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GB2393207A - Circlip connector - Google Patents

Circlip connector Download PDF

Info

Publication number
GB2393207A
GB2393207A GB0222015A GB0222015A GB2393207A GB 2393207 A GB2393207 A GB 2393207A GB 0222015 A GB0222015 A GB 0222015A GB 0222015 A GB0222015 A GB 0222015A GB 2393207 A GB2393207 A GB 2393207A
Authority
GB
United Kingdom
Prior art keywords
circlip
projecting arms
machined
flexible
reconfigured
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
Application number
GB0222015A
Other versions
GB2393207B (en
GB0222015D0 (en
Inventor
Miles Roland William Bozeat
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB0222015A priority Critical patent/GB2393207B/en
Publication of GB0222015D0 publication Critical patent/GB0222015D0/en
Publication of GB2393207A publication Critical patent/GB2393207A/en
Application granted granted Critical
Publication of GB2393207B publication Critical patent/GB2393207B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/06Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips
    • F16B5/0607Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other
    • F16B5/0614Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other in angled relationship
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B12/00Jointing of furniture or the like, e.g. hidden from exterior
    • F16B12/10Jointing of furniture or the like, e.g. hidden from exterior using pegs, bolts, tenons, clamps, clips, or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Clamps And Clips (AREA)

Abstract

A connector assembly comprises a flexible circlip 1 with lugs [2, Figure 1] formed on either arm [5, Figure 1]; and a tapered key piece 8. The circlip 1 is located and held in use, within a shaped recess [3, Figure 3] formed in a surface of a first panel [4, Figure 3] such that the arms protrude from the recess so that they may pass through and engage an aperture 6 provided in a second panel 7. The lugs on the arms overlap the edge of the aperture. The tapered key 8 is then inserted into the space between the arms 5 locking the arms 5 and the lugs so that they cannot be removed from the aperture 6. The circlip is preferably made from a semi-rigid thermoplastic.

Description

MEANS OF ASSEMBLY - BOZZ 2
This invention relates to a means of right angle assembly between two solid plane surfaces.
Quick assembly or " Knock down "assembly systems are well known and popular means for erecting furniture and other structures. Most such systems require the use of tools in the assembly process and require a degree of skill and judgement on the part of the operative.
It is to the above that the present invention provides a resolution.
According to the present invention there is provided a means of assembly wherein a flexible circlip is configured with lugs facilitating location in a preconfigured and / or machined receptacle set into the edge of one of the solid planes to be joined the said flexible circlip is provided with projecting arms at the ends of the "C" which allow the said flexible circlip to have its overall size temporarily reduced by the operator manually squeezing the said projecting arms together so to allow the said flexible circlip to be located in the said preconfigured and / or machined receptacle then to allow the said projecting arms to be released such that the said flexible circle regains its original shape within the said preconfigured and / or machined receptacle and consequently the said flexible circlip is securely located within the said preconfigured and / or machined receptacle the said projecting arms of the said flexible circlip are passed through a preconfigured and / or machined slot in the second of the solid planes to be joined "hereafter the said projecting arms are driven apart by the introduction of a tapered key piece between the two said projecting
arms whereupon locking lugs configured onto the ends of the said projecting arms overlap the ends of the said preconfigured and / or machined slot in the second of the solid planes so to lock the assembly together.
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawings in which: Figures I, 2, 3, 4, 5, 6, 7, 8, 9 show the assembly sequence in both perspective and plan.
Referring to the drawings the means of assembly comprises a flexible circlip I [ preferably manufactured in a semi rigid thermoplastic acetal resin or similar] configured with lugs 2, Fig I facilitating location in a mating preconfigured and / or machined receptacle 3 set into the edge of one of the solid planes 4 to be joined, Fig 3 the said flexible circlip I is provided with projecting arms 5 at the ends of the defining "C"shape which allow the said flexible circlip I to have its overall size temporarily reduced by the operator manually squeezing the said projecting arms 5 together, Fig2 so to allow the said flexible circlip I to be located in the said preconfigured and / or machined receptacle 3, Fig 4 then to allow the said projecting arms 5 to be released such that the said flexible circlip I regains its original shape within the said preconfigured and / or machined receptacle 3 and consequently the said flexible circlip I is securely located within the said preconfigured and / or machined receptacle 3, Fig 5 the said projecting arms 5 of the said flexible circlip I are passed through a preconfigured and / or machined slot 6 in the second of the solid planes 7 to be joined, Fig 6 where after the said projecting arms 5 are driven apart by the introduction of a
tapered key piece 8 [ preferably manufactured in a semi rigid thermoplastic acetal resin or similar] between the two said projecting arms 5, Fig 7 whereupon locking lugs 9 configured onto the ends of the said projecting arms 5 overlap the ends 10 of the said preconfigured and / or machined slot 6 in the second of the solid planes 7 so to lock the assembly together, Figs 8, 9.

Claims (2)

1 A means by which two solid plane surfaces are assembled together wherein a flexible circlip [ preferably manufactured in a semi rigid thermoplastic acetal resin or similar] is configured with lugs facilitating location in a mating preconfigured and / or machined receptacle set into the edge of one of the solid planes to be joined the said flexible circlip is provided with projecting arms at the ends of the defining "C"shape which allow the said flexible circlip to have its overall size temporarily reduced by the operator manually squeezing the said projecting arms together so to allow the said flexible circlip to be located in the said Reconfigured and / or machined receptacle then to allow the said projecting arms to be released such that the said flexible circlip regains its original shape within the said Reconfigured and / or machined receptacle consequently the said flexible circlip is securely located within the said Reconfigured and / or machined receptacle the said projecting arms of the said flexible circlip are passed through a Reconfigured and / or machined slot in the second of the solid planes to be joined "hereafter the said projecting arms are driven apart by the introduction of a tapered key piece [ preferably
manufactured in a semi rigid thermoplastic acetal resin or similar] between the two said projecting arms whereupon locking lugs configured onto the ends of the said projecting arms overlap the ends of the said Reconfigured and / or machined slot in the second of the solid planes so to lock the assembly together.
2 A claim as in claim I wherein the circlip and / or the key piece retain their functionality but have an aesthetically varied shape
GB0222015A 2002-09-21 2002-09-21 Means of assembly Expired - Fee Related GB2393207B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0222015A GB2393207B (en) 2002-09-21 2002-09-21 Means of assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0222015A GB2393207B (en) 2002-09-21 2002-09-21 Means of assembly

Publications (3)

Publication Number Publication Date
GB0222015D0 GB0222015D0 (en) 2002-10-30
GB2393207A true GB2393207A (en) 2004-03-24
GB2393207B GB2393207B (en) 2006-04-12

Family

ID=9944574

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0222015A Expired - Fee Related GB2393207B (en) 2002-09-21 2002-09-21 Means of assembly

Country Status (1)

Country Link
GB (1) GB2393207B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10384758B2 (en) * 2016-01-26 2019-08-20 The Boeing Company Sandwich panel assembly and method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2546526A1 (en) * 1975-10-17 1977-04-28 Heinze Fa R Connector for panels at right angles - has dowel with central spike core held by screw and projecting into dowel hole
GB1508916A (en) * 1975-08-22 1978-04-26 Brown Ltd F Connectors for cabinets
US4693630A (en) * 1983-10-18 1987-09-15 Laura Giovannetti Fastening device for releasable interconnection of panels
DE29800379U1 (en) * 1997-01-13 1998-05-07 Joh. Vaillant Gmbh U. Co, 42859 Remscheid Fastener

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1508916A (en) * 1975-08-22 1978-04-26 Brown Ltd F Connectors for cabinets
DE2546526A1 (en) * 1975-10-17 1977-04-28 Heinze Fa R Connector for panels at right angles - has dowel with central spike core held by screw and projecting into dowel hole
US4693630A (en) * 1983-10-18 1987-09-15 Laura Giovannetti Fastening device for releasable interconnection of panels
DE29800379U1 (en) * 1997-01-13 1998-05-07 Joh. Vaillant Gmbh U. Co, 42859 Remscheid Fastener

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10384758B2 (en) * 2016-01-26 2019-08-20 The Boeing Company Sandwich panel assembly and method

Also Published As

Publication number Publication date
GB2393207B (en) 2006-04-12
GB0222015D0 (en) 2002-10-30

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20170921