FR970723A - Switchgear for gas turbines - Google Patents
Switchgear for gas turbinesInfo
- Publication number
- FR970723A FR970723A FR970723DA FR970723A FR 970723 A FR970723 A FR 970723A FR 970723D A FR970723D A FR 970723DA FR 970723 A FR970723 A FR 970723A
- Authority
- FR
- France
- Prior art keywords
- switchgear
- gas turbines
- turbines
- gas
- 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.)
- Expired
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
- F01D9/045—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial flow machines or engines
-
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US267782XA | 1947-08-29 | 1947-08-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR970723A true FR970723A (en) | 1951-01-08 |
Family
ID=21833738
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR970723D Expired FR970723A (en) | 1947-08-29 | 1948-08-26 | Switchgear for gas turbines |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH267782A (en) |
FR (1) | FR970723A (en) |
GB (1) | GB641709A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2671634A (en) * | 1949-07-01 | 1954-03-09 | Rolls Royce | Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors |
US3043564A (en) * | 1960-03-14 | 1962-07-10 | United Aircraft Corp | Stator construction |
US4820120A (en) * | 1986-06-18 | 1989-04-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Stator assembly for the fan of a multi-flow turbo-jet engine |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681788A (en) * | 1951-05-23 | 1954-06-22 | Solar Aircraft Co | Gas turbine vane structure |
BE570267A (en) * | 1957-08-16 |
-
1948
- 1948-06-09 CH CH267782D patent/CH267782A/en unknown
- 1948-06-15 GB GB16086/48A patent/GB641709A/en not_active Expired
- 1948-08-26 FR FR970723D patent/FR970723A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2671634A (en) * | 1949-07-01 | 1954-03-09 | Rolls Royce | Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors |
US3043564A (en) * | 1960-03-14 | 1962-07-10 | United Aircraft Corp | Stator construction |
US4820120A (en) * | 1986-06-18 | 1989-04-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Stator assembly for the fan of a multi-flow turbo-jet engine |
Also Published As
Publication number | Publication date |
---|---|
GB641709A (en) | 1950-08-16 |
CH267782A (en) | 1950-04-15 |
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