公开(公告)号：US5239831A

公开(公告)日：1993-08-31

申请号：US727116

申请日：1991-07-09

申请人： Michio Kuroda ,  Nobuyuki Iizuka ,  Haruo Urushidani ,  Kazuhiko Kumata ,  Isao Sato ,  Tetsuo Sasada ,  Hajime Toriya ,  Yoshikazu Moritomo ,  Yoji Ishibashi ,  Takashi Ohmori ,  Shigeru Azuhata

发明人： Michio Kuroda ,  Nobuyuki Iizuka ,  Haruo Urushidani ,  Kazuhiko Kumata ,  Isao Sato ,  Tetsuo Sasada ,  Hajime Toriya ,  Yoshikazu Moritomo ,  Yoji Ishibashi ,  Takashi Ohmori ,  Shigeru Azuhata

IPC分类号： F23R3/12 ,  F23R3/16 ,  F23R3/30 ,  F23R3/34

CPC分类号： F23R3/343 ,  F23R3/16

摘要： A burner comprises at least one swirl member for mixing a fuel with an air previously to burning of the fuel, and at least one eddy generating device which is arranged in a flow of a mixture of the fuel and air to generate an eddy flow in the flow so that the eddy flow maintains a shape of a flame of the burned fuel. The at least one eddy generating device is arranged apart from a downstream end of the swirl member by a fixed sufficient distance so that the shape of the flame maintained by the eddy flow is prevented from moving toward the downstream end of the swirler member.

公开(公告)号：US5069029A

公开(公告)日：1991-12-03

申请号：US563191

申请日：1990-08-06

申请人： Michio Kuroda ,  Seiichi Kirikami ,  Katsukuni Hisano ,  Nobuyuki Iizuka ,  Haruo Urushidani ,  Isao Sato ,  Yoji Ishibashi ,  Takashi Ohmori

发明人： Michio Kuroda ,  Seiichi Kirikami ,  Katsukuni Hisano ,  Nobuyuki Iizuka ,  Haruo Urushidani ,  Isao Sato ,  Yoji Ishibashi ,  Takashi Ohmori

IPC分类号： F23C99/00 ,  F23R3/26 ,  F23R3/34 ,  F02C3/14 ,  F23R3/32

CPC分类号： F23R3/26 ,  F23R3/346

摘要： A gas turbine combustor comprising a head combustion chamber and a rear combustion chamber connected to a downstream side of the head combustion chamber, a first stage burner for premixing first stage fuel and air and supplying the resultant fuel and air premixture into the head combustion chamber to effect first stage premix combution, a second stage burner for premixing second stage fuel and air and the resultant fuel and air premixture into the rear combustion chamber to effect premix combustion in addition to the first stage premix combustion, and a device for regulating flow rates of combustion air to be premixed with first and second stage fuel. The combustor is further provided with a pilot burner in the head combustion chamber to form pilot flame and stabilize the first stage premix combustion.

公开(公告)号：US4898001A

公开(公告)日：1990-02-06

申请号：US144646

申请日：1988-01-11

申请人： Michio Kuroda ,  Isao Sato ,  Yoji Ishibashi ,  Yoshihiro Uchiyama ,  Takashi Ohmori ,  Shigeyuki Akatsu ,  Fumio Kato ,  Yorihide Segawa ,  Nobuyuki Iizuka

发明人： Michio Kuroda ,  Isao Sato ,  Yoji Ishibashi ,  Yoshihiro Uchiyama ,  Takashi Ohmori ,  Shigeyuki Akatsu ,  Fumio Kato ,  Yorihide Segawa ,  Nobuyuki Iizuka

IPC分类号： F23R3/04 ,  F23R3/28 ,  F23R3/34 ,  F23R3/44

CPC分类号： F23R3/44 ,  F23R3/04 ,  F23R3/28 ,  F23R3/346

摘要： A gas turbine combustor for reducing a production of NOx. The combustor includes a head combustion chamber and a rear combustion chamber which is larger in diameter than the head combustion chamber. The head combustion chamber is provided with an axially extending hollow frustoconical tubular member to form an annular combustion space therein, air holes for axially jetting air into the annular combustion chamber, air holes formed on a peripheral wall for injecting air and a plurality of fuel nozzles projected into the annular combustion space for injecting fuel into vortex formed by the air jet and the injected air flow whereby the flame is stabilized and lean combustion can be effected. The rear combustion chamber has a fuel and air supply means on the upstream side which includes air inlets formed by whirling vanes and fuel nozzles disposed in the air inlets so that fuel and air are mixed well. The fuel and air mixture is jetted substantially axially while whirling it so that formation of hot spots is avoided and the NOx formation is extremely limited.

摘要翻译： 一种用于减少NOx生产的燃气轮机燃烧器。 燃烧器包括头部燃烧室和直径大于头部燃烧室的后部燃烧室。 头部燃烧室设置有轴向延伸的中空截头圆锥​​形管状构件以在其中形成环形燃烧空间，用于将空气轴向地喷射到环形燃烧室中的气孔，形成在用于喷射空气的周壁上的气孔和多个燃料喷嘴 投射到环形燃烧空间中，用于将燃料喷射到由空气射流和喷射空气流形成的涡流中，从而使火焰稳定并且可以实现贫燃。 后燃烧室在上游侧具有燃料和空气供给装置，其包括由旋转叶片形成的空气入口和设置在空气入口中的燃料喷嘴，使得燃料和空气充分混合。 燃料和空气混合物在旋转时基本上轴向地喷射，从而避免形成热点并且非常限制NOx的形成。

公开(公告)号：US5272637A

公开(公告)日：1993-12-21

申请号：US670196

申请日：1991-03-15

申请人： Haruo Urushidani ,  Tomo Sato ,  Kazuhiko Kumata ,  Tetsuo Sasada ,  Koji Takahashi ,  Akira Shimura ,  Seiichi Kirikami ,  Isao Sato ,  Hideaki Kaneda

发明人： Haruo Urushidani ,  Tomo Sato ,  Kazuhiko Kumata ,  Tetsuo Sasada ,  Koji Takahashi ,  Akira Shimura ,  Seiichi Kirikami ,  Isao Sato ,  Hideaki Kaneda

IPC分类号： F02C9/28 ,  F02C9/32 ,  F02C9/26

CPC分类号： F02C9/32 ,  F02C9/28 ,  F05D2270/02 ,  F05D2270/05

摘要： A fuel supply amount is controlled while the load of a gas turbine is changed so that the fuel supply amount is shifted to a fuel supply amount in accordance with the changed load. A fuel supply control valve is operated at high speed during an initial stage and operated at a lower speed as the fuel supply amount necessary for the changed load is reached. Therefore flameout of a combustor is prevented without increasing the number of revolutions of the gas turbine over a certain upper limit.

摘要翻译： 在改变燃气轮机的负荷的同时控制燃料供给量，使得燃料供给量根据改变的负载转移到燃料供给量。 燃料供给控制阀在初始阶段以高速运行，并且在达到改变的负荷所需的燃料供给量时以较低的速度运行。 因此，在不增加燃气轮机的转数超过一定上限的情况下，能够防止燃烧器的熄火。

公开(公告)号：US5121597A

公开(公告)日：1992-06-16

申请号：US470596

申请日：1990-01-26

申请人： Haruo Urushidani ,  Seiichi Kirikami ,  Isao Sato ,  Nobuo Shimizu ,  Osamu Arai ,  Akira Shimura ,  Michio Kuroda ,  Tsuguaki Koga ,  Tadashi Kurokawa ,  Yoji Ishibashi ,  Katsukuni Hisano

发明人： Haruo Urushidani ,  Seiichi Kirikami ,  Isao Sato ,  Nobuo Shimizu ,  Osamu Arai ,  Akira Shimura ,  Michio Kuroda ,  Tsuguaki Koga ,  Tadashi Kurokawa ,  Yoji Ishibashi ,  Katsukuni Hisano

IPC分类号： F02C7/26 ,  F02C9/34 ,  F23C99/00 ,  F23R3/16 ,  F23R3/20 ,  F23R3/26 ,  F23R3/34

CPC分类号： F02C9/34 ,  F02C7/26 ,  F23R3/16 ,  F23R3/26 ,  F23R3/34 ,  F05D2270/31

摘要： A gas turbine combustor and a method of operating the gas turbine combustor, with the gas turbine combustor comprising a combustion sleeve, a combustion sub-chamber disposed at an upstream side of the combustion sleeve and having an air and fuel supply system, and a combustion main chamber disposed on a downstream side of the sub-chamber and having an air and fuel supply system. The combustion sub-chamber and combustion main chamber are formed in such a manner that the start-up of the gas turbine is effected by the hot combustion gas generated in the sub-chamber. The combustion sub-chamber is provided with an inner sleeve protruding from a side wall of the sub-chamber such that a tip of the inner sleeve is located in the vicinity of a downstream end of the sub-chamber, and a fuel nozzle is provided in a tip of the inner sleeve for increasing the fuel-to-air ratio during an initiating period of an increase in the gas turbine rotation speed.

公开(公告)号：US5319919A

公开(公告)日：1994-06-14

申请号：US984483

申请日：1992-12-02

申请人： Yoshiharu Nakayama ,  Isao Sato ,  Hiraku Ikeda ,  Michio Kuroda ,  Nobuyuki Iizuka ,  Kazuhiko Kumata ,  Fumiyuki Hirose ,  Akira Shimura ,  Minoru Takaba ,  Shoei Takahashi

发明人： Yoshiharu Nakayama ,  Isao Sato ,  Hiraku Ikeda ,  Michio Kuroda ,  Nobuyuki Iizuka ,  Kazuhiko Kumata ,  Fumiyuki Hirose ,  Akira Shimura ,  Minoru Takaba ,  Shoei Takahashi

IPC分类号： F02C7/26 ,  F02C9/28 ,  F23R3/26 ,  F23R3/28 ,  F23R3/34

CPC分类号： F23R3/34 ,  F23R3/26

摘要： A method for controlling a gas turbine combustor which comprises nozzles for injecting fuel into a combustor and which serves to combust the fuel with air in a combustion chamber so as to rotatively drive a gas turbine by combustion gas compressed as a result of combustion of a fuel, wherein the ratio of a flow rate of fuel supplied into the combustor to a flow rate of air supplied into the combustor is changed in accordance with at least one of the states of fuel, air and rotational frequency of the turbine.

摘要翻译： 一种用于控制燃气轮机燃烧器的方法，其包括用于将燃料喷射到燃烧器中并且用于使燃料与燃烧室中的空气燃烧的喷嘴，以便由于燃料燃烧而被压缩的燃烧气体旋转地驱动燃气轮机 其中，供给燃烧器的燃料的流量与供给燃烧器的空气的流量的比率根据涡轮机的燃料，空气和转速的状态中的至少一种而变化。

公开(公告)号：US4766721A

公开(公告)日：1988-08-30

申请号：US917973

申请日：1986-10-14

申请人： Nobuyuki Iizuka ,  Yoji Ishibashi ,  Isao Sato ,  Fumiyuki Hirose ,  Hiroshi Inose ,  Katsukuni Hisano ,  Katsuo Wada ,  Seiichi Kirikami ,  Michio Kuroda ,  Yoshihiro Uchiyama

发明人： Nobuyuki Iizuka ,  Yoji Ishibashi ,  Isao Sato ,  Fumiyuki Hirose ,  Hiroshi Inose ,  Katsukuni Hisano ,  Katsuo Wada ,  Seiichi Kirikami ,  Michio Kuroda ,  Yoshihiro Uchiyama

IPC分类号： F23R3/00 ,  F02C9/18 ,  F23R3/04 ,  F23R3/26 ,  F23R3/28 ,  F23R3/34

CPC分类号： F23R3/34 ,  F02C9/18 ,  F23R3/26 ,  F05D2270/31

摘要： A combustor of two-stage combustion type in which fuel is supplied only from primary fuel nozzles for combustion only in primary combustion chamber under the operating condition where gas turbine load is low, and premixed mixture is supplied into a secondary combustion chamber provided on the downstream side of the primary combustion chamber for combustion in both the primary and secondary combustion chambers under the operating condition where the load is high. An air-bleed passageway opens on a downstream side of air holes for intaking secondary combustion air to be mixed with secondary fuel and communicates with the outside of the combustor. The air-bleed passageway is provided with a regulating valve and the secondary combustion air is bled at the minimum point of the load where the secondary fuel is supplied so that the fuel to air ratio of secondary premixed mixture may not be excessively lean, thereby reducing the production of non-burned components.

摘要翻译： 一种二级燃烧式的燃烧器，其中，在燃气轮机负荷低的运行条件下，燃料仅从主燃料喷嘴供给燃料，仅在一级燃烧室中燃烧，并且将预混合物供给到设置在下游的二次燃烧室 在一次燃烧室中，在负载高的运行条件下在一次燃烧室和二次燃烧室中燃烧。 排气通道在气孔的下游侧开口，用于吸入与二次燃料混合的二次燃烧空气并与燃烧器的外部连通。 排气通道设置有调节阀，二次燃烧空气在供给二次燃料的负载的最小点处排出，使得二次预混混合物的燃料与空气的比例可能不会过度减少，从而减少 生产非烧成分。

公开(公告)号：US4683715A

公开(公告)日：1987-08-04

申请号：US807945

申请日：1985-12-12

申请人： Nobuyuki Iizuka ,  Katsukuni Hisano ,  Ryoichiro Oshima ,  Katsuo Wada ,  Fumiyuki Hirose ,  Michio Kuroda ,  Yoshihiro Uchiyama ,  Yoji Ishibashi ,  Isao Sato ,  Hiroshi Inose

发明人： Nobuyuki Iizuka ,  Katsukuni Hisano ,  Ryoichiro Oshima ,  Katsuo Wada ,  Fumiyuki Hirose ,  Michio Kuroda ,  Yoshihiro Uchiyama ,  Yoji Ishibashi ,  Isao Sato ,  Hiroshi Inose

IPC分类号： F01K23/10 ,  F02C7/26 ,  F02C9/18 ,  F02C9/28 ,  F02C9/52 ,  F23R3/26 ,  F23R3/34

CPC分类号： F23R3/26 ,  F02C7/26 ,  F02C9/18 ,  F23R3/34 ,  F05D2270/31 ,  Y02E20/16

摘要： A method of starting a gas turbine plant, which plant has at least one combustor including a primary combustion chamber into which primary fuel nozzles open and a secondary combustion chamber into which secondary fuel nozzles open, a compressor for supplying the combustor with compressed combustion air, and a gas turbine driven by the combustion gas generated in the combustor and adapted to drive a load such as an electric power generator. When the gas turbine is being accelerated to a rated speed or while the load is still below a normal load range, a fuel is supplied only to the primary fuel nozzle, whereas, in other loaded operation range, the fuel is supplied to both the primary and secondary fuel nozzles. Before the fuel supply to the secondary fuel nozzles is commenced, a part of the compressed air is bled through at least one air bleed pipe leading from the compressor and having an air bleed valve. The air bleed valve is controlled in such a manner that the opening degree thereof is maximized when the fuel supply to the secondary fuel nozzles is commenced and is progressively decreased in accordance with the increase of the load such as to become substantially zero when the load has been increased to the normal load range.

摘要翻译： 一种启动燃气轮机设备的方法，该设备具有至少一个燃烧器，该燃烧器包括初级燃料喷嘴打开的初级燃烧室和次级燃料喷嘴打开的二级燃烧室，用于向燃烧室供应压缩的燃烧空气的压缩机， 以及由在燃烧器中产生的燃烧气体驱动并适于驱动诸如发电机的负载的燃气轮机。 当燃气轮机正在加速到额定转速或负载仍然低于正常负载范围时，仅向主燃料喷嘴供应燃料，而在其他装载操作范围内，将燃料供应给主燃料 和二次燃料喷嘴。 在开始向二次燃料喷嘴供应燃料之前，一部分压缩空气通过至少一个从压缩机引出的排气管排出并具有排气阀。 控制排气阀，使得当向二次燃料喷嘴供应的燃料开始时，其开度最大化，并且随着负载的增加逐渐减小，当负载已经变为基本为零时 增加到正常负载范围。

公开(公告)号：US4587809A

公开(公告)日：1986-05-13

申请号：US677244

申请日：1984-12-03

申请人： Takashi Ohmori ,  Isao Sato ,  Yoji Ishibashi ,  Yoshimitsu Minakawa ,  Michio Kuroda ,  Zensuke Tamura

发明人： Takashi Ohmori ,  Isao Sato ,  Yoji Ishibashi ,  Yoshimitsu Minakawa ,  Michio Kuroda ,  Zensuke Tamura

IPC分类号： F23D14/02 ,  B01F5/04 ,  F23C6/04 ,  F23C15/00 ,  F23C99/00 ,  F23D14/62 ,  F23D14/82 ,  F23R3/34 ,  F02C1/00 ,  F02G3/00

CPC分类号： F23C15/00 ,  B01F5/0451 ,  F23C6/042 ,  F23D14/62 ,  F23D14/82 ,  F23R3/346

摘要： A premixing swirling burner including a burner body having a swirling member at one end for causing fuel introduced into the burner body to flow in vortical form through the swirling member, a burner outer frame mounting the burner body and communicated with an air line for introducing air into the burner body, and a cylindrical member located in the burner outer frame for enclosing the burner body, with an air passage being defined between the inner periphery of the cylindrical member and an outer periphery of a portion of the burner body. A premixing chamber is defined between an outer periphery of a central portion of the burner body and an inner periphery of the cylindrical member for providing a fuel-air premix flowing toward the swirling member. A fuel chamber introduces fuel into the interior of the burner body, and a fuel ejection nozzle is located along an outer surface of the central portion of the burner body. A channel defined between the inner periphery of an end portion of the cylindrical member and an outer peripheral portion of the burner body formed an inlet for the premixing chamber has a cross-sectional area smaller than a cross-sectional area of the air passage.

摘要翻译： 一种预混合旋转燃烧器，包括一端具有旋转构件的燃烧器主体，用于使引入燃烧器本体的燃料通过旋转构件以涡卷形式流动;燃烧器外框架，其安装燃烧器主体并与用于引入空气的空气管路连通 和位于燃烧器外框架中的圆筒形构件，用于封闭燃烧器主体，空气通道限定在圆柱形构件的内周和燃烧器本体的一部分外周之间。 在燃烧器主体的中心部分的外周和圆柱形部件的内周之间限定预混合室，用于提供朝向旋转部件流动的燃料 - 空气预混物。 燃料室将燃料引入燃烧器本体的内部，并且燃料喷射嘴位于燃烧器本体的中心部分的外表面。 形成在圆筒形构件的端部的内周和形成为预混合室的入口的燃烧器主体的外周部之间的通道的横截面积小于空气通道的横截面面积。

公开(公告)号：US5339620A

公开(公告)日：1994-08-23

申请号：US872139

申请日：1992-04-22

申请人： Hiraku Ikeda ,  Tetsuo Sasada ,  Isao Sato ,  Yoshikazu Moritomo ,  Koji Takahashi ,  Minoru Takaba

发明人： Hiraku Ikeda ,  Tetsuo Sasada ,  Isao Sato ,  Yoshikazu Moritomo ,  Koji Takahashi ,  Minoru Takaba

IPC分类号： F02C9/28 ,  F02C9/50 ,  F23R3/26

CPC分类号： F23R3/26

摘要： A control apparatus of a gas turbine combustor obtains a stable combustion with limited NOx emission through a control of a fuel flow rate according to a turbine output and a control of a flow rate of intake air mixed with the fuel. The control apparatus includes an apparatus for detecting at least one of the temperature and the humidity of intake air taken into the combustor, an apparatus for determining and storing, in advance, a stable combustion limit line between a stable combustion region and an unstable combustion region, on a plane of coordinates of a ratio of fuel flow rate to an intake air flow rate or an intake air flow rate and the temperature or the humidity of the intake air, on each turbine load, an apparatus for detecting an instant operational point of the combustor on the plane of coordinates, and an apparatus for correcting the intake air flow rate or the ratio of fuel flow rate to the intake air flow rate according to an increase in the detected temperature or humidity so that the instant operational point does not cross the stable combustion limit line.

摘要翻译： 燃气轮机燃烧器的控制装置通过根据涡轮机输出控制燃料流量和控制与燃料混合的进气的流量来获得具有有限NOx排放的稳定燃烧。 控制装置包括用于检测进入燃烧器的进气的温度和湿度中的至少一个的装置，用于预先确定和存储稳定燃烧区域和不稳定燃烧区域之间的稳定燃烧极限线的装置 在每个涡轮机负载上的燃料流量比与进气流量或进气流量之比的坐标平面和进气的温度或湿度之间，检测即时操作点的装置 坐标平面上的燃烧器，以及用于根据检测到的温度或湿度的增加来校正进气流量或燃料流量与进气流量比的装置，使得即时操作点不交叉 稳定燃烧极限线。