| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 多模式燃烧装置及其使用方法 | CN201080004632.5 | 2010-01-15 | CN102282418B | 2014-11-05 | M.J.沃森; D.J.斯特兰奇; J.K.朱雷塔斯; K.A.利弗 |
| 本发明提供一种用于在正常操作的氧化剂或正常操作的燃料的供应被中断或暂时减少时用燃烧装置来持续燃烧的设备。空气或富含氧气的空气或者氧气和气态燃料或液态燃料或者气态和液态燃料两者被引入到燃烧设备中取代正常氧化剂-燃料混合物以实现燃烧并且在炉中保持加热水平。燃烧器能够以下述九种点火模式中的任何一种进行点火：空气-气体；空气-氧气-气体；氧气-气体；空气-燃油；空气-氧气-燃油；氧气-燃油；空气-燃油-气体；空气-氧气-燃油-气体；氧气-燃油-气体。 | ||||||
| 2 | 燃烧装置 | CN201611096333.4 | 2016-12-02 | CN106524147A | 2017-03-22 | 王成文; 刘晶; 王若言 |
| 本发明公开了一种燃烧装置，用以对重油进行燃烧工作，其包括一油罐、一燃烧主体和一烟囱，油罐用以装设重油，油罐与燃烧主体之间通过供油管道进行导通，一第一重油入口靠近油罐且分别一端连接供油管道，另一端连接燃烧主体，且燃烧主体靠近第一重油入口处还设有喷嘴，燃烧主体内设有点火器，并且点火器上方会产生火焰，于第一重油入口与油罐之间设有一微孔通道，供油管道贯穿微孔通道，一第二重油入口远离油罐且分别一端连接供油管道，另一端连接燃烧主体，且燃烧主体靠近第二重油入口处还设有喷嘴，燃烧主体与烟囱之间透过一烟道相导通，且于燃烧主体与烟囱之间设有一富集燃烧器，烟道贯穿富集燃烧器，充分燃烧且环保。 | ||||||
| 3 | 用于部分氧化液体含碳燃料的燃烧器及方法 | CN201180021041.3 | 2011-03-24 | CN102883993A | 2013-01-16 | 克里斯托弗·拜尔; 洛塔尔·布雷姆; 霍尔格·施利希廷; 冈特·海因茨; 迪特尔·乌尔伯; 于尔根·伯勒 |
| 本发明涉及一种用于使液体含碳燃料部分氧化的燃烧器，所述燃料含有水蒸汽和含氧气体，并涉及一种方法，在该方法中使用了所述燃烧器，其中被导向燃烧室的燃烧器出口孔的部分完全地或部分地设有用于相对于热负荷和/或腐蚀进行保护的涂层或扩散层。 | ||||||
| 4 | 多模式燃烧装置及其使用方法 | CN201080004632.5 | 2010-01-15 | CN102282418A | 2011-12-14 | M.J.沃森; D.J.斯特兰奇; J.K.朱雷塔斯; K.A.利弗 |
| 提供一种用于在正常操作的氧化剂或正常操作的燃料的供应被中断或暂时减少时用燃烧装置来持续燃烧的设备。空气或富含氧气的空气或者氧气和气态燃料或液态燃料或者气态和液态燃料两者被引入到燃烧设备中取代正常氧化剂-燃料混合物以实现燃烧并且在炉中保持加热水平。燃烧器能够以下述九种点火模式中的任何一种进行点火：空气-气体；空气-氧气-气体；氧气-气体；空气-燃油；空气-氧气-燃油；氧气-燃油；空气-燃油-气体；空气-氧气-燃油-气体；氧气-燃油-气体。 | ||||||
| 5 | 液体燃料燃烧系统 | CN99122813.8 | 1999-11-30 | CN1259636A | 2000-07-12 | 奥利维耶·德拉布罗伊; 皮埃尔·博得林; 迈克尔·乔希; 伯纳德·拉贝戈尔; 弗朗索瓦斯·拉卡斯 |
| 一种借助液体燃料和含有20%－100体积%的氧的气体氧化剂的燃烧方法,可保证火焰的稳定性,其中由下式限定的系数S在燃烧过程中保持小于或等于1,右式中d为喷射器的内高度,L为液体燃料喷射器的端部和炉口(1)的下游端之间的距离,Vequi为燃料液滴喷射的当量平均速度。 | ||||||
| 6 | BURNER | EP13827901 | 2013-08-07 | EP2884174A4 | 2015-10-21 | TSUMAGARI ICHIRO; SHIBUYA RYO; KOIDE ATSUSHI |
| A burner (20) includes a first tube portion (30) formed with an ejection port (32) that ejects combustion gas; a second tube portion (40) that extends in the first tube portion (30) toward the ejection port (32) and to which gaseous mixture flows in from a side opposite to the ejection port (32); a third tube portion (50) that is arranged in the first tube portion (30) and internally inserted with the second tube portion (40) and that includes an open end positioned on the ejection port (32) side; a closing portion (51) that closes the open end; a coupling wall portion (41) that closes a gap between the first tube portion (30) and the second tube portion (40); a partition wall (55) that is coupled to the first tube portion (30) and the third tube portion (50), the partition wall (55) being formed with a communication path (56) that communicates a side opposite to the ejection port (32) with the ejection port (32) side with respect to the partition wall (55); and an igniting portion (62) that is arranged on the ejection port (32) side with respect to the partition wall (55) and that ignites the gaseous mixture. | ||||||
| 7 | IMPROVED INDUSTRIAL BURNER FOR FUEL | EP00946131.0 | 2000-07-18 | EP1203188A1 | 2002-05-08 | Crowther, Brian; HOLMES, Michael |
| The reduction in NOx formation for high temperature applications with hot and regenerative combustion air is accomplished with flame control as follows. Initial NOx formation is reduced by introducing internally recirculated waste gases extracted directly from the chamber atmosphere adjacent to the burner quarl and a regulated air flow into the fuel stream. This stream of gases intersects with a ring of combustion air sufficient in flow rate to initiate the combustion process on the heavily diluted gas stream perimeter. Further reduction in NOx formation is accomplished by diluting the combustion air with 'in chamber' waste gases. The lean burning gas stream is allowed to expand onto the hot face of an air baffle at which localised combustion takes place. The high velocity air streams exiting the air baffle induce waste gases into the overall mixture and the combustion process is completed with the desired air/fuel ratio in the furnace chamber. | ||||||
| 8 | Burner | US14419521 | 2013-08-07 | US09746175B2 | 2017-08-29 | Ichiro Tsumagari; Ryo Shibuya; Atsushi Koide |
| A burner includes a first tube portion formed with an ejection port; a second tube portion that extends in the first tube portion toward the ejection port and to which gaseous mixture flows in from a side opposite to the ejection port; a third tube portion arranged in the first tube portion and including an open end positioned on the ejection port side; a closing portion that closes the open end; a coupling wall portion that closes a gap between the first tube portion and the second tube portion; a partition wall that is coupled to the first tube portion and the third tube portion, the partition wall being formed with a communication path; and an igniting portion that is arranged on the ejection port side with respect to the partition wall. | ||||||
| 9 | Liquid-fuel combustion system | US09870500 | 2001-06-01 | US06688876B2 | 2004-02-10 | Olivier Delabroy; Pierre Bodelin; Mahendra Joshi; Bernard Labegore; François Lacas |
| A process for combustion with the aid of a liquid fuel and a gaseous oxidizer containing from 20% to 100% volume of oxygen, in which the fuel is injected with the aid of an injector. The injector, which has a height “d”, is placed inside a glory hole. The glory hole has a height “D” at the end thereof corresponding to the ejection of the gaseous mixture towards the zone of heating of a charge. A coefficient “S” in the following equation is maintained at a value less than or equal to 1 for substantially the entire duration of combustion to ensure the stability of the flame. S = a 1 V equivalent - a 2 L a 3 d ( 2 - e - L / 10 D ) with a1=2.5·10−11 a2=1·10−9, dimensionless a3=(0.875·&ggr;+0.525)·10−6, dimensionless. In the above equation, “L” is defined as the distance between the end of the liquid fuel injector and the downstream end in the fluid flow direction of the glory hole. “Vequivalent” is defined either as the equivalent velocity representative of the average velocity of the spray of drops of liquid fuel in the case of mechanical atomizers and being equal to 2.4 M/(&rgr;&pgr;d2), or a velocity equal to 0.5 times Vatomization, in other cases. “&ggr;” is defined as the overall (volume) percentage of oxygen in the gases at the exit of the glory hole. | ||||||
| 10 | Injector of fuel in the form of a mist for an oil burner, and burner equipped with such an injector | US329993 | 1999-06-10 | US6135366A | 2000-10-24 | Pierre Bodelin; Bernard Labegorre; Patrick Recourt |
| The injector comprises a duct (31) through which a liquid fuel which forms a film lining its wall, and an atomizing fluid, are transmitted to its downstream part, from where the fuel is sprayed, forming a mist with the atomizing fluid.The downstream part has, from the duct (31) towards the free end of the injector, a chamber (32) for destabilizing the film which has a cross section that is larger than that of the duct, a throat (33) for detaching the film extending the destabilization chamber and having a cross section that is smaller than that of this chamber, and a spray orifice (34) which is open at the end of the injector, into which the throat opens, and which has a larger cross section.Use: heating furnaces, especially glass furnaces. | ||||||
| 11 | Fuel burner | US47258374 | 1974-05-22 | US3904349A | 1975-09-09 | PETERSON MORRIS W; KRIPPENE BRETT C; MARSHALL DAVID M |
| An improved fluent fuel burning apparatus including three individual airflow passages and separate means for apportioning the flow of combustion air among the passages so as to achieve complete combustion of the fuel while reducing the formation of nitric oxides.
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| 12 | Burner apparatus for flame propagation control | US18917871 | 1971-10-14 | US3836315A | 1974-09-17 | SHULAR H |
| A burner apparatus comprising a fuel burner and flame tunnel in combination. The tunnel is of a suitable refractory material and is substantially trumpet-shaped in cross section, comprising a first substantially cylindrical section and a second, flared section. The first, substantially cylindrical section preferably diverges in the direction of fuel and air flow at an angle of not more than about 3* and preferably about 1 1/2 * from a cylindrical surface. The length of the substantially cylindrical first section is at least two and one-half and preferably four times as great as the inlet diameter thereof, and the diameter of the large, furnace end of the flared second section is at least two and one-half and preferably four times as large as the inlet diameter of the first section. Combustion air and fuel are injected with a rotational motion into the flame tunnel. Combustion takes place in the flame tunnel, and a high kinetic energy is imposed upon the burning gas and air mixture within the comfines of the first, substantially cylindrical section. The high velocity attained causes the flame to cling to the tunnel walls, forming a substantially hollow flame. The reduced pressure at the center of the flame facing the furance draws in furnace atmosphere and enhances the formation of a flat, hollow flame even at high firing rates.
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| 13 | Liquid fuel burner | US16978762 | 1962-01-30 | US3159200A | 1964-12-01 | SCHULING WILHELMUS C; HENRI VERKOREN; KOSTER HENDRIK J |
| 14 | Oil burner | US2577238D | US2577238A | 1951-12-04 | ||
| 15 | Liquid-fuel burner | US63419123 | 1923-04-23 | US1695215A | 1928-12-11 | STAPLES EARLE I |
| 16 | Oil-burning attachment for furnace fronts | US64402123 | 1923-06-07 | US1666511A | 1928-04-17 | NORMAN SCOTT GEORGE |
| 17 | Multi-mode combustion device and method for using the device | US12688115 | 2010-01-15 | US08727767B2 | 2014-05-20 | Matthew James Watson; Douglas Jay Strange; Joseph Keith Juretus; Kevin Alan Lievre |
| An apparatus for continuation of combustion with a combustion apparatus when the supply of the normal operating oxidant or normal operating fuel is disrupted, or temporally reduced. Air or oxygen enriched air or oxygen and a gaseous fuel or a liquid fuel or both a gaseous and liquid fuel are introduced into the combustion apparatus in place of the normal oxidant-fuel mixture to effect combustion and maintain the heating level in the furnace.A burner capable of firing in any one of the following nine firing modes: Air-Gas; Air-Oxy-Gas; Oxy-Gas; Air-Oil; Air-Oxy-Oil; Oxy-Oil; Air-Oil-Gas; Air-Oxy-Oil-Gas; Oxy-Oil-Gas. | ||||||
| 18 | Multi-Mode Combustion Device and Method for Using the Device | US12688115 | 2010-01-15 | US20100183990A1 | 2010-07-22 | Matthew James Watson; Douglas Jay Strange; Joseph Keith Juretus; Kevin Alan Lievre |
| An apparatus for continuation of combustion with a combustion apparatus when the supply of the normal operating oxidant or normal operating fuel is disrupted, or temporally reduced. Air or oxygen enriched air or oxygen and a gaseous fuel or a liquid fuel or both a gaseous and liquid fuel are introduced into the combustion apparatus in place of the normal oxidant-fuel mixture to effect combustion and maintain the heating level in the furnace.A burner capable of firing in any one of the following nine firing modes: Air-Gas; Air-Oxy-Gas; Oxy-Gas; Air-Oil; Air-Oxy-Oil; Oxy-Oil; Air-Oil-Gas; Air-Oxy-Oil-Gas; Oxy-Oil-Gas | ||||||
| 19 | Fluid fuel fired burner | US832456 | 1986-02-21 | US4708638A | 1987-11-24 | John F. Brazier; Alan H. Young; John E. Viney; Gordon W. Sutton |
| The flame temperature of a fluid fuel fired burner (10) is reduced by mixing flue gas (35) with the combustion air supply (34) before introduction of the fuel and combustion take place. The NOX produced by the process of combustion is thereby reduced. The flue gas (35) may also be induced from the furnace remote from the flame zone of the burner (10) such that the flame is not disturbed. A venturi (21) may be used to induce the flue gas (35) from the furnace. | ||||||
| 20 | Self-recuperative burner | US871063 | 1978-01-20 | US4210411A | 1980-07-01 | Trevor Ward; Clive Ward |
| A self recuperative burner which can be fired with oil or gaseous fuel or both. The oil feed pipe is surrounded by a passage through which compressed air or fuel gas is conveyed to the burner head in such a way that it reduces the tendency for the oil to overheat. Additional cooling means are provided for the oil feed pipe. The burner has a burner head which is supported by a tubular part carried by a common wall between the combustion air supply passage and the combustion products exhaust passage, there being a sliding joint between the burner head and the tubular part which provides a circumferential series of arcuate gaps around the periphery of the burner head for the flow of combustion air between the burner head and the tubular part. The burner has an exhaust flue which is surrounded by a tubular part in which the combustion air inlet port is formed, the flue being cooled by incoming combustion air. | ||||||
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