FR2689965B1 - Combustion chamber comprising at least two fuel injection assemblies. - Google Patents
Combustion chamber comprising at least two fuel injection assemblies.Info
- Publication number
- FR2689965B1 FR2689965B1 FR9204282A FR9204282A FR2689965B1 FR 2689965 B1 FR2689965 B1 FR 2689965B1 FR 9204282 A FR9204282 A FR 9204282A FR 9204282 A FR9204282 A FR 9204282A FR 2689965 B1 FR2689965 B1 FR 2689965B1
- Authority
- FR
- France
- Prior art keywords
- combustion chamber
- fuel injection
- injection assemblies
- assemblies
- fuel
- 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 - Fee Related
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
- F01D5/181—Blades having a closed internal cavity containing a cooling medium, e.g. sodium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9204282A FR2689965B1 (en) | 1992-04-08 | 1992-04-08 | Combustion chamber comprising at least two fuel injection assemblies. |
DE1993602954 DE69302954T2 (en) | 1992-04-08 | 1993-04-07 | Combustion chamber wall |
EP19930400907 EP0565442B1 (en) | 1992-04-08 | 1993-04-07 | Combustion chamber wall |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9204282A FR2689965B1 (en) | 1992-04-08 | 1992-04-08 | Combustion chamber comprising at least two fuel injection assemblies. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2689965A1 FR2689965A1 (en) | 1993-10-15 |
FR2689965B1 true FR2689965B1 (en) | 1995-06-02 |
Family
ID=9428621
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9204282A Expired - Fee Related FR2689965B1 (en) | 1992-04-08 | 1992-04-08 | Combustion chamber comprising at least two fuel injection assemblies. |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0565442B1 (en) |
DE (1) | DE69302954T2 (en) |
FR (1) | FR2689965B1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1813781A1 (en) * | 2006-01-31 | 2007-08-01 | Siemens Aktiengesellschaft | Part of a turbine, turbine and operation method thereof |
US10697635B2 (en) * | 2017-03-20 | 2020-06-30 | Raytheon Technologies Corporation | Impingement cooled components having integral thermal transfer features |
US10627167B2 (en) | 2017-09-12 | 2020-04-21 | General Electric Company | Gas turbine engine having a heat absorption device utilizing phase change material |
US11674396B2 (en) | 2021-07-30 | 2023-06-13 | General Electric Company | Cooling air delivery assembly |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE510847C (en) * | 1928-03-02 | 1930-10-24 | E H Hans Holzwarth Dr Ing | Combustion chamber with ring-shaped cooling chambers, especially for deflagration turbines |
CH269598A (en) * | 1944-01-31 | 1950-07-15 | Power Jets Res & Dev Ltd | Rotor blade on turbomachine working with hot working fluid. |
US3137995A (en) * | 1960-01-26 | 1964-06-23 | Chemical Engineering Dept | Ablation resistant reaction propulsion nozzle |
FR2221621B1 (en) * | 1973-03-13 | 1976-09-10 | Snecma | |
GB2049152B (en) * | 1979-05-01 | 1983-05-18 | Rolls Royce | Perforate laminated material |
JPS56101015A (en) * | 1980-01-18 | 1981-08-13 | Fuji Heavy Ind Ltd | Oil pan for internal-combustion engine |
JPS6119687A (en) * | 1984-07-09 | 1986-01-28 | Mitsui Petrochem Ind Ltd | Thermal energy storage material |
SU1586854A1 (en) * | 1988-10-11 | 1990-08-23 | Днепропетровский Металлургический Институт | Metal mould for centrifugal casting of rolls |
-
1992
- 1992-04-08 FR FR9204282A patent/FR2689965B1/en not_active Expired - Fee Related
-
1993
- 1993-04-07 EP EP19930400907 patent/EP0565442B1/en not_active Expired - Lifetime
- 1993-04-07 DE DE1993602954 patent/DE69302954T2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE69302954D1 (en) | 1996-07-11 |
EP0565442B1 (en) | 1996-06-05 |
DE69302954T2 (en) | 1996-11-28 |
FR2689965A1 (en) | 1993-10-15 |
EP0565442A1 (en) | 1993-10-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licenses | ||
ST | Notification of lapse |