GB201708011D0 - Stiffening structure for an aircraft door or panel - Google Patents
Stiffening structure for an aircraft door or panelInfo
- Publication number
- GB201708011D0 GB201708011D0 GBGB1708011.0A GB201708011A GB201708011D0 GB 201708011 D0 GB201708011 D0 GB 201708011D0 GB 201708011 A GB201708011 A GB 201708011A GB 201708011 D0 GB201708011 D0 GB 201708011D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- panel
- stiffening structure
- aircraft door
- aircraft
- door
- 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 |
|---|---|---|---|
| GBGB1708011.0A GB201708011D0 (en) | 2017-05-18 | 2017-05-18 | Stiffening structure for an aircraft door or panel |
| GB1808031.7A GB2564927B (en) | 2017-05-18 | 2018-05-17 | Stiffening structure for an aircraft door or panel |
| PCT/GB2018/000083 WO2018211232A1 (en) | 2017-05-18 | 2018-05-17 | Stiffening structure for an aircraft door or panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1708011.0A GB201708011D0 (en) | 2017-05-18 | 2017-05-18 | Stiffening structure for an aircraft door or panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB201708011D0 true GB201708011D0 (en) | 2017-07-05 |
Family
ID=59220735
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GBGB1708011.0A Ceased GB201708011D0 (en) | 2017-05-18 | 2017-05-18 | Stiffening structure for an aircraft door or panel |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB201708011D0 (en) |
-
2017
- 2017-05-18 GB GBGB1708011.0A patent/GB201708011D0/en not_active Ceased
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AT | Applications terminated before publication under section 16(1) |