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    SOLAR-THERMAL GAS TURBINE GENERATOR
    1.
    发明申请
    SOLAR-THERMAL GAS TURBINE GENERATOR 失效
    太阳能气体涡轮发电机

    公开(公告)号：US20110233940A1

    公开(公告)日：2011-09-29

    申请号：US13123777

    申请日：2010-06-04

    申请人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Manabu Maeda

    发明人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Manabu Maeda

    IPC分类号： H02K7/18

    CPC分类号： F02C6/18 ,  F01K23/10 ,  F02C1/05 ,  F03G6/064 ,  F03G6/067 ,  Y02E10/46 ,  Y02E20/16

    摘要： A solar-thermal gas turbine generator is equipped with a compressor, a heat receiver, and a turbine. Additionally, there is a generator that is driven by the solar-thermal gas turbine to generate power; and a steam power generation cycle in which high-temperature air exhausted from the turbine is introduced into a steam generator and in which a steam turbine that is operated with steam generated at the steam generator drives a generator to generator power, wherein a solar-thermal steam generator that generates steam by being heated with heat collected by the light collector is provided upstream of the steam turbine of the steam power generation cycle, and a distribution ratio for distributing the sunlight collected by the light collector to the heat receiver and the solar-thermal steam generator is adjusted in accordance with the sunlight intensity.

    摘要翻译： 太阳能热燃气涡轮发电机配备有压缩机，热接收器和涡轮机。 另外，还有一台发电机由太阳热能燃气轮机驱动，以发电; 以及蒸汽发电循环，其中从涡轮机排出的高温空气被引入到蒸汽发生器中，其中在蒸汽发生器处产生的蒸汽操作的蒸汽涡轮驱动发电机发电机功率，其中太阳能热 在蒸汽发电循环的蒸汽涡轮机的上游设置有通过被集光器收集的热量加热而产生蒸汽的蒸汽发生器，并且将由集光器收集的太阳光分配到热接收器和太阳能发电装置的分配比例， 热蒸汽发生器根据阳光强度进行调整。

    Solar-thermal gas turbine generator
    2.
    发明授权
    Solar-thermal gas turbine generator 失效
    太阳能燃气轮机发电机

    公开(公告)号：US08312703B2

    公开(公告)日：2012-11-20

    申请号：US13123777

    申请日：2010-06-04

    申请人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Manabu Maeda

    发明人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Manabu Maeda

    IPC分类号： F02C6/00

    CPC分类号： F02C6/18 ,  F01K23/10 ,  F02C1/05 ,  F03G6/064 ,  F03G6/067 ,  Y02E10/46 ,  Y02E20/16

    摘要： A solar-thermal gas turbine generator is equipped with a compressor, a heat receiver, and a turbine. Additionally, there is a generator that is driven by the solar-thermal gas turbine to generate power; and a steam power generation cycle in which high-temperature air exhausted from the turbine is introduced into a steam generator and in which a steam turbine that is operated with steam generated at the steam generator drives a generator to generator power, wherein a solar-thermal steam generator that generates steam by being heated with heat collected by the light collector is provided upstream of the steam turbine of the steam power generation cycle, and a distribution ratio for distributing the sunlight collected by the light collector to the heat receiver and the solar-thermal steam generator is adjusted in accordance with the sunlight intensity.

    摘要翻译： 太阳能热燃气涡轮发电机配备有压缩机，热接收器和涡轮机。 另外，还有一台发电机由太阳热能燃气轮机驱动，以发电; 以及蒸汽发电循环，其中从涡轮机排出的高温空气被引入到蒸汽发生器中，其中在蒸汽发生器处产生的蒸汽操作的蒸汽涡轮驱动发电机发电机功率，其中太阳能热 在蒸汽发电循环的蒸汽涡轮机的上游设置有通过被集光器收集的热量加热而产生蒸汽的蒸汽发生器，并且将由集光器收集的太阳光分配到热接收器和太阳能发电装置的分配比例， 热蒸汽发生器根据阳光强度进行调整。

    CONCENTRATED SOLAR POWER GAS TURBINE AND CONCENTRATED-SOLAR-POWER-GAS TURBINE POWER GENERATION EQUIPMENT
    4.
    发明申请
    CONCENTRATED SOLAR POWER GAS TURBINE AND CONCENTRATED-SOLAR-POWER-GAS TURBINE POWER GENERATION EQUIPMENT 审中-公开
    浓缩太阳能发电机组和集中式太阳能发电机组发电设备

    公开(公告)号：US20110259007A1

    公开(公告)日：2011-10-27

    申请号：US13126258

    申请日：2010-05-31

    申请人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Masahiro Masuda

    发明人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi ,  Masashi Tagawa ,  Toshiyuki Osada ,  Masahiro Masuda

    IPC分类号： F03G6/04 ,  F01K3/00 ,  F02C1/05

    CPC分类号： F02C1/05 ,  F03G6/064 ,  F05D2260/85 ,  Y02E10/46 ,  Y02E20/14

    摘要： Provided is a concentrated solar power gas turbine that enables efficient operation to allow a reduction in capacity of the start-up driving source used for compensating for the shortage of solar heat quantity at the start-up/acceleration. The concentrated solar power gas turbine (GT1) includes a compressor (1) for taking in air and increasing the pressure thereof, the compressor (1) being provided with a start-up driving source for start-up/acceleration; a solar central receiver (2) for heating the high-pressure air, the pressure of which has been increased by the compressor (1), by the heat of sunlight collected by a heliostat to increase the temperature thereof; and a turbine (3) for converting thermal energy possessed by the high-temperature/high-pressure air to mechanical energy, wherein the fluid flow in the solar central receiver (2) is shut off to store heat in the period from the shutdown of the turbine (3) to the start-up thereof.

    摘要翻译： 提供了一种集中的太阳能燃气轮机，其能够进行有效的操作，以允许降低用于补偿启动/加速时的太阳能热量不足的起动驱动源的容量。 集中太阳能燃气轮机（GT1）包括用于吸入空气并增加其压力的压缩机（1），压缩机（1）设置有用于启动/加速的启动驱动源; 太阳能中央接收器（2），用于通过由定日镜收集的太阳光的热量来加热由压缩机（1）增加的压力的高压空气，以增加其温度; 以及用于将高温/高压空气所具有的热能转换为机械能的涡轮机（3），其中在太阳能中央接收器（2）中的流体流动被截止以在从关闭 涡轮（3）启动。

    SOLAR CENTRAL RECEIVER
    6.
    发明申请
    SOLAR CENTRAL RECEIVER 审中-公开
    太阳能中央接收器

    公开(公告)号：US20110239651A1

    公开(公告)日：2011-10-06

    申请号：US13124963

    申请日：2010-06-08

    申请人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi

    发明人： Kuniaki Aoyama ,  Kei Inoue ,  Kazuta Kobayashi

    IPC分类号： F02C1/05 ,  F24J2/24 ,  F24J2/10

    CPC分类号： F03G6/064 ,  F24S10/70 ,  F24S20/20 ,  F24S23/70 ,  Y02E10/41 ,  Y02E10/44 ,  Y02E10/46 ,  Y02E20/14

    摘要： Heat transfer pipes uniformly heat a compressible working fluid passing there through with a simplified supporting structure and reduced manufacturing costs. A solar central receiver (3) on top of a tower on the ground includes heat transfer pipes (16) arranged in the south-north direction; and a casing (14) accommodating the pipes (16) and has a solar radiation inlet (15) through which sunlight reflected by heliostats on the ground is transmitted to the lower surface side of the pipes (16). The pipes (16) are at equal intervals on a solar radiation receiving surface (11) parallel to a heliostat field on which the collectors are, or inclined with respect to the heliostat field on which the collectors are, and the diameters of the pipes (16) are substantially inversely proportional to the shortest distance from the inlet (15) to the central axes of the respective pipes (16) in the longitudinal direction.

    摘要翻译： 传热管道将通过其的可压缩工作流体均匀地加热，并具有简化的支撑结构并降低制造成本。 位于地面塔顶的太阳能中央接收器（3）包括沿南北方向布置的传热管（16） 以及容纳所述管道（16）并具有太阳辐射入口（15）的壳体（14），所述太阳辐射入口（15）通过所述太阳辐射入口（15）向所述管道（16）的下表面侧透射由所述地面上的定日镜反射的太阳光。 管道（16）在平行于收集器所在的定日镜场的太阳辐射接收表面（11）上相对于相对于收集器所在的定日镜场倾斜的太阳辐射接收表面（11）和管道 16）与在纵向方向上从入口（15）到相应管道（16）的中心轴线的最短距离成反比。

    Combustor containing fuel nozzle
    7.
    发明授权
    Combustor containing fuel nozzle 有权
    含燃料喷嘴的燃烧器

    公开(公告)号：US06931854B2

    公开(公告)日：2005-08-23

    申请号：US10287507

    申请日：2002-11-05

    申请人： Keijirou Saitoh ,  Takashi Kawano ,  Hidemi Niinai ,  Yutaka Kawata ,  Shigemi Mandai ,  Kuniaki Aoyama

    发明人： Keijirou Saitoh ,  Takashi Kawano ,  Hidemi Niinai ,  Yutaka Kawata ,  Shigemi Mandai ,  Kuniaki Aoyama

    IPC分类号： F23D14/02 ,  F23D14/58 ,  F23R3/28 ,  F02C1/00 ,  F02G3/00

    CPC分类号： F23R3/286 ,  F23D2210/00 ,  F23D2900/14004 ,  F23R2900/00014

    摘要： There is provided a combustor comprising a fuel nozzle which is comprised of a rodlike body which has a fuel passage and which is located in an air passage; a plurality of hollow members which are connected to the fuel passage and which extend in radial directions from the rodlike body into the air passage; at least one injection port formed in each hollow member to inject a fuel from the fuel passage into the air passage; and a projection which extends from a farmost inner wall of each hollow member that is most distant from an axis of the rodlike body to the injection port that is most distant from the axis. A hole for leaking fuel that is connected to an air passage may be formed in a farmost inner wall of the hollow member that is more distant from an axis of a rodlike body than the injection port that is most distant from the axis, or may be formed to be adjacent to all the injection ports on an upstream or downstream side in the direction of the airflow. Thus, a vortex does not occur in the hollow column.

    摘要翻译： 提供了一种燃烧器，其包括燃料喷嘴，该燃料喷嘴由具有燃料通道并且位于空气通道中的杆状体构成; 多个中空构件，其连接到燃料通道并且在径向方向上从杆状体延伸到空气通道中; 形成在每个中空构件中的至少一个喷射口，用于将来自燃料通道的燃料喷射到空气通道中; 以及从最远离杆状体的轴线到最远离轴线的喷射口的每个中空构件的农田内壁延伸的突起。 连接到空气通道的用于泄漏燃料的孔可以形成在中空构件的农田内壁中，该中空构件的远离轴线的轴线比距离轴线最远的喷射口更远离杆状体的轴线，或者可以是 形成为与气流方向上游侧或下游侧的所有喷射口相邻。 因此，在中空塔中不会发生涡流。

    Seal structure for gas turbine combustor
    8.
    发明授权
    Seal structure for gas turbine combustor 有权
    燃气轮机燃烧室密封结构

    公开(公告)号：US08069673B2

    公开(公告)日：2011-12-06

    申请号：US12767055

    申请日：2010-04-26

    申请人： Nobuhiro Kunitake ,  Kuniaki Aoyama ,  Kiyoshi Fujimoto ,  Masaharu Minami

    发明人： Nobuhiro Kunitake ,  Kuniaki Aoyama ,  Kiyoshi Fujimoto ,  Masaharu Minami

    IPC分类号： F02C7/20

    CPC分类号： F16J15/0887 ,  F01D9/023 ,  F01D11/005 ,  F02C7/28 ,  F05D2240/57

    摘要： Provided is a seal structure, according to the present invention, for sealing opposite surfaces of flanges between adjacent tail ducts, which can be prevented from being worn or aged deteriorated due to a thermal deformation in a high temperature atmosphere or vibration of a gas turbine combustor, and which can maintain a satisfactory sealing function for a long time. The seal structure is characterized in that recess grooves are formed in opposed surfaces of adjacent flanges at the outlet end of tail ducts, striding between the opposed surfaces, a seal assembly composed of a seal member and a leaf spring is inserted in the recess grooves, the seal member has a pair of continuous beads which are arranged facing the inner surfaces, on the combustion gas passage side, of the recess grooves, striding between the opposed surfaces of the flanges within the recess grooves, the leaf spring is arranged so as to be contact with the seal member within the recess grooves so that the beads are pressed against the surfaces on the combustion gas passage side by the resilient force of the leaf spring so as to create seal surfaces.

    摘要翻译： 根据本发明，提供一种用于密封相邻尾管之间的法兰相对表面的密封结构，其可以防止由于高温气氛中的热变形或燃气轮机燃烧器的振动而被磨损或老化而劣化 ，长时间保持良好的密封功能。 密封结构的特征在于，在尾管的出口端的相邻凸缘的相对的表面上形成凹槽，跨过相对的表面之间，由密封件和片簧组成的密封组件插入凹槽中， 所述密封构件具有一对连续的珠，所述一对连续的珠子相对于所述凹槽的燃烧气体通道侧的内表面布置，跨越所述凹槽内的所述凸缘的相对的表面之间，所述板簧布置成 与凹槽内的密封构件接触，使得珠被片簧的弹力压靠在燃烧气体通路侧的表面上，从而形成密封面。

    Vane for gas turbine
    10.
    发明授权
    Vane for gas turbine 失效
    燃气轮机叶片

    公开(公告)号：US5897294A

    公开(公告)日：1999-04-27

    申请号：US875176

    申请日：1997-10-14

    申请人： Kuniaki Aoyama ,  Masao Terazaki

    发明人： Kuniaki Aoyama ,  Masao Terazaki

    IPC分类号： F01D5/18 ,  F02C7/18

    CPC分类号： F01D5/186 ,  F05D2260/202

    摘要： A gas turbine blade having a plurality of shower head cooling holes (1), bored in a blade leading edge portion, are arranged along a single line which is biased so as to correspond to the direction of swirling flow in a combustor. The swirling flow is clockwise or counter-clockwise. In particular, if the flow is clockwise, the cooling holes (1) are biased to the left hand side, as seen from upstream of the blade, toward a blade hub side (HS) from a blade tip side (TS). Also, if the flow is counter-clockwise, the cooling holes (1) are arrayed on one line which is biased to the reverse side relative to the latter case. The influence of the swirling flow is thus avoided, and the pressure at each position of the cooling holes (1) is constant, so that uniform cooling can be attained.

    摘要翻译： PCT No.PCT / JP96 / 03397 371日期1997年10月14日第 102（e）1997年10月14日PCT PCT 1996年11月20日PCT公布。 公开号WO97 / 19257 日期：1997年5月29日具有多个喷嘴头冷却孔（1）的燃气轮机叶片，其沿叶片前缘部分钻孔，沿着单个管线布置，该线路被偏压以对应于燃烧器中的回旋流的方向 。 旋流是顺时针或逆时针旋转。 特别地，如果流动是顺时针方向的，则从刀片的上游看，冷却孔（1）从叶片顶端侧（TS）向叶片轮毂侧（HS）偏压到左侧。 此外，如果流动是逆时针方向，则冷却孔（1）排列在相对于后一种情况被偏压到相反侧的一条线上。 因此避免了旋流的影响，并且冷却孔（1）的各位置处的压力是恒定的，从而可以获得均匀的冷却。