WO2013106640A1 - Liaison facilement amovible et remplaçable pour portes de conteneurs de fret aérien - Google Patents

Liaison facilement amovible et remplaçable pour portes de conteneurs de fret aérien Download PDF

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Publication number
WO2013106640A1
WO2013106640A1 PCT/US2013/021132 US2013021132W WO2013106640A1 WO 2013106640 A1 WO2013106640 A1 WO 2013106640A1 US 2013021132 W US2013021132 W US 2013021132W WO 2013106640 A1 WO2013106640 A1 WO 2013106640A1
Authority
WO
WIPO (PCT)
Prior art keywords
hook
fabric
strap
loop fastener
pocket
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.)
Ceased
Application number
PCT/US2013/021132
Other languages
English (en)
Inventor
Thomas R. Pherson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Advanced Composite Structures LLC
Original Assignee
Advanced Composite Structures LLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Advanced Composite Structures LLC filed Critical Advanced Composite Structures LLC
Publication of WO2013106640A1 publication Critical patent/WO2013106640A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00Large containers
    • B65D88/02Large containers rigid
    • B65D88/12Large containers rigid specially adapted for transport
    • B65D88/14Large containers rigid specially adapted for transport by air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00Component parts, details or accessories for large containers
    • B65D90/02Wall construction
    • B65D90/021Flexible side walls or doors

Definitions

  • This application relates to air cargo containers having fabric doors, and a connection system for attaching the doors to the containers.
  • This application relates more particularly to an easily removable and replaceable strap connection system for such doors.
  • Cargo containers are used in a variety of transportation fields all over the world.
  • One type of commonly used cargo container is shaped to be loaded into the cargo hold of an airplane. These are often referred to as uniform load devices (ULDs).
  • ULDs uniform load devices
  • these containers will have a top, a bottom and a plurality of side walls. These walls may be contoured to fit efficiently within the curved body of an airplane.
  • These containers have at least one end that is open or openable in order to facilitate the on loading and off loading of cargo. It is however important to close off this openable end of the container to prevent intrusion of dirt, water or UV light into the container. Further, the closure will make sure that the contents of the container are not lost during transportation.
  • This open end of the cargo container has been closed off in a number of different ways. First, solid doors were added. These doors were often constructed from the same metal material as the remainder of the container. These metal doors provided high strength for keeping the cargo inside, but added significant weight to the cargo container as well.
  • Fig. 1 shows a cargo container 1, having a fabric door 2 having traverse straps 3.
  • One aspect of the invention is a two-piece, separable, strap closure member for the fabric curtain that is removably connectable to a clevis or coupling on the side of a cargo container.
  • the two-piece strap closure member includes a pocket sewn onto the face of a container fabric door and a separable strap that connects to the clevis or coupling.
  • the separable strap closure is easy to fasten and unfasten, tightens the door both horizontally and vertically to reduce bulging, and can be easily repaired without sewing.
  • the strap may include hook or loop fastening portions along its face that attach to mating hook or loop fastener portions on the rear face of the pocket of the fabric door.
  • the fabric door can be formed of high strength yarns formed of high performance fibers, such as Ultra-High Molecular Weight Polyethylene.
  • the portion of the strap or hook/loop fastener portion thereon that connects to the rear face of the pocket should include bright or distinctive coloring so a repair worker can tell when the strap is properly positioned and aligned behind the pocket.
  • Another aspect of the invention is a three-piece, separable, strap closure member for the fabric curtain that is removably connectable to a clevis or coupling on the side of a cargo container.
  • the three-piece strap closure member includes a pocket sewn onto the face of a container fabric door, a connection member sewn onto the face of the container fabric door, and a separable strap that attaches the fabric door to the cargo container by joining the connection member to the clevis or coupling.
  • the separable strap closure is easy to fasten and unfasten, tightens the door both horizontally and vertically to reduce bulging, and can be easily repaired without sewing.
  • the strap may include hook or loop fastening portions along its face that attach to mating hook or loop fastener portions on the rear face of the pocket.
  • FIG. 1 shows an air cargo container with a first prior art type fabric door, having traverse straps.
  • FIG. 2 shows an air cargo container with a second prior art type fabric door, having sewn on straps.
  • FIG. 3 shows a cargo container having the fabric door and a two-piece strap closure system of the present disclosure
  • Fig. 4 shows a detailed view of one of the two-piece strap closures of Fig. 3 in the assembled position.
  • Fig. 5 shows the closure assembly of Fig. 4 with the strap removed.
  • Fig. 6 shows a detailed view of strap closure of Fig. 4 with an optional connection member.
  • Fig. 7 shows a detailed view of the strap of the present disclosure in an unfolded position.
  • Fig. 8 shows the strap closure of Fig. 4 in an open, partially assembled, position.
  • FIG. 3 a preferred embodiment of the present disclosure is shown.
  • This embodiment can include a cargo container 10 having a top 14, bottom 18, and sides 22 that suiTound an open end of the cargo container 10,
  • the open end of the container 10 can be closed off by a fabric door 50.
  • the fabric door 50 can be attached to the cargo container 10 by at least one closure assembly 100.
  • a plurality of closure assemblies 100 are placed along each of the side edges of the fabric closure 50 that abut the edges of the side walls 22, By providing the closure assemblies 100 along each lateral edge of the fabric door 50, the closure assemblies 100 are able to tension the fabric door 50 in the lateral direction across the open end of the container 10, [0023] Although not seen in Fig.
  • closure assemblies 100 may be used there also. These additional closure assemblies 100 will be able to provide tension to the fabric door 50 in the vertical direction. A fabric door 50 that is under tension in at least these two directions will better enable the fabric door 50 to be able to hold back the cargo within the container 10. Closure assemblies 100 that are placed along the top and bottom edges of the fabric door 50 will also assist in prevention of small objects being able to pass between the bottom edge of the fabric door 50 and the bottom edge of the open side of the cargo container 10. Since the closure assemblies 100 do not have to be sewn across the entirety of the door 50, the closures 100 are no longer required to be directly across from one another. Further, the closure assemblies 100 can form an oblique angle with the side of the cargo container 10. By acting along an oblique angle, the closure assembly 100 is able to provide a tension force in both the horizontal and vertical directions at the same time.
  • the fabric door 50 may be formed from a variety of materials.
  • the door 50 may be constructed from vinyl-coated polyester.
  • the door 50 will be made from high performance fabrics.
  • high performance fabrics and “high strength yarns” means fabrics or yarns formed from fibers having tenacities equal to or greater than about 7 g/d.
  • these fibers have initial tensile moduli of at least about 150 g/d and energies to break of at least about 8 J/g as measured by ASTM D2256.
  • the terms "initial tensile modulus”, “tensile modulus,” and “modulus” mean the modulus of elasticity as measured by ASTM 2256 for a yarn or by ASTM D638 for an elastomer or matrix material.
  • These high performance fabrics include ultra-high molecular weight polyethylene and others such as ultra high molecular weight aramid. Examples of this material include materials sold under the trade name Spectra®.
  • the fabric for the door is preferably woven, and includes at least 50% (and preferably at least 75%) of these high strength fibers.
  • the material for the fabric doors 50 is preferably waterproof, which may be obtained by laminating a film of ethylene vinyl acetate (EVA), polyethylene, or the like onto the surface. Use of a waterproof material will protect the contents of the cargo container 10 from rain water or other liquids.
  • EVA ethylene vinyl acetate
  • FIG. 4 where a detailed view of an exemplary closure assembly 100 is shown.
  • the closure assembly 100 is configured to interact with a container coupling 25 attached to a respective wall of the cargo container 10.
  • the container coupling 25 is well known in the art and attached to the walls 22 of the conventional containers.
  • the couplings 25 include a mounting portion 30 attached to the wall 22 of the container 10 and a first loop 35 pivotally attached to and extending from the mounting portion 30 toward the open end of the container 10.
  • the mounting portion 30 may be made from fabric or metal, and first loop 35 may be constructed from metal such as steel or aluminum.
  • the closure assembly 100 includes a pocket 110 formed on the fabric door 50,
  • the pocket 110 may be formed by a fabric patch 115, also preferably formed of high strength yarns such as ultra-high molecular weight polyethylene and the like,
  • the fabric patch 115 has an outer surface 120 and an inner surface 125.
  • the patch 115 may have three sections; a top section 130, a middle section 135 and a lower section 140 (see Fig. 5).
  • the top section 130 and the bottom section 140 are fixedly attached to the fabric door 50.
  • the top 130 and bottom sections 140 are sewn onto the fabric door 50 with high strength yarn.
  • the stitching that attaches the top 130 and bottom 140 of patch 115 to the fabric door 50 will run the width of the patch 115 and extend beyond the lateral edges of the patch 115 to securely hold the edges to the door 50. This overlap minimizes the risk of the edges being separated from the door 50.
  • any substantially permanent method may be used to attach the top and bottom sections 130, 140 of the patch 115 to the door 50,
  • the middle section 135 of the patch 115 is spaced from, and not directly attached to the surface of the fabric door 50.
  • the attachment of the top and bottom portions 130, 140 should provide the ability for the middle section 135 to separate slightly from the surface of the fabric door 50. This separation forms a passage below middle section 135 from one side of the patch 115 to the other for passage of strap 300.
  • the middle section 135 will preferably have a width of about 2,5 inches.
  • Each section 130, 135, 140 of the patch 115 may have substantially the same width.
  • the width of the top 130 and bottom 140 sections may be increased or decreased as necessary to provide an attachment area that is sufficient to securely hold the patch 115 to the face of fabric door 50.
  • the middle section 135 of the patch 115 preferably includes a first piece of a hook and loop fastener 145 on the outer surface 120 thereof and a second piece of a hook and loop fastener 150 on the inner surface 125 thereof.
  • Example hook and loop fasteners include Velcro® and DualLock ⁇ .
  • hook and loop fasteners are formed by the joining of two mating surfaces.
  • one mating surface may comprise hooks and the other mating surface may comprise loops.
  • a "piece" of hook and loop fastener refers to one of the first and second mating surfaces. In the case where the mating surfaces are different, the selection of the mating surface will be determined such that when in use, each piece mates with an opposite type surface.
  • the longitudinal axis A of the patch 115 should be substantially normal to the pivot axis B of the first loop 35 of the coupling 25.
  • the longitudinal axis A will be normal to the edge of the fabric door 50 so that the door 50 can be retrofit on a container 10 that previously held the prior art door 2.
  • the closure assemblies 100 of the present invention no long require the couplings 25 to be directly opposite and aligned with one another. Therefore first loops 35 may be designed with pivot axes B that are not aligned with the respective edge of the container 10. This can be advantageous in that the connection assembly 100 will provide a force along the longitudinal axis A thereof. Where this axis A deviates from true horizontal or vertical, the closure assembly 100 will be able to provide a tensioning force in two directions at once.
  • the closure assembly 100 can optionally include a connection member 160.
  • the connection member 160 includes a fixing portion 165 to fix the connection member 160 to the fabric door 50.
  • the fixing portion 165 is made from fabric, particularly a fabric having high strength yarns.
  • the fixing portion 165 can be sewn onto the fabric door 50 using high strength yarns.
  • the connection member 160 further includes a second loop 170.
  • the second loop 170 is attached to the fixing portion 165 such that the second loop 170 can pivot relative to the fixing portion 165.
  • the connection member 160 is to be disposed adjacent to the inward end of pocket 110. Particularly, the second loop 170 should be aligned with the middle section 135 of patch 115'.
  • the pivot axis of the second loop 170 should be parallel to the pivot axis of the first loop 35 and perpendicular to the longitudinal axis of patch 115'.
  • the major tension on the fabric of the door 50 is taken up by patch on fixing portion 165. Therefore, as shown in Fig. 6, if the closure assembly 100 includes connection member 160, the patch 115' can have top and bottom portions 130, 140 with reduced width as compared to the patch 115 of Fig. 4.
  • the addition of the connection member 160 adds strength to the closure assembly 100 that would otherwise require a more robust connection between the patch 115 of Fig. 4 and the fabric door 50.
  • the closure assembly 100 further includes a strap 300 for forming a connection between the pocket 110 and the coupling 25.
  • the strap 300 includes a bottom surface 305 and a top surface 310.
  • the strap 300 further includes an inward portion 315, a middle portion 320 and an outward portion 325.
  • the inward 315 and outward 325 portions are defined relative to the fabric door 50.
  • Each portion 315, 320, 325 of the strap 300 should be slightly longer than the length of the patch 115.
  • the bottom surface 305 of the strap 300 includes third 330 and fourth 335 pieces of a hook and loop fastener connected to the inward 315 and outward 325 portions of the strap 300 respectively.
  • the strap 300 includes a fifth piece 340 of a hook and loop fastener connected to the middle portion 320 of the strap 300 also on the bottom surface 305 thereof.
  • the fifth piece of hook and loop fastener 340 has a high visibility color.
  • the high visibility color can be yellow or orange
  • the fifth piece of hook and loop fastener 340 may simply be a color distinct from the color of the strap 300 and the remainder of the other pieces of fastener. Since hook and loop fasteners are most readily available with both mating surfaces of the same color, it is possible to have the second piece 150 also comprise the distinct or high visibility color. Because the second piece 150 is entirely disposed on the inside surface 125 of patch 115, the color of the second piece 150 will not be visible to distract the repair worker.
  • the strap 300 includes a sixth hook and loop portion 345 aligned with the outward portion 325 on the top surface 310 thereof.
  • the connection system includes a tool 400 (see Fig. 8) that can be disposed between the strap 300 and the patch 115 to facilitate insertion of the strap 300 through the pocket 110.
  • the strap 300 is slid into and through the pocket 110 until the middle portion 320 of the strap 300 is completely covered by the middle section 135 of the patch 115.
  • the tool 400 can also be used to aid in the separation of the hooks and loops on fifth piece 340 on strap 300 from the second piece 150 on the rear surface 125 of the middle section 135 of patch 115. In this regard, the tool 400 is wedged between the hooks of one piece and the loops of the other.
  • the high visibility or distinct coloration of the fifth piece of hook and loop fastener 340 provides the repair worker an important indication of when the strap 300 is properly installed.
  • the high visibility of the fifth piece 340 will quickly and easily cue the worker when the strap 300 needs to be inserted further or when the strap 300 has been inserted too far.
  • the worker will know the strap 300 is properly positioned.
  • the strap 300 will assume a folded position that maximizes the connection area between hook and loop fastener portions.
  • the fifth hook and loop fastener 340 will mate with the second hook and loop fastener 150 on the inside surface 125 of the middle section 135. This mated connection will secure the strap 300 to the fabric door 50 with or without the door 50 installed on the open side of the cargo container 10.
  • the outward portion 325 of the strap 300 is inserted through the first loop 35 of the coupling 25.
  • the outward portion 325 is than folded in an inward direction.
  • the fourth hook and loop portion 335 thereon will then be mated with the first hook and loop portion 145 on the outer surface 120 of the middle portion 135 of the patch 115.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Packages (AREA)
PCT/US2013/021132 2012-01-12 2013-01-11 Liaison facilement amovible et remplaçable pour portes de conteneurs de fret aérien Ceased WO2013106640A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261585957P 2012-01-12 2012-01-12
US61/585,957 2012-01-12

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WO2013106640A1 true WO2013106640A1 (fr) 2013-07-18

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PCT/US2013/021132 Ceased WO2013106640A1 (fr) 2012-01-12 2013-01-11 Liaison facilement amovible et remplaçable pour portes de conteneurs de fret aérien

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2524839A (en) * 2014-04-04 2015-10-07 Whi Safeguard Ltd A skip corner protector
WO2016128944A1 (fr) * 2015-02-13 2016-08-18 Driessen Aerospace Group N.V. Systèmes de fermeture de conteneurs de fret
WO2017037580A1 (fr) * 2015-08-28 2017-03-09 Driessen Aerospace Group N.V. Mécanisme de fermeture de porte de conteneur de fret et procédé
EP3546391A1 (fr) 2018-03-29 2019-10-02 Advanced Composite Structures, LLC Porte de conteneur de fret aérien en tissu, conteneur et méthode avec une telle porte
US11851270B2 (en) 2017-10-10 2023-12-26 Advanced Composite Structures, Llc Latch for air cargo container doors
US11981498B2 (en) 2019-06-28 2024-05-14 Advanced Composite Structures, Llc Thermally insulated air cargo container
CN118439279A (zh) * 2024-06-06 2024-08-06 无锡市航空地面设备有限公司 一种可视化联运集装箱
US12091239B2 (en) 2021-11-11 2024-09-17 Advanced Composite Structures, Llc Formed structural panel with open core

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6755232B1 (en) * 2000-06-26 2004-06-29 Jhrg, Llc Fabric closure for open-end cargo containers
US20110057002A1 (en) * 2009-09-08 2011-03-10 Luke Westra Apparatus for holding objects and methods of using and making the same
GB2479611A (en) * 2010-02-04 2011-10-19 Janette Russell-Rayner Container attachable on the body using detachable straps

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6755232B1 (en) * 2000-06-26 2004-06-29 Jhrg, Llc Fabric closure for open-end cargo containers
US20110057002A1 (en) * 2009-09-08 2011-03-10 Luke Westra Apparatus for holding objects and methods of using and making the same
GB2479611A (en) * 2010-02-04 2011-10-19 Janette Russell-Rayner Container attachable on the body using detachable straps

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2524839A (en) * 2014-04-04 2015-10-07 Whi Safeguard Ltd A skip corner protector
CN107207154A (zh) * 2015-02-13 2017-09-26 戴森航空宇宙集团有限公司 货物集装箱封闭系统
WO2016128944A1 (fr) * 2015-02-13 2016-08-18 Driessen Aerospace Group N.V. Systèmes de fermeture de conteneurs de fret
CN108137223B (zh) * 2015-08-28 2020-08-14 赛峰座舱荷兰有限公司 货物集装箱门封闭机构、方法
CN108137223A (zh) * 2015-08-28 2018-06-08 戴森航空宇宙集团有限公司 货物集装箱门封闭机构、方法
US10059511B2 (en) 2015-08-28 2018-08-28 Driessen Aerospace Group N.V. Cargo container door closure mechanism
TWI680926B (zh) * 2015-08-28 2020-01-01 荷蘭商賽峰機艙荷蘭公司 貨物容器門封閉機構
WO2017037580A1 (fr) * 2015-08-28 2017-03-09 Driessen Aerospace Group N.V. Mécanisme de fermeture de porte de conteneur de fret et procédé
US11851270B2 (en) 2017-10-10 2023-12-26 Advanced Composite Structures, Llc Latch for air cargo container doors
EP3546391A1 (fr) 2018-03-29 2019-10-02 Advanced Composite Structures, LLC Porte de conteneur de fret aérien en tissu, conteneur et méthode avec une telle porte
CN110316483A (zh) * 2018-03-29 2019-10-11 高等复合结构有限责任公司 具有改进的紧固系统的织物空运货物集装箱门
US10894661B2 (en) 2018-03-29 2021-01-19 Advanced Composite Structures, Llc Fabric air cargo container doors having improved fastening system
US11981498B2 (en) 2019-06-28 2024-05-14 Advanced Composite Structures, Llc Thermally insulated air cargo container
US12091239B2 (en) 2021-11-11 2024-09-17 Advanced Composite Structures, Llc Formed structural panel with open core
CN118439279A (zh) * 2024-06-06 2024-08-06 无锡市航空地面设备有限公司 一种可视化联运集装箱

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