GB292426A - Improvements in or relating to skeleton structures such as aircraft fuselages - Google Patents
Improvements in or relating to skeleton structures such as aircraft fuselagesInfo
- Publication number
- GB292426A GB292426A GB34879/27A GB3487927A GB292426A GB 292426 A GB292426 A GB 292426A GB 34879/27 A GB34879/27 A GB 34879/27A GB 3487927 A GB3487927 A GB 3487927A GB 292426 A GB292426 A GB 292426A
- Authority
- GB
- United Kingdom
- Prior art keywords
- longeron
- bracing members
- plates
- clamping plates
- bolt
- 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
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)
- Pivots And Pivotal Connections (AREA)
- Clamps And Clips (AREA)
Abstract
292,426. Sigrist, F., Camm, S., and Hawker Engineering Co., Ltd., H. G. March 31, 1927. Divided on 286,482. Framcwork.-In fuselages and like tubular framework comprising one or more bracing members 2 the ends of which abut against an intermediate portion of a longeron 1, the joint is made by means of a clamping plate 3 or a pair of clamping plates bolted or riveted to the bracing members and bolted to the longeron. The head of the bolt 6 through the longeron is formed as a ball or socket to cooperate with the end of a transverse bracing member 11. The clamping plates may be flat instead of curved as shown at 3<a>. Instead of a pair of plates, a U-shaped plate astride the longeron may be used. The bracing members may be expanded at their ends or flattened to an oval section to make their effective diameter equal to that of the longeron. Where this is not done, the clamping plates are shaped as shown in Fig. 8 and a distance piece 14 is provided. The ends of the bracing members may be cut to conform to the shape of the longeron or to a V-shape. The wiring plates are held by the head of the bolt 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB34879/27A GB292426A (en) | 1927-03-31 | 1927-03-31 | Improvements in or relating to skeleton structures such as aircraft fuselages |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB34879/27A GB292426A (en) | 1927-03-31 | 1927-03-31 | Improvements in or relating to skeleton structures such as aircraft fuselages |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB292426A true GB292426A (en) | 1928-06-21 |
Family
ID=10371037
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB34879/27A Expired GB292426A (en) | 1927-03-31 | 1927-03-31 | Improvements in or relating to skeleton structures such as aircraft fuselages |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB292426A (en) |
-
1927
- 1927-03-31 GB GB34879/27A patent/GB292426A/en not_active Expired
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