GB0022589D0 - Composite joints - Google Patents
Composite jointsInfo
- Publication number
- GB0022589D0 GB0022589D0 GB0022589A GB0022589A GB0022589D0 GB 0022589 D0 GB0022589 D0 GB 0022589D0 GB 0022589 A GB0022589 A GB 0022589A GB 0022589 A GB0022589 A GB 0022589A GB 0022589 D0 GB0022589 D0 GB 0022589D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- composite joints
- joints
- composite
- 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.)
- Ceased
Links
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0022589A GB0022589D0 (en) | 2000-09-14 | 2000-09-14 | Composite joints |
PCT/GB2001/003912 WO2002022440A1 (en) | 2000-09-14 | 2001-08-31 | Composite joints |
AU2001284224A AU2001284224A1 (en) | 2000-09-14 | 2001-08-31 | Composite joints |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0022589A GB0022589D0 (en) | 2000-09-14 | 2000-09-14 | Composite joints |
Publications (1)
Publication Number | Publication Date |
---|---|
GB0022589D0 true GB0022589D0 (en) | 2000-11-01 |
Family
ID=9899474
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0022589A Ceased GB0022589D0 (en) | 2000-09-14 | 2000-09-14 | Composite joints |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU2001284224A1 (en) |
GB (1) | GB0022589D0 (en) |
WO (1) | WO2002022440A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FI119979B (en) * | 2007-03-12 | 2009-05-29 | Patria Aerostructures Oy | Aircraft arch element and composite flange |
GB0712552D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
GB0712553D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
GB0712549D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
US8540833B2 (en) | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
GB0813161D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813146D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
DE102012109737A1 (en) * | 2012-10-12 | 2014-04-17 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | elastomer Zwickel |
US10295438B2 (en) * | 2016-06-24 | 2019-05-21 | The Boeing Company | Modeling and analysis of leading edge ribs of an aircraft wing |
US10605631B2 (en) | 2017-08-03 | 2020-03-31 | Sikorsky Aircraft Corporation | Structural pi joint with integrated fiber optic sensing |
WO2024015588A1 (en) * | 2022-07-15 | 2024-01-18 | Joby Aero, Inc. | Laminate material |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1050884A (en) * | 1900-01-01 | |||
GB1548162A (en) * | 1976-04-07 | 1979-07-04 | Eps Research Dev Ltd | Container |
JPS575777A (en) * | 1980-06-12 | 1982-01-12 | Nissan Motor Co Ltd | Method for bonding part to formed product |
US4331723A (en) * | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
US5789061A (en) * | 1996-02-13 | 1998-08-04 | Foster-Miller, Inc. | Stiffener reinforced assembly and method of manufacturing same |
-
2000
- 2000-09-14 GB GB0022589A patent/GB0022589D0/en not_active Ceased
-
2001
- 2001-08-31 AU AU2001284224A patent/AU2001284224A1/en not_active Abandoned
- 2001-08-31 WO PCT/GB2001/003912 patent/WO2002022440A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
AU2001284224A1 (en) | 2002-03-26 |
WO2002022440A1 (en) | 2002-03-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |