GB1003915A - Combustion apparatus and methods - Google Patents
Combustion apparatus and methodsInfo
- Publication number
- GB1003915A GB1003915A GB2391962A GB2391962A GB1003915A GB 1003915 A GB1003915 A GB 1003915A GB 2391962 A GB2391962 A GB 2391962A GB 2391962 A GB2391962 A GB 2391962A GB 1003915 A GB1003915 A GB 1003915A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fluid
- annular passage
- combustion supporting
- fuel gas
- passages
- 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
1,003,915. Burners. AIR REDUCTION CO. Inc. June 21, 1962 [June 21, 1961], No. 23919/ 62. Heading F4T. A burner discharges parallel streams of fuel gas and combustion supporting fluid, and a stream of an intermediate fluid between the fuel gas and the combustion supporting fluid to delay the mixing of the fuel gas and the combustion supporting fluid. The intermediate fluid may be air, nitrogen, argon, liquid oxygen, liquid nitrogen, water or steam. The combustion supporting fluid may be oxygen, fluorine, chlorine, nitrous oxide, ozone or hydrogen peroxide. The velocity of the intermediate fluid is regulated to control the location of the burner flame and hence the zone of maximum temperature in an open hearth furnace. The burner comprises seven tubes arranged concentrically or eccentrically but one within another to form, starting at the outermost, an annular passage for cooling water, an annular passage for the combustion supporting fluid, an annular passage for the intermediate fluid, a second annular passage for cooling water, an annular passage for the fuel gas and an annular passage for air or steam for atomizing liquid fuel discharged from a nozzle on the end of the innermost tube. The ends of the two cooling water passages are closed and an external pipe connects the two passages. Partitions extend along the length of the water passages. Valves are provided to control the supplies of fuel gas, combustion supporting fluid, intermediate fluid and water. Circular passages instead of annular ones for the combustion reactants may be used.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11872461A | 1961-06-21 | 1961-06-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1003915A true GB1003915A (en) | 1965-09-08 |
Family
ID=22380366
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2391962A Expired GB1003915A (en) | 1961-06-21 | 1962-06-21 | Combustion apparatus and methods |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1003915A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2213455A1 (en) * | 1973-01-08 | 1974-08-02 | Ghelfi Ag | |
GB2001161A (en) * | 1977-07-15 | 1979-01-24 | Zink Co John | Steam injection to zone of conset of combustion in fuel burner |
-
1962
- 1962-06-21 GB GB2391962A patent/GB1003915A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2213455A1 (en) * | 1973-01-08 | 1974-08-02 | Ghelfi Ag | |
GB2001161A (en) * | 1977-07-15 | 1979-01-24 | Zink Co John | Steam injection to zone of conset of combustion in fuel burner |
GB2001161B (en) * | 1977-07-15 | 1982-04-28 | Zink Co John | Steam injection to zone of conset of combustion in fuel burner |
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