Patent
Burner for the combustion of fuel
| العنوان: | Burner for the combustion of fuel |
|---|---|
| Patent Number: | 5,649,494 |
| تاريخ النشر: | July 22, 1997 |
| Appl. No: | 08/386,873 |
| Application Filed: | February 10, 1995 |
| مستخلص: | A burner (10) for the combustion of fuel comprises a passage (32) through which in operation a mixed flow of fuel and air passes for primary combustion at it's outlet. Two further annular passages (34, 36), concentric with and radially outward of the passage (32), are provided through which supplementary flows of air pass to support the primary combustion. The outlets of the two annular passages (34, 36) diverge to discharge the supplementary flows of air at an angle to the mixed flow of fuel and air. Members (62) are provided in the annular passage which obstruct the discharge of the supplementary flow of air. Furnace gases circulate in the region downstream of the obstruction members (62). Circulation of the furnace gases delays the mixing of the fuel and air mixture with the supplementary air flows to reduce the nitrogen oxides produced. |
| Inventors: | Hufton, Peter F. (Etwall, GB2) |
| Assignees: | Rolls-Royce Power Engineering plc (Newcastle Upon Tyne, GB2) |
| Claim: | I claim |
| Claim: | 1. A burner for the combustion of fuel which in operation is mounted in the wall of a furnace and has a discharge plane adjacent the furnace wall comprising |
| Claim: | an at least one passage through which in operation a mixed flow of fuel and air passes for primary combustion at an outlet from said passage; and |
| Claim: | an at least one further annular passage concentric with and radially outward of the first passage through which a supplementary flow of air passes for discharge at an outlet for combustion with the products of said primary combustion, the at least one further annular passage diverging at its outlet to discharge the supplementary flow of air at an angle to the mixed flow of fuel and air, the outlet from the at least one further passage being provided with a plurality of members which pass across the outlet of said at least one further annular passage at the discharge plane of the burner to obstruct a portion of said at least one further annular passage, adjacent obstruction members defining a plurality of discrete apertures in the outlet of the at least one further passage through which the supplementary flow of air discharges, the apertures and orientation of the members being arranged whereby a pressure gradient is provided downstream of the obstruction members causing furnace gasses radially outward of the at least one further passage to flow radially inward and interpose between the mixed flow of air and fuel from the first passage and the supplementary air flow from the further passage, delaying mixing of the flows of the mixed flow of fuel and air and the supplementary flow of air downstream of the obstruction members and reducing the oxygen content of the supplementary air, thereby reducing the nitrogen oxides produced; the inlet to the at least one further passage being convergent and having guide vanes located therein. |
| Claim: | 2. A burner as claimed in claim 1 in which the obstructing members are wedge shaped. |
| Claim: | 3. A burner as claimed in claim 1 in which there are two further annular passages, a radially inner and a radially outer annular passage, both of which are concentric with the at least one first passage and which provide supplementary air flows for combustion with the products of said primary combustion. |
| Claim: | 4. A burner as claimed in claim 3 in which the amount of air passing through the inlet to the inner annular passage is controlled by a sliding damper. |
| Claim: | 5. A burner as claimed in claim 3 in which blades are provided in the radially inner annular passage which swirl the supplementary flow of air passing therethrough. |
| Claim: | 6. A burner as claimed in claim 5 in which the blades are moveable in an axial direction to vary the degree of swirl in the supplementary air passing therethrough. |
| Claim: | 7. A burner as claimed in claim 1 in which the at least one first passage is provided with elements which produce fuel rich areas in the air and fuel mixture passing therethrough and with flow disturbing members which modify the flow pattern of the air and fuel mixture at the outlet of the at least one first passage. |
| Claim: | 8. A burner as claimed in claim 7 in which the flow disturbing members are located in the wake of the flow from the elements. |
| Claim: | 9. A burner as claimed in claim 1 for the combustion of coal in which the obstructing members obstruct of the order of 15% of the supplementary flow of air. |
| Current U.S. Class: | 110/262; 110/104B; 110/264; 110/265; 110/347; 431/184 |
| Current International Class: | F23D 100 |
| Patent References Cited: | 4357134 November 1982 Katsuhige et al. 4443182 April 1984 Wojcieson et al. 4602571 July 1986 Chadshay 4930430 June 1990 Allen et al. 5199355 April 1993 Larue 5231937 August 1993 Kobayashi et al. 5415114 May 1995 Monro et al. |
| Primary Examiner: | Bennett, Henry A. |
| Assistant Examiner: | Tinker, Susanne C. |
| Attorney, Agent or Firm: | Oliff & Berridge |
| رقم الانضمام: | edspgr.05649494 |
| قاعدة البيانات: | USPTO Patent Grants |
| الوصف غير متاح. |