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    • 55. 发明授权
    • Transitional region for a secondary combustion chamber of a gas turbine
    • 燃气轮机二次燃烧室的过渡区域
    • US09097119B2
    • 2015-08-04
    • US13668274
    • 2012-11-04
    • ALSTOM Technology Ltd
    • Thomas Heinz-SchwarzmaierMarc WidmerSelma ZahirovicPaul Marlow
    • F01D9/00F01D9/02F01D11/00F02C6/00
    • F01D9/023F01D11/005F02C6/003F05D2240/127
    • A gas turbine is provided having a secondary combustion chamber and a first guide vane row of a low-pressure turbine, the row being arranged directly downstream of the chamber. The radially outer boundary of the secondary combustion chamber is formed by at least one outer wall segment, which is secured on at least one support element arranged radially outwardly. The flow path of the hot gases is bounded radially outwardly, in the region of the guide vane row, by an outer platform which is secured at least indirectly on at least one guide vane support. A substantially radially extending gap-shaped cavity having a width in the range of 1-25 mm in the axial direction in the inlet region is arranged between the wall segment and the outer platform. At least one step element, which reduces the width by at least 10% in at least one step, extending substantially perpendicularly to the direction of flow of the hot gas in the cavity, is arranged in the inlet region.
    • 提供一种燃气轮机,其具有二次燃烧室和低压涡轮机的第一导向叶片排,该排直接设置在室的下游。 二次燃烧室的径向外边界由至少一个外壁段形成,该外壁段固定在径向向外布置的至少一个支撑元件上。 热气体的流动路径在导向叶片排的区域中径向向外限定外部平台,该外部平台至少间接地固定在至少一个导向叶片支撑件上。 在壁部段和外部平台之间布置有在入口区域中在轴向方向上具有1-25mm范围内的宽度的大致径向延伸的间隙形腔。 在入口区域中布置有至少一个步进元件,其在基本垂直于空腔中的热气体的流动方向的至少一个步骤中将至少10%的宽度减小。
    • 57. 发明授权
    • Method for operating a gas turbine
    • 操作燃气轮机的方法
    • US09091211B2
    • 2015-07-28
    • US13346840
    • 2012-01-10
    • Klaus-Dieter LiedtkeMengbin ZhangAysegul KirecciUlf Schirmeister
    • Klaus-Dieter LiedtkeMengbin ZhangAysegul KirecciUlf Schirmeister
    • F02C9/28F02C9/26F23R3/28
    • F02C9/263F02C9/28F05D2270/091F23R3/28
    • A method for operating a gas turbine includes supplying fuel via at least one control valve regulated using an open-loop control system based on a predetermined load setpoint value. A valve stroke control command (scmd) is generated based on a fuel mass flow control command (mcmd) using a mass flow-valve stroke converter. The valve stroke control command (scmd) is compared with a valve stroke limit value (min{slim1, slim2}) using a variable pressure regulator. A load limit value is generated if the valve stroke control command (scmd) exceeds the valve stroke limit value (min{slim1, slim2}) to reduce the load setpoint value. Operation of the gas turbine is stabilized using a low limit value (xlim) of a pressure drop ratio (x), wherein the pressure drop ratio (x) is a quotient of a pressure drop (dp) which occurs at the control valve and of a pressure (p1) upstream of the control valve.
    • 一种用于操作燃气轮机的方法包括通过基于预定的负载设定值通过使用开环控制系统调节的至少一个控制阀供应燃料。 基于使用质量流量阀行程转换器的燃料质量流量控制指令(mcmd)来生成阀行程控制指令(scmd)。 使用可变压力调节器将阀行程控制命令(scmd)与阀行程限制值(min {slim1,slim2})进行比较。 如果阀行程控制命令(scmd)超过阀行程极限值(min {slim1,slim2})以减小负载设定值,则会产生负载极限值。 使用压降比(x)的下限值(xlim)使燃气轮机的运转稳定,其中压降比(x)是在控制阀处发生的压降(dp)的商, 控制阀上游的压力(p1)。