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1. 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.

2. 发明授权

US5024055A Device for detecting combustion conditions in combustors 失效
标题翻译：用于检测燃烧器中燃烧条件的装置
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
IPC分类号： F02C9/00 , F23C99/00 , F23M11/04 , F23N5/00 , F23R3/00
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。

3. 发明授权

US5107673A Method for detecting combustion conditions in combustors 失效
标题翻译：检测燃烧器燃烧条件的方法
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
IPC分类号： F02C9/00 , F23C99/00 , F23M11/04 , F23N5/00 , F23R3/00
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.

4. 发明授权

US5272637A Method and apparatus for controlling the supply of fuel to a gas turbine during load rejection 失效
标题翻译：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
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。

5. 发明授权

US5281129A Combustion apparatus and control method therefor 失效
标题翻译：燃烧装置及其控制方法
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。

6. 发明授权

US5319919A Method for controlling gas turbine combustor 失效
标题翻译：燃气轮机燃烧器的控制方法
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。

7. 发明授权

US5584171A Gas turbine control method and apparatus 失效
标题翻译：燃气轮机控制方法及装置
公开(公告)号：US5584171A
公开(公告)日：1996-12-17
申请号：US365439
申请日：1994-12-28
申请人： Isao Sato , Fumiyuki Hirose , Minoru Takaba , Akira Shimura , Shoei Takahashi , Hiraku Ikeda
发明人： Isao Sato , Fumiyuki Hirose , Minoru Takaba , Akira Shimura , Shoei Takahashi , Hiraku Ikeda
IPC分类号： F02C9/50
CPC分类号： F02C9/50 , F05D2270/071
摘要： A gas turbine engine control method and apparatus as disclosed for optimizing fuel/air mixture, especially during decreasing load conditions. In a large capacity gas turbine engine system used for generation of electric power, the system is designed to operate at a relatively constant rotational speed of the turbine which drives an electric generator unit. The load of the turbine engine varies throughout the day due to changes in electrical power demands. During normal rated load conditions, the control of the fuel/air mixture is by way of changes in fuel supply, corrected to return the turbine exhaust temperature to a desired rated temperature. During this mode of operation, the compressor inlet guide vanes are maintained in a substantially constant open position. For accommodating decreasing load conditions where the temperature drops below a predetermined temperature level below the rated temperature operation, the system is switched to an inlet guide vane control mode of operation. During the guide vane control mode of operation, the inlet guide vanes are controlled at a more precise temperature correction sensitivity than is the case for normal load operations. This more precise inlet guide vane control during decreasing load conditions assures improved fuel/air mixture during decreasing load and consequent improved efficiency and minimal NO.sub.x compound emissions, especially during changing ambient temperature conditions where cold air would otherwise increase the air supply.
摘要翻译：公开的用于优化燃料/空气混合物的燃气涡轮发动机控制方法和装置，特别是在减小负载条件下。在用于产生电力的大容量燃气涡轮发动机系统中，该系统设计成以驱动发电机单元的涡轮机的相对恒定的转速运行。由于电力需求的变化，涡轮发动机的负载在一整天内变化。在正常的额定负载条件下，燃料/空气混合物的控制是通过燃料供应的变化来进行的，这被校正以将涡轮排气温度恢复到所需的额定温度。在这种操作模式下，压缩机入口导叶保持在基本恒定的打开位置。为了适应温度下降到低于额定温度运行的预定温度水平的降低负载条件，系统被切换到入口导叶控制操作模式。在导叶控制操作模式下，入口导流叶片的控制精度比正常加载操作更为精确。在降低负载条件下，这种更为精确的入口引导叶片控制确保了在减少负载的同时改善了燃料/空气混合物，从而提高了效率和最小化的NOx化合物排放，特别是在其他空气会增加空气供给的环境温度变化的环境中。

8. 发明授权

US5878566A Gas turbine and a gas turbine control method 失效
标题翻译：燃气轮机和燃气轮机控制方法
公开(公告)号：US5878566A
公开(公告)日：1999-03-09
申请号：US976362
申请日：1997-10-21
申请人： Tomoyoshi Endo , Fumiyuki Hirose , Akira Shimura , Takumi Yamanobe , Isao Sato , Hiraku Ikeda
发明人： Tomoyoshi Endo , Fumiyuki Hirose , Akira Shimura , Takumi Yamanobe , Isao Sato , Hiraku Ikeda
IPC分类号： F02C9/00 , F23N5/00 , F23R3/30 , F23R3/34 , F23R3/46 , F02C9/28
CPC分类号： F23N5/003 , F23R3/34 , F05D2270/083 , F05D2270/0831 , F23N2025/10 , F23N2041/20
摘要： A control method of a gas turbine which is provided with a multi can type combustor consisting of a plurality of unit combustors, each of which has a first stage combustion section for diffusion combustion and a second stage combustion section for premix combustion. Combustion states in the first and second stage combustion sections are monitored to take in quantities representative of the combustion conditions as control factors. The combustion in the second stage combustion section is assumed to be abnormal when the taken in quantities exceed an allowable limit and the combustion in the first and second stage combustion sections is changed to independent combustion only in the first stage combustion section when the number of unit combustors, each of which is assumed to be abnormal, exceeds a predetermined number of the unit combustors.
摘要翻译：一种燃气轮机的控制方法，其具备由多台单元燃烧器构成的多罐式燃烧器，所述多台式燃烧器具有扩散燃烧用的第一级燃烧部和预混燃烧用的第二级燃烧部。监测第一和第二阶段燃烧段中的燃烧状态以代表燃烧条件的数量作为控制因素。当第二级燃烧部分的燃烧次数超过允许极限时，第二级燃烧部分中的燃烧被认为是异常的，并且当第一级燃烧部分中的燃烧单元数量单位每个被认为是异常的燃烧器超过预定数量的单元燃烧器。

9. 发明授权

US5327718A Gas turbine apparatus and method of control thereof 失效
标题翻译：燃气轮机装置及其控制方法
公开(公告)号：US5327718A
公开(公告)日：1994-07-12
申请号：US933317
申请日：1992-08-21
申请人： Naohiko Iwata , Yasuhiko Otawara , Akira Shimura , Nobuyuki Iizuka , Isao Sato , Fumiyuki Hirose , Minoru Takaba , Yasutaka Komatsu , Hiraku Ikeda , Takeshi Iwamiya , Takeshi Ishida
发明人： Naohiko Iwata , Yasuhiko Otawara , Akira Shimura , Nobuyuki Iizuka , Isao Sato , Fumiyuki Hirose , Minoru Takaba , Yasutaka Komatsu , Hiraku Ikeda , Takeshi Iwamiya , Takeshi Ishida
IPC分类号： F02C9/16 , F02C7/228 , F02C9/00 , F02C9/28 , F23C99/00 , F23R3/12 , F23R3/26 , F23R3/28
CPC分类号： F23R3/12 , F02C7/228 , F02C9/28 , F23R3/26
摘要： A gas turbine apparatus has a gas turbine and a plurality of burners for providing combustion gas to drive the turbine. A flow control means of each burner for fuel or combustion air is adjusted by control means to control each said burner individually in dependence on a predetermined combustion characteristic of the respective burner. Sensed quantities relating to the combustion performance of the burners are input to the control means which adjusts the flow control means of each burner in dependence on the sensed quantities and the predetermined combustion characteristic of the respective burner.
摘要翻译：燃气轮机装置具有燃气轮机和用于提供燃烧气体以驱动涡轮机的多个燃烧器。用于燃料或燃烧空气的每个燃烧器的流量控制装置通过控制装置进行调节，以根据相应燃烧器的预定燃烧特性分别控制每个所述燃烧器。与燃烧器的燃烧性能相关的感测量被输入到根据感测量和各个燃烧器的预定燃烧特性来调节每个燃烧器的流量控制装置的控制装置。

10. 发明授权

US5926203A Image recording method and apparatus using multiple laser beams 失效
标题翻译：使用多个激光束的图像记录方法和装置
公开(公告)号：US5926203A
公开(公告)日：1999-07-20
申请号：US751732
申请日：1996-11-18
申请人： Akira Shimura , Shuichi Yamazaki , Tomohiro Nakajima , Masaki Narita
发明人： Akira Shimura , Shuichi Yamazaki , Tomohiro Nakajima , Masaki Narita
IPC分类号： B41J2/44 , B41J2/47 , G03G21/00 , G03G21/14 , G06K15/12 , H04N1/113 , B41J2/45 , B41J2/435
CPC分类号： G06K15/1261 , B41J2/473
摘要： A method and apparatus that prevent degradation of an image quality due to a change of a beam pitch in a subscanning direction of each optical beam on a record medium. At a given time, for example, when power is first turned on, a CPU detects a beam pitch on a record medium, e.g., a photosensitive drum, by using a CCD line image sensor. If the detected value differs from a value set according to a currently-selected scanning density, an LD arrangement change motor is rotated via a motor driver so that the beam pitch matches the set value so as to change an arrangement of laser diodes in a laser diode array. Control over the beam pitch occurs for a variety of conditions including control at regular intervals, power-on events, or when a scanning density specification signal indicates a different beam pitch than the detected beam pitch. Similarly, adjustment over the beam pitch is not typically made during a copying operation.
摘要翻译：一种防止由于每个光束在记录介质上的副扫描方向上的光束间距变化引起的图像质量劣化的方法和装置。在给定的时间，例如，当电源首次打开时，CPU通过使用CCD线图像传感器来检测诸如感光鼓的记录介质上的光束间距。如果检测值与根据当前选择的扫描浓度设定的值不同，则通过马达驱动器旋转LD布置改变马达，使得波束间距与设定值匹配，以便改变激光器中的激光二极管的布置二极管阵列。波束间距的控制发生在各种条件下，包括规则间隔的控制，上电事件，或当扫描浓度指示信号表示与检测的光束间距不同的光束间距时。类似地，在复印操作期间通常不会对光束间距进行调整。

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