GB709352A - Fuel burner - Google Patents
Fuel burnerInfo
- Publication number
- GB709352A GB709352A GB18613/52A GB1861352A GB709352A GB 709352 A GB709352 A GB 709352A GB 18613/52 A GB18613/52 A GB 18613/52A GB 1861352 A GB1861352 A GB 1861352A GB 709352 A GB709352 A GB 709352A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- gas
- atomizer
- 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
- F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
709,352. Liquid and gaseous fuel burners. NAAMLOOZE VENNOOTSCHAP DE BATAAFSCHE PETROLEUM MAATSCHAPPIJ. July 23, 1952 [July 25, 1951], No. 18613/52. Class 75 (1) In a burner for the simultaneous combustion of liquid and gaseous fuels an auxiliary combustion chamber 3 for gaseous fuel is arranged around an atomizer 1 for liquid fuel so that the burning gas after leaving the chamber 3 impinges on the liquid fuel emerging from the atomizer, and the chamber 3 is fed exclusively with an oxygen-containing gas mixture. Part of the combustion air is fed through a tube 2 surrounding the atomizer 1. Preferably a gas-air mixture enters the chamber 3 from a supply chamber 4 through slits 5 at the inner edges of which flame stabilizing vortices are formed. Alternatively the stabilizing vortices may be formed by supplying the gas through circular apertures directed so that adjacent jets cross, or by supplying gas streams at different velocities. The mouth 7 of the chamber 3 converges almost to the cone of atomized fuel. A shield 6 protects the atomizer 1 from excessive heating by the gas flames. Secondary combustion air is supplied tangentially to the tubular main combustion chamber 8 through a conduit 9.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL709352X | 1951-07-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB709352A true GB709352A (en) | 1954-05-19 |
Family
ID=19812161
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18613/52A Expired GB709352A (en) | 1951-07-25 | 1952-07-23 | Fuel burner |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB709352A (en) |
-
1952
- 1952-07-23 GB GB18613/52A patent/GB709352A/en not_active Expired
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