GB457369A - Improvements in or relating to sheet metal walls and/or partitions for aircraft - Google Patents
Improvements in or relating to sheet metal walls and/or partitions for aircraftInfo
- Publication number
- GB457369A GB457369A GB9410/36A GB941036A GB457369A GB 457369 A GB457369 A GB 457369A GB 9410/36 A GB9410/36 A GB 9410/36A GB 941036 A GB941036 A GB 941036A GB 457369 A GB457369 A GB 457369A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- aircraft
- partitions
- relating
- sheet metal
- 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
- B64C1/12—Construction or attachment of skin panels
-
- 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)
- Laminated Bodies (AREA)
Abstract
457,369. Aircraft framework. DORNIER METALLBAUTEN GES., Friedrichshafen, Germany. March 30, 1936, No. 9410. Convention date, June 29, 1935. [Class 4] [See also Group X] In a sheet-metal wall or partition 1 for aircraft having on one side laterally flanged strengthening members 2, 3 having in section a U-shaped profile, the members are joined together at their points of intersection by cross-connectors or straps 4, the arms of which are shaped to conform to the shape of the profiled reinforcing members 2, 3. Where one profiled section reinforcing member is at a different level from the other, the arms of the cross straps are arranged at different heights. The flanges of the members 3 are flattened out at the points of intersection with the members 2.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE457369X | 1935-06-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB457369A true GB457369A (en) | 1936-11-26 |
Family
ID=6539306
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9410/36A Expired GB457369A (en) | 1935-06-29 | 1936-03-30 | Improvements in or relating to sheet metal walls and/or partitions for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB457369A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009146958A1 (en) * | 2008-05-30 | 2009-12-10 | Airbus Operations Gmbh | Composite and structure, particularly in the aerospace sector |
JP2011500415A (en) * | 2007-10-18 | 2011-01-06 | エアバス オペレーションズ (エスアーエス) | Aircraft having a stiffener end connection and a method of manufacturing such an aircraft |
US9896180B2 (en) | 2014-05-06 | 2018-02-20 | Airbus Operations Gmbh | Method for manufacturing a load bearing structure and such a load bearing structure |
FR3129203A1 (en) * | 2021-11-18 | 2023-05-19 | Safran Nacelles | Rigid open composite panel |
-
1936
- 1936-03-30 GB GB9410/36A patent/GB457369A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011500415A (en) * | 2007-10-18 | 2011-01-06 | エアバス オペレーションズ (エスアーエス) | Aircraft having a stiffener end connection and a method of manufacturing such an aircraft |
WO2009146958A1 (en) * | 2008-05-30 | 2009-12-10 | Airbus Operations Gmbh | Composite and structure, particularly in the aerospace sector |
CN102046358A (en) * | 2008-05-30 | 2011-05-04 | 空中客车运营有限公司 | Composite and structure, particularly in the aerospace sector |
JP2011521825A (en) * | 2008-05-30 | 2011-07-28 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Composites and structures, especially in the field of aircraft |
US8403263B2 (en) | 2008-05-30 | 2013-03-26 | Airbus Operations Gmbh | Composite and structure, particularly in the aerospace sector |
CN102046358B (en) * | 2008-05-30 | 2013-07-31 | 空中客车运营有限公司 | Composite and structure, particularly in the aerospace sector |
RU2496678C2 (en) * | 2008-05-30 | 2013-10-27 | Эйрбас Оперэйшнз Гмбх | Structural assembly and structure used, in particular, in aircraft engineering |
DE102008002117B4 (en) * | 2008-05-30 | 2013-10-31 | Airbus Operations Gmbh | Composite and structure |
US9896180B2 (en) | 2014-05-06 | 2018-02-20 | Airbus Operations Gmbh | Method for manufacturing a load bearing structure and such a load bearing structure |
FR3129203A1 (en) * | 2021-11-18 | 2023-05-19 | Safran Nacelles | Rigid open composite panel |
WO2023089273A1 (en) * | 2021-11-18 | 2023-05-25 | Safran Nacelles | Rigid open composite panel |
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