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1.发明申请SYSTEMS AND APPARATUS RELATING TO DOWNSTREAM FUEL AND AIR INJECTION IN GAS TURBINES 有权与天然气涡轮机相关的下游燃料和空气注入系统和装置公开(公告)号：US20140260269A1
公开(公告)日：2014-09-18
申请号：US13836503
申请日：2013-03-15
Applicant: General Electric Company
IPC: F23R3/28
Abstract: A gas turbine engine that includes: a combustor coupled to a turbine and a downstream injection system that includes two injection stages, a first stage and a second stage, positioned within an interior flowpath, wherein the first stage comprises an axial position that is aft of the primary air and fuel injection system and the second stage comprising an axial position that is aft of the first stage. Each of the first stage and the second stage include a plurality of circumferentially spaced injectors, each injector of which is configured to inject air and fuel into a flow through the interior flowpath. The first stage and the second stage have a configuration that limits a fuel injected at the second stage to less than 50% of a fuel injected at the first stage.
Abstract translation: 一种燃气涡轮发动机，其包括：联接到涡轮机的燃烧器和下游喷射系统，其包括位于内部流路内的两个喷射级，第一级和第二级，其中所述第一级包括位于后方的轴向位置 主空气和燃料喷射系统以及第二级包括位于第一级后部的轴向位置。 第一阶段和第二阶段中的每一个包括多个周向间隔开的喷射器，其每个喷射器构造成将空气和燃料喷射到通过内部流动路径的流中。 第一阶段和第二阶段具有将在第二阶段喷射的燃料限制为小于第一阶段喷射的燃料的50％的构造。
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2.发明申请公开(公告)号：US20140260303A1
公开(公告)日：2014-09-18
申请号：US13837186
申请日：2013-03-15
Applicant: GENERAL ELECTRIC COMPANY
IPC: F23R3/34
Abstract: A method for use in a gas turbine engine. The method includes the steps of: configuring a downstream injection system within the interior flowpath that includes two injection stages, a first stage and a second stage, wherein the first stage and the second stage are each axially spaced from the other; and circumferentially positioning the injectors of the first stage and the second stage based on: a) a characteristic of an anticipated combustion flow occurring just upstream of the first stage during a mode of operation; and b) the characteristic of an anticipated combustion flow just downstream of the second stage given an anticipated effect of the air and fuel injection from the first stage and the second stage.
Abstract translation: 一种在燃气轮机中使用的方法。 该方法包括以下步骤：在内部流路内配置下游喷射系统，该下游喷射系统包括两个喷射级，第一级和第二级，其中第一级和第二级各自轴向间隔开另一级; 并且基于以下步骤周期性地定位所述第一级和第二级的喷射器：a）在操作模式期间正好在所述第一级的上游发生的预期燃烧流的特性; 以及b）考虑到来自第一阶段和第二阶段的空气和燃料喷射的预期效果，正好在第二阶段下游的预期燃烧流的特征。
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3.发明授权Systems and apparatus relating to downstream fuel and air injection in gas turbines 有权与燃气轮机中的下游燃料和空气喷射有关的系统和设备公开(公告)号：US09528439B2
公开(公告)日：2016-12-27
申请号：US13836703
申请日：2013-03-15
Applicant: General Electric Company
Abstract: A gas turbine engine that includes: an interior flowpath defined through a combustor and a turbine; an aft frame forming an interface between the combustor the turbine, the aft frame comprising a rigid structural member that circumscribes the interior flowpath, wherein the aft frame includes an inner wall that defines an outboard boundary of the interior flowpath; a circumferentially extending fuel plenum formed through the aft frame; and outlet ports formed through the inner wall of the aft frame. The outlet ports may be configured to connect the fuel plenum to the interior flowpath.
Abstract translation: 一种燃气涡轮发动机，包括：通过燃烧器和涡轮限定的内部流路; 后框架，其形成在所述燃烧器与所述涡轮机之间的界面，所述后框架包括限定所述内部流路的刚性结构构件，其中所述后框架包括限定所述内部流路的外侧边界的内壁; 通过后框架形成的周向延伸的燃料增压室; 以及通过后框架的内壁形成的出口。 出口端口可以被配置成将燃料增压室连接到内部流路。
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Patent Agency Ranking
4.发明授权公开(公告)号：US09482434B2
公开(公告)日：2016-11-01
申请号：US13837186
申请日：2013-03-15
Applicant: General Electric Company
Abstract: A method for use in a gas turbine engine. The method includes the steps of: configuring a downstream injection system within the interior flowpath that includes two injection stages, a first stage and a second stage, wherein the first stage and the second stage are each axially spaced from the other; and circumferentially positioning the injectors of the first stage and the second stage based on: a) a characteristic of an anticipated combustion flow occurring just upstream of the first stage during a mode of operation; and b) the characteristic of an anticipated combustion flow just downstream of the second stage given an anticipated effect of the air and fuel injection from the first stage and the second stage.
Abstract translation: 一种在燃气轮机中使用的方法。 该方法包括以下步骤：在内部流路内配置下游喷射系统，该下游喷射系统包括两个喷射级，第一级和第二级，其中第一级和第二级各自轴向间隔开另一级; 并且基于以下步骤周期性地定位所述第一级和第二级的喷射器：a）在操作模式期间正好在所述第一级的上游发生的预期燃烧流的特性; 以及b）考虑到来自第一阶段和第二阶段的空气和燃料喷射的预期效果，正好在第二阶段下游的预期燃烧流的特征。
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5.发明申请SYSTEMS AND APPARATUS RELATING TO DOWNSTREAM FUEL AND AIR INJECTION IN GAS TURBINES 有权与天然气涡轮机相关的下游燃料和空气注入系统和装置公开(公告)号：US20140260270A1
公开(公告)日：2014-09-18
申请号：US13836703
申请日：2013-03-15
Applicant: General Electric Company
IPC: F02C3/14
Abstract: A gas turbine engine that includes: an interior flowpath defined through a combustor and a turbine; an aft frame forming an interface between the combustor the turbine, the aft frame comprising a rigid structural member that circumscribes the interior flowpath, wherein the aft frame includes an inner wall that defines an outboard boundary of the interior flowpath; a circumferentially extending fuel plenum formed through the aft frame; and outlet ports formed through the inner wall of the aft frame. The outlet ports may be configured to connect the fuel plenum to the interior flowpath.
Abstract translation: 一种燃气涡轮发动机，包括：通过燃烧器和涡轮限定的内部流路; 后框架，其形成在所述燃烧器与所述涡轮机之间的界面，所述后框架包括限定所述内部流路的刚性结构构件，其中所述后框架包括限定所述内部流路的外侧边界的内壁; 通过后框架形成的周向延伸的燃料增压室; 以及通过后框架的内壁形成的出口。 出口端口可以被配置成将燃料增压室连接到内部流路。
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公开(公告)号：US09714768B2
公开(公告)日：2017-07-25
申请号：US13836503
申请日：2013-03-15
Applicant: General Electric Company
Abstract: A gas turbine engine that includes: a combustor coupled to a turbine and a downstream injection system that includes two injection stages, a first stage and a second stage, positioned within an interior flowpath, wherein the first stage comprises an axial position that is aft of the primary air and fuel injection system and the second stage comprising an axial position that is aft of the first stage. Each of the first stage and the second stage include a plurality of circumferentially spaced injectors, each injector of which is configured to inject air and fuel into a flow through the interior flowpath. The first stage and the second stage have a configuration that limits a fuel injected at the second stage to less than 50% of a fuel injected at the first stage.
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7.发明授权Systems and apparatus relating to downstream fuel and air injection in gas turbines 有权与燃气轮机中的下游燃料和空气喷射有关的系统和设备公开(公告)号：US09435541B2
公开(公告)日：2016-09-06
申请号：US13836938
申请日：2013-03-15
Applicant: General Electric Company
Abstract: A gas turbine that includes: a combustor coupled to a turbine that together define an interior flowpath, the interior flowpath extending aftward about a longitudinal axis from a primary air and fuel injection system that defines a forward end, through an interface at which the combustor connects to the turbine, and through a row of stator blades in the turbine that defines an aft end; and a downstream injection system that includes two injection stages, a first stage and a second stage, that are axially spaced along the longitudinal axis of the interior flowpath. The first stage and the second stage each includes multiple injectors configured to inject an air and fuel mixture into the interior flowpath.
Abstract translation: 一种燃气轮机，包括：联接到涡轮机的燃烧器，其共同限定内部流动路径，所述内部流动路径从形成前端的一次空气和燃料喷射系统的纵轴线向后延伸，所述主要空气和燃料喷射系统通过燃烧器连接的界面 并且通过涡轮机中定义一个后端的一排定子叶片; 以及下游喷射系统，其包括沿着内部流路的纵向轴线间隔开的两个喷射级，第一级和第二级。 第一阶段和第二阶段各自包括被配置为将空气和燃料混合物注入到内部流动路径中的多个注射器。
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8.发明申请SYSTEMS AND APPARATUS RELATING TO DOWNSTREAM FUEL AND AIR INJECTION IN GAS TURBINES 有权与天然气涡轮机相关的下游燃料和空气注入系统和装置公开(公告)号：US20140260262A1
公开(公告)日：2014-09-18
申请号：US13836938
申请日：2013-03-15
Applicant: GENERAL ELECTRIC COMPANY
IPC: F23R3/34
Abstract: A gas turbine that includes: a combustor coupled to a turbine that together define an interior flowpath, the interior flowpath extending aftward about a longitudinal axis from a primary air and fuel injection system that defines a forward end, through an interface at which the combustor connects to the turbine, and through a row of stator blades in the turbine that defines an aft end; and a downstream injection system that includes two injection stages, a first stage and a second stage, that are axially spaced along the longitudinal axis of the interior flowpath. The first stage and the second stage each includes multiple injectors configured to inject an air and fuel mixture into the interior flowpath.
Abstract translation: 一种燃气轮机，包括：联接到涡轮机的燃烧器，其共同限定内部流动路径，所述内部流动路径从形成前端的一次空气和燃料喷射系统的纵轴线向后延伸，所述主要空气和燃料喷射系统通过燃烧器连接的界面 并且通过涡轮机中定义一个后端的一排定子叶片; 以及下游喷射系统，其包括沿着内部流路的纵向轴线间隔开的两个喷射级，第一级和第二级。 第一阶段和第二阶段各自包括被配置为将空气和燃料混合物注入到内部流动路径中的多个注射器。
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