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公开(公告)号：US08122726B2
公开(公告)日：2012-02-28
申请号：US12367997
申请日：2009-02-09
IPC分类号： F02C7/20
摘要： A combustion chamber of a combustion system has a combustion space, a support structure, a support element, and a heat shield. The heat shield has at least two segments, and each segment includes a liner element facing the combustion space and has an edge region, a gap communicating with the combustion space being formed between edge regions of adjacent segments, and a retaining device. The retaining device fixes the respective liner element on the support structure via the support element and forms a flange region that fits over the edge region of the respective liner element. The retaining device forms a first cooling passage with the support element and has at least one through-opening in the flange region. A cooling gas flows through the through.opening from the first cooling passage to the edge region.
摘要翻译： 燃烧系统的燃烧室具有燃烧空间，支撑结构，支撑元件和隔热罩。 隔热罩具有至少两个区段，并且每个区段包括面向燃烧空间的衬垫元件，并且具有边缘区域，与相邻区段的边缘区域之间形成的与燃烧空间连通的间隙以及保持装置。 保持装置通过支撑元件将相应的衬垫元件固定在支撑结构上，并形成配合在相应衬套元件的边缘区域上的凸缘区域。 保持装置与支撑元件形成第一冷却通道并且在凸缘区域中具有至少一个通孔。 冷却气体从第一冷却通道流过边缘区域。
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公开(公告)号：US08006498B2
公开(公告)日：2011-08-30
申请号：US12367908
申请日：2009-02-09
IPC分类号： F02C1/00
摘要： A combustion chamber of a combustion system comprises a combustion space, a support structure, a heat shield, and at least one through-opening. The heat shield has at least two segments, and each segment has an edge region, a gap communicating with the combustion space being formed between edge regions of adjacent segments, and a retaining device. The adjacent segments include a support element disposed in a bottom region of the gap. The retaining device fixes the respective liner element on the support structure via the respective support element. The at least one through-opening communicates with the gap so as to enable a cooling gas to flow through the through-opening. The at least one through-opening is disposed in at least one of the respective edge region and the support element at the bottom region of the gap.
摘要翻译： 燃烧系统的燃烧室包括燃烧空间，支撑结构，隔热罩和至少一个通孔。 隔热罩具有至少两个区段，并且每个区段具有边缘区域，与相邻区段的边缘区域之间形成的与燃烧空间连通的间隙和保持装置。 相邻的段包括设置在间隙的底部区域中的支撑元件。 保持装置通过相应的支撑元件将相应的衬垫元件固定在支撑结构上。 至少一个通孔与间隙连通，以使冷却气体能够流过通孔。 所述至少一个通孔设置在所述间隙的底部区域中的相应边缘区域和所述支撑元件中的至少一个中。
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公开(公告)号：US20110056200A1
公开(公告)日：2011-03-10
申请号：US12833579
申请日：2010-07-09
申请人： Charles SOOTHILL , Christian Steinbach , Allen Michael Pfeffer , Philippe Jean-Michel Paelinck , Jurgen Hoffmann
发明人： Charles SOOTHILL , Christian Steinbach , Allen Michael Pfeffer , Philippe Jean-Michel Paelinck , Jurgen Hoffmann
CPC分类号： F01K13/02 , Y02E20/16 , Y02E20/18 , Y02E20/326
摘要： Power plant characteristics are operated in a flexible manner by controlling the power consumption of a CO2 capture and compression system. The impact of CO2 capture and compression on the capacity of a power plant can be minimized to maximize the electric power the plant can deliver to the power grid and the impact of CO2 capture and compression on the average plant efficiency can be reduced, by an operating method and a power plant, in which the power consumption of the CO2 capture system is used to control the net output of the plant.
摘要翻译： 通过控制二氧化碳捕获和压缩系统的功率消耗，电厂特性以灵活的方式运行。 CO2捕获和压缩对发电厂容量的影响可以最小化，以最大限度地发挥电厂能够向电网提供的电力，并且通过运行可以减少二氧化碳捕获和压缩对平均工厂效率的影响 方法和发电厂，其中使用二氧化碳捕集系统的功率消耗来控制工厂的净产出。
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公开(公告)号：US20070207431A1
公开(公告)日：2007-09-06
申请号：US11689655
申请日：2007-03-22
IPC分类号： F23D14/62
CPC分类号： F23C7/002 , F23C2900/07002 , F23D11/24 , F23D11/38 , F23R3/343
摘要： A premix burner, for example for a gas turbine, having a conical swirl generator (1) and a cylindrical mixing section (2) which follows it in the direction of flow, includes a high-pressure atomizer nozzle (10) with one or more fuel feed passages. The high-pressure atomizer nozzle (10) includes at least two outlet passages, through which liquid fuel enters the swirl generator (1), these passages being arranged off-center with respect to the longitudinal axis of the nozzle and being configured in such a way that the spray cone (11) of the fuel is oriented at an angle (β) with respect to the longitudinal axis of the swirl generator (1) which is smaller than the cone half-angle (α) of the swirl generator (1). The outlet passages in particular have an internal geometry with a conically narrowed section.
摘要翻译： 包括具有圆锥形涡流发生器（1）的燃气轮机的预混合燃烧器和沿着流动方向跟随其的圆柱形混合部分（2）包括具有一个或多个的高压雾化喷嘴（10） 燃料供给通道。 高压雾化器喷嘴（10）包括至少两个出口通道，液体燃料通过该出口通道进入涡流发生器（1），这些通道相对于喷嘴的纵向轴线偏离中心，并被配置在 燃料的喷雾锥体（11）相对于涡流发生器（1）的纵向轴线以与旋流发生器（1）的锥形半角（α）小的角度（β）定向的方式， ）。 出口通道特别具有内部几何形状，具有锥形变窄的部分。
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35.发明申请Method for reducing the NOx emissions from a burner arrangement comprising a plurality of burners, and burner arrangement for carrying out the method 有权用于减少包括多个燃烧器的燃烧器装置的NOx排放的方法，以及用于执行该方法的燃烧器装置公开(公告)号：US20060144049A1
公开(公告)日：2006-07-06
申请号：US11337499
申请日：2006-01-24
IPC分类号： F02C7/26
CPC分类号： F23N5/082 , F23N1/002 , F23N2035/12 , F23N2037/02 , F23N2041/20
摘要： In a method for reducing the NOx emissions from a burner arrangement comprising a plurality of burners (B1, . . . , Bn), in particular in a gas turbine, which burners (B1, . . . , Bn) are operated in parallel and each burner supplied fuel by means of combustion air to form a flame (F1, . . . , Fn), an effective drop is achieved in a simple way by virtue of the fact that at a predetermined time the flame temperatures of individual burners (B1, . . . , Bn) or burner groups or differences between the flame temperatures of individual burners (B1, . . . , Bn) or burner groups are measured directly or indirectly. The fuel supply to those burners or burner groups whose flame temperature exceeds a predetermined value for the flame temperature is selectively throttled in order to homogenize the flame temperatures of the burners (B1, . . . , Bn).
摘要翻译： 在一种用于减少包括多个燃烧器（B 1，...，Bn）的燃烧器装置的NOx排放的方法中，特别是在燃气轮机（B 1，...，B n）中操作燃烧器 平行和每个燃烧器通过燃烧空气供应燃料以形成火焰（F 1，...，Fn），由于以下事实实现了有效的下降，即在预定时间内个体的火焰温度 燃烧器（B 1，...，Bn）或燃烧器组或个别燃烧器（B 1，...，Bn）或燃烧器组的火焰温度之间的差异直接或间接测量。 火焰温度超过火焰温度的预定值的那些燃烧器或燃烧器组的燃料供应被选择性地节流，以便均化燃烧器（B 1，...，B n）的火焰温度。
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36.发明授权Method for combustion of a liquid fuel in a combustion system, and a combustion system for carrying out the method 失效燃烧系统中的液体燃料的燃烧方法和用于实施该方法的燃烧系统公开(公告)号：US06336806B1
公开(公告)日：2002-01-08
申请号：US09615950
申请日：2000-07-13
IPC分类号： F23D1132
CPC分类号： F23D11/32 , F23D2210/00
摘要： In a method for burning a liquid fuel in a combustion system (10) which comprises a combustion chamber (11) and at least one injection nozzle (13) through which liquid fuel is injected into the combustion chamber (11) in the form of a fuel spray (16) and is burnt there with combustion air being added, disturbance-free operation in a simple manner is distinguished in that, in order to actively suppress hydrodynamic instabilities in the combustion chamber (11), the injected fuel spray (16) is modulated by having an electrical voltage applied to it during the injection process, governed by a selected time function.
摘要翻译： 在用于燃烧燃料系统（10）中的液体燃料的方法中，所述燃烧系统（10）包括燃烧室（11）和至少一个喷射喷嘴（13），液体燃料通过该燃料室喷射到燃烧室（11）中， 燃料喷雾（16），并在其上燃烧有燃烧空气，其区别在于无扰动操作的特征在于为了主动地抑制燃烧室（11）中的流体动力学不稳定性，喷射的燃料喷雾（16） 通过在注入过程期间施加电压而被调制，由所选时间函数控制。
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公开(公告)号：US06331109B1
公开(公告)日：2001-12-18
申请号：US09624258
申请日：2000-07-24
IPC分类号： F23D1446
CPC分类号： F23R3/343 , F23C7/002 , F23C2900/07002 , F23D17/002 , F23D2211/00 , F23D2214/00 , F23R3/286 , F23R3/60
摘要： A premix burner consisting essentially of a swirl generator for a combustion air stream or another gaseous oxidizing medium and of conduits for injecting fuel into the swirl flow thus generated. As a result of a discontinuous cross-sectional widening at the transition to the combustion space, the swirl flow bursts open and a backflow bubble is formed, which serves for flame stabilization. For use under extreme thermal conditions, the burner front is provided with a heat shield which is fastened to a carrier structure in such a way as to allow, as unimpeded as possible, differential thermal expansions. The carrier structure is preferably provided with orifices, through which cooling air for the impact cooling of the heat shield flows. In a preferred variant, the fuel gas supply is designed as pipes which are led through orifices of the swirl generator without any fixed connection. As a result of this design, thermal stresses in the material of the burner are avoided as far as possible.
摘要翻译： 一种预混燃烧器，主要由用于燃烧空气流的漩涡发生器或另一种气态氧化介质组成，以及用于将燃料喷射到由此产生的涡流中的导管。 由于在向燃烧空间的过渡处的不连续的横截面加宽的结果，涡流突然打开，并且形成了用于火焰稳定的回流气泡。 为了在极端的热条件下使用，燃烧器前部设置有热屏蔽件，其以这样的方式固定到承载结构上，以允许尽可能不受阻碍地差热膨胀。 载体结构优选地设置有用于防风罩的冲击冷却的冷却空气流过的孔。 在优选的变型中，燃料气体供应被设计为管道，其被引导通过涡流发生器的孔口而没有任何固定的连接。 作为该设计的结果，尽可能避免了燃烧器材料中的热应力。
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公开(公告)号：US6045351A
公开(公告)日：2000-04-04
申请号：US210738
申请日：1998-12-15
CPC分类号： F23D11/402 , F23C7/002 , F23D17/002 , F23C2900/07002 , F23D2209/20
摘要： In a method of operating a burner of a heat generator, in which the burner essentially includes a swirl generator for a combustion-air flow, a mechanism for injecting at least one fuel into the combustion-air flow, and a number of transition passages for passing a flow formed in the swirl generator into a mixing tube arranged downstream of the transition passages, a predetermined quantity of a second fuel having a good ignition quality is injected into the reaction zone in order to stabilize the combustion in the combustion space.
摘要翻译： 在操作热发生器的燃烧器的方法中，其中燃烧器基本上包括用于燃烧空气流的涡流发生器，用于将至少一种燃料喷射到燃烧空气流中的机构，以及用于 将形成在涡流发生器中的流动通过布置在过渡通道下游的混合管中，将预定量的具有良好点火质量的第二燃料注入到反应区中，以稳定燃烧空间中的燃烧。
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