Shaft structure and bearing structure for tail end of rotor of gas turbine
    41.
    发明授权
    Shaft structure and bearing structure for tail end of rotor of gas turbine 有权
    燃气轮机转子尾端轴结构和轴承结构

    公开(公告)号:US06688847B2

    公开(公告)日:2004-02-10

    申请号:US09942619

    申请日:2001-08-31

    IPC分类号: F01D508

    摘要: A shaft structure of a rotor tail end of a gas turbine in which a steam passage for supplying and recovering a steam for cooling rotor blades of the gas turbine extends along a center axis of the rotor assembly of the gas turbine is provided, wherein a center hole of the rotor tail end coaxial to the center axis of the steam passage is formed in the rotor tail end. Provision is also made of a thermal sleeve between the steam passage and the inner surface of the center hole of the rotor tail end, so that a thermal insulation gas layer is formed between the inner surface of the center hole of the rotor tail end and the thermal sleeve. The thermal insulation gas layer is isolated gas-tightly and liquid-tightly from the outside.

    摘要翻译: 提供一种燃气轮机的转子尾端的轴结构,其中用于供应和回收用于冷却燃气涡轮机的转子叶片的蒸汽的蒸汽通道沿着燃气轮机的转子组件的中心轴延伸,其中中心 在转子尾端形成有与蒸汽通道的中心轴同轴的转子尾端的孔。 在蒸汽通道和转子尾端的中心孔的内表面之间还设置有热套筒,使得在转子尾端的中心孔的内表面和 热套。 绝热气体层从外部气密地液密隔离。

    Gas turbine combined cycle system
    42.
    发明授权
    Gas turbine combined cycle system 有权
    燃气轮机联合循环系统

    公开(公告)号:US06389797B1

    公开(公告)日:2002-05-21

    申请号:US09697136

    申请日:2000-10-27

    IPC分类号: F02C600

    摘要: 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.

    摘要翻译: 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。

    Combined cycle plant having a heat exchanger for compressed air
    43.
    发明授权
    Combined cycle plant having a heat exchanger for compressed air 失效
    具有用于压缩空气的热交换器的联合循环设备

    公开(公告)号:US06244039B1

    公开(公告)日:2001-06-12

    申请号:US09300841

    申请日:1999-04-28

    IPC分类号: F02C600

    CPC分类号: F01K23/106 Y02E20/16

    摘要: A combined cycle plant includes a heat exchanger (3) for recovering heat into compressed air or gas turbine fuel to be supplied into gas turbine (01). The plant is arranged such that steam is used as high temperature side working medium of the heat exchanger (3). Thus, the heating medium supply passage can be made of ordinary steam piping and piping cost is reduced. Also, gas turbine exhaust gas is led directly into a waste heat recovery boiler (02), so that gas turbine efficiency and combined efficiency can be enhanced and plant manufacturing cost is reduced.

    摘要翻译: 联合循环设备包括用于将热量回收到被供应到燃气轮机(01)中的压缩空气或燃气涡轮燃料中的热交换器(3)。 该设备布置成使得蒸汽用作热交换器(3)的高温侧工作介质。 因此,加热介质供给通路可以由普通蒸汽管道制成,并且管道成本降低。 此外,燃气轮机废气直接引入废热回收锅炉(02),从而可以提高燃气轮机效率和组合效率,降低设备制造成本。

    Combined cycle power generating plant and method of supplying cooling steam for gas turbine in same
    44.
    发明授权
    Combined cycle power generating plant and method of supplying cooling steam for gas turbine in same 有权
    联合循环发电厂及其燃气轮机冷却蒸汽供应方法

    公开(公告)号:US06205762B1

    公开(公告)日:2001-03-27

    申请号:US09202452

    申请日:1998-12-15

    IPC分类号: F02G300

    摘要: A combined cycle power plant includes a combination of a gas turbine plant and steam turbine plant. The gas turbine cooling steam temperature is adjusted appropriately so that the gas turbine can be made of easily obtainable material. Steam supplied from the intermediate pressure evaporator is mixed into the cooling steam supply passage for supplying therethrough exhaust steam from the high pressure steam turbine into the gas turbine high temperature portion as cooling steam. Thus, cooling steam temperature is lowered without lowering of the entire efficiency, and material of less heat resistant ability becomes usable as material forming the gas turbine high temperature portion to be cooled. Thus, design and manufacture of the gas turbine may be satisfied by less expensive and easily obtainable material.

    摘要翻译: 联合循环发电厂包括燃气轮机厂和汽轮机厂的组合。 适当调整燃气轮机冷却水温度,使得燃气轮机可以由容易获得的材料制成。 从中压蒸发器供给的蒸汽被混合到冷却蒸汽供应通道中,用于将来自高压蒸汽轮机的排出蒸汽供给到作为冷却蒸汽的燃气轮机高温部分。 因此,冷却蒸汽温度降低而不降低整体效率,耐热能力差的材料可用作形成要冷却的燃气轮机高温部分的材料。 因此,燃气轮机的设计和制造可以通过较便宜且容易获得的材料来实现。

    Rotor shaft
    45.
    发明授权
    Rotor shaft 失效
    转子轴

    公开(公告)号:US5988890A

    公开(公告)日:1999-11-23

    申请号:US18731

    申请日:1998-02-04

    CPC分类号: F16C19/54 F16D3/72

    摘要: A rotor shaft that is supported by a deep groove ball bearing a radial load and a unidirectional thrust load, and by a cylindrical roller bearing for bearing a radial load. Also, a pretension applying means is provided for applying a pretension to the rotor shaft in the same direction as the thrust load which is borne by the deep groove ball bearing.

    摘要翻译: 转子轴由承受径向载荷和单向推力载荷的深沟球轴承,以及用于承受径向载荷的圆柱滚子轴承支撑。 而且,提供了一种预紧施加装置,用于沿与由深沟球轴承承载的推力载荷相同的方向向转子轴施加预紧力。

    Exhaust system for marine gas turbine
    46.
    发明授权
    Exhaust system for marine gas turbine 失效
    船用燃气轮机排气系统

    公开(公告)号:US5951246A

    公开(公告)日:1999-09-14

    申请号:US834277

    申请日:1997-04-15

    摘要: An exhaust system for a marine gas turbine may suppress a reduction of an efficiency even if a space therefor is small. In the exhaust system for a marine gas turbine, in which an end portion of an exhaust diffuser 2 is assembled into an exhaust chamber 1 connected with an upper exhaust eductor 4, the end portion of the exhaust diffuser 2 is disposed in the vicinity of an inlet of the exhaust chamber 1. An outlet 2a of the exhaust diffuser is slanted so that an upper portion of the outlet of an end of the exhaust diffuser is located upstream of a lower portion of the outlet. As a result, the exhaust gas may readily flow around and into the exhaust eductor 4.

    摘要翻译: 用于船用燃气轮机的排气系统即使其空间小也可以抑制效率的降低。 在用于船用燃气轮机的排气系统中,其中排气扩散器2的端部组装到与上排气喷射器4连接的排气室1中,排气扩散器2的端部设置在 排气扩散器的出口2a倾斜,使得排气扩散器的端部的出口的上部位于出口下部的上游。 结果,排气可能容易地流入排气喷射器4中。