BE463581A - - Google Patents
Info
- Publication number
- BE463581A BE463581A BE463581DA BE463581A BE 463581 A BE463581 A BE 463581A BE 463581D A BE463581D A BE 463581DA BE 463581 A BE463581 A BE 463581A
- Authority
- BE
- Belgium
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
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- 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
- 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2529506X | 1944-04-15 | ||
GB7011/44A GB599257A (en) | 1945-03-20 | 1945-04-14 | Improvements relating to burners for liquid or gaseous fuels |
Publications (1)
Publication Number | Publication Date |
---|---|
BE463581A true BE463581A (en) |
Family
ID=32232353
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE463581D BE463581A (en) | 1944-04-15 |
Country Status (4)
Country | Link |
---|---|
US (1) | US2529506A (en) |
BE (1) | BE463581A (en) |
CH (1) | CH264718A (en) |
NL (1) | NL68431C (en) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2639581A (en) * | 1944-09-14 | 1953-05-26 | Power Jets Res & Dev Ltd | Apparatus for burning fuel in a high velocity gas stream |
US2625795A (en) * | 1946-02-26 | 1953-01-20 | Thermal Res And Engineering Co | Combustion stabilization means for high-velocity air streams having a pilot burner and a streamline igniter grill |
US2667033A (en) * | 1947-01-09 | 1954-01-26 | Power Jets Res & Dev Ltd | Combustion apparatus for operation in fast-moving air streams |
US2682148A (en) * | 1947-12-02 | 1954-06-29 | Ralph C Brierly | Apparatus for progressive injection of combustibles in peripheral type burners |
US2730863A (en) * | 1948-04-16 | 1956-01-17 | Lockheed Aircraft Corp | Gaseous fuel turbine power plant having parallel connected compressors |
US2657532A (en) * | 1948-09-02 | 1953-11-03 | Power Jets Res & Dev Ltd | Liquid fuel atomizer located upstream of a flame stabilizing baffle |
US2659195A (en) * | 1948-11-01 | 1953-11-17 | Mcdonnell Aircraft Corp | Flame holder and fuel distributing mechanism for ram-jet engines |
GB650608A (en) * | 1948-11-26 | 1951-02-28 | Lucas Ltd Joseph | Improvements relating to internal combustion engine systems |
US2625788A (en) * | 1948-12-15 | 1953-01-20 | Mcdonnell Aircraft Corp | Flame holder and fuel nozzle supporting mechanism for ram jet engines |
US2729059A (en) * | 1949-05-28 | 1956-01-03 | Onera (Off Nat Aerospatiale) | Continuous flow internal combustion engines, in particular aircraft engines |
US2714287A (en) * | 1950-01-03 | 1955-08-02 | Westinghouse Electric Corp | Flameholder device for turbojet afterburner |
US2726511A (en) * | 1950-05-18 | 1955-12-13 | Solar Aircraft Co | Afterburners |
US2697910A (en) * | 1950-07-29 | 1954-12-28 | Thermal Res And Engineering Co | Fluid fuel burner with self-contained fuel vaporizing unit |
US2720754A (en) * | 1950-09-29 | 1955-10-18 | Mcdonnell Aircraft Corp | Flameholder for ram jet engine |
US2781637A (en) * | 1950-12-15 | 1957-02-19 | Gen Motors Corp | Combustion chamber with fuel vaporizer |
US2651178A (en) * | 1951-01-18 | 1953-09-08 | A V Roe Canada Ltd | Combination injector and stabilizer for gas turbine afterburners |
US2729937A (en) * | 1951-03-20 | 1956-01-10 | United Aircraft Corp | Retractable flameholders for afterburners |
US2693083A (en) * | 1951-03-26 | 1954-11-02 | Roy W Abbott | Combination flame-holder and fuel nozzle |
US3029603A (en) * | 1951-10-26 | 1962-04-17 | Howard E Brown | Air bled fuel injector system |
DE957003C (en) * | 1951-11-20 | 1957-01-24 | Hiller Helicopters | Continuously working ramjet engine for rotor blades of helicopters |
US2740482A (en) * | 1951-11-20 | 1956-04-03 | Hiller Helicopters | Rotor blade mounted jet engine |
US2840990A (en) * | 1952-07-17 | 1958-07-01 | John P Longwell | Multistage fuel injection for ram-jet combustor |
US2775867A (en) * | 1952-08-22 | 1957-01-01 | Continental Aviat & Engineerin | Ram jet engines |
DE1259143B (en) * | 1953-06-27 | 1968-01-18 | Snecma | Flame stabilization device |
NL90169C (en) * | 1953-06-27 | |||
DE1045728B (en) * | 1953-07-15 | 1958-12-04 | Snecma | Incinerator |
US2859588A (en) * | 1953-12-16 | 1958-11-11 | Texas Co | Flame holder structure for ram jet combustor |
US2927427A (en) * | 1955-05-10 | 1960-03-08 | Onera (Off Nat Aerospatiale) | Continuous flow thermal machines and in particular in ram-jets and turbojets |
DE1053873B (en) * | 1955-05-13 | 1959-03-26 | Snecma | Flame stabilization device |
US2999359A (en) * | 1956-04-25 | 1961-09-12 | Rolls Royce | Combustion equipment of gas-turbine engines |
DE1276414B (en) * | 1956-07-13 | 1968-08-29 | Snecma | Incinerator |
DE1049157B (en) * | 1956-08-10 | 1959-01-22 | Ernst Heinkel Fahrzeugbau G M | Combustion or mixing chamber with backflow, especially for jet engines and gas turbines |
US2934894A (en) * | 1957-07-23 | 1960-05-03 | Orenda Engines Ltd | Fuel supply and flame stabilizing apparatus for afterburners for jet engines |
DE1097213B (en) * | 1958-05-22 | 1961-01-12 | Rolls Royce | Incinerator for gas turbine engines |
US3102392A (en) * | 1959-04-21 | 1963-09-03 | Snecma | Combustion equipment for jet propulsion units |
US3205658A (en) * | 1963-09-16 | 1965-09-14 | Aldo B Vanoni | Fuel burner with flame holder |
US4765136A (en) * | 1985-11-25 | 1988-08-23 | United Technologies Corporation | Gas turbine engine augmentor |
CN117109029B (en) * | 2023-08-25 | 2024-02-02 | 西南科技大学 | Blunt body flame stabilizer and aeroengine combustion assembly |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1434021A (en) * | 1922-10-31 | Hydbocabbon bubneb | ||
US1542294A (en) * | 1921-04-08 | 1925-06-16 | James B Blackburn | Burner |
US1988456A (en) * | 1930-03-24 | 1935-01-22 | Milo Ab | Gas turbine system |
US2111432A (en) * | 1935-01-16 | 1938-03-15 | Gen Electric | Fuel burning apparatus and air inlet device therefor |
US2085800A (en) * | 1935-11-25 | 1937-07-06 | Robert H Goddard | Combustion apparatus |
US2164225A (en) * | 1936-11-23 | 1939-06-27 | Int Harvester Co | Liquid fuel burner |
NL82403C (en) * | 1939-12-09 | |||
US2385833A (en) * | 1943-01-27 | 1945-10-02 | Kevork K Nahigyan | Fuel vaporizer for jet propulsion units |
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0
- NL NL68431D patent/NL68431C/xx active
- BE BE463581D patent/BE463581A/xx unknown
-
1945
- 1945-08-08 US US609532A patent/US2529506A/en not_active Expired - Lifetime
-
1946
- 1946-02-27 CH CH264718D patent/CH264718A/en unknown
Also Published As
Publication number | Publication date |
---|---|
CH264718A (en) | 1949-10-31 |
NL68431C (en) | |
US2529506A (en) | 1950-11-14 |