GB245408A - Improvements in or relating to aeroplanes - Google Patents
Improvements in or relating to aeroplanesInfo
- Publication number
- GB245408A GB245408A GB13426/25A GB1342625A GB245408A GB 245408 A GB245408 A GB 245408A GB 13426/25 A GB13426/25 A GB 13426/25A GB 1342625 A GB1342625 A GB 1342625A GB 245408 A GB245408 A GB 245408A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- plane
- angle irons
- girders
- tip
- 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
- B64C3/00—Wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
- Joining Of Building Structures In Genera (AREA)
Abstract
245,408. Renault, L. Dec. 30, 1924, [Convention date]. Planes, construction of.-The upper and lower surfaces 1, 2 of thick planes are built up from a number of sheet metal members 13 fitting one within another and bolted or rivetted together as at 4. The members 13 may be shaped so that the plane tapers in width as shown in Fig. 7. The two faces of the members 13 may be made to approach each other towards the tip of the plane. Angle irons 5 are provided on some or all of the members 13 and are connected to girders formed by two angle irons 6 connected together by a trellis 7 and shaped so that the plane diminishes in depth towards the tip. Angle irons 8 are provided for connecting transverse girders 9. The members 13 are assembled with the end of a frame of the same shape as the girders 9.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR245408X | 1924-12-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB245408A true GB245408A (en) | 1926-04-08 |
Family
ID=8883623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13426/25A Expired GB245408A (en) | 1924-12-30 | 1925-05-22 | Improvements in or relating to aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB245408A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2312483A (en) * | 1996-04-24 | 1997-10-29 | British Aerospace | Joint assembly |
WO2018143802A1 (en) * | 2017-01-31 | 2018-08-09 | Fibercore Ip B.V. | Aerodynamic or hydrodynamic blade made of layered material |
-
1925
- 1925-05-22 GB GB13426/25A patent/GB245408A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2312483A (en) * | 1996-04-24 | 1997-10-29 | British Aerospace | Joint assembly |
US5944286A (en) * | 1996-04-24 | 1999-08-31 | British Aerospace Public Limited Company | Joint assemblies |
GB2312483B (en) * | 1996-04-24 | 2000-02-23 | British Aerospace | Joint assemblies |
WO2018143802A1 (en) * | 2017-01-31 | 2018-08-09 | Fibercore Ip B.V. | Aerodynamic or hydrodynamic blade made of layered material |
NL2018263B1 (en) * | 2017-01-31 | 2018-08-16 | Fibercore Ip Bv | Aerodynamic or hydrodynamic top made of laminated material |
CN110248869A (en) * | 2017-01-31 | 2019-09-17 | 光纤芯Ip有限公司 | Aerodynamic force blade or hydrodynamic blade made of stratified material |
US11753946B2 (en) | 2017-01-31 | 2023-09-12 | Fibercore Ip B.V. | Aerodynamic or hydrodynamic blade made of layered material |
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