FR1134847A - Improvements to combustion equipment for gas turbine engines - Google Patents
Improvements to combustion equipment for gas turbine enginesInfo
- Publication number
- FR1134847A FR1134847A FR1134847DA FR1134847A FR 1134847 A FR1134847 A FR 1134847A FR 1134847D A FR1134847D A FR 1134847DA FR 1134847 A FR1134847 A FR 1134847A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine engines
- combustion equipment
- combustion
- equipment
- 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
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1134847X | 1954-07-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1134847A true FR1134847A (en) | 1957-04-18 |
Family
ID=10876658
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1134847D Expired FR1134847A (en) | 1954-07-20 | 1955-07-19 | Improvements to combustion equipment for gas turbine engines |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1134847A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1108517B (en) * | 1957-09-27 | 1961-06-08 | Rolls Royce | Gas turbine combustor |
DE1198130B (en) * | 1958-08-22 | 1965-08-05 | Snecma | Burner for ring-shaped combustion chambers |
FR2124141A1 (en) * | 1971-02-09 | 1972-09-22 | Snecma | |
FR2450947A2 (en) * | 1979-03-08 | 1980-10-03 | Rolls Royce | IMPROVEMENTS ON TURBOMACHINES |
-
1955
- 1955-07-19 FR FR1134847D patent/FR1134847A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1108517B (en) * | 1957-09-27 | 1961-06-08 | Rolls Royce | Gas turbine combustor |
DE1198130B (en) * | 1958-08-22 | 1965-08-05 | Snecma | Burner for ring-shaped combustion chambers |
FR2124141A1 (en) * | 1971-02-09 | 1972-09-22 | Snecma | |
FR2450947A2 (en) * | 1979-03-08 | 1980-10-03 | Rolls Royce | IMPROVEMENTS ON TURBOMACHINES |
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