公开(公告)号：US20090282833A1

公开(公告)日：2009-11-19

申请号：US12153020

申请日：2008-05-13

Applicant: William K. Hessler ,  Predrag Popovic ,  Charles Nyberg

Inventor： William K. Hessler ,  Predrag Popovic ,  Charles Nyberg

IPC: F02C1/00

CPC classification number: F23R3/06 ,  F23R3/002 ,  F23R3/26 ,  F23R2900/00012 ,  F23R2900/03042

Abstract: A combustor liner includes a forward end and an aft end, the aft end having a reduced diameter portion and a cooling and dilution sleeve overlying the reduced diameter portion thereby establishing a cooling plenum therebetween. A plurality of cooling and dilution air entry holes are formed in the cooling and dilution sleeve and a plurality of cooling and dilution air exit holes formed adjacent an aft edge of the liner such that, in use, cooling and dilution air flows through the cooling and dilution air entry holes, and through the plenum, exiting the cooling and dilution air exit holes, thereby cooling and dilution tuning the aft end of the combustor liner without having to remove the transition piece.

Abstract translation: 燃烧器衬套包括前端和后端，后端具有减小的直径部分，以及覆盖减小直径部分的冷却和稀释套筒，从而在它们之间建立冷却增压室。 在冷却和稀释套筒中形成多个冷却和稀释空气入口，以及在衬套的后边缘附近形成的多个冷却和稀释空气出口，使得在使用中冷却和稀释空气流过冷却和 稀释空气进入孔，并且通过增压室离开冷却和稀释空气出口，从而冷却和稀释调整燃烧器衬套的后端而不必去除过渡件。

公开(公告)号：US20090260340A1

公开(公告)日：2009-10-22

申请号：US12104952

申请日：2008-04-17

Applicant: William Hessler ,  Predrag Popovic

Inventor： William Hessler ,  Predrag Popovic

IPC: F23R3/26 ,  F02C1/00 ,  B21D53/00

CPC classification number: F23R3/06 ,  F23R3/26 ,  F23R2900/00016 ,  Y10T29/49346

Abstract: A combustor of a turbine, a method of retro-fitting a combustor of a turbine and a method of building a combustor of a turbine are each provided. The combustor includes a combustion chamber along which a dilution breach is defined, a casing perimetrically surrounding the combustion chamber so as to define an airflow between the casing and the combustion chamber, the airflow being configured to supply dilution air to the combustion chamber via the dilution breach, and an easy to adjust dilution airflow tuning part disposed on the casing and in communication with the airflow. The dilution airflow tuning part is configured to increase and/or decrease an available amount of the dilution air to be supplied to the combustion chamber.

Abstract translation: 涡轮机的燃烧器，涡轮机的燃烧器的回装方法以及建立涡轮机的燃烧器的方法。 燃烧器包括燃烧室，沿着该燃烧室限定稀释破裂，围绕燃烧室的壳体，以便在壳体和燃烧室之间限定气流，气流被配置成经由稀释液向燃烧室供应稀释空气 以及易于调节的稀释气流调节部件，其设置在壳体上并与气流连通。 稀释气流调节部分被配置为增加和/或减少要供应到燃烧室的稀释空气的可用量。

公开(公告)号：US20080060358A1

公开(公告)日：2008-03-13

申请号：US11531045

申请日：2006-09-12

Applicant: Predrag Popovic ,  Derrick Walter Simons ,  Krishna Kumar Venkataraman

Inventor： Predrag Popovic ,  Derrick Walter Simons ,  Krishna Kumar Venkataraman

IPC: F02C1/00

CPC classification number: F23R3/286 ,  F23R3/10

Abstract: Disclosed is a mixing hole arrangement for improving homogeneity of an air and fuel mixture in a combustor, the mixing hole arrangement comprising a plurality of mixing holes defined by a liner, wherein at least one of the plurality of mixing holes is a mixing hole that is at least one of sized and positioned to impede penetration of a fluid flow into a primary mixing zone located in a head end of the combustor.

Abstract translation: 公开了一种用于改善燃烧器中的空气和燃料混合物的均匀性的混合孔装置，该混合孔装置包括由衬套限定的多个混合孔，其中多个混合孔中的至少一个是混合孔， 至少一个尺寸和定位以阻止流体流入位于燃烧器头端的主混合区中。

公开(公告)号：US09181876B2

公开(公告)日：2015-11-10

申请号：US13343286

申请日：2012-01-04

Applicant: Predrag Popovic ,  William Francis Carnell, Jr. ,  Andrew Mitchell Rodwell

Inventor： Predrag Popovic ,  William Francis Carnell, Jr. ,  Andrew Mitchell Rodwell

IPC: F02C7/16 ,  F02C6/08 ,  F02C7/224

CPC classification number: F02C7/16 ,  F02C6/08 ,  F02C7/143 ,  F02C7/224 ,  F05D2260/20

Abstract: A gas turbine includes a compressor, a combustor downstream from the compressor and a heat transfer system, wherein the heat transfer system receives a compressed working fluid from the compressor. A fluid coupling between the heat transfer system and the combustor, wherein the fluid coupling receives the compressed working fluid from the heat transfer system. A conditioner in fluid communication with the compressor and a fluid coupling between the heat transfer system and the conditioner, wherein the fluid coupling receives a cooling media from the heat transfer system. A method for operating the gas turbine includes flowing a compressed working fluid from the compressor to the heat transfer system, transferring heat energy from the compressed working fluid to the heat transfer system, flowing the compressed working fluid from the heat transfer system to a combustor, and flowing a cooling media from the heat transfer system to a compressor inlet.

Abstract translation: 燃气轮机包括压缩机，压缩机下游的燃烧器和传热系统，其中传热系统从压缩机接收压缩的工作流体。 传热系统和燃烧器之间的流体耦合，其中流体联接器从传热系统接收压缩的工作流体。 与压缩机流体连通的调节器和传热系统和调节器之间的流体联接，其中流体联接器从热传递系统接收冷却介质。 用于操作燃气轮机的方法包括将压缩的工作流体从压缩机流动到传热系统，将热能从压缩的工作流体传递到传热系统，将压缩的工作流体从传热系统流到燃烧器， 并将冷却介质从传热系统流动到压缩机入口。

公开(公告)号：US20130025253A1

公开(公告)日：2013-01-31

申请号：US13191521

申请日：2011-07-27

Applicant: Rajani Kumar Akula ,  Predrag Popovic

Inventor： Rajani Kumar Akula ,  Predrag Popovic

IPC: F23R3/26 ,  F23J7/00

CPC classification number: F23R3/346 ,  F23R2900/00002 ,  F23R2900/03341 ,  Y02E20/344

Abstract: A method for reducing the amount of carbon monoxide and oxygen emissions in an oxyfuel hydrocarbon combustion system, comprising the steps of feeding defined amounts of hydrocarbon fuel and an oxidizer (e.g., air) to one or more combustors in the engine and igniting the mixture to form a first combustor exhaust stream; determining the amount of carbon monoxide present at the head end of a combustor in the initial combustor exhaust stream; identifying one or more target locations within the combustor at a point downstream from the first exhaust stream for injecting free hydrogen and a supplemental oxidizer; injecting hydrogen and the supplemental oxidizer into the combustor at specified downstream locations based on the amount of detected carbon monoxide; and injecting a diluent (e.g., CO2) into the combustor at a point further downstream in the combustor exhaust to control the exhaust temperature.

Abstract translation: 一种用于减少含氧燃料烃燃烧系统中的一氧化碳和氧气排放量的方法，包括以下步骤：将限定量的烃燃料和氧化剂（例如，空气）供给到发动机中的一个或多个燃烧器并点燃混合物 形成第一燃烧器排气流; 确定在初始燃烧器排气流中存在于燃烧器头端的一氧化碳的量; 识别所述燃烧器内在所述第一排气流下游的点处的一个或多个目标位置，用于喷射游离氢气和补充氧化剂; 基于检测到的一氧化碳的量，在特定的下游位置将氢气和补充氧化剂注入燃烧器; 以及在燃烧器排气口的更下游的点处将稀释剂（例如CO 2）注入到燃烧器中以控制排气温度。

公开(公告)号：US08156743B2

公开(公告)日：2012-04-17

申请号：US11418239

申请日：2006-05-04

Applicant: William Kirk Hessler ,  Alberto Jose Negroni ,  Predrag Popovic ,  Krishna Kumar Venkataraman

Inventor： William Kirk Hessler ,  Alberto Jose Negroni ,  Predrag Popovic ,  Krishna Kumar Venkataraman

IPC: F02C1/00

CPC classification number: F23R3/16

Abstract: Disclosed is an arrangement for expanding an annular fluid flow and a center fluid flow, comprising a combustor including a venturi and a centerbody, the centerbody including an upstream end and a downstream end, and a venturi throat defined by the venturi and disposed upstream of 0.19 inches downstream of the downstream end of the centerbody.

Abstract translation: 公开了一种用于扩展环形流体流和中心流体流的装置，其包括包括文丘里管和中心体的燃烧器，该中心体包括上游端和下游端，以及由文氏管限定的文丘里喉部并且设置在0.19 在中心体的下游端下游。

公开(公告)号：US20120036863A1

公开(公告)日：2012-02-16

申请号：US12856107

申请日：2010-08-13

Applicant: Joseph Kirzhner ,  Predrag Popovic ,  Roy Marshall Washam

Inventor： Joseph Kirzhner ,  Predrag Popovic ,  Roy Marshall Washam

IPC: F02C7/22 ,  F02C9/00

CPC classification number: F02C7/22 ,  F02C9/34 ,  F02C9/40

Abstract: In operating a gas turbine, there can be a difference between the desired heating value of the fuel and the actual needs of the fuel for sustainable combustion during various stages of the turbine operation. In one aspect, combustible lean limit operation of the gas turbine free of lean blow out is enabled by adjusting fuel-air-ratio of the fuel and fuel-air mixture properties, based on the operation requirements of the turbine and flammability of the fuel components.

Abstract translation: 在操作燃气轮机时，在涡轮机运行的各个阶段期间燃料的期望的热值与用于可持续燃烧的燃料的实际需要之间可能存在差异。 在一个方面，通过基于涡轮机的操作要求和燃料组分的可燃性调节燃料和燃料 - 空气混合物性质的燃料空气比，能够实现无烟气的燃气轮机的可燃稀薄限制操作 。

公开(公告)号：US08096133B2

公开(公告)日：2012-01-17

申请号：US12153020

申请日：2008-05-13

Applicant: William K. Hessler ,  Predrag Popovic ,  Charles Nyberg

Inventor： William K. Hessler ,  Predrag Popovic ,  Charles Nyberg

IPC: F02C1/00 ,  F02G3/00

CPC classification number: F23R3/06 ,  F23R3/002 ,  F23R3/26 ,  F23R2900/00012 ,  F23R2900/03042

Abstract: A combustor liner includes a forward end and an aft end, the aft end having a reduced diameter portion and a cooling and dilution sleeve overlying the reduced diameter portion thereby establishing a cooling plenum therebetween. A plurality of cooling and dilution air entry holes are formed in the cooling and dilution sleeve and a plurality of cooling and dilution air exit holes formed adjacent an aft edge of the liner such that, in use, cooling and dilution air flows through the cooling and dilution air entry holes, and through the plenum, exiting the cooling and dilution air exit holes, thereby cooling and dilution tuning the aft end of the combustor liner without having to remove the transition piece.

Abstract translation: 燃烧器衬套包括前端和后端，后端具有减小的直径部分，以及覆盖减小直径部分的冷却和稀释套筒，从而在它们之间建立冷却增压室。 在冷却和稀释套筒中形成多个冷却和稀释空气入口，以及在衬套的后边缘附近形成的多个冷却和稀释空气出口，使得在使用中冷却和稀释空气流过冷却和 稀释空气进入孔，并且通过增压室离开冷却和稀释空气出口，从而冷却和稀释调整燃烧器衬套的后端而不必去除过渡件。

公开(公告)号：US20100205970A1

公开(公告)日：2010-08-19

申请号：US12388855

申请日：2009-02-19

Applicant: William Kirk Hessler ,  Richard Gene Lowe ,  Predrag Popovic

Inventor： William Kirk Hessler ,  Richard Gene Lowe ,  Predrag Popovic

IPC: F02C7/22

CPC classification number: F23R3/343

Abstract: Provided are systems, methods, and apparatus providing secondary fuel nozzle assemblies. For example, a secondary fuel nozzle assembly can include a central portion having a proximal end and distal end, and defining a central passage therethrough, which can include at least one coiled tube extending through the central passage from the proximal end to the distal end; a flange having at least one main secondary fuel orifice in fluid communication with the central passage at the proximal end and at least one pilot orifice in fluid communication with the at least one coiled tube at the proximal end; and a tip portion having a proximal end and distal end, and defining at least one passage therethrough, which can be in fluid communication with the distal end of the at least one coiled tube and at least one orifice formed in the distal end of the tip portion.

Abstract translation: 提供了提供二次燃料喷嘴组件的系统，方法和装置。 例如，次级燃料喷嘴组件可以包括具有近端和远端的中心部分，并且限定穿过其中的中心通道，该中心通道可包括从近端延伸到远端延伸穿过中心通道的至少一个螺旋管; 具有至少一个主中间燃料孔口的凸缘，所述至少一个主次级燃料孔口在近端处与中心通道流体连通，以及至少一个引导孔口，其在近端与所述至少一个螺旋管道流体连通; 以及尖端部分，其具有近端和远端，并且限定穿过其中的至少一个通道，其可以与所述至少一个盘管的远端流体连通，并且形成在尖端的远端中的至少一个孔口 一部分。