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公开(公告)号：US5024055A
公开(公告)日：1991-06-18
申请号：US389746
申请日：1989-08-04
申请人： Isao Sato , Seiichi Kirikami , Akira Shimura , Fumiyuki Hirose , Hiroshi Inose , Haruo Urushidani , Osamu Arai
发明人： Isao Sato , Seiichi Kirikami , Akira Shimura , Fumiyuki Hirose , Hiroshi Inose , Haruo Urushidani , Osamu Arai
CPC分类号： F23N5/003 , F05D2270/0831 , F23N2041/20
摘要： A device for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes the combustors and a gas turbine driven by combustion gas from the combustors, comprises a plurality of sensors for measuring concentration of unburnt component in the combustion gas, which is disposed on the downstream side of the gas turbine, a unit for obtaining a distribution pattern of the measured concentration and for investigating the obtained distribution pattern to detect combustion conditions in the combustors.
摘要翻译： 一种用于检测包括燃烧器和由燃烧器的燃烧气体驱动的燃气轮机的燃气轮机装置中的多个燃烧器中的燃烧条件的装置，包括用于测量燃烧气体中未燃烧成分浓度的多个传感器， 设置在燃气轮机的下游侧，用于获得测量浓度的分布模式的单元，并用于调查所获得的分布模式以检测燃烧器中的燃烧条件。
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公开(公告)号：US5107673A
公开(公告)日：1992-04-28
申请号：US693612
申请日：1991-04-30
申请人： Isao Sato , Seiichi Kirikami , Akira Shimura , Fumiyuki Hirose , Hiroshi Inose , Haruo Urushidani , Osamu Arai
发明人： Isao Sato , Seiichi Kirikami , Akira Shimura , Fumiyuki Hirose , Hiroshi Inose , Haruo Urushidani , Osamu Arai
CPC分类号： F23N5/003 , F05D2270/0831 , F23N2041/20
摘要： A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes the combustors and a gas turbine driven by combustion gas from the combustors, comprises a step for measuring concentration of unburnt component in the combustion gas by means of a plurality of sensors disposed on the downstream side of the gas turbine, a step for obtaining a distribution pattern of the measured concentration, and a step for investigating the distribution pattern to detect combustion conditions in the combustors.
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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
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.
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4.发明授权Method and apparatus for controlling the supply of fuel to a gas turbine during load rejection 失效用于在卸载期间控制向燃气轮机供应燃料的方法和装置
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
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。
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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
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。
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公开(公告)号：US4907406A
公开(公告)日：1990-03-13
申请号：US209939
申请日：1988-06-22
申请人： Seiichi Kirikami , Isao Sato , Fumiyuki Hirose , Osamu Arai , Nobuyuki Iizuka
发明人： Seiichi Kirikami , Isao Sato , Fumiyuki Hirose , Osamu Arai , Nobuyuki Iizuka
CPC分类号： F01K23/10 , F04D27/0223 , F04D27/023 , Y02E20/16
摘要： A combined gas turbine plant comprises an air compressor, a combustor including a combustion chamber, a gas turbine, a steam turbine, and an exhaust heat recovery device having a denitration device and arranged at a location through which an exhaust gas passage for leading exhaust gas from the gas turbine to the atmosphere extends. An air extraction pipe equipped with a valve is provided for extracting a part of the air from the air compressor to prevent surging of the air compressor during starting of the plant, and another air extraction pipe equipped with a valve is provided for extracting a part of the air from an air passage extending from the compressor to the combustion chamber to improve stability of a flame and combustibility in the combustion chamber during the plant starting. The extraction pipes extend to and hence lead the extracted air into a portion of the exhaust gas passage located downstream of the denitration device.
摘要翻译： 一种组合式燃气轮机设备包括空气压缩机，包括燃烧室，燃气轮机，蒸汽轮机和具有脱硝装置的排气热回收装置的燃烧器，并且设置在排气通道中， 从燃气轮机到大气延伸。 提供了一种配备有阀的抽气管，用于从空气压缩机中提取一部分空气，以防止在启动设备期间空气压缩机的浪涌，并且提供另一个装有阀的空气抽取管，用于提取一部分 来自空气通道的空气从压缩机延伸到燃烧室，以提高火焰的稳定性和在工厂起动期间在燃烧室中的可燃性。 提取管延伸到并因此将抽出的空气引入位于脱硝装置下游的排气通道的一部分。
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公开(公告)号：US4677822A
公开(公告)日：1987-07-07
申请号：US831855
申请日：1986-02-24
申请人： Nobuyuki Iizuka , Katsukuni Hisano , Katsuo Wada , Masashi Kunihiro , Fumiyuki Hirose , Yoji Ishibashi , Isao Sato , Osamu Arai , Hiroshi Inose , Osamu Sakuda
发明人： Nobuyuki Iizuka , Katsukuni Hisano , Katsuo Wada , Masashi Kunihiro , Fumiyuki Hirose , Yoji Ishibashi , Isao Sato , Osamu Arai , Hiroshi Inose , Osamu Sakuda
CPC分类号： F23R3/26
摘要： A gas turbine combustor having a head combustion chamber and a rear combustion chamber, with a plurality of air supply ports arranged in a circumferential wall of the rear combustion chamber, and a fuel nozzle. An outer cylinder forms a cylindrical air flow passage between the inner cylinder and the outer cylinder. A cylindrical control member is provided which is adapted to be movable in an axial direction for regulating an opening of the air supply ports. The control member is supported by a supporting means which is adapted to maintain a gap between the control member and the wall of the rear combustion chamber. The supporting member includes a flexible member for absorbing a deformation of the control member during the axial movement of the control member so that it is possible to prevent, if not avoid, mechanical wear on the control member and to reduce the No.sub.x concentration as well as obtain a highly reliable operation of the gas turbine combustor.
摘要翻译： 一种具有头燃烧室和后燃烧室的燃气轮机燃烧器，其具有布置在后燃烧室的周壁中的多个供气口和燃料喷嘴。 外筒在内筒和外筒之间形成圆柱形的气流通道。 提供一个圆柱形控制件，其适于在轴向方向上可移动以调节供气口的开口。 控制构件由适于在控制构件和后燃烧室的壁之间保持间隙的支撑装置支撑。 支撑构件包括用于在控制构件的轴向移动期间吸收控制构件的变形的柔性构件，使得可以防止（如果不避免）控制构件上的机械磨损并且降低Nox浓度以及 获得燃气轮机燃烧器的高度可靠的操作。
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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
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.
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公开(公告)号：US5016443A
公开(公告)日：1991-05-21
申请号：US404314
申请日：1989-09-07
申请人： Nobuo Shimizu , Michio Kuroda , Seiichi Kirikami , Isao Sato , Osamu Arai
发明人： Nobuo Shimizu , Michio Kuroda , Seiichi Kirikami , Isao Sato , Osamu Arai
摘要： A fuel-air premixing device of a gas turbine has a double-cylinder structure composed of an inner cylinder and an outer cylinder defining therebetween flow passages such that a fuel is supplied into air flowing through the passages so that a pre-mixture of the fuel and air is formed and discharged. The premixing device further has a plurality of radially spaced fuel nozzles capable of supplying the fuel into the passages, and fuel supply rate regulator valves for independently controlling the rates of supply of the fuel from the radially spaced nozzles.
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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
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。
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