BE533039A - - Google Patents
Info
- Publication number
- BE533039A BE533039A BE533039DA BE533039A BE 533039 A BE533039 A BE 533039A BE 533039D A BE533039D A BE 533039DA BE 533039 A BE533039 A BE 533039A
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB30854/53A GB758669A (en) | 1953-11-06 | 1953-11-06 | Improvements in or relating to axial-flow compressors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE533039A true BE533039A (xx) |
Family
ID=10314175
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE533039D BE533039A (xx) | 1953-11-06 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US2833463A (xx) |
| BE (1) | BE533039A (xx) |
| FR (1) | FR1111000A (xx) |
| GB (1) | GB758669A (xx) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB799896A (en) * | 1955-10-21 | 1958-08-13 | Rolls Royce | Improvements in or relating to axial-flow compressors |
| GB845325A (en) * | 1956-12-18 | 1960-08-17 | Gen Electric | Stator vane assembly for axial flow compressors |
| GB938189A (en) * | 1960-10-29 | 1963-10-02 | Ruston & Hornsby Ltd | Improvements in the construction of turbine and compressor blade elements |
| US3269702A (en) * | 1964-01-13 | 1966-08-30 | United Aircraft Corp | Nozzle vane assembly |
| US4460315A (en) * | 1981-06-29 | 1984-07-17 | General Electric Company | Turbomachine rotor assembly |
| US4907944A (en) * | 1984-10-01 | 1990-03-13 | General Electric Company | Turbomachinery blade mounting arrangement |
| US4688992A (en) * | 1985-01-25 | 1987-08-25 | General Electric Company | Blade platform |
| US5141395A (en) * | 1991-09-05 | 1992-08-25 | General Electric Company | Flow activated flowpath liner seal |
| US8128354B2 (en) * | 2007-01-17 | 2012-03-06 | Siemens Energy, Inc. | Gas turbine engine |
| US8894370B2 (en) * | 2008-04-04 | 2014-11-25 | General Electric Company | Turbine blade retention system and method |
| FR2978197B1 (fr) * | 2011-07-22 | 2015-12-25 | Snecma | Distributeur de turbine de turbomachine et turbine comportant un tel distributeur |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE488535A (xx) * | 1947-02-17 | |||
| US2638743A (en) * | 1949-04-29 | 1953-05-19 | Ruston & Hornsby Ltd | Construction of turbine-inlet and stator elements of gas turbines |
-
0
- BE BE533039D patent/BE533039A/xx unknown
-
1953
- 1953-11-06 GB GB30854/53A patent/GB758669A/en not_active Expired
-
1954
- 1954-10-25 US US464511A patent/US2833463A/en not_active Expired - Lifetime
- 1954-10-27 FR FR1111000D patent/FR1111000A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1111000A (fr) | 1956-02-20 |
| US2833463A (en) | 1958-05-06 |
| GB758669A (en) | 1956-10-10 |