GB893676A - Lap jointed structures - Google Patents

Lap jointed structures

Info

Publication number
GB893676A
GB893676A GB2423858A GB2423858A GB893676A GB 893676 A GB893676 A GB 893676A GB 2423858 A GB2423858 A GB 2423858A GB 2423858 A GB2423858 A GB 2423858A GB 893676 A GB893676 A GB 893676A
Authority
GB
United Kingdom
Prior art keywords
cloth
resin
panels
assembly
sheet metal
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.)
Expired
Application number
GB2423858A
Inventor
John Rees
William Andrew Baker
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.)
Rolls Royce Composite Materials Ltd
Original Assignee
Bristol Aeroplane Plastics Ltd
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 Bristol Aeroplane Plastics Ltd filed Critical Bristol Aeroplane Plastics Ltd
Priority to GB2423858A priority Critical patent/GB893676A/en
Publication of GB893676A publication Critical patent/GB893676A/en
Expired 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
    • F16B11/00Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing

Abstract

893,676. Making composite containers; jointing. BRISTOL AEROPLANE PLASTICS Ltd. Oct. 26, 1959 [July 28, 1958], No. 24238/58. Classes 83 (2) and 83 (4). A method of assembling a lap-jointed structure of sheet metal is characterized in that the sheet metal parts are held in assembled overlapping relation with a layer of pervious material between the opposed faces of the lap joint and a settable free-flowing liquid binder capable of adhering to the sheet metal parts is caused to flow into and to fill the interstices of the pervious material and to set. In an embodiment a container is made with overlapping joints according to the invention by providing flanged side panels 11 and 12 and joggled side panels 13 and 14 (Fig. 2). The bottom of the container is formed from an upwardly flanged panel 15 (Fig. 1). The panels are covered with a cloth coating 16 composed of e.g. acrylic or polyamide fibre bonded with an epoxy resin or glass fibre or jute bonded with a polyester resin. The panels and their cloth coverings are assembled in a collapsible mould 18, the bottom 17 of which is provided with an opening 19 through which the resin binder is supplied. A flexible bag 21 of rubber or polythene filled with liquid or granular material is used to keep the panels in place. Resin binder is also supplied through a pipe 22 leading to the bottom of the bag. When the resin has had time to seep through the cloth coverings and emerges at the top edge of the mould, the resin supply is shut off and the setting is accelerated by warming the assembly. Alternatively, the impregnation of the cloth may be effected by suction in which case no filling material is required in the bag. In a joint between two double walls (Fig. 3), each wall consists of metal sheets 24 and 26 separated by a pervious insulating material 28 enclosed in an impervious skin 30 of hardened resin impregnated cloth. The metal sheets are covered on both faces with cloth 32 as hitherto and a piece of cloth 34 is inserted in the joint between the insulating material. After assembly the cloth 32 and 34 is impregnated with resin which is then caused or allowed to set. In another embodiment the cloth 26 is confined to the overlapping joints of the assembly as shown in Fig. 4 and the side edges of the joints are sealed by adhesive tapes 27 and 28.
GB2423858A 1958-07-28 1958-07-28 Lap jointed structures Expired GB893676A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2423858A GB893676A (en) 1958-07-28 1958-07-28 Lap jointed structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2423858A GB893676A (en) 1958-07-28 1958-07-28 Lap jointed structures

Publications (1)

Publication Number Publication Date
GB893676A true GB893676A (en) 1962-04-11

Family

ID=10208597

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2423858A Expired GB893676A (en) 1958-07-28 1958-07-28 Lap jointed structures

Country Status (1)

Country Link
GB (1) GB893676A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003039851A1 (en) * 2001-11-09 2003-05-15 Bae Systems Plc Manufacture and assembly of structures

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003039851A1 (en) * 2001-11-09 2003-05-15 Bae Systems Plc Manufacture and assembly of structures
US7776769B2 (en) 2001-11-09 2010-08-17 Bae Systems Plc Manufacture and assembly of structures
US7867929B2 (en) 2001-11-09 2011-01-11 Bae Systems Plc Manufacture and assembly of structures

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