GB819964A - Improvements in or relating to burner - Google Patents
Improvements in or relating to burnerInfo
- Publication number
- GB819964A GB819964A GB4991/56A GB499156A GB819964A GB 819964 A GB819964 A GB 819964A GB 4991/56 A GB4991/56 A GB 4991/56A GB 499156 A GB499156 A GB 499156A GB 819964 A GB819964 A GB 819964A
- Authority
- GB
- United Kingdom
- Prior art keywords
- baffle
- fuel
- air
- apertures
- combustion
- 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
- 239000000446 fuel Substances 0.000 abstract 8
- 238000002485 combustion reaction Methods 0.000 abstract 6
- 238000010276 construction Methods 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 239000011819 refractory material Substances 0.000 abstract 1
- 238000002791 soaking Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D99/00—Subject matter not provided for in other groups of this subclass
- F27D99/0001—Heating elements or systems
- F27D99/0033—Heating elements or systems using burners
- F27D99/0035—Heating indirectly through a radiant surface
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
819,964. Liquid fuel burners. BLOOM ENGINEERING CO. Inc. Feb. 17, 1956 [April 26, 1955], No. 4991/56. Class 75(1) [Also in Group XII] In a burner construction for furnaces with a chamber having an admission means for combustion air and gaseous fuel and a discharge end for the combustion air wherein the chamber is closed by a perforated baffle fastened adjacent the burner discharge end and penetrated by a central fuel feed passage supplied by a fuel admission tube the passage terminates close to the forward face of the baffle and is surrounded at its terminal part by air openings which penetrate the baffle with their axis extending in the direction of the fuel admission tube, the baffle has a flush surface on the discharge side thereof and the openings have length sufficient to direct the combustion air, are radially spaced outwardly of the fuel admission tube towards the baffle periphery and are separated peripherally from each other. In the arrangement shown in Fig. 1 air admitted to a channel 13 passes through apertures 25 in a baffle 23 of refractory material into a combustion zone 33 formed by a refractory member 32. The leading edges of apertures 25 are rounded and have a length to diameter ratio of about 3:1. Fuel is fed to the combustion zone 33 through a pipe 14 the forward end of which passes through the baffle 23 and is provided with apertures 31 which direct fuel outwardly between the air streams issuing from the apertures 25. The refractory member 32 may be outwardly, Fig. 1, or inwardly, Fig. 5 (not shown), tapered and the outlet may be of circular or rectangular cross-section. In a modification the tube 14 is open ended at its forward end. Oil atomized by steam or air may also be used. In the arrangement shown in Fig. 3 the burner 10, 32 is located at the top of a soaking pit 34 to uniformly heat ingots 37 and the flue 40 is at the bottom. In a further arrangement shown in Fig. 8 work-pieces 44 are pushed through heating zones 48, 49, 50 and the products of combustion from the burners 10<SP>11</SP> pass in the opposite direction, the movement of the work-pieces 44 and out through a flue 51.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US819964XA | 1955-04-26 | 1955-04-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB819964A true GB819964A (en) | 1959-09-09 |
Family
ID=22167730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4991/56A Expired GB819964A (en) | 1955-04-26 | 1956-02-17 | Improvements in or relating to burner |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB819964A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3209811A (en) * | 1963-03-28 | 1965-10-05 | Loftus Engineering Corp | Combination high velocity burner |
| US3223142A (en) * | 1962-11-19 | 1965-12-14 | James A Harrison | Automatic gas burner with variable flame port area |
-
1956
- 1956-02-17 GB GB4991/56A patent/GB819964A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3223142A (en) * | 1962-11-19 | 1965-12-14 | James A Harrison | Automatic gas burner with variable flame port area |
| US3209811A (en) * | 1963-03-28 | 1965-10-05 | Loftus Engineering Corp | Combination high velocity burner |
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