利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

22 条记录 (耗时 0.026 秒)

    Gas turbine power generator plant and silencer for the same
    1.
    发明授权
    Gas turbine power generator plant and silencer for the same 有权
    燃气轮机发电厂和消声器相同

    公开(公告)号：US07958717B2

    公开(公告)日：2011-06-14

    申请号：US12155704

    申请日：2008-06-09

    申请人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    发明人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    IPC分类号： F02C7/12

    CPC分类号： F02C7/32 ,  F02C7/12 ,  F05D2260/96

    摘要： A gas turbine power generator plant, intended to reduce its noise by making small the intake and exhaust outlets of the cooing air channel of a case, comprises an engine core in which a turbine, a compressor and a generator are installed on the same axis, a combustor for burning air for combustion compressed by the compressor and supplying the air to the turbine, a radiator for cooling a coolant or a lubricant, a cooling fan for ventilating the radiator with cooling air, an electric power converter for converting electric power generated by the generator, and the case for housing these constituent elements. And, a combustion air channel passing the compressor, the combustor and the turbine and a cooling air channel passing the radiator, the cooling fan and the electric power converter are formed as mutually independent channels from intake to exhaust.

    摘要翻译： 旨在通过小型壳体的冷却空气通道的进气和排气出口来减小噪音的燃气轮机发电机组包括其中涡轮机，压缩机和发电机安装在同一轴线上的发动机机芯， 用于燃烧由压缩机压缩的燃烧空气并将空气供给到涡轮机的燃烧器，用于冷却冷却剂或润滑剂的散热器，用于使用冷却空气使散热器通风的冷却风扇，用于转换由 发电机和用于容纳这些组成元件的壳体。 并且，通过压缩机，燃烧器和涡轮机的燃烧空气通道和通过散热器，冷却风扇和电力转换器的冷却空气通道被形成为从进气到排气的相互独立的通道。

    Gas turbine power generator plant with mutually independent cooling air channels from intake to exhaust
    2.
    发明授权
    Gas turbine power generator plant with mutually independent cooling air channels from intake to exhaust 失效
    燃气轮机发电厂具有相互独立的冷却空气通道，从进气到排气

    公开(公告)号：US07409832B2

    公开(公告)日：2008-08-12

    申请号：US11034802

    申请日：2005-01-14

    申请人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    发明人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    IPC分类号： F02C7/20

    CPC分类号： F02C7/32 ,  F02C7/12 ,  F05D2260/96

    摘要： A gas turbine power generator plant, intended to reduce its noise by making small the intake and exhaust outlets of the cooing air channel of a case, comprises an engine core in which a turbine, a compressor and a generator are installed on the same axis, a combustor for burning air for combustion compressed by the compressor and supplying the air to the turbine, a radiator for cooling a coolant or a lubricant, a cooling fan for ventilating the radiator with cooling air, an electric power converter for converting electric power generated by the generator, and the case for housing these constituent elements. And, a combustion air channel passing the compressor, the combustor and the turbine and a cooling air channel passing the radiator, the cooling fan and the electric power converter are formed as mutually independent channels from intake to exhaust.

    摘要翻译： 旨在通过小型壳体的冷却空气通道的进气和排气出口来减小噪音的燃气轮机发电机组包括其中涡轮机，压缩机和发电机安装在同一轴线上的发动机机芯， 用于燃烧由压缩机压缩的燃烧空气并将空气供给到涡轮机的燃烧器，用于冷却冷却剂或润滑剂的散热器，用于使用冷却空气使散热器通风的冷却风扇，用于转换由 发电机和用于容纳这些组成元件的壳体。 并且，通过压缩机，燃烧器和涡轮机的燃烧空气通道和通过散热器，冷却风扇和电力转换器的冷却空气通道被形成为从进气到排气的相互独立的通道。

    Gas turbine power generator plant and silencer for the same
    3.
    发明申请
    Gas turbine power generator plant and silencer for the same 失效
    燃气轮机发电厂和消声器相同

    公开(公告)号：US20050160740A1

    公开(公告)日：2005-07-28

    申请号：US11034802

    申请日：2005-01-14

    申请人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    发明人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    IPC分类号： F01D25/00 ,  F01D25/12 ,  F01D25/24 ,  F01D25/30 ,  F02C6/00 ,  F02C7/00 ,  F02C7/045 ,  F02C7/14 ,  F02C7/18 ,  F02C7/20 ,  F02C7/24 ,  F02C7/32 ,  H02P9/04

    CPC分类号： F02C7/32 ,  F02C7/12 ,  F05D2260/96

    摘要： A gas turbine power generator plant, intended to reduce its noise by making small the intake and exhaust outlets of the cooing air channel of a case, comprises an engine core in which a turbine, a compressor and a generator are installed on the same axis, a combustor for burning air for combustion compressed by the compressor and supplying the air to the turbine, a radiator for cooling a coolant or a lubricant, a cooling fan for ventilating the radiator with cooling air, an electric power converter for converting electric power generated by the generator, and the case for housing these constituent elements. And, a combustion air channel passing the compressor, the combustor and the turbine and a cooling air channel passing the radiator, the cooling fan and the electric power converter are formed as mutually independent channels from intake to exhaust.

    摘要翻译： 旨在通过小型壳体的冷却空气通道的进气和排气出口来减小噪音的燃气轮机发电机组包括其中涡轮机，压缩机和发电机安装在同一轴线上的发动机机芯， 用于燃烧由压缩机压缩的燃烧空气并将空气供给到涡轮机的燃烧器，用于冷却冷却剂或润滑剂的散热器，用于使用冷却空气使散热器通风的冷却风扇，用于转换由 发电机和用于容纳这些组成元件的壳体。 并且，通过压缩机，燃烧器和涡轮机的燃烧空气通道和通过散热器，冷却风扇和电力转换器的冷却空气通道被形成为从进气到排气的相互独立的通道。

    Gas turbine power generator plant and silencer for the same
    4.
    发明申请
    Gas turbine power generator plant and silencer for the same 有权
    燃气轮机发电厂和消声器相同

    公开(公告)号：US20090044536A1

    公开(公告)日：2009-02-19

    申请号：US12155704

    申请日：2008-06-09

    申请人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    发明人： Susumu Nakano ,  Masaya Ichinose ,  Masanori Watanabe ,  Kuniyoshi Tsubouchi ,  Toshihiko Fukushima ,  Masatoshi Watanabe

    IPC分类号： F02C7/24 ,  F01N1/24 ,  F01N1/06

    CPC分类号： F02C7/32 ,  F02C7/12 ,  F05D2260/96

    摘要： A gas turbine power generator plant, intended to reduce its noise by making small the intake and exhaust outlets of the cooing air channel of a case, comprises an engine core in which a turbine, a compressor and a generator are installed on the same axis, a combustor for burning air for combustion compressed by the compressor and supplying the air to the turbine, a radiator for cooling a coolant or a lubricant, a cooling fan for ventilating the radiator with cooling air, an electric power converter for converting electric power generated by the generator, and the case for housing these constituent elements. And, a combustion air channel passing the compressor, the combustor and the turbine and a cooling air channel passing the radiator, the cooling fan and the electric power converter are formed as mutually independent channels from intake to exhaust.

    摘要翻译： 旨在通过小型壳体的冷却空气通道的进气和排气出口来减小噪音的燃气轮机发电机组包括其中涡轮机，压缩机和发电机安装在同一轴线上的发动机机芯， 用于燃烧由压缩机压缩的燃烧空气并将空气供给到涡轮机的燃烧器，用于冷却冷却剂或润滑剂的散热器，用于使用冷却空气使散热器通风的冷却风扇，用于转换由 发电机和用于容纳这些组成元件的壳体。 并且，通过压缩机，燃烧器和涡轮机的燃烧空气通道和通过散热器，冷却风扇和电力转换器的冷却空气通道被形成为从进气到排气的相互独立的通道。

    Radial turbine and method of cooling nozzle of the same
    8.
    发明申请
    Radial turbine and method of cooling nozzle of the same 失效
    径向涡轮机和冷却喷嘴的方法相同

    公开(公告)号：US20080092515A1

    公开(公告)日：2008-04-24

    申请号：US10589976

    申请日：2004-03-09

    申请人： Manabu Yagi ,  Kuniyoshi Tsubouchi ,  Tadaharu Kishibe ,  Susumu Nakano ,  Satoshi Dodo

    发明人： Manabu Yagi ,  Kuniyoshi Tsubouchi ,  Tadaharu Kishibe ,  Susumu Nakano ,  Satoshi Dodo

    IPC分类号： F02C7/18 ,  F04D29/44

    CPC分类号： F01D1/08 ,  F01D5/187 ,  F01D17/165 ,  F02C3/00

    摘要： A turbine nozzle (2) that, among components constructing a turbine, reaches particularly high temperature is efficiently cooled with a relatively simple structure. A double casing structure in which a turbine casing (7) is provided outside a turbine shell (5) is formed. The turbine casing (7) functions as a flow path (24) for compressed air (20→21) before combustion. The turbine shell (5) covers a turbine nozzle (2) and a radial turbine impeller (3) and forms flow paths (15, 16) for combustion gas (10→11→12→13). The compressed air (21) before combustion flowing in the flow path (24), for compressed air, having air-tightness between itself and the outside air is blown to the turbine nozzle (2) through a through-hole (51) penetrating both wall surfaces of the turbine shell (5). By this, the turbine nozzle (2) is cooled and the compressed air used to cool the turbine nozzle is made to flow toward the turbine impeller (3). As a result, the entire volume of compressed air (20) taken into the turbine contributes to mechanical work for driving the turbine impeller (3).

    摘要翻译： 在构成涡轮机的部件达到特别高的温度下的涡轮喷嘴（2）以相对简单的结构被有效地冷却。 形成涡轮壳体（7）外侧的涡轮壳体（5）的双壳体结构。 在燃烧之前，涡轮机壳体（7）用作用于压缩空气（20-> 21）的流动路径（24）。 涡轮壳体（5）覆盖涡轮喷嘴（2）和径向涡轮叶轮（3）并形成用于燃烧气体（10-> 11-> 12-> 13）的流动路径（15,16）。 在流动路径（24）中流动的压缩空气（21）之间的压缩空气（其自身与外部空气之间具有气密性）通过贯穿两者的通孔（51）吹送到涡轮喷嘴（2） 涡轮壳体（5）的壁表面。 由此，涡轮喷嘴（2）被冷却，用于冷却涡轮喷嘴的压缩空气朝向涡轮机叶轮（3）流动。 结果，进入涡轮机的整个体积的压缩空气（20）有助于驱动涡轮叶轮（3）的机械作业。