公开(公告)号：US09540942B2

公开(公告)日：2017-01-10

申请号：US13446707

申请日：2012-04-13

申请人： Xiaoqing Zheng ,  Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles

发明人： Xiaoqing Zheng ,  Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles

IPC分类号： F01D11/00

CPC分类号： F01D11/003 ,  F01D11/04 ,  F05D2220/31 ,  F05D2240/63 ,  F05D2260/6022

摘要： A shaft sealing system and method are disclosed for a high or intermediate pressure turbine section having a rotating member including a shaft and a stationary member surrounding the rotating member and defining a steam flow path. The shaft sealing system comprises at least one seal disposed about each of a first end and a second end of the shaft; and a connection line for conducting steam from the first turbine section to a downstream portion of the turbine. The downstream portion of the turbine is one of a low pressure section and a condenser, and has a lower pressure than both of the first turbine section and ambient pressure conditions.

摘要翻译： 公开了一种用于高压或中压涡轮机部分的轴密封系统和方法，其具有旋转构件，该旋转构件包括轴和围绕旋转构件并限定蒸汽流动路径的静止构件。 所述轴密封系统包括围绕所述轴的第一端和第二端中的每一个设置的至少一个密封件; 以及用于将蒸汽从第一涡轮部分传导到涡轮机的下游部分的连接管线。 涡轮机的下游部分是低压部分和冷凝器之一，并且具有比第一涡轮机部分和环境压力条件都低的压力。

公开(公告)号：US20130270775A1

公开(公告)日：2013-10-17

申请号：US13446696

申请日：2012-04-13

申请人： Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles ,  Xiaoqing Zheng

发明人： Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles ,  Xiaoqing Zheng

IPC分类号： F16J15/40

CPC分类号： F01D11/003 ,  F01D11/04 ,  F02C7/28 ,  F05D2220/31 ,  F05D2240/63 ,  F05D2260/6022

摘要： A shaft sealing system and method are disclosed for a low pressure turbine section having a rotating member including a shaft and a stationary member surrounding the rotating member and defining a steam flow path. The shaft sealing system comprises at least one seal disposed about each of a first end and a second end of the shaft; and a connection line for conducting steam from the first turbine section to a downstream portion of the turbine. The downstream portion of the turbine has a lower pressure than both of the first turbine section and ambient pressure conditions.

摘要翻译： 公开了一种用于低压涡轮机部分的轴密封系统和方法，所述低压涡轮部分具有旋转部件，所述旋转部件包括轴和围绕所述旋转部件并限定蒸汽流动路径的静止部件。 所述轴密封系统包括围绕所述轴的第一端和第二端中的每一个设置的至少一个密封件; 以及用于将蒸汽从第一涡轮部分传导到涡轮机的下游部分的连接管线。 涡轮机的下游部分的压力低于第一涡轮部分和环境压力条件。

公开(公告)号：US20110265488A1

公开(公告)日：2011-11-03

申请号：US12770065

申请日：2010-04-29

申请人： William James Lawson ,  Carlos Andres Rodriguez ,  Ilya Aleksandrovich Slobodyanskiy ,  Daniel Robert Coffey ,  Michael Wayne Blaisdell

发明人： William James Lawson ,  Carlos Andres Rodriguez ,  Ilya Aleksandrovich Slobodyanskiy ,  Daniel Robert Coffey ,  Michael Wayne Blaisdell

IPC分类号： F02C3/30

CPC分类号： F02C3/20 ,  F02C3/30 ,  F02C7/232 ,  F23L7/00 ,  F23R3/36 ,  F23R2900/00002

摘要： A method and system for gas turbine emissions management through delivery of a diluent fluid stream (steam, CO2, N2 etc) into a gas turbine combustion system while the gas turbine is operating on a conventional fuel such as light distillate oil or natural gas. The diluent injection system delivers required diluent-to-fuel ratios over the emissions compliance operating range of the gas turbine. The method for diluent injection is coupling the injection system to a gas turbine compressor discharge purge system, such that the diluent fluid is mixed with compressor discharge air. The mixed compressor discharge purge air and diluent stream are injected into the gas turbine combustor through a non-fueled combustion fuel nozzle passage to achieve emissions guarantee compliance.

摘要翻译： 一种用于燃气轮机排放管理的方法和系统，其通过在燃气轮机在诸如轻质蒸馏油或天然气的常规燃料上操作时将稀释液流（蒸汽，CO 2，N 2等）输送到燃气轮机燃烧系统中。 稀释剂注射系统在燃气轮机的排放顺从操作范围内提供所需的稀释剂与燃料比。 稀释剂注射的方法是将喷射系统耦合到燃气轮机压缩机排气净化系统，使得稀释液与压缩机排放空气混合。 混合压缩机排出净化空气和稀释剂流通过非燃料燃烧燃料喷嘴通道注入燃气轮机燃烧器，以实现排放保证符合性。

公开(公告)号：US20130272872A1

公开(公告)日：2013-10-17

申请号：US13446707

申请日：2012-04-13

申请人： Xiaoqing Zheng ,  Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles

发明人： Xiaoqing Zheng ,  Daniel Robert Coffey ,  Guoqiang Lu ,  John Richard Powers ,  Steven Paul Scarlata ,  Christopher David Suttles

IPC分类号： F01D11/04 ,  F01D11/00

CPC分类号： F01D11/003 ,  F01D11/04 ,  F05D2220/31 ,  F05D2240/63 ,  F05D2260/6022

摘要： A shaft sealing system and method are disclosed for a high or intermediate pressure turbine section having a rotating member including a shaft and a stationary member surrounding the rotating member and defining a steam flow path. The shaft sealing system comprises at least one seal disposed about each of a first end and a second end of the shaft; and a connection line for conducting steam from the first turbine section to a downstream portion of the turbine. The downstream portion of the turbine is one of a low pressure section and a condenser, and has a lower pressure than both of the first turbine section and ambient pressure conditions.

摘要翻译： 公开了一种用于高压或中压涡轮机部分的轴密封系统和方法，其具有旋转构件，该旋转构件包括轴和围绕旋转构件并限定蒸汽流动路径的静止构件。 所述轴密封系统包括围绕所述轴的第一端和第二端中的每一个设置的至少一个密封件; 以及用于将蒸汽从第一涡轮部分传导到涡轮机的下游部分的连接管线。 涡轮机的下游部分是低压部分和冷凝器之一，并且具有比第一涡轮机部分和环境压力条件都低的压力。

公开(公告)号：US20110036092A1

公开(公告)日：2011-02-17

申请号：US12539923

申请日：2009-08-12

申请人： William James Lawson ,  Daniel Robert Coffey ,  Erhan Karaca

发明人： William James Lawson ,  Daniel Robert Coffey ,  Erhan Karaca

IPC分类号： F02C9/40 ,  F02C7/22

CPC分类号： F23K5/002 ,  F23C2900/99011 ,  F23K2401/20 ,  F23R3/36 ,  F23R2900/00002

摘要： A fuel system comprises a fuel nozzle having a first port and a second port, a first manifold connected to the first port, and a first inert gas buffer portion disposed between the first manifold and a source of compressed air.

摘要翻译： 燃料系统包括具有第一端口和第二端口的燃料喷嘴，连接到第一端口的第一歧管以及设置在第一歧管和压缩空气源之间的第一惰性气体缓冲部分。