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    • 3. 发明授权
    • Combined cycle power plant with fuel reformer
    • 燃料重整器联合循环发电厂
    • US06260348B1
    • 2001-07-17
    • US09285066
    • 1999-04-02
    • Hideaki SugishitaHidetaka MoriIchiro FukueKazuo Uematsu
    • Hideaki SugishitaHidetaka MoriIchiro FukueKazuo Uematsu
    • F02C618
    • F01K23/10Y02E20/16Y02E20/344
    • 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 at 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 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 at 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 compressor 1 outlet and high pressure turbine 6 outlet thereby reliability of the high temperature turbine 3 is enhanced.
    • 提供了使用甲醇作为燃料的涡轮机组,其中工作流体被压缩机1压缩并被引导到燃烧器2中。作为添加有O2的燃料的H 2和CO 2的混合物被燃烧以产生在高温涡轮机3工作的高温气体, 流过热交换器4,5,并部分返回到压缩机1并进入底部系统的部分低压涡轮机7工作。 底部系统的冷凝器9的冷凝水由压力泵10加压,流过热交换器4,5,成为高温蒸汽,并在高压汽轮机6工作。其废气混入燃烧器2中。混合物 的甲醇和水被供给到重整器13中以从热交换器4吸收热量,以将其重新形成为供应到燃烧器2中的H 2和CO 2。高温涡轮3的高温部分由从 压缩机1出口和高压涡轮机6出口,从而提高高温涡轮机3的可靠性。
    • 5. 发明授权
    • Hydrogen-oxygen combustion turbine plant
    • 氢氧燃气轮机厂
    • US5809768A
    • 1998-09-22
    • US833690
    • 1997-04-08
    • Kazuo UematsuHidetaka MoriHideaki Sugishita
    • Kazuo UematsuHidetaka MoriHideaki Sugishita
    • F01K25/00F02C3/22F02C3/34F03C3/22
    • F02C3/34F01K25/005F02C3/22F05D2260/212Y02E20/16
    • A hydrogen-oxygen combustion turbine plant having an improved thermal efficiency and capable of being designed in a flexible manner. The plant is constructed as follows. A compressor is divided into a plurality of units (1A and 1B), a water injection device (14) is disposed between the compressor units, and exhaust water from a condenser (10) of a second turbine (6) is utilized as a water supply. A gas turbine is also divided into a plurality of units (3A to 3C) with multiple axes. Further, not only extracted steam (9A and 9B) from the compressors (1A and 1B) but also the extracted steam (12A and 12B) from the second turbine (6) and the extracted steam (13A and 13B) from the exhaust of the third turbine (8) are used as cooled steam for gas turbines (3A to 3C) and the combustion chamber (2).
    • 一种具有改善热效率并能灵活设计的氢氧燃烧涡轮机组。 该植物的构造如下。 压缩机被分成多个单元(1A和1B),在压缩机单元之间设置注水装置(14),并且将来自第二涡轮(6)的冷凝器(10)的废水用作水 供应。 燃气轮机也被分成具有多个轴的多个单元(3A至3C)。 此外,不仅从压缩机(1A和1B)提取蒸汽(9A和9B),而且从第二涡轮机(6)提取的蒸汽(12A和12B)和提取的蒸汽(13A和13B) 第三涡轮(8)用作燃气轮机(3A至3C)和燃烧室(2)的冷却蒸汽。
    • 8. 发明授权
    • Gas turbine combined cycle system
    • 燃气轮机联合循环系统
    • US06389797B1
    • 2002-05-21
    • US09697136
    • 2000-10-27
    • Hideaki SugishitaHidetaka MoriKazuo UematsuHideo Matsuda
    • Hideaki SugishitaHidetaka MoriKazuo UematsuHideo Matsuda
    • F02C600
    • F01K23/106F02C7/224Y02E20/16
    • Gas turbine combined cycle system is improved to enhance gas turbine efficiency and combined efficiency by effecting steam-cooling of combustor tail tube and turbine blades. In the combined cycle system comprising; gas turbine (8) having generator (1), compressor (2), combustor (3), blade cooling air cooler (4), fan (5) and turbine (6); steam turbine (29) having high pressure turbine (21), intermediate pressure turbine (22) and low pressure turbine (23); and waste heat recovery boiler (9), saturated water of intermediate pressure economizer (12) is partially led into fuel heater (30) for heating fuel and the water cooled thereby is supplied to feed water heater (10). Steam of intermediate pressure superheater (16) is led into the combustor tail tube for cooling thereof and the steam is then supplied to inlet of the intermediate pressure turbine (22). Steam of outlet of the high pressure turbine (21) is led into the turbine (6) for cooling blades thereof and the steam used for cooling stationary blades is supplied to the inlet of the intermediate pressure turbine (22) and the steam used for cooling moving blades is supplied to reheater (20). Thus, the efficiency is enhanced.
    • 改进了燃气轮机联合循环系统,通过对燃烧器尾管和涡轮叶片进行蒸汽冷却来提高燃气轮机的效率和综合效率。 在组合循环系统中,包括: 具有发电机(1),压缩机(2),燃烧器(3),叶片冷却空气冷却器(4),风扇(5)和涡轮机(6)的燃气轮机(8) 具有高压涡轮机(21),中压涡轮机(22)和低压涡轮机(23)的汽轮机(29); 和余热回收锅炉(9),将中压节能器(12)的饱和水部分地引入用于加热燃料的燃料加热器(30)中,并且将由此冷却的水供应给给水加热器(10)。 中压过热器(16)的蒸汽被引入燃烧器尾管中以进行冷却,然后将蒸汽供应到中压涡轮(22)的入口。 高压涡轮机(21)的出口蒸汽被引入到涡轮机(6)中,用于冷却叶片,用于冷却静止叶片的蒸汽被供应到中压涡轮机(22)的入口和用于冷却的蒸汽 活动叶片被供应到再热器(20)。 因此,提高效率。
    • 10. 发明授权
    • Gas turbine combined cycle
    • 燃气轮机联合循环
    • US06212873B1
    • 2001-04-10
    • US09256106
    • 1999-02-24
    • Hideaki SugishitaHidetaka MoriYoshiaki TsukudaKazuo UematsuEiji Akita
    • Hideaki SugishitaHidetaka MoriYoshiaki TsukudaKazuo UematsuEiji Akita
    • F02C600
    • F01K23/106Y02E20/14Y02E20/16
    • 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.
    • 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。