GB2435457B - Aircraft wings and their assembly - Google Patents
Aircraft wings and their assemblyInfo
- Publication number
- GB2435457B GB2435457B GB0604017A GB0604017A GB2435457B GB 2435457 B GB2435457 B GB 2435457B GB 0604017 A GB0604017 A GB 0604017A GB 0604017 A GB0604017 A GB 0604017A GB 2435457 B GB2435457 B GB 2435457B
- Authority
- GB
- United Kingdom
- Prior art keywords
- assembly
- aircraft wings
- wings
- aircraft
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
-
- 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
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0604017A GB2435457B (en) | 2006-02-28 | 2006-02-28 | Aircraft wings and their assembly |
PCT/GB2007/000653 WO2007099297A1 (en) | 2006-02-28 | 2007-02-26 | Aircraft wings and their assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0604017A GB2435457B (en) | 2006-02-28 | 2006-02-28 | Aircraft wings and their assembly |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0604017D0 GB0604017D0 (en) | 2006-04-05 |
GB2435457A GB2435457A (en) | 2007-08-29 |
GB2435457B true GB2435457B (en) | 2011-03-09 |
Family
ID=36178957
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0604017A Expired - Fee Related GB2435457B (en) | 2006-02-28 | 2006-02-28 | Aircraft wings and their assembly |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2435457B (en) |
WO (1) | WO2007099297A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4657191B2 (en) * | 2006-11-02 | 2011-03-23 | 本田技研工業株式会社 | Aircraft main wing structure |
DE102007063159A1 (en) | 2007-12-30 | 2010-07-08 | Airbus Deutschland Gmbh | Wing-fuselage structural component for connecting two wings and a fuselage section on an aircraft |
FR2948099B1 (en) * | 2009-07-16 | 2012-05-11 | Airbus Operations Sas | METHOD FOR MANUFACTURING A FIXED SAIL AIRCRAFT |
US10118686B2 (en) * | 2012-09-27 | 2018-11-06 | The Boeing Company | Wing root insert system for an aircraft family |
EP3704018B1 (en) * | 2017-11-03 | 2022-05-04 | Uber Technologies, Inc. | Vtol m-wing configuration |
CN109229373B (en) * | 2018-09-29 | 2020-07-03 | 中船重工(海南)飞船发展有限公司 | Connecting structure of full-composite ground effect wing ship |
US11174042B2 (en) | 2018-10-09 | 2021-11-16 | The Boeing Company | Wing join system and method for a wing assembly |
FR3091259A1 (en) * | 2018-12-26 | 2020-07-03 | Airbus Operations | AIRCRAFT SAIL COMPRISING TWO FIXED WINGS ONE OVER THE OTHER |
EP3998192B1 (en) * | 2021-02-19 | 2024-03-20 | Lilium eAircraft GmbH | Wing spar structure |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2425099A (en) * | 1944-11-30 | 1947-08-05 | Cons Vultee Aircraft Corp | Aircraft wing connection |
GB1348826A (en) * | 1972-07-03 | 1974-03-27 | British Aircraft Corp Ltd | Aircraft |
US5435504A (en) * | 1993-03-09 | 1995-07-25 | Honda Giken Kogyo Kabushiki Kaisha | Aircraft |
US20030192990A1 (en) * | 1999-11-18 | 2003-10-16 | Simpson Craig B. | Single piece co-cure composite wing |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5529629A (en) * | 1978-08-18 | 1980-03-03 | Mitsubishi Heavy Ind Ltd | Aircraft having monolithic wing and body |
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US6190484B1 (en) * | 1999-02-19 | 2001-02-20 | Kari Appa | Monolithic composite wing manufacturing process |
CA2444560C (en) * | 2002-10-21 | 2008-09-23 | The Boeing Company | Method and apparatus for rotatably supporting movable components, including canards |
FR2867151B1 (en) * | 2004-03-04 | 2007-05-25 | Airbus France | FUSELAGE LONGERON FOR AN AIRCRAFT AND CENTRAL BOX EQUIPPED WITH SUCH A LONGERON |
-
2006
- 2006-02-28 GB GB0604017A patent/GB2435457B/en not_active Expired - Fee Related
-
2007
- 2007-02-26 WO PCT/GB2007/000653 patent/WO2007099297A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2425099A (en) * | 1944-11-30 | 1947-08-05 | Cons Vultee Aircraft Corp | Aircraft wing connection |
GB1348826A (en) * | 1972-07-03 | 1974-03-27 | British Aircraft Corp Ltd | Aircraft |
US5435504A (en) * | 1993-03-09 | 1995-07-25 | Honda Giken Kogyo Kabushiki Kaisha | Aircraft |
US20030192990A1 (en) * | 1999-11-18 | 2003-10-16 | Simpson Craig B. | Single piece co-cure composite wing |
Also Published As
Publication number | Publication date |
---|---|
GB0604017D0 (en) | 2006-04-05 |
WO2007099297A1 (en) | 2007-09-07 |
GB2435457A (en) | 2007-08-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20130228 |