FR1248821A - Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamber - Google Patents
Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamberInfo
- Publication number
- FR1248821A FR1248821A FR818768A FR818768A FR1248821A FR 1248821 A FR1248821 A FR 1248821A FR 818768 A FR818768 A FR 818768A FR 818768 A FR818768 A FR 818768A FR 1248821 A FR1248821 A FR 1248821A
- Authority
- FR
- France
- Prior art keywords
- chamber
- airplanes
- gas turbines
- similar
- annular combustion
- 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
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR818768A FR1248821A (en) | 1960-02-17 | 1960-02-17 | Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR818768A FR1248821A (en) | 1960-02-17 | 1960-02-17 | Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamber |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1248821A true FR1248821A (en) | 1960-12-23 |
Family
ID=8725361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR818768A Expired FR1248821A (en) | 1960-02-17 | 1960-02-17 | Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamber |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1248821A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2465080A1 (en) * | 1979-09-17 | 1981-03-20 | Snecma | Turbo-motor combustion chamber support - has radial pins with spherical end fitting in cup and cross pinned flanged cylindrical end |
EP0178242A1 (en) * | 1984-10-11 | 1986-04-16 | United Technologies Corporation | Cooling scheme for combustor vane interface |
-
1960
- 1960-02-17 FR FR818768A patent/FR1248821A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2465080A1 (en) * | 1979-09-17 | 1981-03-20 | Snecma | Turbo-motor combustion chamber support - has radial pins with spherical end fitting in cup and cross pinned flanged cylindrical end |
EP0178242A1 (en) * | 1984-10-11 | 1986-04-16 | United Technologies Corporation | Cooling scheme for combustor vane interface |
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