PL425188A1 - Thin-walled construction, preferably for the aircraft skins - Google Patents
Thin-walled construction, preferably for the aircraft skinsInfo
- Publication number
- PL425188A1 PL425188A1 PL425188A PL42518818A PL425188A1 PL 425188 A1 PL425188 A1 PL 425188A1 PL 425188 A PL425188 A PL 425188A PL 42518818 A PL42518818 A PL 42518818A PL 425188 A1 PL425188 A1 PL 425188A1
- Authority
- PL
- Poland
- Prior art keywords
- thin
- walled construction
- layer
- aircraft skins
- outer layer
- Prior art date
Links
Landscapes
- Laminated Bodies (AREA)
Abstract
Konstrukcja cienkościenna złożona jest z połączonych ze sobą warstwy wewnętrznej (1) i warstwy zewnętrznej (2). Warstwa wewnętrzna (1) ma ukształtowane przetłoczenia usztywniające (4). Przetłoczenia usztywniające (4) tworzą strukturę typu isogrid. Warstwa zewnętrzna (2) zawiera warstwę kompozytową (3), która jest ukształtowana z kompozytu polimerowo-włóknistego. Warstwa wewnętrzna (1) i warstwa zewnętrzna (2) są połączone adhezyjnie.The thin-walled structure is composed of interconnected inner layer (1) and outer layer (2). The inner layer (1) has shaped stiffening ribs (4). The stiffening ribs (4) form an isogrid structure. The outer layer (2) comprises a composite layer (3) which is formed of a polymer-fiber composite. The inner layer (1) and the outer layer (2) are adhesively bonded.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL425188A PL425188A1 (en) | 2018-04-11 | 2018-04-11 | Thin-walled construction, preferably for the aircraft skins |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL425188A PL425188A1 (en) | 2018-04-11 | 2018-04-11 | Thin-walled construction, preferably for the aircraft skins |
Publications (1)
Publication Number | Publication Date |
---|---|
PL425188A1 true PL425188A1 (en) | 2019-10-21 |
Family
ID=68238617
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL425188A PL425188A1 (en) | 2018-04-11 | 2018-04-11 | Thin-walled construction, preferably for the aircraft skins |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL425188A1 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140044914A1 (en) * | 2011-05-02 | 2014-02-13 | Didier Kurtz | Self-stiffened composite panel particularly for aircraft floors and method for manufacturing the same |
PL224527B1 (en) * | 2012-12-05 | 2017-01-31 | Inst Pojazdów Szynowych Tabor | Multi-layer plate |
US20170113777A1 (en) * | 2015-10-22 | 2017-04-27 | Airbus Defence and Space GmbH | Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement |
US20170274577A1 (en) * | 2016-03-24 | 2017-09-28 | The Boeing Company | Composite structures with stiffeners and method of making the same |
-
2018
- 2018-04-11 PL PL425188A patent/PL425188A1/en unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140044914A1 (en) * | 2011-05-02 | 2014-02-13 | Didier Kurtz | Self-stiffened composite panel particularly for aircraft floors and method for manufacturing the same |
PL224527B1 (en) * | 2012-12-05 | 2017-01-31 | Inst Pojazdów Szynowych Tabor | Multi-layer plate |
US20170113777A1 (en) * | 2015-10-22 | 2017-04-27 | Airbus Defence and Space GmbH | Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement |
US20170274577A1 (en) * | 2016-03-24 | 2017-09-28 | The Boeing Company | Composite structures with stiffeners and method of making the same |
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