GB596278A - Improvements in or relating to metal skeleton structures - Google Patents
Improvements in or relating to metal skeleton structuresInfo
- Publication number
- GB596278A GB596278A GB1913245A GB1913245A GB596278A GB 596278 A GB596278 A GB 596278A GB 1913245 A GB1913245 A GB 1913245A GB 1913245 A GB1913245 A GB 1913245A GB 596278 A GB596278 A GB 596278A
- Authority
- GB
- United Kingdom
- Prior art keywords
- web
- primary
- flanges
- welded
- spot
- 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
Links
- 239000002184 metal Substances 0.000 title abstract 4
- 210000002356 Skeleton Anatomy 0.000 title 1
- 210000001503 Joints Anatomy 0.000 abstract 2
- 238000003466 welding Methods 0.000 abstract 2
- 230000023298 conjugation with cellular fusion Effects 0.000 abstract 1
- 230000013011 mating Effects 0.000 abstract 1
- 230000021037 unidirectional conjugation Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/08—Geodetic or other open-frame structures
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/18—Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
- E04B1/24—Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons the supporting parts consisting of metal
- E04B1/2403—Connection details of the elongated load-supporting parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
- Body Structure For Vehicles (AREA)
- Connection Of Plates (AREA)
Abstract
596,278. Metal framework joints. PRESSED STEEL CO., Ltd., and MORPHEW, L. R. July 26, 1945, No. 19132. [Class 20(ii)] [Also in Groups XXXII and XXXIII] Relates to the joints of metal framework, particularly applicable to the chassis frames of vehicles and also to aircraft and buildings, and consists in forming the metal in the web of a channel-sectioned main or primary member where it is to be joined to a secondary member with a conformation consisting of lugs, flanged holes, bulges &c., the secondary member being of channel, angle or closed cross - section, uniform throughout, and mating at its end with the conformation in the primary member. The members are secured together by welding or riveting so that the load at the joint is taken in shear. Numerous applications of the invention are described and shown, examples of which are as follows. As shown in Fig. 1, the primary member 11, a chassis frame side member with the channel opening facing outwards, has an inwardly directed bulge 13, 14 formed in its web. The secondary member 12 is also of channel section, and its web mates at 15 with the surface 14 of the bulge in the primary member, the surfaces being spot-welded together. The flanges of the member 12 also embrace the flanges of the member 11, and are joined to them by spot-welding. In the example shown in Fig. 7, the web of the primary member 11 is apertured and a flange or lug 32 thereby formed, to which the web of the secondary member 12 is spot-welded, the flanges of the member 12 being in this case enveloped by those of the member 11 and spot welded thereto. Figs. 9 and 10 show a hole in the web of the primary member 11, with a flange 33 to which the web of the secondary member 12 is spot-welded. The flanges 36 of the secondary member are enveloped by the flanges 37 of the primary member and welded thereto. The conformations in the primary members may be suitable for different sections of secondary members, for example a circular flanged hole 43, Fig. 14, may be formed for a semicylindrical secondary member 12. Additional components such as plates may be incorporated e.g. Fig. 14 shows in edge view a top panel 46 welded to the flanges 45 of the secondary member 12 and to the upper flange of the primary member 11.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB596278A true GB596278A (en) | 1947-12-31 |
Family
ID=1734462
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1913245A Expired GB596278A (en) | 1945-07-26 | Improvements in or relating to metal skeleton structures |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB596278A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2253455A (en) * | 1991-02-20 | 1992-09-09 | Michael Patrick Walsh | Method of joining fibreglass and aluminium components |
| GB2291080A (en) * | 1994-07-06 | 1996-01-17 | Ancon Clark Ltd | Joints,e.g.welded joints, subject to bending forces |
-
1945
- 1945-07-26 GB GB1913245A patent/GB596278A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2253455A (en) * | 1991-02-20 | 1992-09-09 | Michael Patrick Walsh | Method of joining fibreglass and aluminium components |
| GB2253455B (en) * | 1991-02-20 | 1994-08-31 | Michael Patrick Walsh | The joining of first and second members at least one of which is a fibreglass member |
| GB2291080A (en) * | 1994-07-06 | 1996-01-17 | Ancon Clark Ltd | Joints,e.g.welded joints, subject to bending forces |
| GB2291080B (en) * | 1994-07-06 | 1998-05-27 | Ancon Clark Ltd | "Assembly" |
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