GB1419547A - Heat generators - Google Patents
Heat generatorsInfo
- Publication number
- GB1419547A GB1419547A GB585973A GB585973A GB1419547A GB 1419547 A GB1419547 A GB 1419547A GB 585973 A GB585973 A GB 585973A GB 585973 A GB585973 A GB 585973A GB 1419547 A GB1419547 A GB 1419547A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- combustion
- combustion chamber
- burner
- chamber
- 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
- 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
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M5/00—Casings; Linings; Walls
- F23M5/08—Cooling thereof; Tube walls
- F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
1419547 Combustion apparatus G M GOUBSKY 6 Feb 1973 5859/73 Heading F4B A heat generator comprises a cavity wall structure 1 providing a combustion chamber and a passage surrounding it for preheating the combustion air, an air inlet opening tangentially into the cavity, an air distribution ring 4 with tangential vaned inlets 8, connected to the upper and lower sections of the combustion chamber by spacers 7 providing air gaps, the effect of the inlets and the gaps being to produce toroidal vortices 24, 26 of secondary air in the combustion -chamber. Liquid fuel is fed under pressure to the jet 8 of the burner and the burner is surrounded by a swirler ring 10 for primary combustion air. Ignition electrodes 14 are provided to light the burner. The burning fuel spray from the jet 12 rises in a cone and penetrates the toroid 24. Any droplets not burned here enter and are burned in toroid 26. The hot combustion products leave the combustion chamber at E. In a similar form (Fig. 3, not shown) there are two air distribution rings, one in a narrow part of the combustion chamber near the fuel jet and one higher up in a wider section of the chamber. Such a combustion chamber is shown in Fig. 4. In this form however, the incoming combustion air is distributed via a box 39 to a number of heat-exchange tubes 45, 46 surrounding the combustion chamber, before being introduced into the combustion chamber through the distributer ring 38. There is a similar arrangement for the lower ring 50 and the bottom cone of the combustion chamber is surrounded by a heat exchanger coil 59 for the fuel. The chambers C, D, F containing the heatexchange tubes are filled with a heat transfer medium, e.g. a powder, granules, molten salts, liquids of high thermal conductivity and enthalpy or liquids in vapour phase. Tertiary combustion air is fed by a blower fitted with a damper into the inlet port 41. Primary and secondary air are also supplied under pressure as in the form of Fig. 1. In another form (Figs. 7-9, not shown) the combustion chamber is not cooled by the incoming combustion air but by a circulating cooling liquid. The air is applied to the burner and three successive distributicm rings either direct or after having been preheated.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB585973A GB1419547A (en) | 1973-02-06 | 1973-02-06 | Heat generators |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB585973A GB1419547A (en) | 1973-02-06 | 1973-02-06 | Heat generators |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1419547A true GB1419547A (en) | 1975-12-31 |
Family
ID=9803968
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB585973A Expired GB1419547A (en) | 1973-02-06 | 1973-02-06 | Heat generators |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1419547A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210172601A1 (en) * | 2018-08-20 | 2021-06-10 | Frank Ostermann | Method for operating a combustion arrangement and combustion arrangement |
-
1973
- 1973-02-06 GB GB585973A patent/GB1419547A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210172601A1 (en) * | 2018-08-20 | 2021-06-10 | Frank Ostermann | Method for operating a combustion arrangement and combustion arrangement |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |