FR1318082A - Post-combustion stabilizers for bypass turbo-reactors - Google Patents
Post-combustion stabilizers for bypass turbo-reactorsInfo
- Publication number
- FR1318082A FR1318082A FR891679A FR891679A FR1318082A FR 1318082 A FR1318082 A FR 1318082A FR 891679 A FR891679 A FR 891679A FR 891679 A FR891679 A FR 891679A FR 1318082 A FR1318082 A FR 1318082A
- Authority
- FR
- France
- Prior art keywords
- reactors
- post
- bypass turbo
- combustion stabilizers
- stabilizers
- 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
- F23R3/16—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
-
- 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
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR891679A FR1318082A (en) | 1961-03-21 | 1962-03-20 | Post-combustion stabilizers for bypass turbo-reactors |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10350/61A GB940832A (en) | 1961-03-21 | 1961-03-21 | Improvements in or relating to gas turbine engines |
FR891679A FR1318082A (en) | 1961-03-21 | 1962-03-20 | Post-combustion stabilizers for bypass turbo-reactors |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1318082A true FR1318082A (en) | 1963-02-15 |
Family
ID=26194845
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR891679A Expired FR1318082A (en) | 1961-03-21 | 1962-03-20 | Post-combustion stabilizers for bypass turbo-reactors |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1318082A (en) |
-
1962
- 1962-03-20 FR FR891679A patent/FR1318082A/en not_active Expired
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