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1.发明授权Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper 有权用于燃气轮机燃烧器的亥姆霍兹阻尼器和用于安装亥姆霍兹阻尼器的方法公开(公告)号：US08943825B2
公开(公告)日：2015-02-03
申请号：US13015640
申请日：2011-01-28
IPC分类号： F23R3/00
CPC分类号： F23R3/00 , F23C2900/07002 , F23D2210/00 , F23M20/005 , F23R2900/00016 , F23R2900/03342 , Y10T29/49229
摘要： A Helmholtz damper for a combustor of a gas turbine includes first and second damping volumes. The combustor has a combustion chamber disposed in a housing and closed off by a front plate at which a plurality of burners are exchangeably fastened. The burners are supplied with fuel via fuel lances which extend from outside the housing through a bushing of the housing to the associated burner. The first damping volume has a first end and a second end, the first end of the first damping volume being configured to attach a connecting passage extending to a front panel such that the Helmholtz damper is connectable with the front plate of the combustion chamber in place of one of the burners. The second damping volume has a first end and a second end and is arranged in series with the first damping volume along an axis of the Helmholtz damper with the first end of the second damping volume being detachably connected to the second end of the first damping volume so as to form a combined larger damping volume. The second end of the second damping volume is configured to attach a connecting tube extending from the second damping volume and through the bushing in place of a respective one of the fuel lances.
摘要翻译： 用于燃气涡轮机的燃烧器的亥姆霍兹阻尼器包括第一和第二阻尼体积。 燃烧器具有设置在壳体中的燃烧室，并且被前板封闭，多个燃烧器可交换地固定在该前板上。 燃烧器通过燃料喷枪供应燃料，燃料喷枪从壳体外部延伸穿过壳体的衬套到相关联的燃烧器。 第一阻尼体积具有第一端和第二端，第一阻尼体积的第一端构造成附接延伸到前面板的连接通道，使得亥姆霍兹阻尼器可与燃烧室的前板连接就位 的燃烧器之一。 第二阻尼体积具有第一端和第二端，并且沿着亥姆霍兹阻尼器的轴线与第一阻尼体积串联布置，第二阻尼体积的第一端可拆卸地连接到第一阻尼体积的第二端 以形成组合较大的阻尼体积。 第二阻尼体积的第二端构造成附接从第二阻尼体积延伸并通过套管代替相应的一个燃料喷枪的连接管。
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公开(公告)号：US07632091B2
公开(公告)日：2009-12-15
申请号：US11850849
申请日：2007-09-06
IPC分类号： F23D14/46
CPC分类号： F23D14/02 , F23C7/002 , F23C2900/07002
摘要： A premix burner for producing an ignitable fuel/air mixture has a swirl generator with at least two burner shells (B) which complement one another to form a throughflow body, which in each case have a first burner shell section (1) with a partial cone shape and together enclose an axially conically widening swirl space and which mutually define, in the axial cone longitudinal direction, tangential air inlet slots (LS), through which the combustion feed air (L) passes into the swirl space, in which an axially spreading swirl flow forms, and includes fuel feeds which are arranged at least in sections along the tangentially running air inlet slots (LS). A second burner shell section (8) curved in opposition to the first burner shell section (1), in each case designed in a partial cone shape, is added flush to the first burner shell section (1), a third burner shell section (9) adjoins the second burner shell section (8) flush, the third burner shell section (9) having a curvature tangentially adapted to the second burner shell section (8), and the third burner shell section (9) defines, on the one side in each case, one of the tangential air inlet slots (LS) and provides a leading edge (12) serving for the combustion feed air (L).
摘要翻译： 用于产生可燃燃料/空气混合物的预混合燃烧器具有涡流发生器，其具有至少两个彼此互补的燃烧器壳体（B），以形成通流体，每个燃烧器壳体具有第一燃烧器壳体部分（1） 锥体形状并且一起包围轴向锥形加宽的旋转空间，并且在轴向锥形纵向方向上相互限定切向空气入口狭槽（LS），燃烧进料空气（L）通过该空气入口狭槽进入涡流空间，其中轴向 扩展涡流形式，并且包括至少沿着切向运行的空气入口狭槽（LS）的部分布置的燃料进料。 与第一燃烧器壳体部分（1）相对弯曲的第二燃烧器壳体部分（8）在每种情况下以部分圆锥形状设计，与第一燃烧器壳体部分（1）齐平，第三燃烧器壳体部分 第二燃烧器壳体部分（8）与第二燃烧器壳部分（8）相邻，第三燃烧器壳部分（9）具有切向适合于第二燃烧器壳体部分（8）的曲率，并且第三燃烧器壳体部分（9） 在每个情况下，切向空气入口槽（LS）中的一个并且提供用于燃烧进料空气（L）的前缘（12）。
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公开(公告)号：US08007273B2
公开(公告)日：2011-08-30
申请号：US11838999
申请日：2007-08-15
IPC分类号： F23M3/00
CPC分类号： F23C7/002 , F23C2900/07002 , F23D17/002 , F23D2211/00 , F23R3/286
摘要： A premixing burner has a swirl generator with at least two burner shells (1) which jointly enclose an axia conically widening swirl space and delimit tangential air inlet slits (3) through which combustion supply air passes into the swirl space in which an axially propagating swirl flow is formed, and with fuel injection devices at least partially along the tangentially running air inlet slits (3). The fuel injection devices include a fuel line (6) separate from the burner shell (1) and which is firmly attached to the burner shell (1) so as to be longitudinally movable with respect to the burner shell (1) and releasable perpendicularly to the surface of the burner shell (1). In the burner shell (1), orifices (4) are provided, into which issue fuel injectors (7) which are provided along the fuel line (6) and which project beyond the circumferential edge of the fuel line (6).
摘要翻译： 预混燃烧器具有涡流发生器，其具有至少两个燃烧器壳体（1），该燃烧器壳体联合地包围轴向锥形加宽的涡流空间并限定切向空气入口狭缝（3），燃烧供给空气通过该空气入口狭缝（3）进入涡流空间， 流动形成，并且燃料喷射装置至少部分地沿着切向运行的空气入口狭缝（3）。 燃料喷射装置包括与燃烧器壳体（1）分离并且牢固地附接到燃烧器壳体（1）的燃料管线（6），以便能够相对于燃烧器壳体（1）纵向移动并且可以垂直于 燃烧器壳体（1）的表面。 在燃烧器壳体（1）中，设有孔口（4），其中沿燃料管线（6）设置并且突出超过燃料管线（6）的周边边缘的燃料喷射器（7）。
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4.发明申请HELMHOLTZ DAMPER FOR A COMBUSTOR OF A GAS TURBINE AND A METHOD FOR INSTALLING THE HELMHOLTZ DAMPER 有权用于燃气轮机燃烧器的HELMHOLTZ阻尼器和用于安装HELMHOLTZ阻尼器的方法公开(公告)号：US20110179796A1
公开(公告)日：2011-07-28
申请号：US13015640
申请日：2011-01-28
CPC分类号： F23R3/00 , F23C2900/07002 , F23D2210/00 , F23M20/005 , F23R2900/00016 , F23R2900/03342 , Y10T29/49229
摘要： A Helmholtz damper for a combustor of a gas turbine includes first and second damping volumes. The combustor has a combustion chamber disposed in a housing and closed off by a front plate at which a plurality of burners are exchangeably fastened. The burners are supplied with fuel via fuel lances which extend from outside the housing through a bushing of the housing to the associated burner. The first damping volume has a first end and a second end, the first end of the first damping volume being configured to attach a connecting passage extending to a front panel such that the Helmholtz damper is connectable with the front plate of the combustion chamber in place of one of the burners. The second damping volume has a first end and a second end and is arranged in series with the first damping volume along an axis of the Helmholtz damper with the first end of the second damping volume being detachably connected to the second end of the first damping volume so as to form a combined larger damping volume. The second end of the second damping volume is configured to attach a connecting tube extending from the second damping volume and through the bushing in place of a respective one of the fuel lances.
摘要翻译： 用于燃气涡轮机的燃烧器的亥姆霍兹阻尼器包括第一和第二阻尼体积。 燃烧器具有设置在壳体中的燃烧室，并且被前板封闭，多个燃烧器可交换地固定在该前板上。 燃烧器通过燃料喷枪供应燃料，燃料喷枪从壳体外部延伸穿过壳体的衬套到相关联的燃烧器。 第一阻尼体积具有第一端和第二端，第一阻尼体积的第一端构造成附接延伸到前面板的连接通道，使得亥姆霍兹阻尼器可与燃烧室的前板连接就位 的燃烧器之一。 第二阻尼体积具有第一端和第二端，并且沿着亥姆霍兹阻尼器的轴线与第一阻尼体积串联布置，第二阻尼体积的第一端可拆卸地连接到第一阻尼体积的第二端 以形成组合较大的阻尼体积。 第二阻尼体积的第二端构造成附接从第二阻尼体积延伸并通过套管代替相应的一个燃料喷枪的连接管。
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