GB1427197A - After burner installations for gas turbine engines - Google Patents
After burner installations for gas turbine enginesInfo
- Publication number
- GB1427197A GB1427197A GB2617473A GB2617473A GB1427197A GB 1427197 A GB1427197 A GB 1427197A GB 2617473 A GB2617473 A GB 2617473A GB 2617473 A GB2617473 A GB 2617473A GB 1427197 A GB1427197 A GB 1427197A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- heat
- combustion
- exhaust gas
- gas flow
- 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
- 238000009434 installation Methods 0.000 title 1
- 239000007789 gas Substances 0.000 abstract 13
- 239000000446 fuel Substances 0.000 abstract 10
- 239000000203 mixture Substances 0.000 abstract 7
- 238000002485 combustion reaction Methods 0.000 abstract 6
- 238000011144 upstream manufacturing Methods 0.000 abstract 3
- 239000000567 combustion gas Substances 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 239000002737 fuel gas Substances 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 239000003381 stabilizer Substances 0.000 abstract 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
-
- 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)
- Incineration Of Waste (AREA)
- Combustion Of Fluid Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7219731A FR2188060B1 (enrdf_load_stackoverflow) | 1972-06-01 | 1972-06-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1427197A true GB1427197A (en) | 1976-03-10 |
Family
ID=9099528
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2617473A Expired GB1427197A (en) | 1972-06-01 | 1973-06-01 | After burner installations for gas turbine engines |
Country Status (4)
Country | Link |
---|---|
US (1) | US3899883A (enrdf_load_stackoverflow) |
DE (1) | DE2327187C3 (enrdf_load_stackoverflow) |
FR (1) | FR2188060B1 (enrdf_load_stackoverflow) |
GB (1) | GB1427197A (enrdf_load_stackoverflow) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2472027C1 (ru) * | 2011-07-12 | 2013-01-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Уфимский государственный авиационный технический университет | Фронтовое устройство форсажной камеры со стабилизатором пламени изменяемой геометрии |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3931707A (en) * | 1975-01-08 | 1976-01-13 | General Electric Company | Augmentor flameholding apparatus |
US4005572A (en) * | 1975-04-18 | 1977-02-01 | Giffhorn William A | Gas turbine engine control system |
US4751815A (en) * | 1986-08-29 | 1988-06-21 | United Technologies Corporation | Liquid fuel spraybar |
US5076062A (en) * | 1987-11-05 | 1991-12-31 | General Electric Company | Gas-cooled flameholder assembly |
US5245934A (en) * | 1988-06-08 | 1993-09-21 | Mortimer Technology Holdings Ltd. | Heating matter |
CN116025924B (zh) * | 2023-01-13 | 2024-09-20 | 南京航空航天大学 | 一种加力燃烧室外凹腔火焰稳定器后壁面强制冷却装置 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2711070A (en) * | 1952-07-31 | 1955-06-21 | Westinghouse Electric Corp | Gas turbine apparatus |
US2944388A (en) * | 1955-02-24 | 1960-07-12 | Thompson Ramo Wooldridge Inc | Air atomizing spray bar |
FR1166154A (fr) * | 1957-02-01 | 1958-11-04 | Snecma | Brûleur à semi-vaporisation |
DE1123163B (de) * | 1958-05-23 | 1962-02-01 | Gen Electric | Rueckstosstriebwerk mit Nachverbrennungseinrichtungen |
NL249340A (enrdf_load_stackoverflow) * | 1959-03-13 | |||
FR1588974A (enrdf_load_stackoverflow) * | 1968-10-02 | 1970-03-16 | ||
GB1390031A (en) * | 1971-08-21 | 1975-04-09 | Rolls Royce | Reheat system for a gas turbine engine |
-
1972
- 1972-06-01 FR FR7219731A patent/FR2188060B1/fr not_active Expired
-
1973
- 1973-05-28 DE DE2327187A patent/DE2327187C3/de not_active Expired
- 1973-05-31 US US365402A patent/US3899883A/en not_active Expired - Lifetime
- 1973-06-01 GB GB2617473A patent/GB1427197A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2472027C1 (ru) * | 2011-07-12 | 2013-01-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Уфимский государственный авиационный технический университет | Фронтовое устройство форсажной камеры со стабилизатором пламени изменяемой геометрии |
Also Published As
Publication number | Publication date |
---|---|
DE2327187A1 (de) | 1973-12-20 |
DE2327187C3 (de) | 1981-07-09 |
FR2188060B1 (enrdf_load_stackoverflow) | 1976-06-11 |
DE2327187B2 (de) | 1980-11-27 |
FR2188060A1 (enrdf_load_stackoverflow) | 1974-01-18 |
US3899883A (en) | 1975-08-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3931707A (en) | Augmentor flameholding apparatus | |
US2638745A (en) | Gas turbine combustor having tangential air inlets for primary and secondary air | |
US3055179A (en) | Gas turbine engine combustion equipment including multiple air inlets and fuel injection means | |
US2508420A (en) | Combustion apparatus | |
US3299632A (en) | Combustion chamber for a gas turbine engine | |
GB1180524A (en) | Gas Turbine Jet Engine of the By-Pass Type | |
US2799991A (en) | Afterburner flame stabilization means | |
GB1495672A (en) | Combustion systems for gas turbine engines | |
GB715909A (en) | Improvements in or relating to combustion equipment of gas-turbine engines | |
GB2371110A (en) | Fuel injectors | |
EP2400221B1 (en) | Ejector purge of cavity adjacent exhaust flowpath | |
GB1451354A (en) | Aerodynamic flame holder | |
US2632299A (en) | Precombustion chamber | |
GB884756A (en) | Primary air intake device for the combustion chamber of a gas-turbine unit | |
US2929211A (en) | Afterburner igniter | |
GB1427197A (en) | After burner installations for gas turbine engines | |
GB812201A (en) | Improvements in combustion equipment for continuous-flow internal combustion engines | |
US2982099A (en) | Fuel injection arrangement in combustion equipment for gas turbine engines | |
GB1180929A (en) | Combustion Apparatus, for example for Gas Turbines. | |
GB751013A (en) | Improvements in combustion devices particularly applicable to aircraft jet propulsion units | |
GB774059A (en) | Improvements in or relating to combined gas turbine plant and ram-jet units | |
US2729059A (en) | Continuous flow internal combustion engines, in particular aircraft engines | |
GB719301A (en) | Improvements relating to gas turbine engines | |
GB1242066A (en) | Improvements in reheat combustion apparatus for by-pass gas turbine engines | |
US3087301A (en) | Leading edge fuel manifold |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19920601 |