm, so that the forces generated when inflatable diaphragm is inflated and beats against the patch are transmitted directly to the suction cups.
The patch press is a portable, essentially self-contained unit which can be employed to hold a patch onto an airplane surface and to maintain the patch there under pressure long enough for the adhesive bond to cure.
10 Claims, 10 Drawing Figures Patented May 9, 1972 3 Sheets-Sheet l Patented May 9, 1972 3,661,683
3 Sheets-Sheet 2 "IIIIIIIIIIIIIIIIIIIIIIIIIIIIIII I/IIIIIII IIIIII/IIIIIIIIIIIIIIIIIIIIIIIIIIIIIIL Patented May 9, 1972 3 Sheets-Sheet 5 OOOOOOOOOO PATCH PRESS The present invention relates to an apparatus adapted for use in quick fix, bonded repair systems wherein a patch is adhesively bonded over a damaged region of some surface. In particular, the apparatus is adapted for use in time-limited, field type, bonded repair of aluminum aircraft assemblies.
Modern day airplanes are now constructed with wing and other surface regions of structurally bonded honeycomb panels that can easily be dented, even ruptured locally as, for example, by a dropped wrench, a thrown rock, impact with a bird. Overall, the airplane remains operable and safe, yet, obviously, the damage must be repaired as soon as possible. Needed is a patch which will hold permanently, or, failing that, at least until a convenient time comes to make permanent repair of the damaged region.
A typical repair sequence involves cleaning up the damaged region and removing all dirt and finish from the sound area immediately around the damaged region. Typically, the dented and broken damaged region is filled with an adhesive or other filler material so that the surface of the damaged area is flush with that of the sound metal around the damage. A doubler or patch piece is then adhesively bonded to the damaged area with enough of an overlap onto sound metal to obtain an adhesive metal-to-metal bond adequate to hold the doubler in place. Typically, the doubler may overlap the damaged area from about 1%. to 4 inches in all directions.
Fortunately, high quality quick-curing adhesives are available commercially so that this repair procedure is effective. However, the efficacy of the adhesive bond depends largely upon application of a uniform pressure over the entire area of the doubler plate. In short, the doubler plate must be uniformly pressed against the skin surface regardless of whether the surface is horizontal, vertical, planar or curved. The present invention provides a portable, essentially selfcontained apparatus, i.e., a patch press, capable of applying compliant uniform pressure to the doubler plate being adhered over a damaged surface region, and maintaining such pressure until the adhesive has cured.
For further understanding of this apparatus, reference is now made to the drawing wherein:
FIG. 1 is a top plan view of the patch press;
FIG. 2 is a side view of the patch press;
FIG. 3 is a section taken along line 3-3 ofFIG. 1;
FIG. 4 is an enlarged partial section taken along the line 4- 4 of FIG. 1;
FIG. 5 is an enlarged partial section taken along line 5-5 of FIG. 1;
FIG. 6 is an enlarged partial section taken along line 6-6 of FIG. 1;
FIG. 7 is an exploded section taken along line 7-7 of FIG.
FIG. 8 is a top plan view of a modified form of the invention;
FIG. 9 is a bottom plan view of the device in FIG. 8; and
FIG. 10 is a side elevation of FIG. 8 with parts broken away.
As may be seen best in FIGS. 1, 2 and 3, the present patch press 10 is adapted to seat on a damaged panel 12 through means of a plurality of suction cup assemblies 14 disposed peripherally around the patch press 10. The damaged region 15, shadow illustrated in FIG. 1, is centered under patch press 10. FIG. 3 shows how patch press 10 is seated over a doubler patch 16 and uniformly applies pneumatic pressure thereto by a lower fluid tight elastic diaphragm 18 which form s'a portion of patch press 10. FIG. 2 shows the diaphragm 18 in a flaccid non-inflated state.
Patch press 10 further comprises a square (or rectangular) longitudinally split metallic frame 20 normally fabricated of aluminum. The upper frame member 22 and lower frame member 24 (FIGS. 4 and 5) are secured together by machine screws 26 or other conventional fastening elements (e.g., rivet, nut and bolt, etc.). Locked together between the split halves 22 and 24, are the several layers of sheet material which form part of the present patch press. FIG. 7 is an exploded view illustrating frame members and the several sheet layers in FIG. 7. The cover member is a heavy duty inelastic sheet 28, film or fabric, e.g., heavy canvas, which extends across the open area inside frame 20 and beyond frame 20, as is shown in FIG. 1. The heavy duty sheet 28 serves to carry suction cup assemblies 14 at the peripheral edges thereof. Directly beneath heavy duty sheet 28 is upper elastic diaphragm 30, which desirably may be a rubber sheet (synthetic, natural, or even an elastic resin). Optionally present is an adhesive layer 32 between diaphragm 30 and sheet 28, disposed either on the underside of sheet 28 or on the top side of diaphragm 30 to adhere the two layers together. The lower elastic diaphragm 18 previously alluded to is the bottom layer. Therebeneath is lower frame member 24. Normally, the same (rubber or rubber-like) material would be employed for both diaphragms. The extra layer 34 shown on FIG. 7 is a soft sealing ring 34 whose area is generally co-extensive with that of frame 20 and whose purpose is to provide an airtight seal between upper diaphragm 28 and lower diaphragm 18 so that the space therebetween can serve as a sealed off region into which pressurizing fluid may be added and removed as desired by way of air valve 36. Such valves are standard articles of commerce, e.g., an ordinary tire valve will sufiice, and the details thereof need not be described further. Optionally present may be a pressure gauge 38, should it be desirable to indicate the extent to which the volume inside diaphragms l8 and 30 has been pressurized.
The suction cup assemblies 14 disposed at the periphery of the heavy duty sheet 28 each'comprise (FIG. 6) a suction cup 40 which seats on panel 12 and a threaded shank 42 to which cup 40 is secured. The shank 42 passes up through a grommet 44 which provides a suitable opening in the sheet 28. A knurled internally threaded adjusting nut 46 mounted on grommet 44 is threaded to shank 42. By rotation of adjusting nut 46, the relative position of the grommet 44 and with it the sheet 28 can be adjusted with regard to suction cup 40. A groove 48 or some equivalent structure is provided as part of adjusting nut 46 to retain grommet and nut together and permit nut 46 to rotate freely.
The operation of patch press 10 is virtually self-apparent. Once the patching procedure has reachedthe point where a patch 16, e.g., a doubler plate, has been positioned over the damaged region 15 on panel 12, the patch press 10 may be.
centered over patch 16. The shank 42 of each suction cup assembly 14 is raised or lowered by rotation of adjusting nut 46 so that the various suction cups 40 conform to whatever local curvature exists on panel 12 and suspend the inelastic sheet 28 and frame 20 generally parallel to panel 12 spaced away from panel 12 so that frame 20 clears the highest point on panel 12. The lower diaphragm 18 will then rest on and around the patch 16 in a flaccid state as is illustrated in FIG. 2. However, when a fluid such as air or other gas is pumped into the space between lower diaphragm l8 and upper diaphragm 30, both diaphragms distend. The lower diaphragm 18, being relatively flaccid and unsupported, bears down upon patch 16 and ap plies a uniform pneumatic pressure across the entire area of the patch. The upper diaphragm 30 also distends, but only to the limits set by inelastic sheet 28 against which it bears. All the forces set up by pressurizing the space between diaphragms l8 and 30 are transmitted to the plurality of vacuum cup assemblies 14, tending to unseat vacuum cups 40. In practice, it has been found that moderate pressures, e.g., up to 20 psig, applied between diaphragms l8 and 30 can be withstood by a 12 inch frame patch press 10 constructed with eight standard suction cups 40 (3 inch diameter). It goes without saying that if the patch press 10 were larger than about the 12 inch frame and a 20 inch canvas sheet, the size of the exemplary structure illustrated, then more suction cup assemblies l4 (e.g., 16) may be provided at the periphery of sheet 28.
Standard materials of construction may be utilized for patch press 10. Certainly lower diaphragm 18 should be of an elastic extensible air tight material such asrubber sheeting and frame 20 should be a relatively rigid material, such as aluminum bar or sheet stock, but substitute materials are widely available and may be employed. For upper diaphragm 30, any air tight sheet material maybe employed. Rubber sheeting is convenient, mostly because the two diaphragms may then be identical, and the material of inelastic sheet 28 may then be selected without regard for air permeability. Heavy duty canvas sheeting is preferred for sheet 28. A less preferred altemative is to use a gas tight sheet material that can serve simultaneously for inelastic support sheet 28 and upper diaphragm An alternative more rigid mode of patch press is illustrated in FIGS. 8, 9 and 10. The patch press cover member 128 is a rigid sheet (e.g., aluminum) withthe vacuum cups 40 secured directly at the peripheral edges thereof, being attached to depending skirts l30j'lhe patch press mode illustrated in FIGS. 8 and 9 is particularly adapted for smaller patches and, advantageously, requires fewer members than the previously described patch press mode. Only lower diaphragm l8 and a single frame member 120 are required. Frame 120 is bolted or riveted directly to cover member 128 by fasteners 126. The metallic sheet material of cover 128 is air tight and rigid, so that the space between diaphragm l8 and cover 128 may be sealed off adequately by the sealing ring 34. Air valve 36 and pressure gauge 38 can be readily mounted in cover 128.
Omission of the shank mount for vacuum cups 40 in favor of mounting on depending skirt 130, permits an easy inclusion of a valve 150 at each cup (for breaking the vacuum).
The mode of patch press illustrated in FIGS. 8, 9 and 10 can be made with as little as two suction cups 40, one at each end of the center line, so that parts as narrow as the suction cups can be repaired.
Although the patch press mode of FIGS. 8, 9 and 10 is more rigid than the mode of FIGS. 1-7, the relatively thin, strong aluminum alloys employed for cover 128 are flexible enough to allow for attachment of the patch press to moderately curved surfaces.
Since airplane patching practice normally involves employment of a heat-curing adhesive, thepatch press of the present invention may include provision for heating patch 16. Obviously, steam might be introduced into the space above I diaphragm 18 to provide both heat and pressure. Alternatively, electric resistance wires. may be molded into lower diaphragm l8.
Allusion has already been made to the great extent to which the patch press is a self-contained, portable unit of wide applicability. The patch press is capable of use on curved surfaces. lt is'not sensitive to altitude, and can be employed on vertical surfaces, top surfaces, even on upside down surfaces. This versatility is quite advantageous, since damages rarely occur on the most convenient to patch top horizontal surfaces. Essentially, therefore, thepatch press may be used almost anywhere on modern-day airplanes, allowing high quality patching to be done remote from central maintenance stations.
Inasmuch as patching of airplanes is a substantial problem and the greatest use of the patch press may be in repair of aircraft structure, the present invention has been described within such context. Its use is not limited thereto. Similar circumstances and patch patterns exist in aluminum hulled and fiberglass boats where small damages are repaired by patching the surface. It is believed, then, that the present patch press has wider applicability than in the repair of aircraft structures.
What is claimed is:
1. A patch press comprising:
a frame clamping a multiplicity of layers therein;
a cover member clamped by said frame as the uppermost layer, said cover extending across the framed area and beyond said frame;
a plurality of suction cups peripherally mounted adjacent the outer edges of said cover member, said suction cups serving as the support elements for the patch press with said frame being supported thereby generally parallel to and in s aced apart relation to the surface being patched; a fluid Ug lt diap ragm extending acrossthe framed area beneath said cover member, said diaphragm being clamped gas tight by said frame and being of a flaccid elastic material; and
valve means for adding and removing fluid from the space 3. A patch press as in claim 1 wherein valve means are disposed in said cover member for admitting fluid under pressure to the space between diaphragm and cover.
4. A patch press as in claim 1 wherein a sealing ring coextensive with said frame and disposed between the diaphragm and cover member is clamped by said frame to provide the gas tight sealed space between said diaphragm and cover member.
5. A patch press as in claim 4 wherein said cover member is a heavy duty inextensible fabric and a second fluid tight diaphragm is interposed between the inextensible fabric and the sealing ring.
6. A patch press comprising:
a longitudinally split frame clamping a multiplicity of layers therebetween;
an inextensible sheet clamped by said frame as the uppermost layer clamped therein, said sheet extending across the framed area and beyond said frame;
a plurality of suction cup assemblies mounted adjacent the outer edges of said inextensible sheet around 'the periphery thereof, said suction cup assemblies serving as the support elements for the patch press with said frame being supported thereby generally parallel to and in spaced apart relation to the surface being patched;
an upper and a lower fluid tight diaphragm extending across the framed area, said diaphragms being clamped together in a gas tight seal by said frame, and forming two of the layers clamped by said frame,- the lower diaphragm at least being of a flaccid elastic material; and
valve means for adding and removing fluid from the space between said diaphragms; v
whereby the patch press may be mounted over a patched surface with the patch element positioned inside the framed area and said suction cups seated on undamaged portions of the surface so that when the space between the said diaphragm is filled with fluid under pressure, the lower diaphragm distends into full contact with the patch element applying pressure uniformlythereto.
7. A patch press as in claim 6 wherein both diaphragms are rubber, and the inextensible sheet is a heavy duty fabric.
8. A patch press as in claim 6 wherein a sealing ring coextensive with said frame and disposed between the diaphragms forms an additional layer clamped by said frame to provide a gas tight sealed space between said diaphragms.
9. A patch press as in claim 6 wherein the upper diaphragm is adhesively attached to the inextensible fabric.
10. A patch press as in claim 6 wherein each suction cup assembly comprises:
a suction cup mounted at the base end of a threaded shank;
and
an internally threaded adjusting nut means to which the inextensible sheet is secured, said adjusting nut means being threaded on said shank whereby the spacing between the inextensible sheet and each suction cup may be adjusted so that the patch press can be fitted to curved surfaces.

Claims (10)

1. A patch press comprising: a frame clamping a multiplicity of layers therein; a cover member clamped by said frame as the uppermost layer, said cover extending across the framed area and beyond said frame; a plurality of suction cups peripherally mounted adjacent the outer edges of said cover member, said suction cups serving as the support elements for the patch press with said frame being supported thereby generally parallel to and in spaced apart relation to the surface being patched; a fluid tight diaphragm extending across the framed area beneath said cover member, said diaphragm being clamped gas tight by said frame and being of a flaccid elastic material; and valve means for adding and removing fluid from the space between said cover and said diaphragm; whereby the patch press may be supported by the suction cup so as to position a patch element inside the framed area of the patch press so that when the space between the said diaphragm and cover member is filled with fluid under pressure, the diaphragm distends into full contact with the patch element applying pressure uniformly thereto.
2. A patch press as in claim 1 wherein said cover member is a metallic sheet member.
3. A patch press as in claim 1 wherein valve means are disposed in said cover member for admitting fluid under pressure to the space between diaphragm and cover.
4. A patch press as in claim 1 wherein a sealing ring coextensive with said frame and disposed between the diaphragm and cover member is clamped by said frame to provide the gas tight sealed space between said diaphragm and cover member.
5. A patch press as in claim 4 wherein said cover member is a heavy duty inextensible fabric and a second fluid tight diaphragm is interposed between the inextensible fabric and the sealing ring.
6. A patch press comprising: a longitudinally split frame clamping a multiplicity of layers therebetween; an inextensible sheet clamped by said frame as the uppermost layer clamped therein, said sheet extending across the framed area and beyond said frame; a plurality of suction cup assemblies mounted adjacent the outer edges of said inextensible sheet around the periphery thereof, said suction cup assemblies serving as the support elements for the patch press with saId frame being supported thereby generally parallel to and in spaced apart relation to the surface being patched; an upper and a lower fluid tight diaphragm extending across the framed area, said diaphragms being clamped together in a gas tight seal by said frame, and forming two of the layers clamped by said frame, the lower diaphragm at least being of a flaccid elastic material; and valve means for adding and removing fluid from the space between said diaphragms; whereby the patch press may be mounted over a patched surface with the patch element positioned inside the framed area and said suction cups seated on undamaged portions of the surface so that when the space between the said diaphragm is filled with fluid under pressure, the lower diaphragm distends into full contact with the patch element applying pressure uniformly thereto.
7. A patch press as in claim 6 wherein both diaphragms are rubber, and the inextensible sheet is a heavy duty fabric.
8. A patch press as in claim 6 wherein a sealing ring coextensive with said frame and disposed between the diaphragms forms an additional layer clamped by said frame to provide a gas tight sealed space between said diaphragms.
9. A patch press as in claim 6 wherein the upper diaphragm is adhesively attached to the inextensible fabric.
10. A patch press as in claim 6 wherein each suction cup assembly comprises: a suction cup mounted at the base end of a threaded shank; and an internally threaded adjusting nut means to which the inextensible sheet is secured, said adjusting nut means being threaded on said shank whereby the spacing between the inextensible sheet and each suction cup may be adjusted so that the patch press can be fitted to curved surfaces.
US86437A 1970-11-03 1970-11-03 Patch press Expired - Lifetime US3661683A (en)

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US4065116A (en) * 1975-12-02 1977-12-27 Varta Batterie Aktiengesellschaft Clamping of battery plate block assemblies
DE3034101A1 (en) * 1979-09-13 1981-04-02 Physical Systems, Inc., Carson City, Nev. DEVICE FOR PRODUCING ADHESIVE BINDINGS
DE3036345A1 (en) * 1980-09-26 1982-06-24 Andreas Peter Istvan 8035 Gauting Pöhl PRESS, ESPECIALLY FOR COATING TABLED BODIES
US4337105A (en) * 1980-09-04 1982-06-29 The United States Of America As Represented By The Secretary Of The Navy Spherical segment inner surface force applicator for laminating non-planar surfaces
US4338151A (en) * 1979-09-13 1982-07-06 Physical Systems, Inc. Method of securing an adhesive attachment assembly to a substrate
US4390576A (en) * 1980-09-19 1983-06-28 Physical Systems, Inc. Adhesive attachment assembly
US4668546A (en) * 1985-09-04 1987-05-26 Physical Systems, Inc. Fixture for securing an adhesive attachment to a substrate
DE3624000A1 (en) * 1986-07-16 1988-01-28 Festo Kg CLAMPING DEVICE
US4778702A (en) * 1985-09-04 1988-10-18 Physical Systems, Inc. Adhesive attachment and mounting fixture
US4822656A (en) * 1985-09-04 1989-04-18 Physical Systems, Inc. Fixture for securing an adhesive attachment to a substrate
US4842912A (en) * 1985-09-04 1989-06-27 Physical Systems, Inc. Adhesive attachment and mounting fixture
US5042772A (en) * 1990-04-06 1991-08-27 Madjeski Terry M Mirror aligning device
DE4111246C1 (en) * 1991-04-08 1992-09-10 Maschinen- Und Stahlbau Julius Lippert Gmbh & Co, 8487 Pressath, De
US5246216A (en) * 1992-10-30 1993-09-21 Oberst E Ernest Vise jaw attachment for irregular shaped workpieces
US5374388A (en) * 1993-04-22 1994-12-20 Lockheed Corporation Method of forming contoured repair patches
US5442156A (en) * 1991-04-09 1995-08-15 The Boeing Company Heating apparatus for composite structure repair
US5660380A (en) * 1995-08-15 1997-08-26 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US5728258A (en) * 1995-12-15 1998-03-17 E-Systems, Inc. Portable non-gravitational positive pressure generator and method of use
US5820116A (en) * 1997-05-02 1998-10-13 Haese; Robert W. Suction attachable retaining clamp
US5975183A (en) * 1998-03-23 1999-11-02 Northrop Grumman Corporation Repair pressure applicator for in the field damaged aircraft
US6080343A (en) * 1997-03-17 2000-06-27 Sandia Corporation Methods for freeform fabrication of structures
US6182957B1 (en) * 1999-08-12 2001-02-06 International Business Machines Corporation Apparatus and method for holding a flexible product in a flat and secure position
US6270603B1 (en) * 1991-04-09 2001-08-07 The Boeing Company Repair method for uniformly heating composite structure
US6435242B1 (en) 1998-03-23 2002-08-20 Northrop Grumman Corp Repair pressure applicator
US6680099B1 (en) * 1995-10-20 2004-01-20 The United States Of America As Represented By The Secretary Of Transportation Enhancing damage tolerance of adhesive bonds
US20040041356A1 (en) * 2000-05-12 2004-03-04 Aviation Devices And Electronic Components, Llc. Gasket material having a PTFE core and a method of making a using the same
US20040047837A1 (en) * 1997-03-21 2004-03-11 Yuman Fong Rapid production of autologous tumor vaccines
US20040256045A1 (en) * 2003-06-19 2004-12-23 Carl Reis Positive pressure hot bonder
US20050056742A1 (en) * 2003-07-22 2005-03-17 Peress Sass M. Support structure for mounting a solar panel
WO2005120794A1 (en) 2004-06-09 2005-12-22 Industrial Composites Engineering Pty Ltd Method for forming or curing polymer composites
US20070164479A1 (en) * 2006-01-13 2007-07-19 Hexcel Corporation Pressurized molding of composite parts
US20090071591A1 (en) * 2007-09-13 2009-03-19 Essilor International (Compagnie Generale D'optique) Process for Applying a Coating Film onto a Surface of a Lens Substrate
US20100015265A1 (en) * 2008-07-21 2010-01-21 United Technologies Corporation Pressure bladder and method for fabrication
AU2005251829C1 (en) * 2004-06-09 2011-02-03 Industrial Composites Engineering Pty Ltd Method for forming or curing polymer composites
WO2011022581A1 (en) * 2009-08-21 2011-02-24 Open Water Products, Llc Lighted dive buoy
US20120137484A1 (en) * 2010-12-06 2012-06-07 Hermann Benthien Method for Repairing an Aircraft Structure Component
US20120152438A1 (en) * 2010-12-06 2012-06-21 Hermann Benthien Method of Repairing an Aircraft Structure Component
FR2999974A1 (en) * 2012-12-20 2014-06-27 Airbus Operations Sas System for applying repair kit to face of structure to be repaired e.g. fuselage panel of aircraft, has backpressure device with surface arranged in opposite to goldbeater's skin, and connection units that connects device to frame
US20150158258A1 (en) * 2010-09-30 2015-06-11 The Boeing Company Systems and Methods for On-Aircraft Composite Repair Using Double Vacuum Debulking
US20160136941A1 (en) * 2014-11-19 2016-05-19 The Boeing Company Installation tool and associated method for applying a patch to a surface
CN106112549A (en) * 2016-08-22 2016-11-16 山东太古飞机工程有限公司 Aircraft curved surface sheet material component damage modularity device for excising
USD824470S1 (en) * 2017-03-27 2018-07-31 Rodney D. Bragg Above ground swimming pool patch panel
US10307977B2 (en) * 2014-02-17 2019-06-04 The Boeing Company Verifiable quick patch repair for composite structures
US10507626B2 (en) * 2016-05-16 2019-12-17 Alkar-Rapidpak, Inc. Bladder devices for moving components of web packaging machines
US11312507B2 (en) * 2019-09-03 2022-04-26 The Boeing Company Repair assembly to repair an area on a member of a vehicle

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Cited By (67)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4065116A (en) * 1975-12-02 1977-12-27 Varta Batterie Aktiengesellschaft Clamping of battery plate block assemblies
DE3034101A1 (en) * 1979-09-13 1981-04-02 Physical Systems, Inc., Carson City, Nev. DEVICE FOR PRODUCING ADHESIVE BINDINGS
US4338151A (en) * 1979-09-13 1982-07-06 Physical Systems, Inc. Method of securing an adhesive attachment assembly to a substrate
US4337105A (en) * 1980-09-04 1982-06-29 The United States Of America As Represented By The Secretary Of The Navy Spherical segment inner surface force applicator for laminating non-planar surfaces
US4390576A (en) * 1980-09-19 1983-06-28 Physical Systems, Inc. Adhesive attachment assembly
DE3036345A1 (en) * 1980-09-26 1982-06-24 Andreas Peter Istvan 8035 Gauting Pöhl PRESS, ESPECIALLY FOR COATING TABLED BODIES
US4778702A (en) * 1985-09-04 1988-10-18 Physical Systems, Inc. Adhesive attachment and mounting fixture
US4822656A (en) * 1985-09-04 1989-04-18 Physical Systems, Inc. Fixture for securing an adhesive attachment to a substrate
US4842912A (en) * 1985-09-04 1989-06-27 Physical Systems, Inc. Adhesive attachment and mounting fixture
US4668546A (en) * 1985-09-04 1987-05-26 Physical Systems, Inc. Fixture for securing an adhesive attachment to a substrate
DE3624000A1 (en) * 1986-07-16 1988-01-28 Festo Kg CLAMPING DEVICE
US5042772A (en) * 1990-04-06 1991-08-27 Madjeski Terry M Mirror aligning device
DE4111246C1 (en) * 1991-04-08 1992-09-10 Maschinen- Und Stahlbau Julius Lippert Gmbh & Co, 8487 Pressath, De
EP0508141A1 (en) 1991-04-08 1992-10-14 Maschinen- und Stahlbau Julius Lippert GmbH & Co. Device for clamping pressure sensitive ceramic objects
US5442156A (en) * 1991-04-09 1995-08-15 The Boeing Company Heating apparatus for composite structure repair
US6270603B1 (en) * 1991-04-09 2001-08-07 The Boeing Company Repair method for uniformly heating composite structure
US5246216A (en) * 1992-10-30 1993-09-21 Oberst E Ernest Vise jaw attachment for irregular shaped workpieces
US5374388A (en) * 1993-04-22 1994-12-20 Lockheed Corporation Method of forming contoured repair patches
US5492466A (en) * 1993-04-22 1996-02-20 Lockheed Corporation Vacuum mold and heating device for processing contoured repair patches
US5906363A (en) * 1995-08-15 1999-05-25 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US5660380A (en) * 1995-08-15 1997-08-26 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US5782152A (en) * 1995-08-15 1998-07-21 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US5800661A (en) * 1995-08-15 1998-09-01 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US5870937A (en) * 1995-08-15 1999-02-16 W. L. Gore & Associates, Inc. Vacuum fixture and method for dimensioning and manipulating materials
US6680099B1 (en) * 1995-10-20 2004-01-20 The United States Of America As Represented By The Secretary Of Transportation Enhancing damage tolerance of adhesive bonds
US5846362A (en) * 1995-12-15 1998-12-08 Raytheon E-Systems, Inc. Portable non-gravitational positive pressure generator and method of use
US5728258A (en) * 1995-12-15 1998-03-17 E-Systems, Inc. Portable non-gravitational positive pressure generator and method of use
US6080343A (en) * 1997-03-17 2000-06-27 Sandia Corporation Methods for freeform fabrication of structures
US20040047837A1 (en) * 1997-03-21 2004-03-11 Yuman Fong Rapid production of autologous tumor vaccines
US5820116A (en) * 1997-05-02 1998-10-13 Haese; Robert W. Suction attachable retaining clamp
US6435242B1 (en) 1998-03-23 2002-08-20 Northrop Grumman Corp Repair pressure applicator
US6318433B1 (en) 1998-03-23 2001-11-20 Northrop Grumman Corporation Repair pressure applicator for in the field damaged aircraft
US5975183A (en) * 1998-03-23 1999-11-02 Northrop Grumman Corporation Repair pressure applicator for in the field damaged aircraft
US6182957B1 (en) * 1999-08-12 2001-02-06 International Business Machines Corporation Apparatus and method for holding a flexible product in a flat and secure position
US20040041356A1 (en) * 2000-05-12 2004-03-04 Aviation Devices And Electronic Components, Llc. Gasket material having a PTFE core and a method of making a using the same
US20040256045A1 (en) * 2003-06-19 2004-12-23 Carl Reis Positive pressure hot bonder
US6835262B1 (en) 2003-06-19 2004-12-28 Northrop Grumman Corporation Positive pressure hot bonder
WO2005000574A2 (en) * 2003-06-19 2005-01-06 Northrop Grumman Corporation Positive pressure hot bonder
WO2005000574A3 (en) * 2003-06-19 2005-03-24 Northrop Grumman Corp Positive pressure hot bonder
US20050056742A1 (en) * 2003-07-22 2005-03-17 Peress Sass M. Support structure for mounting a solar panel
US8088237B2 (en) 2004-06-09 2012-01-03 Industrial Composites Engineering Pty Ltd Method for forming or curing polymer composites
AU2005251829C1 (en) * 2004-06-09 2011-02-03 Industrial Composites Engineering Pty Ltd Method for forming or curing polymer composites
US20070113953A1 (en) * 2004-06-09 2007-05-24 Haywood Alex M Method for forming or curing polymer composites
WO2005120794A1 (en) 2004-06-09 2005-12-22 Industrial Composites Engineering Pty Ltd Method for forming or curing polymer composites
US8034278B2 (en) * 2006-01-13 2011-10-11 Hexcel Corporation Pressurized molding of composite parts
US20070164479A1 (en) * 2006-01-13 2007-07-19 Hexcel Corporation Pressurized molding of composite parts
US20090071591A1 (en) * 2007-09-13 2009-03-19 Essilor International (Compagnie Generale D'optique) Process for Applying a Coating Film onto a Surface of a Lens Substrate
US20100015265A1 (en) * 2008-07-21 2010-01-21 United Technologies Corporation Pressure bladder and method for fabrication
US20110065342A1 (en) * 2009-08-21 2011-03-17 Hudson Jack F Lighted Dive Buoy
WO2011022581A1 (en) * 2009-08-21 2011-02-24 Open Water Products, Llc Lighted dive buoy
US20150158258A1 (en) * 2010-09-30 2015-06-11 The Boeing Company Systems and Methods for On-Aircraft Composite Repair Using Double Vacuum Debulking
US10336019B2 (en) * 2010-09-30 2019-07-02 The Boeing Company Systems and methods for on-aircraft composite repair using double vacuum debulking
US9382017B2 (en) * 2010-12-06 2016-07-05 Airbus Operations Gmbh Method for repairing an aircraft structure component
US20120137484A1 (en) * 2010-12-06 2012-06-07 Hermann Benthien Method for Repairing an Aircraft Structure Component
US20120152438A1 (en) * 2010-12-06 2012-06-21 Hermann Benthien Method of Repairing an Aircraft Structure Component
US8623160B2 (en) * 2010-12-06 2014-01-07 Airbus Operations Gmbh Method of repairing an aircraft structure component
FR2999974A1 (en) * 2012-12-20 2014-06-27 Airbus Operations Sas System for applying repair kit to face of structure to be repaired e.g. fuselage panel of aircraft, has backpressure device with surface arranged in opposite to goldbeater's skin, and connection units that connects device to frame
US10307977B2 (en) * 2014-02-17 2019-06-04 The Boeing Company Verifiable quick patch repair for composite structures
US10207468B2 (en) * 2014-11-19 2019-02-19 The Boeing Company Installation tool and associated method for applying a patch to a surface
US20190152173A1 (en) * 2014-11-19 2019-05-23 The Boeing Company Installation tool and associated method for applying a patch to a surface
US20160136941A1 (en) * 2014-11-19 2016-05-19 The Boeing Company Installation tool and associated method for applying a patch to a surface
US10675821B2 (en) 2014-11-19 2020-06-09 The Boeing Company Installation tool and associated method for applying a patch to a surface
AU2015227522B2 (en) * 2014-11-19 2020-11-19 The Boeing Company Installation tool and associated method for applying a patch to a surface
US10507626B2 (en) * 2016-05-16 2019-12-17 Alkar-Rapidpak, Inc. Bladder devices for moving components of web packaging machines
CN106112549A (en) * 2016-08-22 2016-11-16 山东太古飞机工程有限公司 Aircraft curved surface sheet material component damage modularity device for excising
USD824470S1 (en) * 2017-03-27 2018-07-31 Rodney D. Bragg Above ground swimming pool patch panel
US11312507B2 (en) * 2019-09-03 2022-04-26 The Boeing Company Repair assembly to repair an area on a member of a vehicle

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