IMPURITY DETECTION IN COMBUSTOR SYSTEMS
    1.
    发明申请
    IMPURITY DETECTION IN COMBUSTOR SYSTEMS 有权
    COMBUSTOR系统中的检测

    公开(公告)号:US20110138813A1

    公开(公告)日:2011-06-16

    申请号:US12635742

    申请日:2009-12-11

    IPC分类号: F02C7/22 F01N11/00 G01N7/00

    CPC分类号: G01N21/72 F23N5/082

    摘要: The present invention discloses a combustor system and method of measuring impurities in the combustion system. The combustion system includes an up-stream fuel injection point; a down-stream turbine combustor; a flame zone in the turbine combustor comprising a plurality of axial sub-zones; an optical port assembly configured to obtain a non-axial, direct, optical view of at least one of the plurality of axial sub-zones, and an impurity detection system in optical communication with the optical port assembly.

    摘要翻译: 本发明公开了一种在燃烧系统中测量杂质的燃烧器系统和方法。 燃烧系统包括上游燃料喷射点; 下游涡轮机燃烧器; 涡轮机燃烧器中的火焰区域包括多个轴向子区域; 光学端口组件,被配置为获得所述多个轴向子区域中的至少一个的非轴向,直接光学视图,以及与所述光学端口组件光学连通的杂质检测系统。

    Impurity detection in combustor systems
    2.
    发明授权
    Impurity detection in combustor systems 有权
    燃烧器系统中的杂质检测

    公开(公告)号:US08505303B2

    公开(公告)日:2013-08-13

    申请号:US12635742

    申请日:2009-12-11

    IPC分类号: F02C7/22

    CPC分类号: G01N21/72 F23N5/082

    摘要: The present invention discloses a combustor system and method of measuring impurities in the combustion system. The combustion system includes an up-stream fuel injection point; a down-stream turbine combustor; a flame zone in the turbine combustor comprising a plurality of axial sub-zones; an optical port assembly configured to obtain a non-axial, direct, optical view of at least one of the plurality of axial sub-zones, and an impurity detection system in optical communication with the optical port assembly.

    摘要翻译: 本发明公开了一种在燃烧系统中测量杂质的燃烧器系统和方法。 燃烧系统包括上游燃料喷射点; 下游涡轮机燃烧器; 涡轮机燃烧器中的火焰区域包括多个轴向子区域; 光学端口组件,被配置为获得所述多个轴向子区域中的至少一个的非轴向,直接光学视图,以及与所述光学端口组件光学连通的杂质检测系统。

    High speed carburetion system for compressed air assisted injection
    3.
    发明授权
    High speed carburetion system for compressed air assisted injection 失效
    用于压缩空气辅助注射的高速化油系统

    公开(公告)号:US06578562B1

    公开(公告)日:2003-06-17

    申请号:US09518578

    申请日:2000-03-03

    IPC分类号: F02B1300

    摘要: An internal combustion engine having a crankcase, a cylinder connected to the crankcase, a compressed air assisted fuel injection system connected between the crankcase and the cylinder, and a reciprocating piston head located in the cylinder. The improvement comprises a fuel delivery system having two carburetors that switch delivery of fuel to two different locations based upon the speed of the engine. The system uses an accumulator with piston ported reflected compression wave delivery of scavenged compressed air to deliver fuel at a wide open throttle position.

    摘要翻译: 具有曲轴箱,连接到曲轴箱的气缸,连接在曲轴箱和气缸之间的压缩空气辅助燃料喷射系统和位于气缸中的往复活塞头的内燃机。 该改进包括具有两个化油器的燃料输送系统,该化油器基于发动机的速度将燃料的输送切换到两个不同的位置。 该系统使用具有活塞端口的反射压缩波输送被清除的压缩空气的蓄能器,以在较宽的打开节气门位置输送燃料。

    Systems and methods for exhaust gas recirculation (EGR) for turbine engines
    6.
    发明授权
    Systems and methods for exhaust gas recirculation (EGR) for turbine engines 有权
    用于涡轮发动机的废气再循环(EGR)的系统和方法

    公开(公告)号:US08051638B2

    公开(公告)日:2011-11-08

    申请号:US12033183

    申请日:2008-02-19

    IPC分类号: F02C7/08 F02C6/00 F02C9/00

    CPC分类号: F02C1/08 F02C6/18 Y02E20/16

    摘要: Systems and methods may be provided for exhaust gas recirculation. The systems and methods may include receiving, via an intake section, inlet air at an input of a compressor, generating compressed air at the compressor using the received inlet air, and providing the compressed air from the compressor to a combustor, where the combustor produces combustion involving the compressed air and fuel. The systems and methods may also include receiving combustion products associated with the combustion at a turbine component, where the turbine component releases exhaust gases, and recirculating at least a portion of the exhaust gases to the intake section via a recirculation line, where the recirculated exhaust gases raise a temperature of the inlet air.

    摘要翻译: 可以提供用于废气再循环的系统和方法。 系统和方法可以包括经由进气部分接收在压缩机的输入处的入口空气,使用接收的入口空气在压缩机处产生压缩空气,以及将压缩空气从压缩机提供给燃烧器,其中燃烧器产生 涉及压缩空气和燃料的燃烧。 系统和方法还可以包括接收与涡轮机部件处的燃烧相关联的燃烧产物,其中涡轮机部件释放废气,并且经由再循环管线将废气的至少一部分再循环到进气部分,其中再循环的排气 气体升高入口空气的温度。

    Systems and Methods for Exhaust Gas Recirculation (EGR) for Turbine Engines
    7.
    发明申请
    Systems and Methods for Exhaust Gas Recirculation (EGR) for Turbine Engines 有权
    涡轮发动机排气再循环系统和方法(EGR)

    公开(公告)号:US20090205334A1

    公开(公告)日:2009-08-20

    申请号:US12033183

    申请日:2008-02-19

    IPC分类号: F02B33/44

    CPC分类号: F02C1/08 F02C6/18 Y02E20/16

    摘要: Systems and methods may be provided for exhaust gas recirculation. The systems and methods may include receiving, via an intake section, inlet air at an input of a compressor, generating compressed air at the compressor using the received inlet air, and providing the compressed air from the compressor to a combustor, where the combustor produces combustion involving the compressed air and fuel. The systems and methods may also include receiving combustion products associated with the combustion at a turbine component, where the turbine component releases exhaust gases, and recirculating at least a portion of the exhaust gases to the intake section via a recirculation line, where the recirculated exhaust gases raise a temperature of the inlet air.

    摘要翻译: 可以提供用于废气再循环的系统和方法。 系统和方法可以包括经由进气部分接收在压缩机的输入处的入口空气,使用接收的入口空气在压缩机处产生压缩空气,以及将压缩空气从压缩机提供给燃烧器,其中燃烧器产生 涉及压缩空气和燃料的燃烧。 系统和方法还可以包括接收与涡轮机部件处的燃烧相关联的燃烧产物,其中涡轮机部件释放废气,并且经由再循环管线将废气的至少一部分再循环到进气部分,其中再循环的排气 气体升高入口空气的温度。

    Injection port for internal combustion engine
    8.
    发明授权
    Injection port for internal combustion engine 失效
    内燃机喷油口

    公开(公告)号:US06564759B2

    公开(公告)日:2003-05-20

    申请号:US09941379

    申请日:2001-08-28

    申请人: Samer Aljabari

    发明人: Samer Aljabari

    IPC分类号: F02B7502

    摘要: An internal combustion engine having a cylinder with a piston movement area; a piston movably mounted in the cylinder; an ignition system connected to the cylinder; and a fuel delivery system connected to the cylinder. The fuel delivery system has a combined fuel and air injection port extending into the cylinder. The injection port has an end at the piston movement area with a top surface and a different shaped bottom. The bottom surface has an inwardly tapering shape to form a bottom portion of the end of the injection port with a generally semi-conical shape.

    摘要翻译: 一种具有活塞运动区域的气缸的内燃机; 活塞可移动地安装在气缸中; 连接到气缸的点火系统; 以及连接到气缸的燃料输送系统。 燃料输送系统具有延伸到气缸中的组合的燃料和空气喷射端口。 注射口在活塞运动区域具有一个端部,顶部表面和不同形状的底部。 底面具有向内渐缩的形状,以形成具有大致半圆锥形状的注射口端部的底部。

    Two cycle engine having a decompression slot
    9.
    发明授权
    Two cycle engine having a decompression slot 失效
    具有减压槽的两循环发动机

    公开(公告)号:US5799635A

    公开(公告)日:1998-09-01

    申请号:US898049

    申请日:1997-07-22

    申请人: Samer Aljabari

    发明人: Samer Aljabari

    摘要: A two-cycle engine having an enclosed crankcase assembly and a cylinder assembly. A cylinder wall is sized to sealingly cooperate with the piston as it reciprocates relative thereto. The cylinder assembly is provided with an exhaust port in a first plane and a pair of diametrically opposed recessed transfer ports positioned in a second plane along the cylinder axis. The cylinder assembly is provided with a pair of decompression slots each formed in the cylinder wall in communication with one of the opposed transfer ports and extending towards the combustion chamber end of the cylinder assembly. The decompression slots having a circumferential width W which is substantially constant and a radially measured depth D which varies generally linearly from a maximum depth at the intersection of the decompression slot and the transfer port to a minimum depth at the uppermost end of the decompression slot.

    摘要翻译: 具有封闭式曲轴箱组件和气缸组件的双冲程发动机。 气缸壁的尺寸设计成当活塞相对于其往复运动时与活塞密封配合。 气缸组件设置有位于第一平面中的排气口和沿着气缸轴线定位在第二平面中的一对直径相对的凹入传送口。 气缸组件设置有一对减压槽,每个减压槽形成在气缸壁中,与相对的传送口中的一个连通并朝向气缸组件的燃烧室端延伸。 减压槽具有基本恒定的周向宽度W和径向测量的深度D,该深度D大体上线性地从解压缩槽和传送端口的交点处的最大深度线性变化到解压缩槽的最上端处的最小深度。