公开(公告)号：US06631614B2

公开(公告)日：2003-10-14

申请号：US09756188

申请日：2001-01-09

申请人： Shigemi Mandai ,  Tetsuo Gora ,  Katsunori Tanaka ,  Kouichi Nishida

发明人： Shigemi Mandai ,  Tetsuo Gora ,  Katsunori Tanaka ,  Kouichi Nishida

IPC分类号： F23R330

CPC分类号： F23D23/00 ,  F23D17/002 ,  F23D2900/00008 ,  F23R3/286 ,  F23R3/34

摘要： A gas turbine combustor, in which plural pre-mixers that inject fuel into swirling air passages are arranged to surround a pilot burner, and a pilot flame, guided by a pilot cone in the shape of a flaring pipe and provided at the rear end of the pilot burner, is mixed with a pre-mixture blown out from the pre-mixers to obtain a combustion gas, comprising flame-stabilizing means. The flame-stabilizing means lower the disturbance in a region where the pre-mixture and the pilot flame are mixed or stabilize the pilot flame, so that the flame generated by igniting the pre-mixture with the pilot flame is stabilized. By stabilizing the flame, combustion with a leaner air-fuel ratio is possible, and thereby the amount of NOx can be decreased.

摘要翻译： 一种燃气轮机燃烧器，其中将燃料喷射到旋流空气通道中的多个预混合器被布置成围绕引燃燃烧器和引燃火焰，引导火焰由扩口管形式的先导锥体引导并且设置在 引燃燃烧器与从预混合器吹出的预混合物混合以获得包含火焰稳定装置的燃烧气体。 火焰稳定装置降低预混合物和引燃火焰混合或稳定引燃火焰的区域中的扰动，使得通过用引燃火焰点燃预混合物而产生的火焰是稳定的。 通过稳定火焰，可以用较稀的空燃比进行燃烧，从而可以减少NOx的量。

公开(公告)号：US6105372A

公开(公告)日：2000-08-22

申请号：US145499

申请日：1998-09-02

申请人： Shigemi Mandai ,  Masataka Ota ,  Katsunori Tanaka ,  Shinji Akamatsu

发明人： Shigemi Mandai ,  Masataka Ota ,  Katsunori Tanaka ,  Shinji Akamatsu

IPC分类号： F02C7/18 ,  F23R3/10 ,  F23R3/42 ,  F02C1/00

CPC分类号： F23R3/10 ,  F05B2260/202

摘要： A gas turbine combustor having a combustion chamber (10) with a steam-cooled peripheral wall (2) has an air hole (1) for injecting dilution air therethrough bored in the peripheral wall (2) on an upstream side of the combustion chamber (10). The air is thereby supplied through the air hole (1) into the vicinity of an inner surface of the peripheral wall (2) to form a film flow of air, and an increase of the fuel concentration there is suppressed. The dilution air is preferably supplied from a gas turbine compressor (6).

摘要翻译： 具有具有蒸汽冷却周边壁（2）的燃烧室（10）的燃气轮机燃烧器具有用于在燃烧室的上游侧的周壁（2）中喷射稀释空气的空气孔（1） 10）。 因此，空气通过空气孔（1）供给到周壁（2）的内表面附近，形成空气的膜流，抑制了燃料浓度的增加。 稀释空气优选地从燃气涡轮压缩机（6）供给。

公开(公告)号：US07669421B2

公开(公告)日：2010-03-02

申请号：US11334744

申请日：2006-01-19

申请人： Keijiro Saitoh ,  Masataka Ohta ,  Satoshi Tanimura ,  Shigemi Mandai

发明人： Keijiro Saitoh ,  Masataka Ohta ,  Satoshi Tanimura ,  Shigemi Mandai

IPC分类号： F02C3/00

CPC分类号： F23R3/14 ,  F23C2900/07001 ,  Y02E20/344 ,  Y02T50/675

摘要： A gas turbine combustor having an inner tube and a transition pipe connected together is provided. The combustor includes an internal swirler and an external swirler. The internal swirler is composed of a cylindrical inward swirler ring disposed concentrically with respect to a central axis of the inner tube, and a plurality of inward swirler vanes provided on an outer peripheral surface of the inward swirler ring. The external swirler is composed of a cylindrical outward swirler ring disposed on an outer peripheral side of the inward swirler vanes and concentrically with respect to the inward swirler ring, and a plurality of outward swirler vanes provided on an outer peripheral surface of the outward swirler ring. The internal swirler and the external swirler are disposed within the inner tube.

摘要翻译： 提供了具有连接在一起的内管和过渡管的燃气轮机燃烧器。 燃烧器包括内部旋流器和外部旋流器。 内部旋流器由相对于内管的中心轴线同心设置的圆筒形向内旋流器环以及设置在向内旋流器环的外周表面上的多个向内旋流叶片组成。 外部旋流器由设置在向内旋流叶片的外周侧并相对于向内旋流器环同心的圆柱形向外旋流器环组成，并且设置在外旋流器环的外周表面上的多个向外旋流叶片 。 内部旋流器和外部旋流器设置在内管内。

公开(公告)号：US6068467A

公开(公告)日：2000-05-30

申请号：US244031

申请日：1999-02-04

申请人： Shigemi Mandai ,  Koichi Nishida ,  Masataka Ota ,  Satoshi Tanimura ,  Kotaro Miyauchi ,  Mitsuru Inada ,  Shinji Akamatsu ,  Hideki Haruta

发明人： Shigemi Mandai ,  Koichi Nishida ,  Masataka Ota ,  Satoshi Tanimura ,  Kotaro Miyauchi ,  Mitsuru Inada ,  Shinji Akamatsu ,  Hideki Haruta

IPC分类号： F23D14/02 ,  F23D23/00 ,  F23C5/00

CPC分类号： F23D23/00 ,  F23D14/02 ,  F23D2206/10 ,  F23D2209/10 ,  F23D2900/14021

摘要： A combustor has a pilot nozzle 02 arranged at a central portion of an inner cylinder 01 opening at its end into a combustion chamber 018 and includes a plurality of main nozzles 03 arranged around its outer circumference. Along the outer circumference of a flame holding cone 014 for igniting a fuel F injected from the main nozzles 03 there are disposed elliptical extension pipes 016 of an elliptical sectional shape which are extended from the fronts of the main nozzles 03 to have openings at the axial position of the opening of the flame holding cone 014. As a result, a hot premixed flame 013 does not flow back to a main swirler zone 015 of the circumferential edges of the openings of the main nozzles 03 so that mixing between the fuel F and an air flow A can be improved, reducing the Nox emission while eliminating the burning of a base plate 04 and the main nozzles 03.

摘要翻译： 燃烧器具有引导喷嘴02，其设置在内筒01的中心部分处，内筒01在其端部处开放到燃烧室018中，并且包括围绕其外圆周布置的多个主喷嘴03。 沿着用于点燃从主喷嘴03喷射的燃料F的火焰保持锥体014的外圆周，设置椭圆形截面形状的椭圆形延伸管016，其从主喷嘴03的前面延伸，以在轴向上具有开口 火焰保持锥体014的开口的位置。结果，热预混火焰013不流回到主喷嘴03的开口的周缘的主旋流器区域015，使得燃料F和 可以改善空气流A，减少Nox排放，同时消除基板04和主喷嘴03的燃烧。

公开(公告)号：US09957893B2

公开(公告)日：2018-05-01

申请号：US14007253

申请日：2012-03-14

申请人： Satoshi Takiguchi ,  Keijiro Saito ,  Teruhiro Matsumoto ,  Kenji Sato ,  Hidenobu Tamai ,  Shigemi Mandai

发明人： Satoshi Takiguchi ,  Keijiro Saito ,  Teruhiro Matsumoto ,  Kenji Sato ,  Hidenobu Tamai ,  Shigemi Mandai

IPC分类号： F02C1/00 ,  F02C7/18 ,  F23R3/42 ,  F23R3/00 ,  F23R3/28 ,  F01D9/02 ,  F01D25/14

CPC分类号： F02C7/18 ,  F01D9/023 ,  F01D25/14 ,  F23R3/002 ,  F23R3/286 ,  F23R3/42 ,  F23R2900/00012

摘要： A combustor (10) according to the invention includes: a combustor basket (14) in which compressed air and fuel are mixed with each other and the mixture is combusted; a transition piece (17) in which a tip portion of the combustor basket (14) is inserted with a gap (C) therebetween; a spring clip (19) that seals the gap between the combustor basket (14) and the transition piece (17); a throttle section (21) that is provided in an opening portion (Ck) of the gap (C) that is opened to the transition piece (17) on the tip side of the combustor basket (14), and narrows an opening area of the opening portion (Ck), compared to the base end side; and cooling device (22) for cooling the throttle section (21).

公开(公告)号：US09719419B2

公开(公告)日：2017-08-01

申请号：US13817384

申请日：2012-02-28

申请人： Satoshi Sometani ,  Satoshi Takiguchi ,  Shigemi Mandai

发明人： Satoshi Sometani ,  Satoshi Takiguchi ,  Shigemi Mandai

IPC分类号： F02C7/00 ,  F23R3/10 ,  F23R3/54 ,  F23R3/28 ,  F23R3/34

CPC分类号： F02C7/00 ,  F23R3/10 ,  F23R3/286 ,  F23R3/343 ,  F23R3/54 ,  F23R2900/00014

摘要： A gas turbine combustor includes: an external cylinder (31); an inner cylinder (32) provided inside the external cylinder (31) to form an air passage (30) between the external cylinder (31) and the inner cylinder (32); a pilot nozzle (35) provided in a center part of the inner cylinder (32) along a direction of a combustor axis (S); a plurality of main nozzles (36) provided on an inner peripheral surface of the inner cylinder (32) along a circumferential direction thereof so as to surround the pilot nozzle (35), the plurality of main nozzles (36) premixing fuel with combustion air introduced to the air passage (30) and ejecting the fuel into the inner cylinder (32); and a top hat nozzle (41) provided inside the air passage (30) across a circumferential direction to mix fuel with the combustion air prior to reaching the plurality of main nozzles (36).

公开(公告)号：US08950190B2

公开(公告)日：2015-02-10

申请号：US13388204

申请日：2010-11-05

申请人： Keijiro Saito ,  Shinji Akamatsu ,  Kenji Sato ,  Shigemi Mandai

发明人： Keijiro Saito ,  Shinji Akamatsu ,  Kenji Sato ,  Shigemi Mandai

IPC分类号： F23R3/06 ,  F23R3/46 ,  F23R3/16 ,  F23R3/42 ,  F02C7/18

CPC分类号： F23R3/06 ,  F02C7/18 ,  F23R3/16 ,  F23R3/42 ,  F23R3/46 ,  F23R2900/03045

摘要： In a gas turbine combustor and a gas turbine, an air passage (54) that supplies combustion high-pressure air, a pilot nozzle (44), a main fuel nozzle (45), and a top hat nozzle (47) that supply fuel, and openings (64) that supply film air (cooling air) are provided with respect to a combustor inner cylinder (42), and contraction members (71, 72, and 73) are arranged along a circumferential direction on an inner wall surface in a downstream of a flow direction of combustion gas in the inner cylinder (42). The contraction members (71, 72, and 73) are provided in a predetermined area in the circumferential direction excluding penetrating portions (74, 75, and 76), which do not disturb the flow of cooling air, thereby enabling to suppress generation of carbon monoxide and the like and to suppress the occurrence of unstable combustion.

摘要翻译： 在燃气轮机燃烧器和燃气轮机中，提供燃烧高压空气的空气通道（54），提供燃料的先导喷嘴（44），主燃料喷嘴（45）和顶帽喷嘴（47） ，并且相对于燃烧器内筒（42）设置供给膜空气（冷却空气）的开口部（64），在内壁面上沿着圆周方向配置收缩部件（71,72,73） 在内筒（42）中的燃烧气体的流动方向的下游。 收缩构件（71,72和73）设置在不妨碍冷却空气流动的穿透部（74,75,76）的周向的规定区域中，能够抑制碳的产生 一氧化物等，并抑制不稳定燃烧的发生。

公开(公告)号：US06502399B2

公开(公告)日：2003-01-07

申请号：US09794134

申请日：2001-02-28

申请人： Shigemi Mandai ,  Masataka Ohta ,  Mitsuru Inada ,  Shinji Akamatsu

发明人： Shigemi Mandai ,  Masataka Ohta ,  Mitsuru Inada ,  Shinji Akamatsu

IPC分类号： F23R314

CPC分类号： F23R3/14

摘要： A pre-mixture forming swirler in a gas turbine pre-mixed flame type low NOx combustor is improved so as to accelerate mixing of fuel and air and to prevent the occurrence of flame stagnation and burning of components. In particular, a three-dimensional swirler is constructed such that each swirler vane is twisted from a hub side thereof to a tip side so that a fitting angle of the tip side relative to a center axis of a fuel nozzle is larger than an angle of the hub side. Thereby, while the angle of the hub side is set smaller so that flame stagnation and burning of components resulted therefrom may be prevented from occurring, the angle of the tip side may be selected so that the shearing flow necessary for appropriate mixing of fuel and air is obtained. Thus, favorable pre-mixing is achieved, life deterioration due to burning, etc., is prevented and combustion efficiency is enhanced.

摘要翻译： 在燃气轮机预混合火焰型低NOx燃烧器中形成旋流器的预混合物得到改善，以加速燃料和空气的混合，并防止部件火焰停滞和燃烧。 特别地，三维旋流器被构造成使得每个旋流器叶片从其轮毂侧扭转到尖端侧，使得尖端侧相对于燃料喷嘴的中心轴线的配合角度大于 集线器侧。 由此，在将轮毂侧的角度设定得较小的同时，能够防止由此引起的部件产生火焰停滞和燃烧的情况下，可以选择前端侧的角度，使得适当地混合燃料和空气所需的剪切流 获得。 因此，可以实现良好的预混合，防止燃烧等引起的寿命劣化，提高燃烧效率。

公开(公告)号：US06389796B1

公开(公告)日：2002-05-21

申请号：US09666188

申请日：2000-09-21

申请人： Shigemi Mandai ,  Hidetaka Mori ,  Hideaki Sugishita ,  Eiji Akita

发明人： Shigemi Mandai ,  Hidetaka Mori ,  Hideaki Sugishita ,  Eiji Akita

IPC分类号： F02C330

CPC分类号： F01K23/10 ,  F01K21/047 ,  Y02E20/16

摘要： A gas turbine system and a combined plant including the gas turbine system provides a higher effect in realizing a high plant efficiency and reduction of NOx generation. The gas turbine system includes a compressor (1) for compressing combustion air, a combustor (2) for burning fuel with the combustion air, and a gas turbine (3) driven by high temperature gas generated at the combustor (2). A portion of the exhaust gas discharged from the gas turbine (3) is recirculated back into the combustor (2). A combined plant can also include the gas turbine system.

摘要翻译： 燃气轮机系统和包括燃气轮机系统的组合设备在实现高设备效率和减少NOx产生方面提供更高的效果。 燃气轮机系统包括用于压缩燃烧空气的压缩机（1），用于燃烧燃烧空气的燃料的燃烧器（2）和由燃烧器（2）产生的高温气体驱动的燃气轮机（3）。 从燃气轮机（3）排出的废气的一部分再循环回到燃烧器（2）中。 组合式工厂还可以包括燃气轮机系统。

公开(公告)号：US6116018A

公开(公告)日：2000-09-12

申请号：US35615

申请日：1998-03-05

申请人： Satoshi Tanimura ,  Shigemi Mandai ,  Tetsuo Gora ,  Hiroyuki Nishida

发明人： Satoshi Tanimura ,  Shigemi Mandai ,  Tetsuo Gora ,  Hiroyuki Nishida

IPC分类号： F02C3/30 ,  F02C7/16 ,  F02C7/18 ,  F23M5/08 ,  F23R3/42

CPC分类号： F23M5/085 ,  F02C3/30 ,  F02C7/16 ,  F05D2260/2322

摘要： A gas turbine plant having a compressor, gas turbine, and combustor, comprising a cooling system adapted to cool the wall of the combustor by means of air compressed by the combustor when the load of the gas turbine and/or the combustion load of the combustor is low, and an additional cooling system adapted to cool the wall of the combustor by means of a cooling medium different from the air in addition to the cooling by means of the air when the load of the gas turbine is increased.

摘要翻译： 一种具有压缩机，燃气轮机和燃烧器的燃气轮机设备，包括冷却系统，该冷却系统适用于当燃气轮机的负载和/或燃烧器的燃烧负荷时由燃烧器压缩的空气来冷却燃烧器的壁 以及另外的冷却系统，其适于通过不同于空气的冷却介质来冷却燃烧器的壁，以及当燃气轮机的负载增加时，借助于空气的冷却。