GB857384A - Flameholder for stabilising combustion in gas passages, such as the afterburners of aircraft jet engines - Google Patents
Flameholder for stabilising combustion in gas passages, such as the afterburners of aircraft jet enginesInfo
- Publication number
- GB857384A GB857384A GB3341258A GB3341258A GB857384A GB 857384 A GB857384 A GB 857384A GB 3341258 A GB3341258 A GB 3341258A GB 3341258 A GB3341258 A GB 3341258A GB 857384 A GB857384 A GB 857384A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vanes
- velocity
- axis
- flameholder
- gas
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 4
- 230000003019 stabilising effect Effects 0.000 title 1
- 238000009792 diffusion process Methods 0.000 abstract 2
- 238000011144 upstream manufacturing Methods 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
- F23R3/02—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)
- Incineration Of Waste (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH6593358A CH425349A (fr) | 1958-11-07 | 1958-11-07 | Guide-flamme pour chambre de combustion de propulseur à réaction |
Publications (1)
Publication Number | Publication Date |
---|---|
GB857384A true GB857384A (en) | 1960-12-29 |
Family
ID=4526753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3341258A Expired GB857384A (en) | 1958-11-07 | 1958-10-20 | Flameholder for stabilising combustion in gas passages, such as the afterburners of aircraft jet engines |
Country Status (3)
Country | Link |
---|---|
BE (1) | BE572738A (enrdf_load_stackoverflow) |
CH (1) | CH425349A (enrdf_load_stackoverflow) |
GB (1) | GB857384A (enrdf_load_stackoverflow) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104896510A (zh) * | 2015-05-13 | 2015-09-09 | 广东电网有限责任公司电力科学研究院 | 火焰稳定器和带有该火焰稳定器的地面燃机燃烧室 |
CN114719293A (zh) * | 2022-03-24 | 2022-07-08 | 西北工业大学 | 一种环腔加力燃烧室结构 |
-
0
- BE BE572738D patent/BE572738A/xx unknown
-
1958
- 1958-10-20 GB GB3341258A patent/GB857384A/en not_active Expired
- 1958-11-07 CH CH6593358A patent/CH425349A/fr unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104896510A (zh) * | 2015-05-13 | 2015-09-09 | 广东电网有限责任公司电力科学研究院 | 火焰稳定器和带有该火焰稳定器的地面燃机燃烧室 |
CN104896510B (zh) * | 2015-05-13 | 2017-02-01 | 广东电网有限责任公司电力科学研究院 | 火焰稳定器和带有该火焰稳定器的地面燃机燃烧室 |
CN114719293A (zh) * | 2022-03-24 | 2022-07-08 | 西北工业大学 | 一种环腔加力燃烧室结构 |
Also Published As
Publication number | Publication date |
---|---|
CH425349A (fr) | 1966-11-30 |
BE572738A (enrdf_load_stackoverflow) |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3299632A (en) | Combustion chamber for a gas turbine engine | |
US3374624A (en) | Gas turbine engine combustion equipment | |
US3643431A (en) | Flow control devices | |
US2475911A (en) | Combustion apparatus | |
US2676460A (en) | Burner construction of the can-an-nular type having means for distributing airflow to each can | |
US4177637A (en) | Inlet for annular gas turbine combustor | |
GB1427146A (en) | Combustion apparatus for gas turbine engines | |
US2977760A (en) | Annular combustion chambers for use with compressors capable of discharging combustion supporting medium with a rotary swirl through an annular outlet | |
GB1247144A (en) | Combustion chambers, especially for use in gas turbine engines | |
US3383855A (en) | Gas turbine engine | |
GB1179166A (en) | An Annular Combustion Chamber for a Gas Turbine Engine. | |
GB981848A (en) | Gas turbine plant | |
US3026675A (en) | Device for the air intake into the primary zone of a combustion chamber in a turbo-machine | |
US3896615A (en) | Gas turbine engine for subsonic flight | |
US3451216A (en) | Combustion equipment | |
GB970189A (en) | Combustion equipment for a gas turbine engine | |
US3082603A (en) | Combustion chamber with primary and secondary air flows | |
US3364678A (en) | Means for stabilizing fluid flow in diffuser-combustor systems in axial flow gas turbine engines | |
US2709337A (en) | Boundary layer control for the diffuser of a gas turbine | |
US3019605A (en) | Combustion apparatus of gas turbine engines with means controlling air flow conditions in the combustion apparatus | |
US3119234A (en) | Combustion chamber for a gas turbine engine | |
GB836117A (en) | Improvements in or relating to combustion equipment for gas-turbine engines | |
GB1090147A (en) | Thrust nozzle for supersonic gas turbine jet engines of the by-pass type | |
US3447317A (en) | Combustion chamber | |
GB857384A (en) | Flameholder for stabilising combustion in gas passages, such as the afterburners of aircraft jet engines |