BE570267A - - Google Patents
Info
- Publication number
- BE570267A BE570267A BE570267DA BE570267A BE 570267 A BE570267 A BE 570267A BE 570267D A BE570267D A BE 570267DA BE 570267 A BE570267 A BE 570267A
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US678693A US2937000A (en) | 1957-08-16 | 1957-08-16 | Stator units |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE570267A true BE570267A (en:Method) |
Family
ID=24723873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE570267D BE570267A (en:Method) | 1957-08-16 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US2937000A (en:Method) |
| BE (1) | BE570267A (en:Method) |
| CH (1) | CH362268A (en:Method) |
| DE (1) | DE1185865B (en:Method) |
| FR (1) | FR1201329A (en:Method) |
| GB (1) | GB879337A (en:Method) |
| NL (1) | NL104794C (en:Method) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB904138A (en) * | 1959-01-23 | 1962-08-22 | Bristol Siddeley Engines Ltd | Improvements in or relating to stator structures, for example for axial flow gas turbine engines |
| US3038652A (en) * | 1959-10-21 | 1962-06-12 | United Aircraft Corp | Intermediate compressor case |
| US3062499A (en) * | 1960-05-18 | 1962-11-06 | United Aircraft Corp | Vane mounting and seal |
| US3075744A (en) * | 1960-08-16 | 1963-01-29 | United Aircraft Corp | Turbine nozzle vane mounting means |
| US3314648A (en) * | 1961-12-19 | 1967-04-18 | Gen Electric | Stator vane assembly |
| GB1086432A (en) * | 1965-09-21 | 1967-10-11 | Bristol Siddeley Engines Ltd | Gas turbine engines |
| FR1339521A (fr) * | 1966-06-10 | 1963-10-11 | Rolls Royce | Machine à circulation de fluide |
| US3423071A (en) * | 1967-07-17 | 1969-01-21 | United Aircraft Corp | Turbine vane retention |
| US3511577A (en) * | 1968-04-10 | 1970-05-12 | Caterpillar Tractor Co | Turbine nozzle construction |
| US4184689A (en) * | 1978-10-02 | 1980-01-22 | United Technologies Corporation | Seal structure for an axial flow rotary machine |
| US4566851A (en) * | 1984-05-11 | 1986-01-28 | United Technologies Corporation | First stage turbine vane support structure |
| US4741667A (en) * | 1986-05-28 | 1988-05-03 | United Technologies Corporation | Stator vane |
| CA2070511C (en) * | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
| US7025563B2 (en) | 2003-12-19 | 2006-04-11 | United Technologies Corporation | Stator vane assembly for a gas turbine engine |
| US9702252B2 (en) * | 2012-12-19 | 2017-07-11 | Honeywell International Inc. | Turbine nozzles with slip joints and methods for the production thereof |
| US11002147B2 (en) | 2018-08-28 | 2021-05-11 | Raytheon Technologies Corporation | Fixed vane pack retaining ring |
| US12312979B1 (en) | 2024-02-21 | 2025-05-27 | Rolls-Royce North American Technologies Inc. | Retainer rings for vane assemblies used in gas turbine engines |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB277663A (en) * | 1926-09-20 | 1928-01-26 | Lorenzen Turbinen Ag | Improvements in or relating to turbines |
| GB589542A (en) * | 1941-09-22 | 1947-06-24 | Karl Baumann | Improvements in internal combustion turbines |
| BE487115A (en:Method) * | 1946-04-05 | |||
| GB618525A (en) * | 1946-06-18 | 1949-02-23 | Adrian Albert Lombard | Improvements in or relating to gas-turbine engines |
| FR965713A (en:Method) * | 1947-05-07 | 1950-09-20 | ||
| CH267782A (de) * | 1947-08-29 | 1950-04-15 | Westinghouse Electric Corp | Leitvorrichtung für eine Gasturbine. |
| US2625013A (en) * | 1948-11-27 | 1953-01-13 | Gen Electric | Gas turbine nozzle structure |
| US2609176A (en) * | 1950-01-21 | 1952-09-02 | A V Roe Canada Ltd | Turbine nozzle guide vane construction |
-
0
- NL NL104794D patent/NL104794C/xx active
- BE BE570267D patent/BE570267A/xx unknown
-
1957
- 1957-08-16 US US678693A patent/US2937000A/en not_active Expired - Lifetime
-
1958
- 1958-08-02 DE DEU5514A patent/DE1185865B/de active Pending
- 1958-08-12 CH CH362268D patent/CH362268A/de unknown
- 1958-08-14 FR FR1201329D patent/FR1201329A/fr not_active Expired
- 1958-08-18 GB GB26510/58A patent/GB879337A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1201329A (fr) | 1959-12-29 |
| NL104794C (en:Method) | |
| GB879337A (en) | 1961-10-11 |
| US2937000A (en) | 1960-05-17 |
| DE1185865B (de) | 1965-01-21 |
| CH362268A (de) | 1962-05-31 |