GB970222A - Improvements in liquid fuel burning apparatus - Google Patents
Improvements in liquid fuel burning apparatusInfo
- Publication number
- GB970222A GB970222A GB1251863A GB1251863A GB970222A GB 970222 A GB970222 A GB 970222A GB 1251863 A GB1251863 A GB 1251863A GB 1251863 A GB1251863 A GB 1251863A GB 970222 A GB970222 A GB 970222A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- chamber
- combustion
- fuel
- combustion chamber
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/02—Disposition of air supply not passing through burner
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Spray-Type Burners (AREA)
Abstract
970,222. Liquid fuel combustion apparatus. A. F. ANDEN. March 29, 1963 [April 17, 1962; Feb. 23, 1963], No. 12518/63. Heading F4B. [Also in Division F1] Liquid fuel combustion apparatus comprises a combustion chamber of circular cross-section open at one end, a nozzle for the supply of atomized fuel at the other end, which is connected to a source of compressed primary air, and a plurality of inclined guide vanes in the combustion zone extending nearly across the width of the chamber. In one embodiment, Fig. 1, the primary air and atomized fuel from the nozzle 7 are given a rotation by vanes 6 in the air supply cone 3 which is of the opposite sense to that given to air passing through the annular passage 4 by vanes 5. Helicoidal wings 14 mounted on a hub 15 in the combustion chambers directs the fuel-air mixture towards the walls of the chamber with a rotation which is opposed to that of the secondary air flowing in through channels 13, which are inclined towards the fuel supply end of the chamber. The secondary air flows through annular channels 11, 9 to the inlets 13, forming a cooling jacket and becoming heated. In a modification, Fig. 3, the wings 34a, 34b in the combustion chamber 23 are formed by inclined plates which are adjustable longitudinally of the chamber. A secondary combustion chamber 24 of enlarged crosssection, has tertiary air supply passages 32, supplying air with a whirl opposed to that of the air supplied to the combustion chamber 23 by passages 31. Further air is supplied near the outlet of the secondary combustion chamber 24 by passages 33 having an inclination opposed to that of inlets 32.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE424462A SE189130C1 (en) | 1962-04-17 | 1962-04-17 | |
SE1999/63A SE305273B (en) | 1963-02-23 | 1963-02-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB970222A true GB970222A (en) | 1964-09-16 |
Family
ID=26654310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1251863A Expired GB970222A (en) | 1962-04-17 | 1963-03-29 | Improvements in liquid fuel burning apparatus |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1451328A1 (en) |
DK (1) | DK102875C (en) |
GB (1) | GB970222A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4013395A (en) * | 1971-05-11 | 1977-03-22 | Wingaersheek, Inc. | Aerodynamic fuel combustor |
US4661135A (en) * | 1985-01-25 | 1987-04-28 | Isover Saint-Gobain | Burner for manufacturing mineral fibers |
GB2196394A (en) * | 1986-10-14 | 1988-04-27 | Gen Electric | Propulsion device |
US4835959A (en) * | 1986-10-14 | 1989-06-06 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
-
1963
- 1963-03-29 GB GB1251863A patent/GB970222A/en not_active Expired
- 1963-03-29 DK DK142863A patent/DK102875C/en active
- 1963-04-05 DE DE19631451328 patent/DE1451328A1/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4013395A (en) * | 1971-05-11 | 1977-03-22 | Wingaersheek, Inc. | Aerodynamic fuel combustor |
US4661135A (en) * | 1985-01-25 | 1987-04-28 | Isover Saint-Gobain | Burner for manufacturing mineral fibers |
GB2196394A (en) * | 1986-10-14 | 1988-04-27 | Gen Electric | Propulsion device |
US4835959A (en) * | 1986-10-14 | 1989-06-06 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
GB2196394B (en) * | 1986-10-14 | 1991-06-26 | Gen Electric | Rocket propulsion system. |
Also Published As
Publication number | Publication date |
---|---|
DE1451328A1 (en) | 1968-12-19 |
DK102875C (en) | 1965-10-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2601000A (en) | Combustor for thermal power plants having toroidal flow path in primary mixing zone | |
US3030773A (en) | Vortex type combustion with means for supplying secondary air | |
US2679137A (en) | Apparatus for burning fuel in a fast moving gas stream | |
US4348170A (en) | Dual register, split stream burner assembly with divider cone | |
GB1371116A (en) | Dual fuel air-atomized fuel nozzle | |
GB1256951A (en) | ||
US2541170A (en) | Air intake arrangement for air jacketed combustion chambers | |
US2577918A (en) | Air jacketed combustion chamber flame tube | |
GB970189A (en) | Combustion equipment for a gas turbine engine | |
US2018582A (en) | Gas burner or the like | |
GB944445A (en) | Combustion apparatus for the combustion of gaseous and liquid fuels | |
GB970222A (en) | Improvements in liquid fuel burning apparatus | |
US2674846A (en) | Combustion chamber with baffle means to control secondary air | |
GB1001032A (en) | Improvements in or relating to multiple fuel burner assemblies | |
US3208502A (en) | Fuel burners having air control means | |
US4145880A (en) | Vorbix augmenter configuration with diffuser and vorbix swirler | |
US2407188A (en) | Burner | |
GB1414813A (en) | Vortex burner with swirling auxiliary air flow | |
ES8300192A1 (en) | Dual register, split stream burner assembly | |
GB1135104A (en) | Combustion equipment | |
GB1305994A (en) | ||
GB791225A (en) | Burners | |
SU382880A1 (en) | GAS-BURNER | |
SU128965A1 (en) | Furnace for pyrolysis of hydrocarbon gases | |
GB1299133A (en) | Gas burner |