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：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：US5281129A

公开(公告)日：1994-01-25

申请号：US840813

申请日：1992-02-25

申请人： Haruo Urushidani ,  Seisaku Takihana ,  Kazuhiko Kumata ,  Akira Shimura ,  Osamu Arai ,  Takeshi Iwamiya ,  Hiraku Ikeda

发明人： Haruo Urushidani ,  Seisaku Takihana ,  Kazuhiko Kumata ,  Akira Shimura ,  Osamu Arai ,  Takeshi Iwamiya ,  Hiraku Ikeda

IPC分类号： F02C9/16 ,  F02C9/34 ,  F02C9/40 ,  F23C99/00 ,  F23R3/26 ,  F23R3/30 ,  F23N5/00

CPC分类号： F02C9/40 ,  F23R3/26 ,  F23R2900/00002

摘要： To provide a combustion apparatus and a controlling method therefor which are capable of preventing the flame-out and backfire of the flame of a premix burner and the increase of the NOx concentration attributable to the change of the calorific value of the fuel, the amount of air supplied to the premix burner is so controlled as to achieve a low NOx within the range in which the premix burner effects a stable combustion in accordance with the calorie of the fuel supplied to the combustion apparatus, and a change of the output of the combustion apparatus attributable to this control of the amount of air is compensated by the control of the amount of the fuel supplied to the diffusion burner.

摘要翻译： 为了提供能够防止预混燃烧器的火焰的熄火和回火以及归因于燃料的热值的变化引起的NOx浓度的增加的燃烧装置及其控制方法， 供给到预混燃烧器的空气被控制为在预混燃烧器根据供给到燃烧装置的燃料的热量实现稳定燃烧的范围内实现低的NOx，并且燃烧的输出的变化 通过控制供给到扩散燃烧器的燃料的量来补偿归因于该空气量的这种控制的装置。

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：US6077615A

公开(公告)日：2000-06-20

申请号：US991610

申请日：1997-12-16

申请人： Masami Yada ,  Takao Funamoto ,  Takamitsu Nakazaki ,  Kei Kobayashi ,  Norio Yokoba ,  Nobuyuki Iizuka ,  Kazuhiko Kumata

发明人： Masami Yada ,  Takao Funamoto ,  Takamitsu Nakazaki ,  Kei Kobayashi ,  Norio Yokoba ,  Nobuyuki Iizuka ,  Kazuhiko Kumata

IPC分类号： F01D5/28 ,  B23K35/30 ,  C22C19/07 ,  F01D5/00 ,  F01D9/02 ,  B32B15/00

CPC分类号： B23P6/007 ,  B23K35/3046 ,  B23P6/045 ,  F01D5/005 ,  Y10T428/12 ,  Y10T428/12222 ,  Y10T428/12639 ,  Y10T428/12646 ,  Y10T428/12861

摘要： A Co-base alloy including, by weight, 0.03-0.10% C, not more than 1.0% Si, not more than 1.0% Mn, 20-30% Cr, 15-23% Ni, 3-10% W, 5-10% Ta and 0.05-0.7% Zr, is used as a welding material. A gas turbine nozzle has a crack repaired with a multi-layer weld using the Co-base alloy and a gas turbine for power generation employs the nozzle.

摘要翻译： 一种Co基合金，包括0.03-0.10％C，不大于1.0％Si，不大于1.0％Mn，20-30％Cr，15-23％Ni，3-10％W，5- 10％Ta和0.05-0.7％Zr用作焊接材料。 燃气轮机喷嘴具有使用Co基合金的多层焊接修复的裂缝，并且用于发电的燃气轮机使用喷嘴。

公开(公告)号：US4967552A

公开(公告)日：1990-11-06

申请号：US229811

申请日：1988-08-08

申请人： Kazuhiko Kumata ,  Nobuyuki Iizuka ,  Masashi Kunihiro ,  Soichi Kurosawa

发明人： Kazuhiko Kumata ,  Nobuyuki Iizuka ,  Masashi Kunihiro ,  Soichi Kurosawa

IPC分类号： F02C7/18 ,  F01D5/08 ,  F01D11/24 ,  F01D19/02

CPC分类号： F01D11/24 ,  F01D19/02 ,  F01D5/08

摘要： A method and apparatus for controlling a temperature of a turbine casing and a turbine rotor in a gas turbine, which method and apparatus enables a maintaining of an optimum gap at a tip end of the rotor blades of the gas turbine over an entire operating range by independently controlling the amounts of heat energy supplied to a space of the turbine casing and the turbine rotor.

摘要翻译： 一种用于控制燃气轮机中的涡轮机壳体和涡轮机转子的温度的方法和装置，该方法和装置能够在整个工作范围内在整个工作范围内维持燃气轮机的转子叶片的末端处的最佳间隙， 独立地控制供应到涡轮机壳体和涡轮机转子的空间的热能的量。

公开(公告)号：US5259182A

公开(公告)日：1993-11-09

申请号：US17174

申请日：1993-02-12

申请人： Kazumi Iwai ,  Hiromi Koizumi ,  Kazuhiko Kumata ,  Yoshikazu Moritomo

发明人： Kazumi Iwai ,  Hiromi Koizumi ,  Kazuhiko Kumata ,  Yoshikazu Moritomo

IPC分类号： F23R3/08 ,  F23R3/14 ,  F23R3/06

CPC分类号： F23R3/14 ,  F23R3/08 ,  F23R2900/00002

摘要： A combustion apparatus comprises a combustor liner forming a combustion chamber, and a swirler for introducing a fuel gas into the combustion chamber in the form of a swirl. The combustor liner has an air film forming device provided on the wall thereof and capable of forming a film of cooling air on the inner peripheral wall of the combustor liner so as to protect the combustor liner from the hot combustion gas in the combustion chamber. The air film forming means is formed such that the flowing direction of the air forming the film becomes the same direction as the swirling direction of the combustion gas, so that the film of the cooling air is not broken by the hot combustion gas.

摘要翻译： 燃烧装置包括形成燃烧室的燃烧器衬套和用于以涡流形式将燃料气体引入燃烧室的旋流器。 燃烧器衬套具有设置在其壁上并能够在燃烧器衬套的内周壁上形成冷却空气膜的空气膜形成装置，以保护燃烧器衬套免受燃烧室内的热燃烧气体的影响。 空气膜形成装置形成为使得形成膜的空气的流动方向与燃烧气体的旋转方向成相同的方向，使得冷却空气的膜不被热燃烧气体破坏。

公开(公告)号：US4872312A

公开(公告)日：1989-10-10

申请号：US27730

申请日：1987-03-19

申请人： Nobuyuki Iizuka ,  Kazuhiko Kumata ,  Michio Kuroda

发明人： Nobuyuki Iizuka ,  Kazuhiko Kumata ,  Michio Kuroda

IPC分类号： F02C7/18 ,  F01D9/02 ,  F23R3/00 ,  F23R3/02 ,  F23R3/06 ,  F23R3/42

CPC分类号： F23R3/002 ,  F01D9/023 ,  F05D2260/201 ,  F23R2900/03044

摘要： A gas turbine cooling apparatus is disclosed in which a flow sleeve is provided to surround a combustor liner and a tail pipe substantially over their full length. A group of small holes for impinge-cooling an outer wall of the tail pipe are formed in a region of the flow sleeve close to a turbine. Further, opening portion for introducing cooling air are provided closer to the combustor liner than the small holes. Thus, the outer wall of the tail pipe and the wall of the combustor liner are cooled by the cooling air flowing between the tail pipe, the combustor liner and the flow sleeve.

摘要翻译： 公开了一种燃气轮机冷却装置，其中提供流动套筒以围绕燃烧器衬套和基本上在其全长上的尾管。 一组用于冲击冷却尾管外壁的小孔形成在靠近涡轮的流动套管的区域中。 此外，用于引入冷却空气的开口部分设置成比小孔更靠近燃烧器衬套。 因此，尾管的外壁和燃烧器衬套的壁由在尾管，燃烧器衬套和流动套筒之间流动的冷却空气来冷却。

公开(公告)号：US4767259A

公开(公告)日：1988-08-30

申请号：US888007

申请日：1986-07-22

申请人： Soichi Kurosawa ,  Kazuhiko Kumata

发明人： Soichi Kurosawa ,  Kazuhiko Kumata

IPC分类号： F02C7/14 ,  F01P7/02 ,  F02C7/18 ,  F02C9/18 ,  F04D29/58

CPC分类号： F02C7/185 ,  F01P7/026 ,  F05D2270/3013

摘要： Stator blades and rotor blades are cooled by discharge air discharged from an air compressor coupled directly with gas turbine. A signal of the compressor discharge pressure and a signal of turbine exhaust gas temperature are obtained, and cooling air flow is controlled based on these signals.

摘要翻译： 定子叶片和转子叶片由直接与燃气轮机连接的空气压缩机排出的排放空气冷却。 获得压缩机排出压力的信号和涡轮废气温度的信号，并且基于这些信号来控制冷却空气流。