BE763178A - Moteur a turbine a gaz avec dispositif de postcombustion perfectionne - Google Patents
Moteur a turbine a gaz avec dispositif de postcombustion perfectionneInfo
- Publication number
- BE763178A BE763178A BE763178A BE763178A BE763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A
- Authority
- BE
- Belgium
- Prior art keywords
- advanced
- gas turbine
- turbine engine
- combustion device
- combustion
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US4029870A | 1970-05-25 | 1970-05-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE763178A true BE763178A (fr) | 1971-07-16 |
Family
ID=21910234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE763178A BE763178A (fr) | 1970-05-25 | 1971-02-19 | Moteur a turbine a gaz avec dispositif de postcombustion perfectionne |
Country Status (6)
Country | Link |
---|---|
US (1) | US3646763A (enrdf_load_stackoverflow) |
BE (1) | BE763178A (enrdf_load_stackoverflow) |
CA (1) | CA927616A (enrdf_load_stackoverflow) |
DE (1) | DE2108690A1 (enrdf_load_stackoverflow) |
FR (1) | FR2090250B1 (enrdf_load_stackoverflow) |
GB (1) | GB1335746A (enrdf_load_stackoverflow) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2122308B1 (enrdf_load_stackoverflow) * | 1971-01-19 | 1976-03-05 | Snecma Fr | |
FR2551500B1 (fr) * | 1983-09-07 | 1985-11-08 | Snecma | Anneau-bruleur pour postcombustion de moteur a reaction |
FR2586792B1 (fr) * | 1985-09-03 | 1989-06-16 | Snecma | Dispositif de liaison entre un anneau bruleur ou accroche-flammes en materiau composite et un canal de chambre de post-combustion d'un turboreacteur |
US4815283A (en) * | 1987-06-25 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Air Force | Afterburner flameholder construction |
US5103638A (en) * | 1990-01-29 | 1992-04-14 | Rolls-Royce Inc. | Mounting arrangement |
EP0550126A1 (en) * | 1992-01-02 | 1993-07-07 | General Electric Company | Thrust augmentor heat shield |
US6351941B1 (en) * | 2000-02-29 | 2002-03-05 | General Electric Company | Methods and apparatus for reducing thermal stresses in an augmentor |
US7712315B2 (en) * | 2006-04-20 | 2010-05-11 | United Technologies Corporation | Augmentor variable vane flame stabilization |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2714287A (en) * | 1950-01-03 | 1955-08-02 | Westinghouse Electric Corp | Flameholder device for turbojet afterburner |
GB821286A (en) * | 1956-06-05 | 1959-10-07 | Rolls Royce | Improvements in or relating to reheat combustion equipment of jet-propulsion engines |
US3102392A (en) * | 1959-04-21 | 1963-09-03 | Snecma | Combustion equipment for jet propulsion units |
US3056261A (en) * | 1959-09-01 | 1962-10-02 | Gen Electric | Flameholder configuration |
FR1245920A (fr) * | 1960-01-19 | 1960-11-10 | Le Ministre De La Defense Nati | Collecteur de distribution de combustible isolé |
FR1265727A (fr) * | 1960-08-23 | 1961-06-30 | Gen Electric | Structure de tubes à flammes pour brûleurs de post-combustion de turbo-réacteurs |
GB944202A (en) * | 1961-07-11 | 1963-12-11 | Rolls Royce | Improvements in or relating to combustion equipment and ignition devices therefor |
FR1406603A (fr) * | 1964-06-09 | 1965-07-23 | Snecma | Dispositif de brûleur et son montage dans une chambre de combustion |
-
1970
- 1970-05-25 US US40298A patent/US3646763A/en not_active Expired - Lifetime
-
1971
- 1971-02-19 BE BE763178A patent/BE763178A/xx unknown
- 1971-02-24 DE DE19712108690 patent/DE2108690A1/de active Pending
- 1971-02-24 FR FR7106351A patent/FR2090250B1/fr not_active Expired
- 1971-03-16 CA CA107807A patent/CA927616A/en not_active Expired
- 1971-04-19 GB GB2400071*A patent/GB1335746A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3646763A (en) | 1972-03-07 |
FR2090250A1 (enrdf_load_stackoverflow) | 1972-01-14 |
FR2090250B1 (enrdf_load_stackoverflow) | 1975-01-17 |
CA927616A (en) | 1973-06-05 |
DE2108690A1 (de) | 1972-08-10 |
GB1335746A (en) | 1973-10-31 |
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