GB613512A - Improvements in floors for airplanes, vehicles of all types and other applications - Google Patents
Improvements in floors for airplanes, vehicles of all types and other applicationsInfo
- Publication number
- GB613512A GB613512A GB10675/45A GB1067545A GB613512A GB 613512 A GB613512 A GB 613512A GB 10675/45 A GB10675/45 A GB 10675/45A GB 1067545 A GB1067545 A GB 1067545A GB 613512 A GB613512 A GB 613512A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sheet
- top surface
- supporting
- floors
- stress
- 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
- B64C1/18—Floors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Floor Finish (AREA)
- Laminated Bodies (AREA)
Abstract
613,512. Floors. SOC. ANON. DES USINES CHAUSSON. April 27, 1945, No. 10675. Convention date, June 17, 1944. [Class 20(iv)] A floor for aeroplanes and other applications comprises a top surface sheet 7, interposed stress transmitting elements 9, 10 and 11 and a supporting sheet 8 which is hung from a framework 3, 4, 5 and 6 to form catenary curves. Thin sheet metal, plywood or other light material, or even the top surface of the element transmitting the stress, where such provide a plane surface, may be used for the said top surface 7, whereas the supporting sheet 8 is of sheet metal having a high limit of elasticity. The intermediate stress transmitting element may be in the form of projections, bosses and protuberances secured to the top surface sheet or to the supporting sheet, or may be in the form of a light filling material, such as spongy ebonite, having insulating waterproof, soundproof properties and the like, and secured between the top and supporting sheets.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR613512X | 1944-06-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB613512A true GB613512A (en) | 1948-11-30 |
Family
ID=8979545
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10675/45A Expired GB613512A (en) | 1944-06-17 | 1945-04-27 | Improvements in floors for airplanes, vehicles of all types and other applications |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB613512A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012028263A1 (en) * | 2010-08-30 | 2012-03-08 | Airbus Operations Gmbh | Aircraft structural assembly |
| US9902483B2 (en) | 2013-08-28 | 2018-02-27 | Airbus Operations Gmbh | Window panel for an airframe and method of producing same |
-
1945
- 1945-04-27 GB GB10675/45A patent/GB613512A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012028263A1 (en) * | 2010-08-30 | 2012-03-08 | Airbus Operations Gmbh | Aircraft structural assembly |
| CN103269950A (en) * | 2010-08-30 | 2013-08-28 | 空中客车作业有限公司 | Aircraft structural assembly |
| RU2576647C2 (en) * | 2010-08-30 | 2016-03-10 | Эйрбас Оперейшнз Гмбх | Aircraft structural assembly |
| US9327821B2 (en) | 2010-08-30 | 2016-05-03 | Airbus Operations Gmbh | Aircraft structural assembly having an area element which comprises a core and an outer layer |
| US9902483B2 (en) | 2013-08-28 | 2018-02-27 | Airbus Operations Gmbh | Window panel for an airframe and method of producing same |
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