Combined cycle power plant
    31.
    发明授权

    公开(公告)号:US06430916B1

    公开(公告)日:2002-08-13

    申请号:US09866710

    申请日:2001-05-30

    IPC分类号: F02C618

    摘要: Provided is turbine plant using methanol as fuel in which working fluid is compressed by compressor 1 and led into combustor 2. A mixture of H2 and CO2 as fuel added with O2 is burned to generate high temperature gas, which works in high temperature turbine 3, flows through heat exchangers 4, 5 and returns partly to the compressor 1 and enters partly low pressure turbine 7 of a bottoming system to work. Condensed water from condenser 9 of the bottoming system is pressurized by pressure pump 10 and flows through the heat exchangers 4, 5 to become high temperature steam and to work in high pressure turbine 6. Exhaust gas thereof is mixed into the combustor 2. A mixture of methanol and water is supplied into reformer 13 to absorb heat from the heat exchanger 4 to be reformed into H2 and CO2, which is supplied into the combustor 2. A high temperature portion of the high temperature turbine 3 is cooled by cooling medium extracted from the compressor 1 outlet and high pressure turbine 6 outlet thereby reliability of the high temperature turbine 3 is enhanced.

    Recovery type steam cooled gas turbine
    32.
    发明授权
    Recovery type steam cooled gas turbine 有权
    回收式蒸汽冷却燃气轮机

    公开(公告)号:US06367242B2

    公开(公告)日:2002-04-09

    申请号:US09197604

    申请日:1998-11-23

    IPC分类号: F02C100

    CPC分类号: F02C7/18 Y02E20/16

    摘要: In a recovery type steam cooled gas turbine, dew condensation is prevented when feeding steam in a starting operation of the gas turbine, and penetration of high temperature combustion gas into a steam cooling passage is prevented. Also, residual steam is removed in the stopping operation of the gas turbine. The gas turbine (1) has moving and stationary blade steam cooling passages (4a, 4b). The steam from steam cooling pipes (9, 10) flows through these passages to cool them. The steam after cooling is recovered. In the starting operation of the gas turbine, air from a compressor (2) flows through a valve (15) and a flow rate regulator (7). Also, a portion of the air is subjected to a temperature adjustment in a temperature adjuster (5) and flows through three-way valves (11, 12) to a steam cooling passage (4a, 4b) to be discharged through three-way valves (13, 14) and a flow rate regulator valve (8) to warm the passages (4a, 4b). Also, valves (15, 16) are closed and a valve (17) is opened so that outside air or inert gas from a medium feed source (6) may flow. After the warming up operation in the starting operation, the three-way valves (11 to 14) are switched to allow the steam to flow from the pipes (9, 10) to the passages (4a, 4b) to perform cooling during regular operation. Furthermore, after the stopping operation, it is possible to purge the residual steam within the passages (4a, 4b) with air.

    摘要翻译: 在回收式蒸汽冷却式燃气轮机中,在燃气轮机的起动动作中供给蒸汽时,能够防止结露,能够防止高温燃烧气体进入蒸汽冷却通路。 此外,在燃气轮机的停止操作中除去残余蒸汽。燃气轮机(1)具有移动和静止的叶片蒸汽冷却通道(4a,4b)。 来自蒸汽冷却管道(9,10)的蒸汽流过这些通道以冷却它们。 回收冷却后的蒸汽。 在燃气轮机的启动操作中,来自压缩机(2)的空气流经阀(15)和流量调节器(7)。 另外,一部分空气在温度调节器(5)中进行温度调节,并且通过三通阀(11,12)流到蒸汽冷却通道(4a,4b),以通过三通阀 (13,14)和流量调节阀(8),以加热通道(4a,4b)。 此外,阀(15,16)关闭并且阀(17)打开,使得来自介质进料源(6)的外部空气或惰性气体可能流动。 在起动运转中的预热运转之后,切换三通阀(11〜14),使蒸汽从管道(9,10)流向通道(4a,4b),以在正常运行中进行冷却 。 此外,在停止操作之后,可以用空气吹扫通道(4a,4b)内的残余蒸汽。

    Gas turbine combined cycle
    33.
    发明授权
    Gas turbine combined cycle 失效
    燃气轮机联合循环

    公开(公告)号:US06212873B1

    公开(公告)日:2001-04-10

    申请号:US09256106

    申请日:1999-02-24

    IPC分类号: F02C600

    摘要: The invention provides a gas turbine combined cycle structured such that an intermediate cooling device for cooling a compression air discharged from a low pressure compressor, so as to reduce a load of a high pressure compressor, is provided. The gas turbine combined cycle in accordance with the invention is structured such as to branch water from a condenser to a steam generating device for generating steam. Exhaust gas discharged from a steam turbine is condensed to water. Compression air discharged from a low pressure compressor is cooled by being supplied to an intermediate cooling device, and is then supplied to a high pressure compressor. Steam which heats and operates the steam turbine is generated by the heat recovered by the cooling of the compression air in the intermediate cooling device. Accordingly, there can be obtained a gas turbine combined cycle having the advantage of the conventional intermediate cooling type gas turbine combined cycle, but exhibiting an improved combined efficiency.

    摘要翻译: 本发明提供了一种燃气轮机联合循环,其结构使得用于冷却从低压压缩机排出的压缩空气以减少高压压缩机的负荷的中间冷却装置。 根据本发明的燃气轮机联合循环被构造为将水从冷凝器分配到用于产生蒸汽的蒸汽发生装置。 从汽轮机排出的排气被冷凝成水。 从低压压缩机排出的压缩空气通过供给到中间冷却装置而冷却,然后供给高压压缩机。 通过中间冷却装置中的压缩空气冷却回收的热量产生加热和操作蒸汽轮机的蒸汽。 因此,可以获得具有传统的中间冷却型燃气轮机联合循环的优点的燃气轮机联合循环,但是显示出提高的组合效率。

    Cooling structure around L shaped vertical type gas turbine output shaft
    34.
    发明授权
    Cooling structure around L shaped vertical type gas turbine output shaft 失效
    L型垂直式燃气轮机输出轴周围的冷却结构

    公开(公告)号:US6120245A

    公开(公告)日:2000-09-19

    申请号:US252936

    申请日:1999-02-19

    CPC分类号: F01D5/08 F01D25/12 F02C7/18

    摘要: A cooling structure around the output shaft of an L-shaped vertical gas turbine, for cooling the output shaft effectively by a natural ventilation. A gas generator 5 is arranged horizontally whereas an output turbine 1 is arranged vertically, and a pump or the like is driven by an output shaft 3. A cylinder 20 is fitted in a space 12 between the output shaft 3 and a cylindrical casing 13 and is fixed at a cylindrical flange 20a. Cooling air 30 is caused to flow upward from between the cylinder 20 and the output shaft 3 by the ejector effect of an exhaust gas from below a baseplate 8 and by the vacuum in the casing and then to flow downward from the upper end of the cylinder 20 between the cylinder 20 and the cylindrical casing 13, so that it flows out from the lower portion into the package. The output shaft of the L-shaped vertical type gas turbine having a compact narrow space is effectively cooled therearound by the natural ventilation without providing any fan or the like.

    摘要翻译: L型立式燃气轮机输出轴周围的冷却结构,用于通过自然通风有效地冷却输出轴。 气体发生器5水平布置,而输出涡轮机1垂直布置,泵等通过输出轴3驱动。气缸20装配在输出轴3和圆柱形壳体13之间的空间12中, 固定在圆柱形凸缘20a上。 使得冷却空气30从气缸20和输出轴3之间通过来自底板8下方的排出气体的喷射效应和壳体中的真空向上流动,然后从气缸的上端向下流动 20在圆筒20和圆柱形壳体13之间,使得其从下部流出到包装中。 具有紧凑型狭窄空间的L形立式燃气轮机的输出轴通过自然通风被有效地冷却,而不需要任何风扇等。

    Recovery type steam-cooled gas turbine
    35.
    发明授权
    Recovery type steam-cooled gas turbine 有权
    回收式蒸汽冷却燃气轮机

    公开(公告)号:US6007299A

    公开(公告)日:1999-12-28

    申请号:US145497

    申请日:1998-09-02

    申请人: Kazuo Uematsu

    发明人: Kazuo Uematsu

    摘要: In a recovery type steam-cooled gas turbine, a steam passage leading to a moving blade is provided on a central side of a rotor for reducing leakage of the steam. Cooling steam 70 of a low temperature and high pressure is led into moving blades 1, 2 through supply side steam passages 12, 13 and steam passages 15, 16. After being used for cooling, it flows into a cavity 22 through steam passages 16, 17 to be recovered as recovery steam 71 of a high temperature and low pressure at a rotor end 20 through recovery side steam passages 19, 21. The cooling steam 70 of low temperature and high pressure passes on an inner side of the recovery steam 71 in the rotor, hence there are fewer places from where the high pressure steam leaks outside as compared with the prior art, in which the high pressure steam is supplied from the outer side in the rotor, and the leakage amount of steam is reduced.

    摘要翻译: 在回收式蒸汽冷却燃气轮机中,在转子的中心侧设有通向动叶片的蒸汽通道,用于减少蒸汽泄漏。 低温高压的冷却水70通过供给侧蒸气通路12,13和蒸汽通路15,16被引导到动叶片1,2中。冷却后,通过蒸汽通路16流入空腔22, 17通过回收侧蒸汽通道19,21在转子端20处作为高温低压的回收蒸汽71回收。低温高压的冷却水70在回收蒸汽71的内侧通过 因此与现有技术相比,高压蒸汽从外部泄漏的位置较少,其中高压蒸汽从转子的外侧供应,并且蒸汽的泄漏量减少。

    Gas turbine and turbine rotor for a gas turbine

    公开(公告)号:US07114915B2

    公开(公告)日:2006-10-03

    申请号:US10339293

    申请日:2003-01-10

    IPC分类号: F01D5/08

    摘要: A refrigerant supplied from a refrigerant supply pipe flows into a first space, being a passage of the refrigerant, from a space between first stage and second stage rotor disks. The refrigerant supplied to the first space is guided to second, third and forth spaces through a gap between a spindle bolt and a bolt hole, during which the rotor disks are warmed up or cooled. In the second stage rotor disk, a refrigerant through hole axially penetrating this rotor disk is provided near the center thereof. The refrigerant flowing into the first space passes through the refrigerant through hole to flow into the second space, to thereby promote the convection in the first, second, third and fourth spaces and equalization of temperatures in the rotor disks.

    Combined cycle gas turbine system
    39.
    发明授权
    Combined cycle gas turbine system 失效
    联合循环燃气轮机系统

    公开(公告)号:US06966171B2

    公开(公告)日:2005-11-22

    申请号:US10657175

    申请日:2003-09-09

    摘要: A combined cycle gas turbine system is improved to enhance a gas turbine efficiency and a combined efficiency by effecting steam-cooling of a combustor transition piece and a turbine blade. The combined cycle system has a gas turbine (8) having a generator (1), a compressor (2), a combustor (3), a blade cooling air cooler (4) and a turbine (6), a steam turbine (29) having a high pressure turbine (21), an intermediate pressure turbine (22) and a low pressure turbine (23), and a waste heat recovery boiler (9). Saturated water of a high pressure pump (27) is partially led into a demineralizer (118) and a water sprayer (116) for cooling steam to be supplied into a moving blade (52). The steam, after being used for cooling, is recovered into a reheater (20). Outlet steam of the high pressure turbine (21) is led into a stationary blade (53) for cooling thereof and the steam is then recovered into an inlet of the intermediate pressure turbine (22). Also, steam of an intermediate pressure superheater (16) is led into a combustor transition piece (54) for cooling thereof and the steam is recovered into the inlet of the intermediate pressure turbine (22). Thus, moving blade cooling steam is reduced and the combined efficiency is enhanced.

    摘要翻译: 改进了联合循环燃气轮机系统以通过实现燃烧器过渡件和涡轮叶片的蒸汽冷却来提高燃气轮机效率和组合效率。 联合循环系统具有燃气轮机(8),其具有发电机(1),压缩机(2),燃烧器(3),叶片冷却空气冷却器(4)和涡轮机(6),汽轮机 )具有高压涡轮(21),中压涡轮机(22)和低压涡轮机(23)和废热回收锅炉(9)。 高压泵(27)的饱和水部分地被引入软化器(118)和用于冷却蒸汽的水喷雾器(116)以供应到动叶片(52)中。 用于冷却后的蒸汽被回收到再热器(20)中。 高压涡轮机(21)的出口蒸汽被引入固定叶片(53)以进行冷却,然后将蒸汽回收到中压涡轮机(22)的入口。 此外,中压过热器(16)的蒸汽被引入燃烧器过渡件(54)以进行冷却,并且蒸汽被回收到中压涡轮机(22)的入口中。 因此,移动叶片冷却蒸汽减少并且组合效率提高。