GB654340A - Improvements in or relating to gas burners - Google Patents
Improvements in or relating to gas burnersInfo
- Publication number
- GB654340A GB654340A GB29797/48A GB2979748A GB654340A GB 654340 A GB654340 A GB 654340A GB 29797/48 A GB29797/48 A GB 29797/48A GB 2979748 A GB2979748 A GB 2979748A GB 654340 A GB654340 A GB 654340A
- Authority
- GB
- United Kingdom
- Prior art keywords
- manifold
- ports
- jets
- burner
- tubes
- 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
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/34—Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
Abstract
<PICT:0654340/III/1> A gas burner particularly for use in the manufacture of carbon black by a process employing a high velocity blast flame, e.g. as described in U.S.A. Specification 2,378,055, comprises a fuel gas manifold adapted to be moved back and forth within a wind-box supplied with air under super-atmospheric pressure, a plurality of substantially parallel burner ports extending through a refractory block of substantial thickness, and a plurality of gas jets each connected with the manifold by a tube of length substantially greater than the depth of the burner ports, the jets and connecting tubes being positioned coaxially with the respective burner ports, and maintained in alignment therewith during said back and forth movement. The wind-box 19, Fig. 2, is divided by partitions 22 into three sections in each of which is mounted a fuel gas manifold 24 supported by carriages 25 running on tracks 26. Each manifold 24 carries four rows of three burner jets 28 connected to the manifold by tubes 27 coaxial with flared metal tubes 17 projecting from ports 15 in a block 7 of refractory material, the length of a tube 27 being greater than the combined lengths of a tube 17 and a port 15. On starting up the burner the jets 28 are moved downstream of the block 7 by moving each carriage 25 by rotating a rod 34, screw-threaded through a boss 36 on the end wall of the wind-box, and connected by a swivel coupling 39 with the manifold 24. The fuel supply pipe 30 connected with each manifold 24 is slidable through a gland 31 in the end wall of the wind-box and is provided with calibration marks which co-operate with an indicator finger 32 to provide means for determining the relative positions of the jets 28 and the ports 15. When combustion has been established the jets 28 are withdrawn to positions near the entrance to the ports 15. The air supply may be controlled by adjustable dampers 23. The hydrocarbon gas to be decomposed to form carbon black is introduced into the flame downstream of the ports 15 through tubes projecting through the furnace walls. In a modified construction the hydrocarbon is supplied through tubes passing through the refractory block 7. U.S.A. Specifications 2,440,423 and 2,440,424 also are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US654340XA | 1948-01-15 | 1948-01-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB654340A true GB654340A (en) | 1951-06-13 |
Family
ID=22062689
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29797/48A Expired GB654340A (en) | 1948-01-15 | 1948-11-16 | Improvements in or relating to gas burners |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB654340A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007098735A2 (en) * | 2006-03-02 | 2007-09-07 | Weiher, Thomas | Combustion process and fuel reservoir therefor |
WO2010002762A3 (en) * | 2008-06-30 | 2010-03-25 | Praxair Technology, Inc. | Reliable ignition of hot oxygen generator |
-
1948
- 1948-11-16 GB GB29797/48A patent/GB654340A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007098735A2 (en) * | 2006-03-02 | 2007-09-07 | Weiher, Thomas | Combustion process and fuel reservoir therefor |
WO2007098735A3 (en) * | 2006-03-02 | 2007-12-06 | Weiher Thomas | Combustion process and fuel reservoir therefor |
WO2010002762A3 (en) * | 2008-06-30 | 2010-03-25 | Praxair Technology, Inc. | Reliable ignition of hot oxygen generator |
JP2011526998A (en) * | 2008-06-30 | 2011-10-20 | プラクスエア・テクノロジー・インコーポレイテッド | Reliable ignition of high temperature oxygen generator |
US8105074B2 (en) | 2008-06-30 | 2012-01-31 | Praxair Technology, Inc. | Reliable ignition of hot oxygen generator |
CN102077025B (en) * | 2008-06-30 | 2013-03-27 | 普莱克斯技术有限公司 | Method and device of hot oxygen generator |
RU2511902C2 (en) * | 2008-06-30 | 2014-04-10 | Праксайр Текнолоджи, Инк. | Reliable ignition of hot oxygen generator |
AU2009267144B2 (en) * | 2008-06-30 | 2015-05-07 | Praxair Technology, Inc. | Reliable ignition of hot oxygen generator |
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