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1. 发明授权

US09296038B2 Method and apparatus for swaged liquid injector spoke 有权
标题翻译：冲压液体注射器辐条的方法和装置
公开(公告)号：US09296038B2
公开(公告)日：2016-03-29
申请号：US13560192
申请日：2012-07-27
申请人： Alexander Ilich Krichever , Mario Eugene Abreu , Norm Turoff , John Frederick Lockyer , Christopher Zdzislaw Twardochleb , David Marc Stansel
发明人： Alexander Ilich Krichever , Mario Eugene Abreu , Norm Turoff , John Frederick Lockyer , Christopher Zdzislaw Twardochleb , David Marc Stansel
IPC分类号： F23R3/20 , F23R3/28 , F23R3/34 , F02C7/22 , F23R3/14 , B21K25/00
CPC分类号： B21K25/00 , F02C7/22 , F23R3/14 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00017 , Y10T29/49231
摘要： A liquid fuel injection spoke for a gas turbine engine. The liquid fuel injection spoke may include an inlet end and an outlet end. The liquid fuel injection spoke may further include a head located at the inlet end and a stem extending along a longitudinal axis from the head to the outlet end. The stem may define a fluid passageway therein. The head may include a cavity with an inner wall. The inner wall may include an annular protrusion.
摘要翻译：液体燃料喷射器用于燃气涡轮发动机。液体燃料喷射轮辐可以包括入口端和出口端。液体燃料喷射轮辐还可以包括位于入口端的头部和沿着从头部到出口端的纵向轴线延伸的杆。杆可以在其中限定流体通道。头部可以包括具有内壁的空腔。内壁可以包括环形突起。

2. 发明授权

US09151227B2 End-fed liquid fuel gallery for a gas turbine fuel injector 有权
标题翻译：用于燃气轮机燃料喷射器的末端馈送液体燃料库
公开(公告)号：US09151227B2
公开(公告)日：2015-10-06
申请号：US12943064
申请日：2010-11-10
申请人： John Frederick Lockyer , Christopher Zdzislaw Twardochleb , Mario Eugene Abreu
发明人： John Frederick Lockyer , Christopher Zdzislaw Twardochleb , Mario Eugene Abreu
IPC分类号： F23R3/28 , F02C7/22 , F02K9/52 , F02C7/224 , F23R3/14 , F23R3/30
CPC分类号： F02C7/222 , F02C7/224 , F02K9/52 , F23R3/14 , F23R3/283 , F23R3/30
摘要： A fuel injector for a gas turbine engine may include an injector housing extending along a longitudinal axis and configured to be fluidly coupled to a combustor of the turbine engine. The fuel injector may also include a flow path for a fuel air mixture to the combustor extending longitudinally within the injector housing, and a gallery for liquid fuel encircling the flow path. The gallery may include a plurality of fuel spokes that are configured to deliver liquid fuel from the gallery to the flow path. The gallery may extend from a feed end to a terminal end that overlaps the feed end. The feed end may be a region where liquid fuel enters the gallery and the terminal end may be a region where the gallery terminates.
摘要翻译：用于燃气涡轮发动机的燃料喷射器可以包括沿着纵向轴线延伸并被配置为流体地联接到涡轮发动机的燃烧器的喷射器壳体。燃料喷射器还可以包括用于在喷射器壳体内纵向延伸到燃烧器的燃料空气混合物的流动路径，以及用于环绕流动路径的液体燃料的通道。画廊可以包括多个燃料辐条，其被构造成将液体燃料从画廊输送到流动路径。画廊可以从馈送端延伸到与馈送端重叠的终端。进料端可以是液体燃料进入料仓的区域，而终端可以是储存库终止的区域。

3. 发明申请

US20120111016A1 END-FED LIQUID FUEL GALLERY FOR A GAS TURBINE FUEL INJECTOR 有权
标题翻译：燃气涡轮燃油喷射器的终端液体燃料图库
公开(公告)号：US20120111016A1
公开(公告)日：2012-05-10
申请号：US12943064
申请日：2010-11-10
申请人： John Frederick Lockyer , Christopher Zdzislaw Twardochleb , Mario Eugene Abreu
发明人： John Frederick Lockyer , Christopher Zdzislaw Twardochleb , Mario Eugene Abreu
IPC分类号： F02C7/22
CPC分类号： F02C7/222 , F02C7/224 , F02K9/52 , F23R3/14 , F23R3/283 , F23R3/30
摘要： A fuel injector for a gas turbine engine may include an injector housing extending along a longitudinal axis and configured to be fluidly coupled to a combustor of the turbine engine. The fuel injector may also include a flow path for a fuel air mixture to the combustor extending longitudinally within the injector housing, and a gallery for liquid fuel encircling the flow path. The gallery may include a plurality of fuel spokes that are configured to deliver liquid fuel from the gallery to the flow path. The gallery may extend from a feed end to a terminal end that overlaps the feed end. The feed end may be a region where liquid fuel enters the gallery and the terminal end may be a region where the gallery terminates.
摘要翻译：用于燃气涡轮发动机的燃料喷射器可以包括沿着纵向轴线延伸并被配置为流体地联接到涡轮发动机的燃烧器的喷射器壳体。燃料喷射器还可以包括用于在喷射器壳体内纵向延伸到燃烧器的燃料空气混合物的流动路径，以及用于环绕流动路径的液体燃料的通道。画廊可以包括多个燃料辐条，其被构造成将液体燃料从画廊输送到流动路径。画廊可以从馈送端延伸到与馈送端重叠的终端。进料端可以是液体燃料进入料仓的区域，而终端可以是储存库终止的区域。

4. 发明授权

US07966832B1 Combustor 有权
公开(公告)号：US07966832B1
公开(公告)日：2011-06-28
申请号：US11024070
申请日：2004-12-29
申请人： John Frederick Lockyer , Stuart Alexander Greenwood
发明人： John Frederick Lockyer , Stuart Alexander Greenwood
IPC分类号： F02C7/20 , F23R3/50
CPC分类号： F23R3/002 , F23R2900/00017
摘要： A combustor includes a first wall, a second wall, an injector grommet, a combustor longitudinal axis, and a connection assembly indirectly connecting the first wall to the second wall. A portion of the injector grommet is disposed within a groove of the connection assembly.

5. 发明申请

US20130168472A1 METHOD AND APPARATUS FOR SWAGED LIQUID INJECTOR SPOKE 有权
标题翻译：改变液体注射器的方法和装置
公开(公告)号：US20130168472A1
公开(公告)日：2013-07-04
申请号：US13560192
申请日：2012-07-27
申请人： Alexander Ilich Krichever , Mario Eugene Abreu , Norm Turoff , John Frederick Lockyer , Christopher Zdzislaw Twardochleb , David Marc Stansel
发明人： Alexander Ilich Krichever , Mario Eugene Abreu , Norm Turoff , John Frederick Lockyer , Christopher Zdzislaw Twardochleb , David Marc Stansel
IPC分类号： F02M63/00 , B21K3/00
CPC分类号： B21K25/00 , F02C7/22 , F23R3/14 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00017 , Y10T29/49231
摘要： A liquid fuel injection spoke for a gas turbine engine. The liquid fuel injection spoke may include an inlet end and an outlet end. The liquid fuel injection spoke may further include a head located at the inlet end and a stem extending along a longitudinal axis from the head to the outlet end. The stem may define a fluid passageway therein. The head may include a cavity with an inner wall. The inner wall may include an annular protrusion.
摘要翻译：液体燃料喷射器用于燃气涡轮发动机。液体燃料喷射轮辐可以包括入口端和出口端。液体燃料喷射轮辐还可以包括位于入口端的头部和沿着从头部到出口端的纵向轴线延伸的杆。杆可以在其中限定流体通道。头部可以包括具有内壁的空腔。内壁可以包括环形突起。

6. 发明授权

US08099940B2 Low cross-talk gas turbine fuel injector 有权
标题翻译：低排气燃气轮机燃油喷射器
公开(公告)号：US08099940B2
公开(公告)日：2012-01-24
申请号：US12314904
申请日：2008-12-18
申请人： Christopher Zdzislaw Twardochleb , John Frederick Lockyer , Mario Eugene Abreu
发明人： Christopher Zdzislaw Twardochleb , John Frederick Lockyer , Mario Eugene Abreu
IPC分类号： F02G3/00
CPC分类号： F23R3/286 , F23R3/343 , F23R3/36
摘要： A pilot assembly for a fuel injector of a gas turbine engine may include a longitudinal passageway having an outlet end. A mass flow in the longitudinal passageway may generally flow towards the outlet end during operation of the engine. The pilot assembly may also include a liquid fuel nozzle that is positioned to direct a mixture of liquid fuel and air near the outlet end, and a compressed air inlet that is configured to direct air compressed by a compressor of the engine to a compressor discharge pressure into the longitudinal passageway without a substantial loss of pressure. The longitudinal passageway may also include a flow restriction section. The flow restriction section may be a narrowed section of the longitudinal passageway, in which an upstream side of the flow restriction section may have compressed air at substantially the compressor discharge pressure and a downstream side may have air at a lower pressure and a higher velocity. The pilot assembly may further include a nozzle for injecting one of assist air or gaseous fuel into the longitudinal passageway. The nozzle may be positioned at the flow restriction section or on an upstream side of the flow restriction section to reduce cross-talk.
摘要翻译：用于燃气涡轮发动机的燃料喷射器的导向组件可以包括具有出口端的纵向通道。在发动机操作期间，纵向通道中的质量流通常可以朝向出口端流动。导向组件还可以包括液体燃料喷嘴，该液体燃料喷嘴被定位成引导出口端附近的液体燃料和空气的混合物;以及压缩空气入口，其构造成将由发动机的压缩机压缩的空气引导到压缩机排气压力进入纵向通道而没有显着的压力损失。纵向通道还可以包括流动限制部分。流量限制部分可以是纵向通道的狭窄部分，其中流动限制部分的上游侧可以具有基本上压缩机排出压力的压缩空气，并且下游侧可以具有较低压力和较高速度的空气。驾驶员组件还可以包括用于将辅助空气或气体燃料中的一种喷射到纵向通道中的喷嘴。喷嘴可以位于流动限制部分处或流动限制部分的上游侧，以减少串扰。

7. 发明申请

US20110030377A1 COMBUSTOR 有权
公开(公告)号：US20110030377A1
公开(公告)日：2011-02-10
申请号：US12907128
申请日：2010-10-19
申请人： John Frederick LOCKYER , Stuart Alexander GREENWOOD
发明人： John Frederick LOCKYER , Stuart Alexander GREENWOOD
IPC分类号： F02C3/14
CPC分类号： F23R3/002 , F23R2900/00017
摘要： A combustor includes a first wall, a second wall, an injector grommet, a combustor longitudinal axis, and a connection assembly indirectly connecting the first wall to the second wall. A portion of the injector grommet is disposed within a groove of the connection assembly.
摘要翻译：燃烧器包括第一壁，第二壁，喷射器护环，燃烧器纵向轴线以及将第一壁间接地连接到第二壁的连接组件。注射器护环的一部分设置在连接组件的凹槽内。

8. 发明申请

US20100154424A1 Low cross-talk gas turbine fuel injector 有权
标题翻译：低排气燃气轮机燃油喷射器
公开(公告)号：US20100154424A1
公开(公告)日：2010-06-24
申请号：US12314904
申请日：2008-12-18
申请人： Christopher Zdzislaw Twardochleb , John Frederick Lockyer , Mario Eugene Abreu
发明人： Christopher Zdzislaw Twardochleb , John Frederick Lockyer , Mario Eugene Abreu
IPC分类号： F02C7/22 , B05B7/06
CPC分类号： F23R3/286 , F23R3/343 , F23R3/36
摘要： A pilot assembly for a fuel injector of a gas turbine engine may include a longitudinal passageway having an outlet end. A mass flow in the longitudinal passageway may generally flow towards the outlet end during operation of the engine. The pilot assembly may also include a liquid fuel nozzle that is positioned to direct a mixture of liquid fuel and air near the outlet end, and a compressed air inlet that is configured to direct air compressed by a compressor of the engine to a compressor discharge pressure into the longitudinal passageway without a substantial loss of pressure. The longitudinal passageway may also include a flow restriction section. The flow restriction section may be a narrowed section of the longitudinal passageway, in which an upstream side of the flow restriction section may have compressed air at substantially the compressor discharge pressure and a downstream side may have air at a lower pressure and a higher velocity. The pilot assembly may further include a nozzle for injecting one of assist air or gaseous fuel into the longitudinal passageway. The nozzle may be positioned at the flow restriction section or on an upstream side of the flow restriction section to reduce cross-talk.
摘要翻译：用于燃气涡轮发动机的燃料喷射器的导向组件可以包括具有出口端的纵向通道。在发动机操作期间，纵向通道中的质量流通常可以朝向出口端流动。导向组件还可以包括液体燃料喷嘴，该液体燃料喷嘴被定位成引导出口端附近的液体燃料和空气的混合物;以及压缩空气入口，其构造成将由发动机的压缩机压缩的空气引导到压缩机排气压力进入纵向通道而没有显着的压力损失。纵向通道还可以包括流动限制部分。流量限制部分可以是纵向通道的狭窄部分，其中流动限制部分的上游侧可以具有基本上压缩机排出压力的压缩空气，并且下游侧可以具有较低压力和较高速度的空气。驾驶员组件还可以包括用于将辅助空气或气体燃料中的一种喷射到纵向通道中的喷嘴。喷嘴可以位于流动限制部分处或流动限制部分的上游侧，以减少串扰。

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