公开(公告)号：US06623268B2

公开(公告)日：2003-09-23

申请号：US09942151

申请日：2001-08-29

申请人： George B. Diamond ,  Ralph H. Helmrich ,  Kihong Kim ,  Chung Han Kim

发明人： George B. Diamond ,  Ralph H. Helmrich ,  Kihong Kim ,  Chung Han Kim

IPC分类号： F23D1100

CPC分类号： F23D14/28

摘要： A butane fuel supply container for a cooking stove, the container has a thin side wall held rigid by the vapor pressure of the fuel, but the side wall can be finger deformed when the can has been depressurized or hand crushed with the exit valve of the container open, the vapor therein being expelled as the container is deformed or crushed. The vapor tube has a vapor entrance in the vapor pocket above the pool of liquid fuel when the container is correctly oriented in the stove. The vapor tube passes vapor through a valve at the dome of the container.

公开(公告)号：US06425755B1

公开(公告)日：2002-07-30

申请号：US09583253

申请日：2000-05-31

申请人： Jean-Claude Pillard ,  Jacques Pizant

发明人： Jean-Claude Pillard ,  Jacques Pizant

IPC分类号： F23D1100

CPC分类号： F23D11/103

摘要： The invention relates to liquid fuel burners having low NOx and dust emission, and it also relates to liquid atomizers or sprayers for such burners. The removable atomizer for a liquid fuel burner head is made as a single piece, has a longitudinal central orifice for passing fuel plus a plurality of longitudinal peripheral orifices for passing a spray fluid, and on each of its faces it further includes a depression surrounding said central orifice.

摘要翻译： 本发明涉及具有低NOx和粉尘排放的液体燃料燃烧器，并且还涉及用于这种燃烧器的液体雾化器或喷雾器。 用于液体燃料燃烧器头的可移除雾化器被制成单件，具有用于使燃料加上多个纵向外围孔以便通过喷射流体的纵向中心孔，并且在其每个表面上还包括围绕所述 中心孔。

公开(公告)号：US06551095B2

公开(公告)日：2003-04-22

申请号：US09781155

申请日：2001-02-13

申请人： Guy Tackels ,  Patrick Rouchy ,  Joseph Vernaz

发明人： Guy Tackels ,  Patrick Rouchy ,  Joseph Vernaz

IPC分类号： F23D1100

CPC分类号： F23D11/107 ,  F23C5/06 ,  F23D2214/00

摘要： In a combustion process, especially one used for melting glass, the delivery of fuel is ensured by an apparatus having at least one burner (5) which is equipped with at least one injector (1) that includes a liquid fuel delivery tube (2) which has at least one internal wall (25) and an injected fluid delivery tube (3) arranged concentrically with respect to the liquid fuel delivery tube. Immediately before injecting the liquid fuel from its delivery tube, one puts it in the shape of a hollow jet basically assuming the shape of the internal wall. This has application for the reduction of NOx in a glass-making oven.

摘要翻译： 在燃烧过程中，特别是用于熔化玻璃的燃烧过程中，通过具有至少一个燃烧器（5）的装置来确保燃料输送，所述燃烧器（5）装备有至少一个包括液体燃料输送管（2）的喷射器（1） 其具有至少一个相对于液体燃料输送管同心布置的内壁（25）和注射流体输送管（3）。 在从其输送管注入液体燃料之前，立即以基本上呈内壁形状的中空射流的形状。 这适用于在玻璃制造炉中还原NOx。

公开(公告)号：US06632085B1

公开(公告)日：2003-10-14

申请号：US09830054

申请日：2001-05-22

申请人： Motohiro Suzuki ,  Tatsuo Fujita ,  Yoshitaka Kawasaki ,  Tetsuo Terashima

发明人： Motohiro Suzuki ,  Tatsuo Fujita ,  Yoshitaka Kawasaki ,  Tetsuo Terashima

IPC分类号： F23D1100

CPC分类号： F23C13/00 ,  F23C13/02 ,  F23D11/40 ,  F23D11/402 ,  F23D11/441

摘要： A catalyst combustion apparatus, includes: a fuel feed course for feeding liquid fuel; an air feed course for feeding air; a mixing unit for mixing fuel to be fed from the fuel feed course with air to be fed from the air feed course; a vaporizing unit for heating mixture-obtained by mixing in the mixing unit to vaporize the liquid fuel; a catalyst heating unit disposed on the downstream side of the vaporizing unit in contact with or in close proximity to the vaporizing unit in terms of conduction of heat, for carrying an oxidation catalyst component; and a catalyst combustion unit provided on the downstream of the catalyst heating unit, having a multiplicity of conductive holes, and the vaporizing unit is capable of utilizing heat from the catalyst heating unit.

摘要翻译： 一种催化剂燃烧装置，包括：用于供给液体燃料的燃料供给路径; 用于喂食空气的空气进料路线; 混合单元，用于将从燃料供给路线供给的燃料与从供气路线供给的空气混合; 蒸发单元，用于加热通过在所述混合单元中混合而获得的混合物，以蒸发所述液体燃料; 催化剂加热单元，其设置在蒸发单元的下游侧，与蒸发单元接触或接近热传导，用于承载氧化催化剂组分; 以及催化剂燃烧单元，其设置在催化剂加热单元的下游，具有多个导电孔，并且所述蒸发单元能够利用来自所述催化剂加热单元的热量。

公开(公告)号：USRE37383E1

公开(公告)日：2001-09-18

申请号：US08641867

申请日：1996-05-02

申请人： Joseph Gerstmann ,  Andrew D. Vasilakis

发明人： Joseph Gerstmann ,  Andrew D. Vasilakis

IPC分类号： F23D1100

CPC分类号： F24H1/43 ,  F23D14/36 ,  F23M11/02

摘要： Combustion apparatus (10) includes a combustion chamber (12, 212), a cover (24, 208) covering an end wall (14, 210) of the combustion chamber and defining a buffer space (26, 206) therebetween, and a blower (32, 202) external to the cover and supplying air to the buffer space and pressurizing the buffer space to a higher pressure than the combustion chamber such that leakage at penetrations (46) and/or interface (334, 336) flows from the buffer space into the combustion chamber, rather than the reverse, eliminating the need for leak-tight seals, and instead permitting leakage in a desired direction. In one embodiment, a first conduit (58) supplies air along a path (34) from the blower to the mixer and burner assembly without passing through the buffer space, and a second conduit (60) independently supplies air from the blower to the buffer space. A pressure dropping orifice (36) is provided between the blower and the mixer and burner assembly. A gas inlet port (40) is external to the cover (24) and downstream of the pressure dropping orifice (36). The buffer space (26) communicates with the blower (32) along an air flow path (44) upstream of the pressure dropping orifice (36). In another embodiment, air flows through the buffer space (20) to the mixer and burner assembly. The buffer space (26, 206) is thin and flat, and the cover (24, 208) covers only one end wall (14, 210) of the combustion chamber, not the other end wall nor the sidewall, such that the latter are accessible without removing the cover.

摘要翻译： 燃烧装置（10）包括燃烧室（12,212），覆盖燃烧室的端壁（14,210）并在其间限定缓冲空间（26,206）的盖（24,208）和鼓风机 （32,202），并且将空气供应到缓冲空间并将缓冲空间加压到比燃烧室更高的压力，使得穿透（46）和/或界面（334,336）处的泄漏从缓冲器 进入燃烧室的空间，而不是相反的，消除了对密封件的密封，而是允许在所需方向上泄漏。 在一个实施例中，第一管道（58）沿着路径（34）从鼓风机向混合器和燃烧器组件供应空气，而不通过缓冲空间，而第二管道（60）独立地将来自鼓风机的空气供给缓冲器 空间。 在鼓风机和混合器和燃烧器组件之间设置有压力降口（36）。 气体入口（40）在盖（24）的外部和压降孔（36）的下游。 缓冲空间26沿着压降口36的上游的空气流路44与鼓风机32连通。 在另一个实施例中，空气流过缓冲空间（20）进入混合器和燃烧器组件。 缓冲空间（26,206）薄且平坦，盖（24,208）仅覆盖燃烧室的一个端壁（14,210），而不仅覆盖另一端壁和侧壁， 无需拆卸盖子即可进入。

公开(公告)号：US06688876B2

公开(公告)日：2004-02-10

申请号：US09870500

申请日：2001-06-01

申请人： Olivier Delabroy ,  Pierre Bodelin ,  Mahendra Joshi ,  Bernard Labegore ,  François Lacas

发明人： Olivier Delabroy ,  Pierre Bodelin ,  Mahendra Joshi ,  Bernard Labegore ,  François Lacas

IPC分类号： F23D1100

CPC分类号： F23M5/025 ,  F23D11/002 ,  F23D2209/20 ,  F23D2900/00006

摘要： 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.

摘要翻译： 借助于液体燃料和含有20％至100％体积的氧的气态氧化剂的燃烧过程，其中借助于喷射器喷射燃料。 具有高度“d”的喷射器放置在光亮孔内。 荣耀孔在其端部具有高度“D”，其对应于气体混合物向加料区域的喷射。 在几乎整个燃烧持续时间内，下列公式中的系数“S”保持在小于或等于1的值，以确保火焰的稳定性.a1 = 2.5.10 <-11> a2 = 1.10 <-9 >，无量纲3 =（0.875.gamma + 0.525）.10 -6，无量纲。在上式中，“L”定义为液体燃料喷射器的端部与流体流动方向上的下游端之间的距离 的荣耀之穴。 “Vequivalent”定义为等效速度，表示在机械雾化器情况下液体燃料滴喷射的平均速度等于2.4M /（rhopid2）或等于0.5倍的速度的等效速度 在其他情况下，分解。 “伽马”定义为荣耀孔出口处气体中氧气的总体积（体积）百分比。

公开(公告)号：US06174161B1

公开(公告)日：2001-01-16

申请号：US09364438

申请日：1999-07-30

申请人： Aleksandar G. Slavejkov ,  Bryan C. Hoke, Jr. ,  Thomas M. Gosling ,  John J. Lewnard ,  David R. Ruprecht

发明人： Aleksandar G. Slavejkov ,  Bryan C. Hoke, Jr. ,  Thomas M. Gosling ,  John J. Lewnard ,  David R. Ruprecht

IPC分类号： F23D1100

CPC分类号： F23D11/107 ,  F23D2900/00006 ,  F23D2900/00014 ,  F23G7/04

摘要： Method and apparatus for combusting and/or gasifying a generally viscous liquid or a slurry wherein the liquid or slurry are atomized in a central atomization device within a burner housing the central atomization device using a portion of a gaseous oxidant introduced into the burner to atomize the liquid or slurry as it exits the atomization device.

摘要翻译： 用于燃烧和/或气化大体上粘稠的液体或浆料的方法和设备，其中液体或浆料在燃烧器内的中心雾化装置中被雾化，所述中心雾化装置使用引入燃烧器中的一部分气态氧化剂容纳中心雾化装置，以雾化 液体或浆料离开雾化装置时。