公开(公告)号：US08646278B2

公开(公告)日：2014-02-11

申请号：US13023226

申请日：2011-02-08

Applicant: Kwanwoo Kim ,  Geoffrey David Myers ,  Venkateswarlu Narra ,  Shiva Kumar Srinivasan

Inventor： Kwanwoo Kim ,  Geoffrey David Myers ,  Venkateswarlu Narra ,  Shiva Kumar Srinivasan

IPC: G01M15/14

CPC classification number: F23N5/16 ,  F23N2041/20 ,  F23R2900/00013

Abstract: A condition measurement apparatus is provided and includes a gas turbine engine combustor having an end cover, a liner defining a liner interior and a fuel nozzle communicative with the liner interior, the end cover being formed to separate a cold side thereof, which is a relatively low temperature environment, from a hot side thereof, which is a relatively high temperature environment in which the liner and the fuel nozzle are disposed, the combustor being formed to define a fuel flow path extending through piping disposed at the cold side of the end cover by which fuel is deliverable to the fuel nozzle, and a condition sensing device operably mounted on the piping.

Abstract translation: 提供了一种状态测量装置，其包括具有端盖的燃气涡轮发动机燃烧器，限定衬套内部的衬套和与衬里内部连通的燃料喷嘴，所述端盖形成为分离其冷侧，所述冷侧是相对的 低温环境，从设置有衬套和燃料喷嘴的较高温度环境的热侧起，形成燃烧器，以形成延伸穿过配置在端盖的冷侧的配管的燃料流路 燃料可以输送到燃料喷嘴，以及可操作地安装在管道上的条件感测装置。

公开(公告)号：US20110072826A1

公开(公告)日：2011-03-31

申请号：US12567534

申请日：2009-09-25

Applicant: Venkateswarlu Narra ,  Lewis Berkley Davis, Jr. ,  Fei Han ,  Kwanwoo Kim ,  Kapil Kumar Singh ,  Shiva Kumar Srinivasan ,  Krishna Kumar Venkataraman

Inventor： Venkateswarlu Narra ,  Lewis Berkley Davis, Jr. ,  Fei Han ,  Kwanwoo Kim ,  Kapil Kumar Singh ,  Shiva Kumar Srinivasan ,  Krishna Kumar Venkataraman

IPC: F02C7/228

CPC classification number: F02C7/228 ,  F02C9/26 ,  F05D2270/14

Abstract: In exemplary embodiments, a gas turbine system is provided. The gas turbine system can include a compressor configured to compress air and combustor cans in flow communication with the compressor, the combustor cans being configured to receive compressed air from the compressor and to combust a fuel stream. The gas turbine system can also include a multi-circuit manifold coupled to the combustor cans and configured to provide a split fuel stream from the fuel stream to the combustor cans.

Abstract translation: 在示例性实施例中，提供燃气轮机系统。 燃气轮机系统可以包括被配置为压缩与压缩机流动连通的空气和燃烧器罐的压缩机，燃烧器罐被构造成从压缩机接收压缩空气并燃烧燃料流。 燃气轮机系统还可以包括耦合到燃烧器罐的多回路歧管并且构造成提供从燃料流到燃烧器罐的分离燃料流。

公开(公告)号：US20120198857A1

公开(公告)日：2012-08-09

申请号：US13023226

申请日：2011-02-08

Applicant: KWANWOO KIM ,  GEOFFREY DAVID MYERS ,  VENKATESWARLU NARRA ,  SHIVA KUMAR SRINIVASAN

Inventor： KWANWOO KIM ,  GEOFFREY DAVID MYERS ,  VENKATESWARLU NARRA ,  SHIVA KUMAR SRINIVASAN

IPC: F02C7/20 ,  G01M15/14 ,  G01L11/04

CPC classification number: F23N5/16 ,  F23N2041/20 ,  F23R2900/00013

Abstract: A condition measurement apparatus is provided and includes a gas turbine engine combustor having an end cover, a liner defining a liner interior and a fuel nozzle communicative with the liner interior, the end cover being formed to separate a cold side thereof, which is a relatively low temperature environment, from a hot side thereof, which is a relatively high temperature environment in which the liner and the fuel nozzle are disposed, the combustor being formed to define a fuel flow path extending through piping disposed at the cold side of the end cover by which fuel is deliverable to the fuel nozzle, and a condition sensing device operably mounted on the piping.

Abstract translation: 提供了一种状态测量装置，其包括具有端盖的燃气涡轮发动机燃烧器，限定衬套内部的衬套和与衬里内部连通的燃料喷嘴，所述端盖形成为分离其冷侧，所述冷侧是相对的 低温环境，从设置有衬套和燃料喷嘴的较高温度环境的热侧起，形成燃烧器，以形成延伸穿过配置在端盖的冷侧的配管的燃料流路 燃料可以输送到燃料喷嘴，以及可操作地安装在管道上的条件感测装置。