GB201916667D0 - A turbomachine blade - Google Patents
A turbomachine bladeInfo
- Publication number
- GB201916667D0 GB201916667D0 GBGB1916667.7A GB201916667A GB201916667D0 GB 201916667 D0 GB201916667 D0 GB 201916667D0 GB 201916667 A GB201916667 A GB 201916667A GB 201916667 D0 GB201916667 D0 GB 201916667D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbomachine blade
- turbomachine
- blade
- 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.)
- Withdrawn
Links
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1916667.7A GB2588955A (en) | 2019-11-15 | 2019-11-15 | A turbomachine blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1916667.7A GB2588955A (en) | 2019-11-15 | 2019-11-15 | A turbomachine blade |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB201916667D0 true GB201916667D0 (en) | 2020-01-01 |
| GB2588955A GB2588955A (en) | 2021-05-19 |
Family
ID=69063224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1916667.7A Withdrawn GB2588955A (en) | 2019-11-15 | 2019-11-15 | A turbomachine blade |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2588955A (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB736835A (en) * | 1952-09-11 | 1955-09-14 | Maschf Augsburg Nuernberg Ag | Improvements in or relating to blading for axial flow turbo-engines |
| GB0001399D0 (en) * | 2000-01-22 | 2000-03-08 | Rolls Royce Plc | An aerofoil for an axial flow turbomachine |
| EP1785589A1 (en) * | 2005-11-10 | 2007-05-16 | Siemens Aktiengesellschaft | Turbine blade, in particular for a turbine of a thermal power plant |
| US8016567B2 (en) * | 2007-01-17 | 2011-09-13 | United Technologies Corporation | Separation resistant aerodynamic article |
| GB2481822B (en) * | 2010-07-07 | 2013-09-18 | Rolls Royce Plc | Rotor blade |
| WO2015065659A1 (en) * | 2013-10-31 | 2015-05-07 | United Technologies Corporation | Gas turbine engine airfoil with auxiliary flow channel |
-
2019
- 2019-11-15 GB GB1916667.7A patent/GB2588955A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| GB2588955A (en) | 2021-05-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |