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公开(公告)号：US20120047898A1
公开(公告)日：2012-03-01
申请号：US13218065
申请日：2011-08-25
CPC分类号： F23R3/12 , F23C2900/07002 , F23D2900/14021 , F23R3/286 , Y10T29/4932 , Y10T29/49716
摘要： A premix burner is provided for a gas turbine, in the form of a double-cone burner, which has two partial cone shells which are arranged nested one inside the other, forming air inlet ducts between them, through which combustion air from the outside flows into a conical inner space of the premix burner. Linear rows of holes of injection openings, which extend transversely to the flow direction of the combustion air, are arranged on the outer walls of the air inlet ducts and through which a gaseous fuel is injected into the combustion air which flows past transversely to them. A method for reworking such premix burners is also provided.
摘要翻译： 为双燃烧器形式的燃气轮机提供了一种预混燃烧器，该双燃烧器具有两个部分锥形壳体，两个部分锥形壳体嵌套在一起，在它们之间形成空气入口管道，来自外部的燃烧空气流经 进入预混燃烧器的锥形内部空间。 在空气入口管道的外壁上布置有横向于燃烧空气的流动方向延伸的注射开口的直线排，并且气体燃料通过该排气喷射到横向流过的燃烧空气中。 还提供了一种用于重新加工这种预混燃烧器的方法。
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公开(公告)号：US09170022B2
公开(公告)日：2015-10-27
申请号：US13218065
申请日：2011-08-25
CPC分类号： F23R3/12 , F23C2900/07002 , F23D2900/14021 , F23R3/286 , Y10T29/4932 , Y10T29/49716
摘要： A premix burner is provided for a gas turbine, in the form of a double-cone burner, which has two partial cone shells which are arranged nested one inside the other, forming air inlet ducts between them, through which combustion air from the outside flows into a conical inner space of the premix burner. Linear rows of holes of injection openings, which extend transversely to the flow direction of the combustion air, are arranged on the outer walls of the air inlet ducts and through which a gaseous fuel is injected into the combustion air which flows past transversely to them. A method for reworking such premix burners is also provided.
摘要翻译： 为双燃烧器形式的燃气轮机提供了一种预混燃烧器，该双燃烧器具有两个部分锥形壳体，两个部分锥形壳体嵌套在一起，在它们之间形成空气入口管道，来自外部的燃烧空气流经 进入预混燃烧器的锥形内部空间。 在空气入口管道的外壁上布置有横向于燃烧空气的流动方向延伸的注射开口的直线排，并且气体燃料通过该排气喷射到横向流过的燃烧空气中。 还提供了一种用于重新加工这种预混燃烧器的方法。
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公开(公告)号：US08434312B2
公开(公告)日：2013-05-07
申请号：US13241983
申请日：2011-09-23
申请人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
发明人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
IPC分类号： F02C7/228
CPC分类号： F02C9/26 , F02C6/003 , F23C6/042 , F23N1/022 , F23N2037/02 , F23N2041/20 , F23R7/00 , F23R2900/03341 , Y02E20/16
摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the air ratio (λ) of the operative burners (9) of the second combustor (15) is kept below a maximum air ratio (λmax) at part load In order to reduce the maximum air ratio (λ), a series of modifications in the operating concept of the gas turbine are carried out individually or in combination. One modification is an opening of the row of variable compressor inlet guide vanes (14) before engaging the second combustor (15). For engaging the second combustor, the row of variable compressor inlet guide vanes (14) is quickly closed and fuel is introduced in a synchronized manner into the burner (9) of the second combustor (15). A further modification is the deactivating of individual burners (9) at part load.
摘要翻译： 在具有顺序燃烧的燃气轮机的低CO排放部分负荷操作的方法中，第二燃烧器（15）的操作燃烧器（9）的空气比（λ）保持在最大空气比（lambdamax）以下） 在部分负载下为了降低最大空气比（lambda），对燃气轮机的操作概念进行一系列修改，可单独进行或组合进行。 一个变型是在接合第二燃烧器（15）之前的一排可变压缩机入口导叶（14）的开口。 为了接合第二燃烧器，可变压缩机入口导叶（14）的排被快速关闭，燃料以同步的方式被引入第二燃烧器（15）的燃烧器（9）。 进一步的修改是在部分负载下单个燃烧器（9）的停用。
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公开(公告)号：US07082768B2
公开(公告)日：2006-08-01
申请号：US10869942
申请日：2004-06-18
CPC分类号： F23D17/002 , F23C7/002 , F23C2900/07002 , F23D11/402 , F23D14/76 , F23D2900/00015 , F23D2900/00016
摘要： In a fuel lance by means of which fuels can be injected, via at least two separate passages, into a combustion chamber alternately or simultaneously at an injection location arranged substantially at the lance tip, reliable operation is achieved, without the risk of flashbacks and also without coking, by virtue of the fact that the fuel lance, in addition to fuel, also passes purge air to the injection location, and that the purge air, at the injection location, is routed between the two fuel systems, in such a manner that these systems are shielded from one another by the purge air.
摘要翻译： 在燃料喷枪中，燃料可以通过至少两个独立的通道在基本上布置在喷枪尖端处的喷射位置处交替地或同时地喷射到燃烧室中，实现可靠的操作，而没有回火的风险，并且还 由于除了燃料之外，燃料喷枪也将吹扫空气通过到喷射位置，并且在喷射位置处的吹扫空气以这种方式在两个燃料系统之间布置 这些系统被吹扫空气彼此隔离。
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公开(公告)号：US20050028532A1
公开(公告)日：2005-02-10
申请号：US10869942
申请日：2004-06-18
CPC分类号： F23D17/002 , F23C7/002 , F23C2900/07002 , F23D11/402 , F23D14/76 , F23D2900/00015 , F23D2900/00016
摘要： In a fuel lance by means of which fuels can be injected, via at least two separate passages, into a combustion chamber alternately or simultaneously at an injection location arranged substantially at the lance tip, reliable operation is achieved, without the risk of flashbacks and also without coking, by virtue of the fact that the fuel lance, in addition to fuel, also passes purge air to the injection location, and that the purge air, at the injection location, is routed between the two fuel systems, in such a manner that these systems are shielded from one another by the purge air.
摘要翻译： 在燃料喷枪中，燃料可以通过至少两个独立的通道在基本上布置在喷枪尖端处的喷射位置处交替地或同时地喷射到燃烧室中，实现可靠的操作，而没有回火的风险，并且还 由于除了燃料之外，燃料喷枪也将吹扫空气通过到喷射位置，并且在喷射位置处的吹扫空气以这种方式在两个燃料系统之间布置 这些系统被吹扫空气彼此隔离。
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公开(公告)号：US20120017601A1
公开(公告)日：2012-01-26
申请号：US13241983
申请日：2011-09-23
申请人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
发明人： Adnan Eroglu , Klaus Knapp , Peter Flohr , Hans Peter Knöpfel , Weiqun Geng
CPC分类号： F02C9/26 , F02C6/003 , F23C6/042 , F23N1/022 , F23N2037/02 , F23N2041/20 , F23R7/00 , F23R2900/03341 , Y02E20/16
摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the air ratio (λ) of the operative burners (9) of the second combustor (15) is kept below a maximum air ratio (λmax) at part load In order to reduce the maximum air ratio (λ), a series of modifications in the operating concept of the gas turbine are carried out individually or in combination. One modification is an opening of the row of variable compressor inlet guide vanes (14) before engaging the second combustor (15). For engaging the second combustor, the row of variable compressor inlet guide vanes (14) is quickly closed and fuel is introduced in a synchronized manner into the burner (9) of the second combustor (15). A further modification is the deactivating of individual burners (9) at part load.
摘要翻译： 在具有顺序燃烧的燃气轮机的低CO排放部分负荷运行的方法中，第二燃烧器（15）的操作燃烧器（9）的空气比（λ）保持在最大空气比（λmax）以下， 在部分负载下为了降低最大空气比（λ），对燃气轮机的操作概念的一系列修改单独地或组合地进行。 一个变型是在接合第二燃烧器（15）之前的一排可变压缩机入口导叶（14）的开口。 为了接合第二燃烧器，可变压缩机入口导叶（14）的排被快速关闭，燃料以同步的方式被引入第二燃烧器（15）的燃烧器（9）。 进一步的修改是在部分负载下单个燃烧器（9）的停用。
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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：US20080163626A1
公开(公告)日：2008-07-10
申请号：US11426924
申请日：2006-06-27
IPC分类号： F02C1/00
CPC分类号： F23D17/002 , F23C7/002 , F23C2900/07002 , F23D11/402 , F23D14/76 , F23D2900/00015 , F23D2900/00016
摘要： In a fuel lance by means of which fuels can be injected, via at least two separate passages, into a combustion chamber alternately or simultaneously at an injection location arranged substantially at the lance tip, reliable operation is achieved, without the risk of flashbacks and also without coking, by virtue of the fact that the fuel lance, in addition to fuel, also passes purge air to the injection location, and that the purge air, at the injection location, is routed between the two fuel systems, in such a manner that these systems are shielded from one another by the purge air.
摘要翻译： 在燃料喷枪中，燃料可以通过至少两个独立的通道在基本上布置在喷枪尖端处的喷射位置处交替地或同时地喷射到燃烧室中，实现可靠的操作，而没有回火的风险，并且还 由于除了燃料之外，燃料喷枪也将吹扫空气通过到喷射位置，并且在喷射位置处的吹扫空气以这种方式在两个燃料系统之间布置 这些系统被吹扫空气彼此隔离。
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9.发明授权公开(公告)号：US07406827B2
公开(公告)日：2008-08-05
申请号：US11426924
申请日：2006-06-27
CPC分类号： F23D17/002 , F23C7/002 , F23C2900/07002 , F23D11/402 , F23D14/76 , F23D2900/00015 , F23D2900/00016
摘要： In a fuel lance by means of which fuels can be injected, via at least two separate passages, into a combustion chamber alternately or simultaneously at an injection location arranged substantially at the lance tip, reliable operation is achieved, without the risk of flashbacks and also without coking, by virtue of the fact that the fuel lance, in addition to fuel, also passes purge air to the injection location, and that the purge air, at the injection location, is routed between the two fuel systems, in such a manner that these systems are shielded from one another by the purge air.
摘要翻译： 在燃料喷枪中，燃料可以通过至少两个独立的通道在基本上布置在喷枪尖端处的喷射位置处交替地或同时地喷射到燃烧室中，实现可靠的操作，而没有回火的风险，并且还 由于除了燃料之外，燃料喷枪也将吹扫空气通过到喷射位置，并且在喷射位置处的吹扫空气以这种方式在两个燃料系统之间布置 这些系统被吹扫空气彼此隔离。
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公开(公告)号：US20080070176A1
公开(公告)日：2008-03-20
申请号：US11850849
申请日：2007-09-06
IPC分类号： F23D14/62
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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