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1. 发明授权

US4829764A Combustion air flow rate adjusting device for gas turbine combustor 失效
标题翻译：燃气轮机燃烧器燃烧空气流量调节装置
公开(公告)号：US4829764A
公开(公告)日：1989-05-16
申请号：US110426
申请日：1987-10-20
申请人： Nobuyuki Iizuka , Katsukuni Hisano , Katsuo Wada , Fumiyuki Hirose , Osamu Arai
发明人： Nobuyuki Iizuka , Katsukuni Hisano , Katsuo Wada , Fumiyuki Hirose , Osamu Arai
IPC分类号： F23R3/26
CPC分类号： F23R3/26 , Y10T74/18968
摘要： In a combustion air flow rate adjusting device in which a cylindrical regulating ring fitted about an outer peripheral surface of an inner cylinder of a gas turbine combustor is translated along the outer peripheral surface of the inner cylinder in order to vary an opening area of air intake ports formed in the peripheral wall of the inner cylinder, an arcuately moving part at a forward end of a lever fixedly connected to a forward end of a shaft extending inwardly through a peripheral wall of an outer cylinder of the gas turbine combustor is connected to a part reciprocating together with the regulating ring, by leaf springs.

2. 发明授权

US4677822A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
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
IPC分类号： F02C9/16 , F23R3/26 , F02C3/14
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。

3. 发明授权

US4766721A Combustor for gas turbine 失效
标题翻译：燃气轮机燃烧器
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。

4. 发明授权

US4683715A Method of starting gas turbine plant 失效
标题翻译：启动燃气轮机厂的方法
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。

5. 发明授权

US3973404A Low pressure turbine installation 失效
标题翻译：低压涡轮机安装
公开(公告)号：US3973404A
公开(公告)日：1976-08-10
申请号：US542820
申请日：1975-01-21
申请人： Nobuyuki Iizuka , Katsukuni Hisano , Satoshi Ninomiya , Yasuhiko Otawara
发明人： Nobuyuki Iizuka , Katsukuni Hisano , Satoshi Ninomiya , Yasuhiko Otawara
IPC分类号： F01D3/02 , F01D25/24 , F01D25/30 , F01K7/38 , F01K11/02
CPC分类号： F01K7/38 , F01D3/02 , F01K11/02
摘要： Low pressure turbine installation comprising a casing, at least two groups of turbine stages mounted in said casing, each turbine stage having blades so arranged that a flow of steam passes through the respective turbine stages in contraflow manner, partition means in said casing for separating the opposed final stages of said turbine stages from each other, and steam exhausting means opened in the side walls of said casing in a direction substantially perpendicular to the axis of said turbine, said steam exhausting means being connected to condensers.
摘要翻译：低压涡轮机设备包括壳体，安装在所述壳体中的至少两组涡轮级，每个涡轮级具有如下布置的叶片，使得蒸汽流以反向方式通过相应的涡轮级，所述壳体中的分隔装置用于将所述涡轮级的相对最后阶段彼此相反，并且蒸汽排出装置在基本上垂直于所述涡轮机的轴线的方向上在所述壳体的侧壁中敞开，所述蒸汽排出装置连接到冷凝器。

6. 发明授权

US5121597A Gas turbine combustor and methodd of operating the same 失效
标题翻译：燃气轮机及其运行方法
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.

7. 发明授权

US5069029A Gas turbine combustor and combustion method therefor 失效
标题翻译：燃气轮机燃烧器及其燃烧方法
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.

8. 发明授权

US4662820A Turbine stage structure 失效
标题翻译：涡轮舞台结构
公开(公告)号：US4662820A
公开(公告)日：1987-05-05
申请号：US752860
申请日：1985-07-08
申请人： Tetsuo Sasada , Takeshi Sato , Haruo Urushidani , Katsukuni Hisano , Ryoichi Kaneko , Kazuo Ikeuchi , Kunio Tsuji
发明人： Tetsuo Sasada , Takeshi Sato , Haruo Urushidani , Katsukuni Hisano , Ryoichi Kaneko , Kazuo Ikeuchi , Kunio Tsuji
IPC分类号： F01D9/02 , F01D11/08 , F01D11/02
CPC分类号： F04D29/161 , F01D11/08
摘要： A stage structure of an axial turbine includes a stationary inner ring, a stationary outer wall, a row of stationary blades mounted on the stationary inner ring and outer wall, a row of moving blades, and a shroud ring mounted on the tips of the moving blades. An annular solid substance, disposed immediately downstream of an axial gap formed between an axial end of the shroud ring and surface of the outer wall axially facing the axial end of the shroud ring, reduces an expansion space provided immediately downstream of the axial gap, whereby circulation of an ejection flow from a main stream through the axial gap is reduced so that the turbine stage efficiency is improved. The annular solid substance may be a ring fixed to the stationary outer wall, a protrusion or a cylinder formed by a portion of the outer wall.
摘要翻译：轴流式涡轮机的级结构包括固定内环，固定外壁，安装在固定内环和外壁上的一排固定叶片，一排活动叶片和安装在移动的尖端上的护罩环刀片。设置在形成在护罩环的轴向端部和轴向面向护罩环的轴向端部的外壁的表面之间的轴向间隙的紧邻下游的环形固体物质减小了紧邻轴向间隙的下游的膨胀空间，由此从主流通过轴向间隙的喷射流的循环减少，从而提高了涡轮级的效率。环状固体物质可以是固定在静止的外壁上的环，由外壁的一部分形成的突起或圆筒。

9. 发明授权

US4478082A Method and apparatus for detecting rubbing in a rotary machine 失效
标题翻译：用于检测旋转机器中的摩擦的方法和装置
公开(公告)号：US4478082A
公开(公告)日：1984-10-23
申请号：US408949
申请日：1982-08-17
申请人： Ichiya Sato , Takao Yoneyama , Tsuguaki Koga , Kazuo Ikeuchi , Katsukuni Hisano
发明人： Ichiya Sato , Takao Yoneyama , Tsuguaki Koga , Kazuo Ikeuchi , Katsukuni Hisano
IPC分类号： G01M13/04 , G01H1/00 , G01H1/04 , G01H17/00 , G01M99/00 , G01N29/12 , G01M13/00
CPC分类号： G01N29/12 , G01H1/003 , G01N2291/014 , G01N2291/101 , G01N2291/2693
摘要： A method and apparatus for detecting the occurrence of rubbing in a rotary machine, in which at least one acoustic sensor is mounted on at least the rotor part or the stator part of the rotary machine, and the output signal from the acoustic sensor is detected and then filtered to extract a frequency component having a frequency substantially equal to the rotational frequency of the rotary machine, so as to detect the occurrence of rubbing in the rotary machine as early as possible and also to locate the source of the rubbing. Even when the occurrence of abnormal metal-to-metal contact at a bearing of the rotary machine is detected, it is discriminated from rubbing so that the occurrence of the rubbing can be reliably detected.
摘要翻译：一种在旋转机器中检测摩擦发生的方法和装置，其中至少一个声传感器安装在至少旋转机器的转子部分或定子部分上，并且检测来自声传感器的输出信号，然后过滤以提取频率基本上等于旋转机的旋转频率的频率分量，以便尽可能早地检测旋转机器中的摩擦的发生并且还可以定位摩擦源。即使检测到在旋转机械的轴承处发生异常金属对金属的接触，也可以将其与摩擦进行区别，从而能够可靠地检测摩擦的发生。

10. 发明授权

US4187685A Method and system for effecting control governing of a steam turbine 失效
标题翻译：实现蒸汽轮机控制控制的方法和系统
公开(公告)号：US4187685A
公开(公告)日：1980-02-12
申请号：US876944
申请日：1978-02-10
申请人： Kunio Tsuji , Katsukuni Hisano , Akira Sakai , Shozo Nakamura
发明人： Kunio Tsuji , Katsukuni Hisano , Akira Sakai , Shozo Nakamura
IPC分类号： F01D17/24 , F01K13/02
CPC分类号： F01K13/02
摘要： A method and system for effecting control governing of a steam turbine wherein the steam chamber of a first stage nozzle is divided into a plurality of steam compartments, control valves each connected to one of the steam compartments are individually operated for controlling the flow rate of steam introduced into the turbine, and the governing of the nozzle is effected by adjusting the flow rate of steam in accordance with a load. At low load, the degree of opening of the control valves is kept constant and the turbine is driven by steam of a reduced pressure by reducing the pressure of the steam at the inlet of the turbine so as to maintain, in a low load region, the volume flow rate of steam for a high load region. To cope with a change in the value of the load, the degree of opening corresponding to a predetermined change in the value of the load is set beforehand for each control valve. When the change in the value of the load is smaller than the predetermined change in the value of the load, the degree of opening of the control valve involved is adjusted. Conversely, when the change in the value of the load is greater than the predetermined change in the value of the load, the pressure of the steam at the inlet of the turbine is controlled.
摘要翻译：一种用于实现蒸汽轮机的控制控制的方法和系统，其中第一级喷嘴的蒸汽室被分成多个蒸汽隔间，各自连接到一个蒸汽隔间的控制阀被单独操作以控制蒸汽的流量引入涡轮机，并且通过根据负载调节蒸汽的流量来实现喷嘴的调节。在低负载下，控制阀的开度保持恒定，并且通过减小涡轮入口处的蒸汽的压力使涡轮由减压蒸汽驱动，以便在低负荷区域中保持，高负荷区域的蒸汽体积流量。为了应对负载值的变化，对于每个控制阀，预先设定对应于负载值的预定变化的开度。当负载值的变化小于负载值的预定变化时，调节所涉及的控制阀的开度。相反，当负载值的变化大于负载值的预定变化时，控制涡轮入口处的蒸汽的压力。

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