-
公开(公告)号：US20080044782A1
公开(公告)日：2008-02-21
申请号：US11791097
申请日：2005-11-15
IPC分类号： F23Q9/00
CPC分类号： F23R3/286 , F02C7/26 , F23D17/002 , F23L7/00 , F23L2900/07002 , F23N2027/02 , F23R3/343
摘要： The invention relates to a method for starting a burner for combusting synthesis gases, wherein said burner comprises first and second fuel passages, the first fuel passage encompasses the second fuel passage in a substantially concentric manner and the gas transferred to the burner is mixed with combusting air and is combusted. According to said invention, in order to start the burner, the second fuel passage is first loaded with a synthesis gas to a predefined burner power at a first starting phase and the first fuel passage is loaded with the synthesis gas at a second starting phase.
摘要翻译： 本发明涉及一种启动用于燃烧合成气的燃烧器的方法，其中所述燃烧器包括第一和第二燃料通道，第一燃料通道以基本同心的方式包围第二燃料通道，并且转移到燃烧器的气体与燃烧 空气燃烧。 根据所述发明，为了启动燃烧器，第一燃料通道在第一起动阶段首先被加载到预定的燃烧器功率，并且第一燃料通道在第二起动阶段装入合成气。
-
公开(公告)号：US20120167583A1
公开(公告)日：2012-07-05
申请号：US13419839
申请日：2012-03-14
CPC分类号： F23R3/286 , F02C7/26 , F23D17/002 , F23L7/00 , F23L2900/07002 , F23N2027/02 , F23R3/343
摘要： A method for starting a burner for combusting synthesis gases is provided. The burner includes first and second fuel passages, the first fuel passage encompasses the second fuel passage in a substantially concentric manner and the gas transferred to the burner is mixed with combusting air and is combusted. In order to start the burner, the second fuel passage is first loaded with a synthesis gas to a predefined burner power at a first starting phase and the first fuel passage is loaded with the synthesis gas at a second starting phase.
摘要翻译： 提供了一种启动用于燃烧合成气的燃烧器的方法。 燃烧器包括第一和第二燃料通道，第一燃料通道以基本上同心的方式包围第二燃料通道，并且转移到燃烧器的气体与燃烧空气混合并燃烧。 为了启动燃烧器，第一燃料通道首先在第一启动阶段将合成气装载到预定的燃烧器功率，并且第一燃料通道在第二起动阶段装入合成气。
-
公开(公告)号：US09033697B2
公开(公告)日：2015-05-19
申请号：US13419839
申请日：2012-03-14
CPC分类号： F23R3/286 , F02C7/26 , F23D17/002 , F23L7/00 , F23L2900/07002 , F23N2027/02 , F23R3/343
摘要： A method for starting a burner for combusting synthesis gases is provided. The burner includes first and second fuel passages, the first fuel passage encompasses the second fuel passage in a substantially concentric manner and the gas transferred to the burner is mixed with combusting air and is combusted. In order to start the burner, the second fuel passage is first loaded with a synthesis gas to a predefined burner power at a first starting phase and the first fuel passage is loaded with the synthesis gas at a second starting phase.
摘要翻译： 提供了一种启动用于燃烧合成气的燃烧器的方法。 燃烧器包括第一和第二燃料通道，第一燃料通道以基本上同心的方式包围第二燃料通道，并且转移到燃烧器的气体与燃烧空气混合并燃烧。 为了启动燃烧器，第一燃料通道首先在第一启动阶段将合成气装载到预定的燃烧器功率，并且第一燃料通道在第二起动阶段装入合成气。
-
公开(公告)号：US08177547B2
公开(公告)日：2012-05-15
申请号：US11791097
申请日：2005-11-15
IPC分类号： F23Q9/00
CPC分类号： F23R3/286 , F02C7/26 , F23D17/002 , F23L7/00 , F23L2900/07002 , F23N2027/02 , F23R3/343
摘要： The invention relates to a method for starting a burner for combusting synthesis gases, wherein said burner comprises first and second fuel passages, the first fuel passage encompasses the second fuel passage in a substantially concentric manner and the gas transferred to the burner is mixed with combusting air and is combusted. According to said invention, in order to start the burner, the second fuel passage is first loaded with a synthesis gas to a predefined burner power at a first starting phase and the first fuel passage is loaded with the synthesis gas at a second starting phase.
摘要翻译： 本发明涉及一种启动用于燃烧合成气的燃烧器的方法，其中所述燃烧器包括第一和第二燃料通道，第一燃料通道以基本同心的方式包围第二燃料通道，并且转移到燃烧器的气体与燃烧 空气燃烧。 根据所述发明，为了启动燃烧器，第一燃料通道在第一起动阶段首先被加载到预定的燃烧器功率，并且第一燃料通道在第二起动阶段装入合成气。
-
公开(公告)号：US20070275337A1
公开(公告)日：2007-11-29
申请号：US10590379
申请日：2005-02-15
申请人： Andreas Heilos , Berthold Kostlin , Bernd Prade
发明人： Andreas Heilos , Berthold Kostlin , Bernd Prade
IPC分类号： F23R3/36
CPC分类号： F23R3/14 , F23D14/583 , F23R3/286 , F23R2900/00002
摘要： The invention relates to a pre-mix burner for burning a low-calorie combustion gas, said burner comprising an air duct which extends along an axis of the burner and can be used to supply combustion air. A swirling device is arranged in the air duct and is used to apply a swirling motion to the combustion air. An injection device for the low-calorie combustion gas is provided downstream of the swirling device. The injection device comprises inlets for the combustion gas, such that the formation of wake regions in the air channel is prevented. The invention also relates to a method for burning a low-calorie combustion gas, according to which a swirling motion is applied to the combustion air, low-calorie combustion gas is injected into the swirled combustion air and intensively mixed therewith, and the mixture is then burned.
摘要翻译： 本发明涉及一种用于燃烧低热量燃烧气体的预混合燃烧器，所述燃烧器包括沿燃烧器的轴线延伸并可用于供应燃烧空气的空气管道。 涡流装置布置在空气管道中，并用于向燃烧空气施加旋转运动。 用于低热量燃烧气体的注射装置设置在旋转装置的下游。 注射装置包括用于燃烧气体的入口，从而防止在空气通道中形成尾流区。 本发明还涉及一种用于燃烧低热量燃烧气体的方法，根据该方法，对燃烧空气施加旋转运动，将低热燃烧气体注入涡流燃烧空气中并与其集中混合，并且混合物 然后烧了
-
公开(公告)号：US07726133B2
公开(公告)日：2010-06-01
申请号：US10482388
申请日：2002-07-08
CPC分类号： F02C3/28 , F01K23/067 , F23D17/00 , F23D2204/00 , F23L7/002 , F23R3/286 , F23R2900/00002 , Y02E20/18
摘要： A method is for operating a burner of a gas turbine. A fossil fuel is gasified and the gasified fossil fuel is fed as synthesis gas into the burner for combustion. The burner is connected to the gas turbine. The synthesis gas is divided into a first partial current and a second partial current and the partial currents are each fed into the burner for combustion. A power plant, particularly a gas and steam turbine system, includes a gasification device for a fossil fuel.
摘要翻译： 一种用于操作燃气轮机的燃烧器的方法。 化石燃料气化，气化的化石燃料作为合成气体进入燃烧器进行燃烧。 燃烧器连接到燃气轮机。 合成气被分成第一部分电流和第二部分电流，并且各部分电流被馈送到燃烧器中用于燃烧。 发电厂，特别是燃气和汽轮机系统，包括用于化石燃料的气化装置。
-
公开(公告)号：US20100043440A1
公开(公告)日：2010-02-25
申请号：US12224482
申请日：2007-02-20
申请人： Andreas Heilos , Werner Krebs , Jaap Van Kampen
发明人： Andreas Heilos , Werner Krebs , Jaap Van Kampen
IPC分类号： F02C7/22
摘要： The invention is based on a gas turbine burner comprising a combustion zone for burning a mixture consisting of combustion exhaust gas to which fuel gas is added, and comprising a fuel intermixing arrangement having a fuel nozzle for spraying the fuel gas into the combustion exhaust gas. In order to achieve low-pollutant and uniform combustion, it is proposed that the fuel intermixing arrangement be designed for spraying the fuel gas into the combustion exhaust gas at at least 0.2 times the speed of sound.
摘要翻译： 本发明是基于一种燃气轮机燃烧器，其包括用于燃烧由添加有燃料气体的燃烧废气组成的混合物的燃烧区，并且包括具有用于将燃料气体喷射到燃烧废气中的燃料喷嘴的燃料混合装置。 为了实现低污染和均匀的燃烧，建议燃料混合装置被设计成以至少0.2倍于声速喷射到燃烧废气中的燃料混合装置。
-
8.发明申请Method of Optimum Controlled Outlet, Impingement Cooling and Sealing of a Heat Shield and a Heat Shield Element 审中-公开热屏蔽和热屏蔽元件的最佳控制出口，冲击冷却和密封方法公开(公告)号：US20070245742A1
公开(公告)日：2007-10-25
申请号：US11666119
申请日：2005-10-21
申请人： Stefan Dahlke , Uwe Gruschka , Andreas Heilos , Roland Liebe
发明人： Stefan Dahlke , Uwe Gruschka , Andreas Heilos , Roland Liebe
IPC分类号： F23R3/00
CPC分类号： F23R3/002 , F02K1/82 , F05D2260/201 , F23M2900/05005 , F23R3/005 , F23R2900/03041 , F23R2900/03044 , Y02T50/675
摘要： There is described a method for cooling and sealing of a heat shield element, comprising a main wall with an inner side, which is restricted by side walls or rims, and an outer side, which can be exposed to a hot fluid, and wherein a coolant is introduced into an impingement region of that heat shield element and an impingement flow of said coolant is directed on a surface area of that inner side through a plurality of impingement holes, effecting an impingement pressure drop. In the method discharge flow is metered through a number of discharge holes through said side wall or rims from the inner side to the outer side of the main wall, generating a discharge pressure drop in series with the impingement pressure drop. The impingement pressure drop and the discharge pressure drop are matched to one another so that a required coolant flow is generated which yields a required predetermined heat-transfer coefficient of the main wall. Discharging coolant into the gaps between side opposing walls of neighbouring heat shield elements only allows for an effective sealing against hot gas pingestion. Furthermore, the invention relates to a heat shield element, preferably to a single chamber or double chamber metallic heat shield element, which can be exposed to hot gases. In particular the heat shield element is suitable for being used in a combustion chamber of a gas turbine installation.
摘要翻译： 描述了一种用于冷却和密封隔热元件的方法，包括具有受侧壁或边缘限制的内侧的主壁和可暴露于热流体的外侧，其中， 冷却剂被引入该隔热元件的冲击区域中，并且所述冷却剂的冲击流通过多个冲击孔被引导到该内侧的表面区域，从而实现冲击压降。 在该方法中，通过穿过所述侧壁或从主壁的内侧到外侧的边缘的多个排出孔计量排出流量，产生与冲击压降串联的排出压降。 冲击压降和排出压降彼此匹配，从而产生所需的冷却剂流量，其产生主壁所需的预定传热系数。 将冷却剂排放到相邻的热屏蔽元件的相对的侧壁之间的间隙中仅允许有效的密封来防止热气体的腐蚀。 此外，本发明涉及一种隔热元件，优选地可以暴露于热气体的单室或双室金属隔热元件。 特别地，隔热元件适用于燃气轮机装置的燃烧室。
-
公开(公告)号：US08739543B2
公开(公告)日：2014-06-03
申请号：US12665049
申请日：2008-01-18
申请人： Eberhard Deuker , Anil Gulati , Andreas Heilos
发明人： Eberhard Deuker , Anil Gulati , Andreas Heilos
IPC分类号： F02C9/26
摘要： A method for operating a burner including a burner outlet opening with at least two sectors, each sector is assigned at least one fuel nozzle, is provided. The method is characterized in that fuel is supplied separately to the fuel nozzles of different sectors. Also described is a burner which includes at least two sectors wherein each sector is assigned at least one fuel nozzle. The burner includes at least two separate fuel supply lines and a device for adjusting the fuel mass flow which flows through the respective fuel supply line. The fuel supply lines supply fuel to the fuel nozzles of different sectors. Also described is a gas turbine which is fitted with at least one burner.
摘要翻译： 一种用于操作燃烧器的方法，其包括具有至少两个扇区的燃烧器出口开口，每个扇区被分配至少一个燃料喷嘴。 该方法的特征在于，燃料单独供应到不同扇区的燃料喷嘴。 还描述了一种燃烧器，其包括至少两个扇区，其中每个扇区分配有至少一个燃料喷嘴。 燃烧器包括至少两个单独的燃料供应管线和用于调节流过各个燃料供应管线的燃料质量流量的装置。 燃料供应管线向不同部门的燃料喷嘴供应燃料。 还描述了装配有至少一个燃烧器的燃气轮机。
-
公开(公告)号：US07870738B2
公开(公告)日：2011-01-18
申请号：US11540030
申请日：2006-09-29
申请人： James M. Zborovsky , Andreas Heilos
发明人： James M. Zborovsky , Andreas Heilos
CPC分类号： F01D9/023 , F01D11/005 , F02C7/28 , F05D2240/55 , Y02T50/675
摘要： The present invention is directed to a seal for sealing a gap between transition sections of adjacent can annular combustors in a turbine engine such that the seal is usable in applications for sealing pressure drops of 0.5 bar or greater. The seal includes a plate configured to extend between adjacent transition sections and the plate may have at least one perforation extending from the front surface of the plate to the rear surface of plate. The seal further includes a porous matrix formed from materials capable of withstanding turbine combustion gas temperatures, wherein a portion of the porous matrix may be fixedly attached to a surface of the plate.
摘要翻译： 本发明涉及用于密封涡轮发动机中相邻罐式环形燃烧器的过渡部分之间的间隙的密封件，使得该密封件可用于密封0.5巴或更大的压降。 密封件包括被配置为在相邻过渡部分之间延伸的板，并且板可以具有从板的前表面延伸到板的后表面的至少一个穿孔。 密封件还包括由能够承受涡轮机燃烧气体温度的材料形成的多孔基体，其中一部分多孔基体可以固定地附接到板的表面。
-
-
-
-
-
-
-
-
-
搜索结果
30 条记录 (耗时 0.054 秒)
