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1.发明授权Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or firing installation 失效用于操作内燃机的燃烧器，燃气轮机组的燃烧室或点火装置
公开(公告)号：US5375995A
公开(公告)日：1994-12-27
申请号：US181438
申请日：1994-01-14
CPC分类号： F23D17/002 , F23C2900/07002
摘要： In a double-cone burner, at least one row of nozzles (10) for a gaseous fuel containing highly reactive components and having a medium calorific value are arranged on the periphery of the partial conical bodies (1, 2) of the burner near the burner outlet at a distance of approximately 30% of the nominal burner diameter. In addition, there is a fuel conduit (11) and a distributing passage (17), placed in the region of the nozzles (10), for the highly reactive fuel. The gaseous fuel (15) containing highly reactive components is injected at high velocity through the nozzles (10), which have a diameter which is smaller than 1% of the nominal burner diameter, into the zones of high air velocity and the penetration depth and the direction of the fuel jets are matched to one another in such a way that ignition only takes place behind the burner, after mixing has occurred.
摘要翻译： 在双锥形燃烧器中，用于含有高反应性组分并具有中等热值的气态燃料的至少一排喷嘴（10）布置在燃烧器附近的燃烧器的部分圆锥体（1,2）的周边上 燃烧器出口距离标称燃烧器直径的约30％。 此外，在喷嘴（10）的区域中，存在用于高反应性燃料的燃料导管（11）和分配通道（17）。 含有高反应性组分的气体燃料（15）通过直径小于标称燃烧器直径的1％的喷嘴（10）以高速喷射到高空气速度和穿透深度的区域中， 燃料喷嘴的方向彼此匹配，使得在发生混合之后点燃仅发生在燃烧器后面。
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公开(公告)号：US5489203A
公开(公告)日：1996-02-06
申请号：US292268
申请日：1994-08-18
CPC分类号： F23C7/002 , F23D11/40 , F23D14/62 , F23D17/002 , F23C2900/07002 , F23D2214/00
摘要： A premixing burner (X) which consists essentially of at least two hollow partial bodies (1, 2), which are positioned one above the other and whose center lines (1b, 2b) extend offset relative to one another in the longitudinal direction of the partial bodies (1, 2), is employed for hot gas generation, for example in a firing plant. Due to this offset, tangential inlet slots (21, 22) respectively occur through which a combustion airflow (15) flows into the internal space (14) of the premixing burner (X). Venturi mixers (32) with fuel nozzles (36), through which a fuel (31) is introduced into the combustion air (15) flowing past at this point, are arranged in the region of these tangential inlet slots (21, 22).
摘要翻译： 一种预混合燃烧器（X），其基本上由至少两个中空部分体（1,2）组成，所述至少两个中空部分体（1,2）一个位于另一个之上并且其中心线（1b，2b）在其纵向方向上相对于彼此偏移地延伸 部分体（1,2）用于产生热气体，例如在燃烧装置中。 由于这种偏移，分别出现切向入口狭槽（21,22），燃烧气流（15）通过该入口狭槽流入预混合燃烧器（X）的内部空间（14）。 具有燃料喷嘴（36）的文丘里混合器（32）布置在这些切向入口狭槽（21,22）的区域中，燃料（31）通过该燃料喷嘴（36）引入到此时流过的燃烧空气（15）中。
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公开(公告)号：US5584684A
公开(公告)日：1996-12-17
申请号：US415210
申请日：1995-03-31
CPC分类号： F23R3/346 , F23C6/047 , F23C2201/20 , F23C2900/07002
摘要： In the case of a heat generator which essentially consists of a premix burner (100) and a flame tube (1), the hot gases (10) from the combustion in the premix burner (100) are fed into the flame tube (1), and there undergo staged post-combustion. This post-combustion takes place by means of a first post-combustion stage (11) and a second post-combustion stage (12). The air/fuel mixture (11a, 12a) is provided for each post-combustion stage (11, 12) in individual mixers (200, 300). These mixers are arranged axially with respect to the flame tube (1) and work in such a way that injection of the corresponding mixture (11a, 12a) makes it possible to obtain different combustion zones which extend in a staged sequence over the flame tube (1). By virtue of this staged post-combustion mode NO.sub.x emissions can be reduced by a factor of 5 compared to conventional techniques.
摘要翻译： 在基本由预混燃烧器（100）和火焰管（1）组成的发热体的情况下，来自预混合燃烧器（100）中的燃烧的热气体（10）被送入火焰管（1） ，并且分段后燃。 该后燃烧通过第一后燃烧阶段（11）和第二后燃烧阶段（12）进行。 为各个混合器（200,300）中的每个后燃烧级（11,12）设置空气/燃料混合物（11a，12a）。 这些混合器相对于火焰管（1）轴向地布置并且以这样的方式进行加工，使得相应的混合物（11a，12a）的注入使得可以获得在火焰管上分阶段延伸的不同燃烧区（ 1）。 由于这种分段后燃烧模式，与常规技术相比，NOx排放可以降低5倍。
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公开(公告)号：US5244380A
公开(公告)日：1993-09-14
申请号：US844169
申请日：1992-03-02
CPC分类号： F23D17/002 , F23D11/402 , F23R3/12 , F23R3/286 , F23R3/30 , F23C2900/07002
摘要： In a burner for premixing-type combustion of a liquid and/or gaseous fuel, which essentially comprises hollow conical part-bodies (1, 2) positioned one upon the other, the center lines of which extend mutually offset in the longitudinal direction, whereupon tangential inlet openings (1b, 2b) are formed on both sides of the burner, a fuel (5a) is admixed to the combustion air (13) flowing into the interior (3) of the burner in that area. This admixture is accomplished via a number of nozzles (9, 10), which act in the region of the inlet openings (1b, 2b). The fuel through these nozzles is injected with a small spray cone angle in the longitudinal direction of the slot. The fuel vaporization takes place essentially only in the inlet openings of the burner, with the result that only a fuel vapor enters the interior (3). A further central nozzle (4) supplied with a liquid and/or gaseous fuel provides assistance in the form of a limit fuel quantity. The ignition of the mixture (4a, 5a, 13) takes place at the outlet of the burner, stabilization of the flame front (14) being brought about in the region of the burner aperture by a return flow zone (15).
摘要翻译： 在用于液体和/或气体燃料的预混合燃烧的燃烧器中，其基本上包括一个彼此定位的中空圆锥形部分体（1,2），其中心线在纵向方向上相互偏移地延伸，于是， 切向入口开口（1b，2b）形成在燃烧器的两侧，燃料（5a）与流入燃烧器内部（3）的燃烧空气（13）相混合。 该混合物通过多个在入口（1b，2b）的区域中起作用的喷嘴（9,10）来实现。 通过这些喷嘴的燃料在槽的长度方向上以小的喷雾锥角注入。 燃料蒸发基本上仅在燃烧器的入口开口中发生，结果是只有燃料蒸汽进入内部（3）。 提供有液体和/或气体燃料的另一个中心喷嘴（4）以极限燃料量的形式提供帮助。 混合物（4a，5a，13）的点燃发生在燃烧器的出口处，火焰前沿（14）的稳定性通过返回流动区（15）进入燃烧器孔的区域。
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公开(公告)号：US5433596A
公开(公告)日：1995-07-18
申请号：US215252
申请日：1994-03-21
IPC分类号： F23D14/24 , B01F5/04 , B01F5/06 , F15D1/00 , F23C7/00 , F23D14/62 , F23D17/00 , F23D23/00 , F23M9/02 , F23D14/46
CPC分类号： B01F5/061 , B01F5/0471 , F15D1/0015 , F23C7/002 , F23D17/002 , F23M9/02 , F23C2900/07002
摘要： A premixing burner on the double-cone principle consists essentially of two hollow conical partial bodies (111, 112) which are interleaved in the flow direction and whose respective center lines (113, 114) are offset relative to one another. The adjacent walls of the two partial bodies form tangential gaps (20) in their longitudinal extent for the combustion air. Gas inlet openings (117) distributed in the longitudinal direction are provided in the walls of the two partial bodies. The air is guided into the tangential gaps (20) via vortex generators (9) of which a plurality are arranged adjacent to one another. The fuel is introduced into the gaps (20) in the immediate region of the vortex generators (9).Using the novel static mixer which the three-dimensional vortex generators represent, longitudinal vortices without recirculation region can be generated in the inlet gap through which flow occurs. It is therefore possible to achieve extraordinarily short mixing distances at the inlet to the burner with a small pressure loss at the same time.
摘要翻译： 双锥体原理的预混合燃烧器基本上由两个中空圆锥形部分体（111,112）组成，它们在流动方向上交错并且其各自的中心线（113,114）相对于彼此偏移。 两个部分体的相邻壁在其燃烧空气的纵向范围内形成切向间隙（20）。 在两个部分体的壁上设置沿长度方向分布的气体入口（117）。 空气通过多个彼此相邻布置的涡流发生器（9）引导到切向间隙（20）中。 燃料被引入涡流发生器（9）的直接区域中的间隙（20）中。 使用三维涡流发生器所代表的新型静态混合器，可以在流动发生的入口间隙中产生不具有再循环区域的纵向旋涡。 因此，可以在燃烧器的入口处同时具有小的压力损失来实现非常短的混合距离。
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公开(公告)号：US5918457A
公开(公告)日：1999-07-06
申请号：US654119
申请日：1996-05-28
CPC分类号： F23C6/042
摘要： In a method of operating a plant with staged combustion, the first combustion stage (1a) is operated with a fuel/air mixture (3) whose air coefficient is larger than the overall air coefficient of the combustion system. The hot combustion gases (5) from the first combustion stage (1a) are mixed with an additional fuel/air mixture (4) whose air coefficient is smaller than the overall air coefficient of the combustion system, before the further combustion in the second stage (2a) takes place. Since hot-gas backmixing is no longer required in the second stage (2a) for the flame stabilization, this combined mixture burns without the formation of further NOx emissions.
摘要翻译： 在操作具有分段燃烧的设备的方法中，第一燃烧阶段（1a）与空气系数大于燃烧系统的总体空气系数的燃料/空气混合物（3）一起操作。 来自第一燃烧阶段（1a）的热燃烧气体（5）与第二阶段进一步燃烧之前的空气系数小于燃烧系统的总体空气系数的附加燃料/空气混合物（4）混合 （2a）发生。 由于在第二阶段（2a）中不再需要热气回混用于火焰稳定化，所以该组合混合物燃烧而不形成进一步的NOx排放。
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公开(公告)号：US5807097A
公开(公告)日：1998-09-15
申请号：US760688
申请日：1996-12-04
IPC分类号： F23R3/20 , F23C7/00 , F23D11/24 , F23D11/40 , F23D17/00 , F23R3/12 , F23R3/28 , F23R3/30 , F23D14/62
CPC分类号： F23C7/002 , F23D17/002 , F23R3/12 , F23R3/283 , F23R3/30 , F23C2900/07002
摘要： The object of the invention is to provide a novel cone burner for gaseous and/or liquid fuels which has a reduced NOx and CO emission. According to the invention, this is achieved in that the sectional cone bodies (1, 2) have a common outlet diffuser (27) at their downstream end. They have a transition region (28) to the outlet diffuser (27), in which the size of the air-inlet slots (7, 8) decreases continuously in the direction (3) of flow. The outlet diffuser (27) is designed to be circular and without air-inlet slots (7, 8).
摘要翻译： 本发明的目的是提供一种用于气体和/或液体燃料的新型锥形燃烧器，其具有减少的NOx和CO排放。 根据本发明，这是通过截面锥体（1,2）在其下游端具有公共出口扩散器（27）来实现的。 它们具有到出口扩散器（27）的过渡区域（28），其中进气狭槽（7,8）的尺寸沿流动方向（3）连续减小。 出口扩散器（27）被设计成圆形且没有空气入口狭槽（7,8）。
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公开(公告)号：US06202402B1
公开(公告)日：2001-03-20
申请号：US09106095
申请日：1998-06-29
申请人： Thomas Sattelmayer
发明人： Thomas Sattelmayer
IPC分类号： F02C710
摘要： Described are a gas-turbine construction and a method of operating this gas-turbine construction, having an air compressor, a heat exchanger connected downstream of the air compressor, a combustion chamber, and a turbine which can be driven by hot combustion gases and from which the combustion gases are fed to the heat exchanger for heating the compressed supply air coming from the air compressor. The invention is distinguished by the fact that the heat exchanger and the combustion chamber are integrated in a common unit, and that fuel can be added to the supply air before entry into the unit, which fuel can be ignited catalytically in the form of an air/fuel mixture inside the unit, in which a catalyst is provided.
摘要翻译： 描述了一种燃气轮机结构和操作该燃气轮机结构的方法，其具有空气压缩机，连接在空气压缩机下游的热交换器，燃烧室和能够被热燃烧气体驱动的涡轮机， 这些燃烧气体被供给到热交换器以加热来自空气压缩机的压缩空气。本发明的特征在于，热交换器和燃烧室集成在共同的单元中，并且可以添加燃料 在进入该单元之前的供给空气中，该燃料可以以单元内的空气/燃料混合物的形式催化地点燃，其中提供催化剂。
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公开(公告)号：US5857846A
公开(公告)日：1999-01-12
申请号：US839645
申请日：1997-04-15
申请人： Thomas Sattelmayer , Martin Valk
发明人： Thomas Sattelmayer , Martin Valk
IPC分类号： F23D17/00
CPC分类号： F23D17/00 , F23D2209/20
摘要： In a burner (1) for a heat generator, having a throughflow passage (3) for the throughflow of a combustion-air flow (12), a hentral main fuel lance (5) acts inside the said throughflow passage (3). A number of mixing elements (6) are arranged in an annular manner around this main fuel lance (5), and the remaining annular throughflow cross section is covered concentrically hereto by swirl generators. The mixing elements (6) are fed with a fuel (13a) and a partial combustion-air quantity (12a). The mode of operation of these mixing elements (6) corresponds to that of a pilot stage, whereby the flame stability is increased, while the NOx emissions remain at a low level.
摘要翻译： 在用于热发生器的燃烧器（1）中，具有用于燃烧空气流（12）的通流的通流通道（3），中心主燃料喷枪（5）作用在所述通流通道（3）的内部。 多个混合元件（6）围绕该主燃料喷枪（5）以环形方式布置，并且剩余的环形通流横截面同心地被涡流发生器覆盖。 混合元件（6）被供给燃料（13a）和部分燃烧空气量（12a）。 这些混合元件（6）的操作模式对应于先导级的操作模式，由此在NOx排放保持在低水平的同时增加火焰稳定性。
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公开(公告)号：US5557918A
公开(公告)日：1996-09-24
申请号：US414810
申请日：1995-03-31
申请人： Yau-Pin Chyou , Thomas Sattelmayer , Peter Senior
发明人： Yau-Pin Chyou , Thomas Sattelmayer , Peter Senior
摘要： A gas turbine apparatus for higher pressure and temperature ratio operation, improved thermal efficiency and minimized NO.sub.x emissions includes a high pressure compressor, a high pressure turbine, a low pressure turbine and combustion chambers for each of the turbines. A diffuser guides exhaust gas from the high pressure turbine and retards the velocity of the gases. A 180.degree. bend downstream of the diffuser changes the flow direction of the gases. Fuel lances extend into the bend at the outlet end to inject fuel into the gases after the direction change. The bend directs the gas and fuel into a reversal combustion chamber where the gases and fuel again changes direction by 180.degree., and a ring vortex in the flow is produced. The fuel and air is ignited and combusted, and the combusted gases directed into the low pressure turbine.
摘要翻译： 用于更高压力和温度比的操作，改善的热效率和最小化的NOx排放的燃气轮机设备包括用于每个涡轮机的高压压缩机，高压涡轮机，低压涡轮机和燃烧室。 扩散器引导来自高压涡轮机的废气并延缓气体的速度。 扩散器下游180°弯曲处改变气体的流动方向。 燃料喷枪延伸到出口端的弯头，在方向改变之后将燃料喷射到气体中。 弯道将气体和燃料引导到反向燃烧室，在那里气体和燃料再次将方向改变180°，并且产生流动中的环形涡流。 燃料和空气被点燃和燃烧，并且燃烧的气体被导入低压涡轮。
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