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1. 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。

2. 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。

3. 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。

4. 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.

5. 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。

6. 发明授权

US4228359A Rotor-stress preestimating turbine control system 失效
标题翻译：转子应力预估涡轮机控制系统
公开(公告)号：US4228359A
公开(公告)日：1980-10-14
申请号：US929130
申请日：1978-07-28
申请人： Hiroshi Matsumoto , Yoshio Sato , Shigeyoshi Kawano , Yoshiyuki Nakano , Fumio Kato , Katsukuni Hisano , Katsuto Kashiwahara , Yasuhiko Otawara , Toshihiko Higashi , Yasuhiro Tennichi , Jube Matsumura , Koichiro Fukushima
发明人： Hiroshi Matsumoto , Yoshio Sato , Shigeyoshi Kawano , Yoshiyuki Nakano , Fumio Kato , Katsukuni Hisano , Katsuto Kashiwahara , Yasuhiko Otawara , Toshihiko Higashi , Yasuhiro Tennichi , Jube Matsumura , Koichiro Fukushima
IPC分类号： F01D19/02 , F01K7/16
CPC分类号： F01K7/165 , F01D19/02
摘要： The present stress in the turbine rotor is estimated at each control period, from the steam temperature and pressure at the turbine inlet. In addition, the future turbine inlet steam temperature or pressure is preestimated once every n.sub.T control cycles, for a given speed or load changing rate, making use of data concerning the changing rate of the turbine steam inlet temperature or pressure in relation with the change of the speed or load, which has been obtained by a learning of the past turbine operating condition. This future steam temperature or pressure at the turbine inlet is used as a factor for preestimating the future stress expected to be caused in the turbine rotor. The preestimation of the rotor stress is performed for a plurality of assumed speed or load changing rates. The turbine is controlled at the maximum speed increase-rate or load changing rate which would not cause the future stress preestimated over a given preestimation time to exceed a limit stress. An observation of the present stress is made at each control period to check whether the limit stress is not exceeded by the present stress.
摘要翻译：根据涡轮机入口处的蒸汽温度和压力，在每个控制周期估计涡轮转子中的当前应力。另外，对于给定的速度或负荷变化率，在每个nT控制循环中预先设想未来的涡轮进口蒸汽温度或压力一次，利用关于涡轮机进气温度或压力变化率的数据与通过学习过去的涡轮机操作条件而获得的速度或负载。涡轮机入口处的未来蒸汽温度或压力被用作预先估计在涡轮转子中引起的未来应力的因素。对于多个假想速度或负载变化率来执行转子应力的预测。涡轮机以最大速度增加速率或负载变化率进行控制，这不会导致在给定预测时间内预测的未来应力超过极限应力。在每个控制周期进行当前应力的观察，以检查当前应力是否超过极限应力。

7. 发明授权

US5127229A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US5127229A
公开(公告)日：1992-07-07
申请号：US728729
申请日：1991-07-11
申请人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
发明人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
IPC分类号： F02C7/22 , F02C7/26 , F23C99/00 , F23R3/34
CPC分类号： F23R3/34
摘要： A gas turbine combustor including a first-stage combustion chamber being arranged to serve as a premix chamber for a second-stage combustion chamber and an auxiliary burner provided in the first-stage combustion chamber and arranged to effect, when fired, combustion and holding of a flame in the first-stage combustion chamber and to effect, when extinguished, feed a flame from the first-stage combustion chamber to the second-stage combustion chamber.
摘要翻译：一种燃气轮机燃烧器，其包括第一级燃烧室，其被设置为用作第二级燃烧室的预混合室和设置在第一级燃烧室中的辅助燃烧室，并且被布置成在燃烧时燃烧和保持第一级燃烧室中的火焰并且当熄灭时，将火焰从第一级燃烧室供给到第二级燃烧室。

8. 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.

9. 发明授权

US4245950A Turbine rotorconstructions 失效
标题翻译：涡轮转子结构
公开(公告)号：US4245950A
公开(公告)日：1981-01-20
申请号：US879737
申请日：1978-02-21
申请人： Koki Shiohata , Masaharu Ohno , Fumio Fujisawa , Kazuo Sato , Sho Kusumoto , Katsukuni Hisano
发明人： Koki Shiohata , Masaharu Ohno , Fumio Fujisawa , Kazuo Sato , Sho Kusumoto , Katsukuni Hisano
IPC分类号： F01D5/06 , F01D3/02 , F01D5/02 , F01C3/02
CPC分类号： F01D3/02 , F01D5/025 , Y10T403/7021
摘要： Steam introduced into a turbine casing from a steam inlet is longitudinally divided and each divided steam portion flows in respective first stages which are disposed on the shaft adjacent to each other. The shaft and a plurality of disks which are manufactured independently are made integral by a thermal shrink. In order to reduce the thermal distortion effects on the shaft caused by keys interconnecting the disks and shaft, first key grooves formed on an outer surface of the shaft and an inner surface of the disks of one first stage and a first key closely disposed in the first key grooves are arranged in symmetry with respect to the center of the shaft, to second key grooves formed on an inner surface of the disk of the other first stage with a second key closely disposed in the second grooves. Other preferred embodiments include dummy grooves and keys to balance the thermal distortion effects of the keys interconnecting the disks and shaft.
摘要翻译：从蒸汽入口引入涡轮机壳体的蒸汽被纵向地分开，并且每个分开的蒸汽部分流动在彼此相邻设置在轴上的相应的第一级中。独立制造的轴和多个盘通过热收缩而成为一体。为了减少由连接盘和轴的键引起的对轴的热变形影响，形成在轴的外表面上的第一键槽和一个第一级的盘的内表面和紧密地设置在该第一键的第一键第一键槽相对于轴的中心对称地布置成形成在另一个第一平台的盘的内表面上的第二键槽，具有紧密地布置在第二凹槽中的第二键。其他优选实施例包括虚拟凹槽和键，以平衡互连盘和轴的键的热变形效应。

10. 发明授权

US5054280A Gas turbine combustor and method of running the same 失效
标题翻译：燃气轮机燃烧器及其运行方法
公开(公告)号：US5054280A
公开(公告)日：1991-10-08
申请号：US582395
申请日：1990-09-12
申请人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
发明人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
IPC分类号： F02C7/22 , F02C7/26 , F23C99/00 , F23R3/34
CPC分类号： F23R3/34
摘要： A gas turbine combustor including a first-stage combustion chamber being arranged to serve as a premix chamber for a second-stage combustion chamber and an auxiliary burner provided in the first-stage combustion chamber and arranged to effect, when fired, combustion and holding of a flame in the first-stage combustion chamber and to effect, when extinguished, feed a flame from the first-stage combustion chamber to the second-stage combustion chamber; and a method of driving the gas turbine combustor including a step of preparing the auxiliary burner in the first stage combustion chamber, the auxiliary burner being sparked when said combustion is fired, and causing the first-stage combustion camber to serve as the premixing chamber for the second-stage combustion chamber by extinguished the auxiliary burner.
摘要翻译：一种燃气轮机燃烧器，其包括第一级燃烧室，其被设置为用作第二级燃烧室的预混合室和设置在第一级燃烧室中的辅助燃烧室，并且被布置成在燃烧时燃烧和保持第一级燃烧室中的火焰，并且当熄灭时，将火焰从第一级燃烧室供给到第二级燃烧室; 以及驱动所述燃气轮机燃烧器的方法，其包括在所述第一级燃烧室中准备所述辅助燃烧器的步骤，所述辅助燃烧器在所述燃烧被点火时被点火，并且使所述第一级燃烧室用作所述预混合室，第二级燃烧室通过熄灭辅助燃烧器。

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