WO1991015681A1 - Dispositifs de liaison ameliores - Google Patents
Dispositifs de liaison ameliores Download PDFInfo
- Publication number
- WO1991015681A1 WO1991015681A1 PCT/GB1991/000544 GB9100544W WO9115681A1 WO 1991015681 A1 WO1991015681 A1 WO 1991015681A1 GB 9100544 W GB9100544 W GB 9100544W WO 9115681 A1 WO9115681 A1 WO 9115681A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- sections
- locking rib
- wedge portion
- wall
- end portions
- Prior art date
Links
- 239000003566 sealing material Substances 0.000 claims description 5
- 238000010276 construction Methods 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 description 4
- 238000007789 sealing Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000013521 mastic Substances 0.000 description 2
- 239000000565 sealant Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000012812 sealant material Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/10—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of bayonet connections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS 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
- B65D53/00—Sealing or packing elements; Sealings formed by liquid or plastics material
- B65D53/06—Sealings formed by liquid or plastic material
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/0004—Joining sheets, plates or panels in abutting relationship
- F16B5/0032—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates, or panels or the interlocking key parallel to the abutting edge
- F16B5/004—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates, or panels or the interlocking key parallel to the abutting edge and using C-shaped clamps
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B3/00—Key-type connections; Keys
Definitions
- sectional panel tanks are made usually in steel using flanged joints with a sealant and requiring many bolts. They are expensive to manufacture and install and suffer from several disadvantages namely, they are prone to leakage at the joint, they suffer from corrosion even when coated with glass, epoxy, etc. due to damage and wear, and have a limited life span.
- a connecting structure of two sections of a wall of a member wherein integral portions at the ends of each of the two sections are positioned adjacent one another and together define the wedge portion of a dovetail joint, and a locking rib which defines the groove portion of the dovetail joint is positioned over that wedge portion to lock the two sections together, the end portions of the sections and the wedge portion being located in a recess or within the curve of the inner wall of the structure so as to define a relatively smooth continuation of the walls of the sections across the connecting structure.
- the dovetail joint when the parts are connected together, creates a very secure connection and provides the possibility that the jointed areas between the parts of the joint can be filled with a sealing material.
- this sealing material will be situated in the region between the facing end portions of the sections.
- a compression member can readily be provided in that region.
- sealing material may be situated in the space between the abutting walls of the wedge portion and the locking rib of the dovetail joint. It is also possible for sealing material to be formed over the joint areas of the dovetail joint.
- a single piece locking rib can be slid or snapped over the wedge portion of the dovetail joint.
- the locking rib might be formed in two halves with temporary or permanent securing means holding them together.
- a further preferred possibility is for the end portions to be held in tight relationship within the locking rib by a locking wedge driven between the two portions after the locking rib is located over the end portions.
- Figures 6 and 7 are sections through a further type of connecting structure of the invention as shown in two stages of construction.
- the basic form of connecting structure shown in Figure 1 is used to interconnect two sections 1 and 2 of a wall. Respective enlargements 3 and 4 are created which between them define a wedge portion 5 of a dovetail joint. Comple ⁇ mentary nesting formations 6 help to locate the two parts 3 and 4 together.
- a locking rib 7 is slid over the wedge portion 5 so as to hold the two parts 3 and 4 together. This locking rib fits closely against the adjacent wall surfaces of the parts 3 and 4 of the wall sections 1 and 2 and in turn helps to define a smooth wall surface 8 which is contiguous with the walls 1 and 2, the connecting structure effectively being situated within a recessed portion of the inner wall.
- a sealant material will be introduced into the spaces of the connecting structure, such as in the regions 9. The sealant can be a mastic or resin introduced into the joint during assembly or injected after assembly.
- FIG. 2 shows how the locking rib 7 may be formed in two halves 7A and 7B which each incorporate a projecting flange 12. The flanges 12 are fixed together by securing bolts 13. This enables the locking rib to be located in position on to the wedge portion 5 relatively easily and indeed allows the connecting structure to be disassembled if required by removing the bolts 13.
- the wall sections 1 and 2 are curved and the connecting structure comprising the enlargements 3 and 4 and the wedge portion 5 are located within the inner curve of the wall of the member so that a relatively smooth inner surface is achieved.
- the curvature of the outer face of the member is maintained in this design so that a smooth wound sealing overlay can be applied to the outer wall surface.
- the structure illustrated in Figures 6 and 7 is so formed that the ends of the enlargements 3 and 4 can be butted together to define a wedge portion of a width which enables the locking rib 7 to be placed over the wedge from the side as shown in Figure 6.
- the enlargements 3 and 4 are then forced apart so that they enter the grooves in the rib 7 to form a tight joint, and are locked in place by a locking piece 14 which can be held there by a suitable mastic.
- This form of connecting system enables the construction of large tanks or the like from smaller or more compact initial components.
- large tanks can be formed from circumferential sections which are linked together at vertical joints.
- the sections could be ready-shaped (for example curved) or flexible so that they can be bent into the required shape.
- a flexible cylindrical section could be closed into a tight spiral (held by strapping) for transportation, then opened out on site to full size for fixing in position.
- Such tanks can also be built up vertically in sections with horizontal joints.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
Structure de liaison reliant les deux sections (1 et 2) d'une paroi. Des agrandissements respectifs (3 et 4) définissent entre elles le coin (5) d'un joint en queue d'aronde. Une nervure de blocage (7) se glisse sur le coin (5) pour maintenir en contact les deux parties (3 et 4). Cette nervure de blocage se fixe étroitement contre les surfaces de paroi contiguës des parties (3 et 4) des sections de paroi (1 et 2) et, à son tour, contribue à définir une surface de paroi lisse (8), contiguë aux parois (1 et 2), la structure de liaison étant effectivement située dans une partie creuse de la paroi intérieure.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9007827.0 | 1990-04-06 | ||
GB909007827A GB9007827D0 (en) | 1990-04-06 | 1990-04-06 | Improvements relating to connecting arrangements |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1991015681A1 true WO1991015681A1 (fr) | 1991-10-17 |
Family
ID=10674010
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB1991/000544 WO1991015681A1 (fr) | 1990-04-06 | 1991-04-08 | Dispositifs de liaison ameliores |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU7650891A (fr) |
GB (1) | GB9007827D0 (fr) |
WO (1) | WO1991015681A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2348260A (en) * | 1999-03-25 | 2000-09-27 | David Paul Aviram | Interlocking panels |
WO2003072956A2 (fr) * | 2002-02-25 | 2003-09-04 | Rubbermaid Incorporated | Appareil et procede de panneaux adjacents |
US7091817B2 (en) | 2001-09-28 | 2006-08-15 | Delta Energy Systems (Switzerland) Ag | Planar transformer comprising plug-in secondary windings |
GB2439743A (en) * | 2006-07-01 | 2008-01-09 | Barry David Palmer | Wedged joint |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AUPO927397A0 (en) * | 1997-09-19 | 1997-10-09 | Gro-Guard Australia Pty Ltd | Improvements in and relating to tubular plant guards |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405643A (en) * | 1944-02-07 | 1946-08-13 | Lockheed Aircraft Corp | Structural connector |
US3594028A (en) * | 1969-08-07 | 1971-07-20 | Macomber Inc | Sheet metal joint for panels and sheets |
EP0342662A1 (fr) * | 1988-05-20 | 1989-11-23 | Tefo Ag | Dispositif pour assembler des éléments de grilles décoratives |
EP0358930A1 (fr) * | 1988-09-16 | 1990-03-21 | Peter Schmitz | Panneau de construction léger composé de modules plats |
-
1990
- 1990-04-06 GB GB909007827A patent/GB9007827D0/en active Pending
-
1991
- 1991-04-08 WO PCT/GB1991/000544 patent/WO1991015681A1/fr unknown
- 1991-04-08 AU AU76508/91A patent/AU7650891A/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405643A (en) * | 1944-02-07 | 1946-08-13 | Lockheed Aircraft Corp | Structural connector |
US3594028A (en) * | 1969-08-07 | 1971-07-20 | Macomber Inc | Sheet metal joint for panels and sheets |
EP0342662A1 (fr) * | 1988-05-20 | 1989-11-23 | Tefo Ag | Dispositif pour assembler des éléments de grilles décoratives |
EP0358930A1 (fr) * | 1988-09-16 | 1990-03-21 | Peter Schmitz | Panneau de construction léger composé de modules plats |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2348260A (en) * | 1999-03-25 | 2000-09-27 | David Paul Aviram | Interlocking panels |
US6668514B2 (en) | 2001-05-18 | 2003-12-30 | Rubbermaid Incorporated | Apparatus and method for connecting adjacent panels |
US7091817B2 (en) | 2001-09-28 | 2006-08-15 | Delta Energy Systems (Switzerland) Ag | Planar transformer comprising plug-in secondary windings |
WO2003072956A2 (fr) * | 2002-02-25 | 2003-09-04 | Rubbermaid Incorporated | Appareil et procede de panneaux adjacents |
WO2003072956A3 (fr) * | 2002-02-25 | 2003-11-13 | Rubbermaid Inc | Appareil et procede de panneaux adjacents |
GB2439743A (en) * | 2006-07-01 | 2008-01-09 | Barry David Palmer | Wedged joint |
GB2439743B (en) * | 2006-07-01 | 2008-05-21 | Barry David Palmer | Jigsaw coupling/de coupling system |
Also Published As
Publication number | Publication date |
---|---|
GB9007827D0 (en) | 1990-06-06 |
AU7650891A (en) | 1991-10-30 |
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