GB702216A - Improvements in liquid fuel burners - Google Patents
Improvements in liquid fuel burnersInfo
- Publication number
- GB702216A GB702216A GB2823050A GB2823050A GB702216A GB 702216 A GB702216 A GB 702216A GB 2823050 A GB2823050 A GB 2823050A GB 2823050 A GB2823050 A GB 2823050A GB 702216 A GB702216 A GB 702216A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- passage
- gas
- stem
- liquid fuel
- 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)
Abstract
702,216. Liquid-fuel burners. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Nov. 14, 1951 [Nov. 17, 1950], No. 28230/50. Class 75 (1) A liquid fuel burner assembly comprises two nested tubes 7, 8 constituting a stem having at its upper end a fixing head, e.g. a flange 13 for securing it to the wall of a combustion chamber, the inner tube 7 being connected to a supply of atomizing gas, e.g., air and the outer tube 8 being connected to a liquid fuel supply, and a gas-blast atomizing injector fixed to the lower end of the stem and formed internally firstly with a gas blast passage 2a. terminating in a discharge orifice 4d, and a fuel passage 4c leading transversely inwardly into the gas blast passage from a surrounding fuel chamber 4b, and secondly with two transferports 1e, 1d, connecting, respectively, the outer tube 8 with the gas blast passage 3. and the inner tube 7 with the fuel chamber 4b. The fuel passage 4c is annular and discharges fuel radially inward as in the liquid fuel injector described in Specification 702,215. The iujector body comprises a part 1 connected by a union 9 to the tube 7 and having threaded thereinto a lower part 2 providing the air passage 2a and containing a stem 3 having a helical swirling thread 3a. A cooling shroud 6 may be screwed on to the lower end of the casing 4 surrounding the injector body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2823050A GB702216A (en) | 1950-11-17 | 1950-11-17 | Improvements in liquid fuel burners |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2823050A GB702216A (en) | 1950-11-17 | 1950-11-17 | Improvements in liquid fuel burners |
Publications (1)
Publication Number | Publication Date |
---|---|
GB702216A true GB702216A (en) | 1954-01-13 |
Family
ID=10272377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2823050A Expired GB702216A (en) | 1950-11-17 | 1950-11-17 | Improvements in liquid fuel burners |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB702216A (en) |
-
1950
- 1950-11-17 GB GB2823050A patent/GB702216A/en not_active Expired
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