GB839212A - Burner for liquid fuel - Google Patents
Burner for liquid fuelInfo
- Publication number
- GB839212A GB839212A GB20322/57A GB2032257A GB839212A GB 839212 A GB839212 A GB 839212A GB 20322/57 A GB20322/57 A GB 20322/57A GB 2032257 A GB2032257 A GB 2032257A GB 839212 A GB839212 A GB 839212A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- liquid fuel
- burner
- axial
- producing
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
839,212. Spray burners. ENTREPRISE GENERALE DE CHAUFFAGE INDUSTRIEL PILLARD FRERES & CIE. S.A. June 27, 1957 [July 2, 1956; April 18, 1957], No. 20322/57. Class 75(1) A liquid fuel burner of the spray type comprises a primary nozzle 6, an annular element 5a co-axial with the nozzle and having tangential passages for producing a rotary motion of the primary fuel stream, a wall 11 downstream of the nozzle 6 having a cylindrical orifice 11a coaxial with and of greater diameter than the nozzle, an annular element 15 co-axial with the nozzle 6 and between this and the wall 11 having tangential passages for producing a rotary motion of the secondary fuel stream, and means for controlling the flow of each stream independently.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR839212X | 1956-07-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB839212A true GB839212A (en) | 1960-06-29 |
Family
ID=9299412
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20322/57A Expired GB839212A (en) | 1956-07-02 | 1957-06-27 | Burner for liquid fuel |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB839212A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2128107A (en) * | 1982-10-01 | 1984-04-26 | Spraying Systems Co | Whirl spray nozzle |
FR2578630A1 (en) * | 1985-03-05 | 1986-09-12 | Deutsche Forsch Luft Raumfahrt | FUEL ATOMIZATION METHOD AND BURNER FOR COMBUSTION OR GASIFICATION |
US4664314A (en) * | 1982-10-01 | 1987-05-12 | Spraying Systems Co. | Whirl spray nozzle |
-
1957
- 1957-06-27 GB GB20322/57A patent/GB839212A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2128107A (en) * | 1982-10-01 | 1984-04-26 | Spraying Systems Co | Whirl spray nozzle |
US4664314A (en) * | 1982-10-01 | 1987-05-12 | Spraying Systems Co. | Whirl spray nozzle |
FR2578630A1 (en) * | 1985-03-05 | 1986-09-12 | Deutsche Forsch Luft Raumfahrt | FUEL ATOMIZATION METHOD AND BURNER FOR COMBUSTION OR GASIFICATION |
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