GB309110A - Improvements in or relating to light metal structures - Google Patents
Improvements in or relating to light metal structuresInfo
- Publication number
- GB309110A GB309110A GB198/28A GB19828A GB309110A GB 309110 A GB309110 A GB 309110A GB 198/28 A GB198/28 A GB 198/28A GB 19828 A GB19828 A GB 19828A GB 309110 A GB309110 A GB 309110A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flanges
- secured
- members
- boom
- bracing
- 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 3
- 241000269319 Squalius cephalus Species 0.000 abstract 1
- 230000001788 irregular Effects 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000000284 resting effect 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
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Joining Of Building Structures In Genera (AREA)
Abstract
309,110. Bristol Aeroplane Co., Ltd., and Pollard, H. J. Jan. 3, 1328. Framework.-Aircraft wings, fuselages, and other light structures comprising tubular members built up from two or more metal strips with out-turned flanges and continuous from and to end of the member, have gusset plates secured to adjoining flanges on the tubular members and bracing members are secured to the gusset plates so that the line of action of each member of the structure passes through the centroid of that member. The tubular members are formed from two, three, or four metal strips extending the whole length of the member, as described in Specification 264,626. Figs. 7 and 8 show a joint for a fuselage wherein a. gusset plate 34 is secured between the flanges of a tubular boom 23 and also between the. flanges of two tubular bracing members 37, 42. A bracing member 41 is similarly secured to the boom 33. A plate 44 having bent flanges 45, 46 is secured to the: flanges of the members 37, 41 and the flanges of a diagonal member 43 are secured thereto on opposite sides. Alternatively, the flanges of the boom may be embraced by pairs of gusset plates secured between the flanges of the bracing members. Fig. 15 shows a modification in which two bracing members 81, 82 are secured to a single gusset plate having a bent portion 84 resting against the boom 83. The ends of the bracing members may be reinforced internally or externally by sleeves, or by flat plates butted against the edges of the gusset plates and riveted between the flanges. For building up irregular outlines, the gusset plates or the flanges of the boom may be bent into the plane of the bracing member. Specification 24948/96, [Class 20, Buildings &c.], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB198/28A GB309110A (en) | 1928-01-03 | 1928-01-03 | Improvements in or relating to light metal structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB198/28A GB309110A (en) | 1928-01-03 | 1928-01-03 | Improvements in or relating to light metal structures |
Publications (1)
Publication Number | Publication Date |
---|---|
GB309110A true GB309110A (en) | 1929-04-03 |
Family
ID=9700141
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB198/28A Expired GB309110A (en) | 1928-01-03 | 1928-01-03 | Improvements in or relating to light metal structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB309110A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3563580A (en) * | 1967-10-16 | 1971-02-16 | Anthony Frederick Black | Frame joint |
GB2585474A (en) * | 2019-05-23 | 2021-01-13 | Bae Systems Plc | A method and apparatus for producing at least part of a structural frame of a vehicle |
US11338939B2 (en) | 2018-06-28 | 2022-05-24 | Bae Systems Plc | Method and apparatus for producing at least part of an aircraft airframe |
-
1928
- 1928-01-03 GB GB198/28A patent/GB309110A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3563580A (en) * | 1967-10-16 | 1971-02-16 | Anthony Frederick Black | Frame joint |
US11338939B2 (en) | 2018-06-28 | 2022-05-24 | Bae Systems Plc | Method and apparatus for producing at least part of an aircraft airframe |
US11401050B2 (en) | 2018-06-28 | 2022-08-02 | Bae Systems Plc | Method and apparatus for assembling aircraft airframes |
US11851212B2 (en) | 2018-06-28 | 2023-12-26 | Bae Systems Plc | Method and apparatus for producing component parts of aircraft airframes |
US11970289B2 (en) | 2018-06-28 | 2024-04-30 | Bae Systems Plc | Method and apparatus for producing shims |
GB2585474A (en) * | 2019-05-23 | 2021-01-13 | Bae Systems Plc | A method and apparatus for producing at least part of a structural frame of a vehicle |
GB2585474B (en) * | 2019-05-23 | 2022-02-16 | Bae Systems Plc | A method and apparatus for producing at least part of a structural frame of a vehicle |
US11731788B2 (en) | 2019-05-23 | 2023-08-22 | Bae Systems Plc | Method and apparatus for producing at least part of a structural frame of a vehicle |
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