GB188025A - Improvements in or relating to burners for fluid-fuel - Google Patents
Improvements in or relating to burners for fluid-fuelInfo
- Publication number
- GB188025A GB188025A GB1796721A GB1796721A GB188025A GB 188025 A GB188025 A GB 188025A GB 1796721 A GB1796721 A GB 1796721A GB 1796721 A GB1796721 A GB 1796721A GB 188025 A GB188025 A GB 188025A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- fuel
- steam
- burner
- tapered
- 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
Abstract
188,025. Bliss, J. July 1, 1921. Air and steam pressure sprayers.-The fuelsupply tube 10 of a liquid-fuel burner is secured at one end in a bored plug 11 which closes one end of a jacket 12 to which steam, hot air, or other atomizing-fluid or gas is supplied through an inlet 24. A nozzle 14 secured to the outlet end of the fuel tube has a cylindrical exterior middle portion 17 and a tapered extremity 18 fitting in a burner nozzle 19 which is tapered inwardly to a restriction 23 and then flared outwardly. The fuel passes through a restriction 16 in the nozzle 14 and issues into the nozzle 19 through an outwardly flared bore on which it is met and partially atomized by steam from the jacket space delivered through converging conduits 31. The atomization of the mixture is completed in the nozzle 19 by swirling streams of the steam delivered through inclined passages 21 in the cylindrical portion 17 of the nozzle 14 and the tapered annular space 22 between the nozzles 14, 19. The passages 21, 22 may alternatively be formed in the burner nozzle 19 or be partly in the fuel nozzle 14 and partly in the burner nozzle 19.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1796721A GB188025A (en) | 1921-07-01 | 1921-07-01 | Improvements in or relating to burners for fluid-fuel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1796721A GB188025A (en) | 1921-07-01 | 1921-07-01 | Improvements in or relating to burners for fluid-fuel |
Publications (1)
Publication Number | Publication Date |
---|---|
GB188025A true GB188025A (en) | 1922-11-01 |
Family
ID=10104329
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1796721A Expired GB188025A (en) | 1921-07-01 | 1921-07-01 | Improvements in or relating to burners for fluid-fuel |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB188025A (en) |
-
1921
- 1921-07-01 GB GB1796721A patent/GB188025A/en not_active Expired
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