CH365910A - Afterburner on a jet engine - Google Patents
Afterburner on a jet engineInfo
- Publication number
- CH365910A CH365910A CH6213358A CH6213358A CH365910A CH 365910 A CH365910 A CH 365910A CH 6213358 A CH6213358 A CH 6213358A CH 6213358 A CH6213358 A CH 6213358A CH 365910 A CH365910 A CH 365910A
- Authority
- CH
- Switzerland
- Prior art keywords
- afterburner
- jet engine
- jet
- engine
- Prior art date
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
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- 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
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1514458A GB842197A (en) | 1958-07-23 | 1958-05-12 | Improvements in afterburner combustion equipment of a gas turbine jet propulsion engine |
DEG24595A DE1123163B (en) | 1958-05-23 | 1958-05-23 | Recoil engine with afterburners |
CH6213358A CH365910A (en) | 1958-07-23 | 1958-07-23 | Afterburner on a jet engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH6213358A CH365910A (en) | 1958-07-23 | 1958-07-23 | Afterburner on a jet engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CH365910A true CH365910A (en) | 1962-11-30 |
Family
ID=4524103
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH6213358A CH365910A (en) | 1958-05-23 | 1958-07-23 | Afterburner on a jet engine |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH365910A (en) |
GB (1) | GB842197A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2873168B1 (en) * | 2004-07-16 | 2008-10-31 | Snecma Moteurs Sa | TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER |
GB201907834D0 (en) * | 2019-06-03 | 2019-07-17 | Rolls Royce Plc | A fuel sparay nozzle arrangement |
-
1958
- 1958-05-12 GB GB1514458A patent/GB842197A/en not_active Expired
- 1958-07-23 CH CH6213358A patent/CH365910A/en unknown
Also Published As
Publication number | Publication date |
---|---|
GB842197A (en) | 1960-07-20 |
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