FR1146227A - Improvements to jet propulsion engines with gas turbines - Google Patents
Improvements to jet propulsion engines with gas turbinesInfo
- Publication number
- FR1146227A FR1146227A FR1146227DA FR1146227A FR 1146227 A FR1146227 A FR 1146227A FR 1146227D A FR1146227D A FR 1146227DA FR 1146227 A FR1146227 A FR 1146227A
- Authority
- FR
- France
- Prior art keywords
- gas turbines
- jet propulsion
- propulsion engines
- engines
- jet
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
-
- 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
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
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 |
---|---|---|---|
GB1146227X | 1955-02-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1146227A true FR1146227A (en) | 1957-11-07 |
Family
ID=10877568
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1146227D Expired FR1146227A (en) | 1955-02-24 | 1956-02-24 | Improvements to jet propulsion engines with gas turbines |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1146227A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1153215B (en) * | 1959-03-13 | 1963-08-22 | Rolls Royce | Twin-flow gas turbine jet engine |
EP0315485A2 (en) * | 1987-11-05 | 1989-05-10 | General Electric Company | Gas-cooled flameholder assembly |
-
1956
- 1956-02-24 FR FR1146227D patent/FR1146227A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1153215B (en) * | 1959-03-13 | 1963-08-22 | Rolls Royce | Twin-flow gas turbine jet engine |
EP0315485A2 (en) * | 1987-11-05 | 1989-05-10 | General Electric Company | Gas-cooled flameholder assembly |
EP0315485A3 (en) * | 1987-11-05 | 1990-05-23 | General Electric Company | Gas-cooled flameholder assembly |
US5076062A (en) * | 1987-11-05 | 1991-12-31 | General Electric Company | Gas-cooled flameholder assembly |
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