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1. 发明授权

US5323614A Combustor for gas turbine 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US5323614A
公开(公告)日：1994-06-28
申请号：US3608
申请日：1993-01-13
申请人： Satoshi Tsukahara , Hiroshi Inoue , Noriyuki Hayashi , Kazumi Iwai , Tamio Innami , Yoji Ishibashi , Michio Kuroda , Yasuhiko Otawara , Hiraku Ikeda , Kazuyuki Itoh , Shozo Nakamura , Hidekazu Fujimura , Kazuhito Koyama
发明人： Satoshi Tsukahara , Hiroshi Inoue , Noriyuki Hayashi , Kazumi Iwai , Tamio Innami , Yoji Ishibashi , Michio Kuroda , Yasuhiko Otawara , Hiraku Ikeda , Kazuyuki Itoh , Shozo Nakamura , Hidekazu Fujimura , Kazuhito Koyama
IPC分类号： F02C9/28 , F23R3/28 , F23R3/34 , F02C1/00
CPC分类号： F23R3/286 , F23R3/34
摘要： A premixed combustor for a gas turbine, comprises, a combustion chamber for burning a fuel with an air therein, at least two premixed fuel/air mixture outlets which are juxtaposed with each other, and through each of which a premixed fuel/air mixture flows out into the combustion chamber, and a flow deflection member arranged between the premixed fuel/air mixture outlets, urging the permixed fuel/air mixture from one of the premixed fuel/air mixture outlets to go away from another one of the premixed fuel/air mixture outlets, and terminating in the combustion chamber so that the premixed fuel/air mixture from the one of the premixed fuel/air mixture outlets is permitted to move toward the premixed fuel/air mixture flowing out from the another one of the premixed fuel/air mixture outlets after going away from the another one of the premixed fuel/air mixture outlets.
摘要翻译：一种用于燃气轮机的预混合燃烧器包括：用于燃烧燃料的燃烧室，其中具有空气的至少两个预混合燃料/空气混合物出口彼此并置，并且通过其中预混燃料/空气混合物流动并且设置在预混燃料/空气混合物出口之间的流动偏转构件，从预混合的燃料/空气混合物出口之一推动经过混合的燃料/空气混合物以远离另一种预混燃料/空气混合物出口，并且终止于燃烧室，使得来自预混燃料/空气混合物出口之一的预混合燃料/空气混合物被允许朝向从另一个预混燃料/空气混合物出口流出的预混燃料/空气混合物移动，在离开另一个预混合燃料/空气混合物出口之后的空气混合物出口。

2. 发明授权

US4275563A Power-generating plant having increased circulating force of working fluid 失效
标题翻译：发电厂具有增加工作流体的循环力
公开(公告)号：US4275563A
公开(公告)日：1981-06-30
申请号：US4577
申请日：1979-01-18
申请人： Michio Kuroda , Shozo Nakamura , Satoshi Tsukahara , Yasuaki Akatu , Shigehisa Sugita , Kojiro Kaneko , Seiichiro Sakaguchi , Ryoichiro Oshima
发明人： Michio Kuroda , Shozo Nakamura , Satoshi Tsukahara , Yasuaki Akatu , Shigehisa Sugita , Kojiro Kaneko , Seiichiro Sakaguchi , Ryoichiro Oshima
IPC分类号： F28C3/08 , F01K25/08 , F22B3/02 , F01K25/06
CPC分类号： F01K25/08 , F22B3/02
摘要： A power generating plant which includes a direct contact-type heat exchanger. A low-boiling point medium such as freon and a heat-source medium such as heated oil, are injected from a lower portion of the heat exchanger so that the two media are brought into direct contact with each other thereby vaporizing the gaseous low-boiling point medium. The low-boiling medium acts as a working fluid while it circulates through a closed cycle of the plant which includes a turbine and a condenser. The heat-source medium, circulates in a closed cycle of the plant which includes a heating unit.
摘要翻译：一种包括直接接触式热交换器的发电厂。从热交换器的下部注入诸如氟利昂和热源介质如加热油的低沸点介质，使得两个介质彼此直接接触，从而汽化气态低沸点点媒体。低沸点介质充当工作流体，同时循环通过包括涡轮机和冷凝器的设备的封闭循环。热源介质在包括加热单元的设备的封闭循环中循环。

3. 发明授权

US5461855A Method and device for controlling combustors for gasturbine 失效
标题翻译：用于控制燃气燃烧器的方法和装置
公开(公告)号：US5461855A
公开(公告)日：1995-10-31
申请号：US193354
申请日：1994-02-03
申请人： Hiroshi Inoue , Satoshi Tsukahara , Kazumi Iwai
发明人： Hiroshi Inoue , Satoshi Tsukahara , Kazumi Iwai
IPC分类号： F02C9/00 , F01D17/08 , F23R3/26 , F23C1/00
CPC分类号： F01D17/085 , F23R3/26
摘要： A method for controlling a plurality of combustors supplying a pressurized gas to a gas turbine, with each of the combustors including a first air supply for supplying a combustion air into the combustor and a second air supply for adjusting an amount of air supplied into the combustor to change a combustion condition in the combustor. The method comprises the steps of measuring the combustion condition of each of the combustors, measuring a difference between the measured combustion condition of each of the combustors and a desired combustion condition, and changing a rate of the amount of air supplied into the combustor by the second air supply means in relation to an amount of combustion air supplied into the combustor by the first air supply in each of the combustors according to the measured difference of each of the combustors to change the combustion condition of each of the combustors so that the combustion conditions of the combustors are changed to the desired combustion condition.
摘要翻译：一种用于控制向燃气轮机供应加压气体的多个燃烧器的方法，其中每个燃烧器包括用于向燃烧器供应燃烧空气的第一空气供应器和用于调节供应到燃烧器中的空气量的第二空气供应器以改变燃烧器中的燃烧状态。该方法包括以下步骤：测量每个燃烧器的燃烧条件，测量每个燃烧器的测量的燃烧条件与期望的燃烧条件之间的差异，以及改变供应到燃烧器中的空气的量的速率第二空气供给装置相对于通过每个燃烧器中的第一空气供应供应到燃烧器中的燃烧空气的量，根据每个燃烧器的测量差异来改变每个燃烧器的燃烧条件，使得燃烧燃烧器的条件改变为期望的燃烧条件。

4. 发明授权

US5836164A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US5836164A
公开(公告)日：1998-11-17
申请号：US593087
申请日：1996-01-29
申请人： Satoshi Tsukahara , Shohei Yoshida , Masahiko Yamagishi , Kazumi Iwai , Hiromi Koizumi , Yoichi Yoshinaga
发明人： Satoshi Tsukahara , Shohei Yoshida , Masahiko Yamagishi , Kazumi Iwai , Hiromi Koizumi , Yoichi Yoshinaga
IPC分类号： F23C6/04 , F23R3/28 , F23R3/34 , F02C1/00
CPC分类号： F23R3/286 , F23C6/047 , F23R3/34 , F23R3/346 , F23D2900/00008
摘要： A gas turbine combustor includes a diffusion combustor arranged at an axis portion of a combustion chamber for effecting diffusion combustion, a plurality of first premixing combustors arranged at an outer periphery of the diffusion combustor for effecting premixed combustion, each of the plurality of first premixing combustors being formed so that a mixture outlet end thereof projects more downstream than a fuel outlet end of the diffusion combustor, and a plurality of second premixing combustors each formed so that a mixture outlet thereof projects more downstream than the mixture outlet end of the first combustor, wherein the first premixing combustors and the second premixing combustors are arranged alternately at the outer periphery of the diffusion combustor, and wherein a swirler is provided on the first premixing combustor in the vicinity of the mixture outlet end thereof for swirling mixture.
摘要翻译：燃气轮机燃烧器包括布置在燃烧室的轴线部分以进行扩散燃烧的扩散燃烧器，多个第一预混合燃烧器，其布置在扩散燃烧室的外周处以实现预混合燃烧;多个第一预混合燃烧器形成为使得其混合物出口端比扩散燃烧器的燃料出口端更下游突出，并且多个第二预混合燃烧器各自形成为使得其混合物出口比第一燃烧器的混合物出口端更下游突出，其中所述第一预混合燃烧器和所述第二预混合燃烧器交替地布置在所述扩散燃烧器的外周，并且其中在所述第一预混合燃烧器的混合物出口端附近设置旋流器以进行旋转混合。

5. 发明授权

US5328355A Combustor and combustion apparatus 失效
标题翻译：燃烧器和燃烧装置
公开(公告)号：US5328355A
公开(公告)日：1994-07-12
申请号：US765835
申请日：1991-09-26
申请人： Hironobu Kobayashi , Shigeru Azuhata , Masayuki Taniguchi , Tadayoshi Murakami , Kiyoshi Narato , Michio Kuroda , Satoshi Tsukahara
发明人： Hironobu Kobayashi , Shigeru Azuhata , Masayuki Taniguchi , Tadayoshi Murakami , Kiyoshi Narato , Michio Kuroda , Satoshi Tsukahara
IPC分类号： C08F259/04 , C08F259/00 , F23C7/02 , F23C9/00 , F23D11/10 , F23D23/00 , F23K5/20 , F23R3/16 , F23D11/40 , F23D11/44
CPC分类号： F23K5/20 , F23C7/02 , F23C9/006 , F23D11/107 , F23D23/00 , F23R3/16 , F23D2900/11101
摘要： In a combustor including a premixing type combustion burner which has an atomizer for ejecting a liquid fuel together with combustion air to atomize the liquid fuel, the atomizer is comprised of an inner shell to an inner peripheral surface of which the liquid fuel is supplied, an outer shell defining a passage for the combustion air running substantially straightly between the outer shell itself and an outer peripheral surface of the inner shell, and a swirling-flow guide plate for swirling the combustion air passed into the inner shell, while directing it in a downstream direction. The combustor further includes a resistor abruptly decreased in sectional area downstream and provided substantially downstream of the center of the swirling flow and in the vicinity of an outlet of the premixing type combustion burner for providing a resistance to a premixture ejected from the premixing type combustion burner.
摘要翻译：在包括预混合型燃烧器的燃烧器中，其具有用于与燃烧空气一起喷射液体燃料以雾化液体燃料的雾化器，雾化器包括内壳，其内部表面供应液体燃料，外壳限定用于在外壳本身与内壳的外周表面之间大致直线运行的燃烧空气的通道，以及用于旋转流入内壳的燃烧空气的旋流引导板，同时将其引导到下游方向。燃烧器还包括一个电阻器，其下游的截面积突然减小，并且基本上设置在旋流中心的下游，并且在预混合型燃烧器的出口附近，用于提供对从预混合型燃烧器喷出的预混合物的阻力。

6. 发明授权

US08591004B2 Head unit, liquid jet device, and method for adjusting position of liquid jet head 有权
标题翻译：头部单元，液体喷射装置以及用于调节液体喷头位置的方法
公开(公告)号：US08591004B2
公开(公告)日：2013-11-26
申请号：US13162480
申请日：2011-06-16
申请人： Yoshihiro Kobayashi , Satoshi Tsukahara
发明人： Yoshihiro Kobayashi , Satoshi Tsukahara
IPC分类号： B41J2/165
CPC分类号： B41J25/304 , B41J25/001 , Y10T29/49723
摘要： A head unit for fixing a liquid jet head which ejects liquid includes a base component and movable component that slides on the base component and to which the liquid jet head is fixed. A fixing screw fixes the movable component to the base component. A locating member attached to the base component limits a movement direction in which the movable component moves. The movable component has a contact portion touching the locating member and first and second tapered surfaces formed thereon. A vector normal to the first tapered surface has a first component vector extending in the movement direction. A vector normal to the second tapered surface has a second component vector that is opposite the first component vector and extends in the movement direction. The base component has first and second pins accessible to the first and second tapered surfaces, respectively.
摘要翻译：用于固定喷射液体的液体喷射头的头部单元包括基部部件和在基部部件上滑动并且液体喷射头固定到其上的可移动部件。固定螺钉将可移动部件固定到基部部件。附接到基座部件的定位部件限制可移动部件移动的移动方向。可移动部件具有接触定位构件的接触部分和形成在其上的第一和第二锥形表面。与第一锥形表面垂直的矢量具有在移动方向上延伸的第一分量矢量。与第二锥形表面垂直的矢量具有与第一分量矢量相反并沿运动方向延伸的第二分量矢量。基座部件分别具有可分别到达第一和第二锥形表面的第一和第二销。

7. 发明授权

US4472936A Method and apparatus for controlling combustion of gasified fuel 失效
标题翻译：用于控制气化燃料燃烧的方法和装置
公开(公告)号：US4472936A
公开(公告)日：1984-09-25
申请号：US334175
申请日：1981-12-24
申请人： Yoshihiro Uchiyama , Zensuke Tamura , Shigehisa Sugita , Satoshi Tsukahara
发明人： Yoshihiro Uchiyama , Zensuke Tamura , Shigehisa Sugita , Satoshi Tsukahara
IPC分类号： F02C3/28 , F02C9/40 , F23N5/00 , F02C7/26 , G05D7/00
CPC分类号： F02C3/28 , F02C9/40 , F23N5/003 , F23N2021/10 , F23N2023/06
摘要： In combustion of gasified fuel by gasifying a low quality fuel and combusting the gasified fuel in a combustor, combustion of gasified fuel is controlled by sampling the gasified fuel at a constant flow rate at the upstream side of the combustor, combusting the sampled gasified fuel, detecting an overall energy level of sensible heat and heating value possessed per unit weight of the gasified fuel on the basis of the combustion temperature of the sampled gasified fuel, and controlling the flow rate of gasified fuel to be led to the combustor in accordance with a fluctuation in the detected overall energy level. Unstable combustion due to a fluctuation in the heating value of the gasified fuel and blow-out due to deficiency of the heating value can be prevented.
摘要翻译：通过气化低质量燃料并燃烧燃烧器中的气化燃料，在气化燃料的燃烧中，气化燃料的燃烧是通过在燃烧器的上游侧以恒定的流量取样气化燃料来进行燃烧，燃烧采样的气化燃料，根据采样的气化燃料的燃烧温度，检测每单位重量的气化燃料所具有的显热和发热值的总能量水平，并且根据气体燃料的燃烧温度控制气化燃料的流量检测到的总能量水平的波动。可以防止由于气化燃料的发热值的变动而引起的不稳定的燃烧和由于热值的不足引起的吹出。

8. 发明授权

US4226088A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US4226088A
公开(公告)日：1980-10-07
申请号：US880109
申请日：1978-02-22
申请人： Satoshi Tsukahara , Isao Sato , Yoshihiro Uchiyama , Masanobu Kusaba
发明人： Satoshi Tsukahara , Isao Sato , Yoshihiro Uchiyama , Masanobu Kusaba
IPC分类号： F23R3/12 , F23C99/00 , F23R3/04 , F23R3/54 , F02C7/22
CPC分类号： F23R3/04 , F23R3/54
摘要： A combustor for gas turbines includes a stepped cylindrical tube defining first, second and main combustion spaces. Primary air supply openings are formed in the tube portion defining the first combustion space, secondary air supply openings in the tube portion defining the second combustion space, and diluting air supply openings in the tube portion defining the main combustion space. To achieve effective cooling of the combustion gas within the combustion chamber, particularly in the second combustion space, and especially in the central portion thereof, and at the same time to maintain a stable combustion, the tube is formed so, and the cross-sectional areas of the primary, secondary and diluting air supply openings are dimensioned so, that 25 to 32% of the total amount of air supplied to the combustion chamber are used as primary air in the first combustion space, 38 to 50% as secondary air in the second combustion space, and less than 30% as diluting air in the main combustion space.
摘要翻译：用于燃气轮机的燃烧器包括限定第一，第二和主燃烧空间的阶梯形圆柱形管。主要空气供应开口形成在限定第一燃烧空间的管部分中，限定第二燃烧空间的管部分中的二次空气供应开口，以及限定主燃烧空间的管部分中的稀释空气供应开口。为了有效地冷却燃烧室内的燃烧气体，特别是在第二燃烧空间，特别是在其中心部分，并且同时保持燃烧稳定的燃烧气体，管形成为这样，并且横截面初级，次级和稀释空气供应开口的区域尺寸使得供应到燃烧室的空气总量的25％至32％用作第一燃烧空间中的一次空气，作为二次空气中的38％至50％第二燃烧空间，并且在主燃烧空间中稀释空气小于30％。

9. 发明授权

US4131432A Apparatus for the treatment of gas turbine exhaust gas 失效
标题翻译：用于处理燃气轮机废气的设备
公开(公告)号：US4131432A
公开(公告)日：1978-12-26
申请号：US767612
申请日：1977-02-10
申请人： Isao Sato , Yoshihiro Uchiyama , Youji Ishibashi , Satoshi Tsukahara , Ryoichiro Oshima , Yukio Hishinuma
发明人： Isao Sato , Yoshihiro Uchiyama , Youji Ishibashi , Satoshi Tsukahara , Ryoichiro Oshima , Yukio Hishinuma
IPC分类号： B01D53/94 , B01D53/86 , F01D25/30 , F01N1/10 , F01N3/08 , F01N3/20 , F01N3/28 , F01N13/02 , F01N13/04 , F02C7/00 , B01J8/04 , C10B21/20 , F01N3/15 , F01N3/16
CPC分类号： F01N3/2066 , B01D53/8625 , F01D25/305 , F01N1/10 , F01N13/0097 , F01N13/017 , F01N3/2839 , F01N2230/04 , F01N2290/04 , F01N2310/02 , F01N2330/08 , F01N2610/02 , F01N2610/1453 , Y02T10/24 , Y10S55/30
摘要： A reducing agent such as ammonia, urea or hydrazine effecting selective reduction reaction with an exhaust gas from a gas turbine is injected into a duct of the turbine along with water, and at the same time compressed air from a compressor for the turbine is jetted in the duct to atomize the reducing agent. An amount of the water is controlled so that the surrounding temperature will be suitable for reduction of nitrogen oxides of the exhaust gas. The atomized reducing agent flowing in the duct is decelerated by silencers disposed in the duct, especially by a particular arrangement thereof, so that the reducing agent will be in good contact with the exhaust gas to sufficiently reduce the nitrogen oxides. Catalyst layers are used according to kinds of the reducing agent. The catalyst layers are disposed in the silencers or at the positions that the silencers are disposed.
摘要翻译：将与来自燃气轮机的废气进行选择性还原反应的还原剂如氨，尿素或肼一起注入到涡轮机的管道中，并且同时将来自用于涡轮机的压缩机的压缩空气喷射到管道以使还原剂雾化。控制一定量的水，使得周围温度适合于还原废气的氮氧化物。在管道中流动的雾化还原剂尤其是通过其特定布置而被设置在管道中的消音器减速，使得还原剂与废气良好接触以充分还原氮氧化物。根据还原剂的种类使用催化剂层。催化剂层设置在消音器中或在消声器被设置的位置处。

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