BE530261A - - Google Patents
Info
- Publication number
- BE530261A BE530261A BE530261DA BE530261A BE 530261 A BE530261 A BE 530261A BE 530261D A BE530261D A BE 530261DA BE 530261 A BE530261 A BE 530261A
- Authority
- BE
- Belgium
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1929753A GB741508A (en) | 1953-07-11 | 1953-07-11 | Air cooled turbine blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE530261A true BE530261A (en:Method) |
Family
ID=10127057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE530261D BE530261A (en:Method) | 1953-07-11 |
Country Status (3)
| Country | Link |
|---|---|
| BE (1) | BE530261A (en:Method) |
| FR (1) | FR1106326A (en:Method) |
| GB (1) | GB741508A (en:Method) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3017159A (en) * | 1956-11-23 | 1962-01-16 | Curtiss Wright Corp | Hollow blade construction |
| MX161567A (es) * | 1985-03-13 | 1990-11-08 | Westinghouse Electric Corp | Mejoras en aspa fabricada con conductos longitudinales de enfriamiento para turbina de gas |
| GB0700499D0 (en) | 2007-01-11 | 2007-02-21 | Rolls Royce Plc | Aerofoil configuration |
| US8157527B2 (en) * | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
| US9777575B2 (en) | 2014-01-20 | 2017-10-03 | Honeywell International Inc. | Turbine rotor assemblies with improved slot cavities |
-
0
- BE BE530261D patent/BE530261A/xx unknown
-
1953
- 1953-07-11 GB GB1929753A patent/GB741508A/en not_active Expired
-
1954
- 1954-06-28 FR FR1106326D patent/FR1106326A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB741508A (en) | 1955-12-07 |
| FR1106326A (fr) | 1955-12-16 |