公开(公告)号：US20140013754A1

公开(公告)日：2014-01-16

申请号：US14008219

申请日：2011-03-31

Applicant: Ilya Aleksandrovich Slobodyanskiy ,  Sergey Maskhutovich Khayrulin ,  Dmitry Vladlenovich Tretyakov ,  Steven Gumpangkum

Inventor： Ilya Aleksandrovich Slobodyanskiy ,  Sergey Maskhutovich Khayrulin ,  Dmitry Vladlenovich Tretyakov ,  Steven Gumpangkum

IPC: F23R3/40

CPC classification number: F01D9/023 ,  F02C3/305 ,  F02C5/11 ,  F05D2260/96 ,  F23L7/005 ,  F23M20/005 ,  F23R3/00 ,  F23R2900/00013 ,  Y02E20/16

Abstract: A power augmentation system for a gas turbine engine which may include a transition piece of a combustor and a steam manifold positioned about the transition piece. The transition piece may include a number of transition piece passageways therethrough and the steam manifold may include a number of manifold passageways therethrough. The manifold passageways align with the transition piece passageways.

Abstract translation: 一种用于燃气涡轮发动机的动力增强系统，其可以包括燃烧器的过渡件和围绕过渡件定位的蒸汽歧管。 过渡件可以包括许多通过其的过渡件通道，并且蒸汽歧管可以包括通过其中的多个歧管通道。 歧管通道与过渡件通道对准。

公开(公告)号：US20120192565A1

公开(公告)日：2012-08-02

申请号：US13195799

申请日：2011-08-01

Applicant: Dmitry Vladlenovich Tretyakov ,  Ilya Alexandrovich Slobodyanskiy ,  Sergey Victorovich Koshevets

Inventor： Dmitry Vladlenovich Tretyakov ,  Ilya Alexandrovich Slobodyanskiy ,  Sergey Victorovich Koshevets

IPC: F02C7/22 ,  B05B7/04

CPC classification number: F23R3/12 ,  F02C7/22 ,  F02K9/52 ,  F23D11/40 ,  F23D14/62 ,  F23D2900/14021 ,  F23D2900/14701 ,  F23R3/286 ,  F23R3/36

Abstract: According to various embodiments, a system includes a turbine fuel nozzle. The turbine fuel nozzle includes a first fuel passage extending to a downstream mixing region, a first air passage extending from an exterior of the turbine fuel nozzle to the downstream mixing region, and a second fuel passage extending into the first air passage upstream of the downstream mixing region.

Abstract translation: 根据各种实施例，系统包括涡轮燃料喷嘴。 涡轮燃料喷嘴包括延伸到下游混合区域的第一燃料通道，从涡轮燃料喷嘴的外部延伸到下游混合区域的第一空气通道，以及延伸到下游侧上游的第一空气通道的第二燃料通道 混合区域。

公开(公告)号：US20150075171A1

公开(公告)日：2015-03-19

申请号：US14389294

申请日：2012-03-29

Applicant: Alexander Nikolay Sokolov ,  Dmitry Vladlenovich Tretyakov ,  Ilya Aleksandrovich Slobodyanskiy

Inventor： Alexander Nikolay Sokolov ,  Dmitry Vladlenovich Tretyakov ,  Ilya Aleksandrovich Slobodyanskiy

IPC: F23R3/04 ,  F23R3/00

CPC classification number: F23R3/04 ,  F02C3/04 ,  F02C7/18 ,  F05D2240/35 ,  F23C7/02 ,  F23C9/08 ,  F23C2900/06041 ,  F23R3/002 ,  F23R3/283 ,  F23R3/286 ,  F23R2900/03041

Abstract: A turbomachine combustor assembly includes a combustor body, and a combustor liner arranged within the combustor body. The combustor liner defines a combustion chamber having a head end and a discharge end. A plurality of combustor nozzles are arranged in an annular array at the head end of the combustion chamber, and a fluid delivery nozzle is arranged substantially centrally within the annular array at the head end of the combustion chamber. The fluid delivery nozzle includes a first end portion that extends to a second end portion through a wall portion. The wall portion includes at least one combustion chamber outlet. The fluid delivery nozzle is configured to deliver a non-combustible fluid into the at least one of the plurality of combustor nozzles and the combustion chamber.

公开(公告)号：US20140238034A1

公开(公告)日：2014-08-28

申请号：US13983878

申请日：2011-11-17

Applicant: Ilya Aleksandrovich Slobodyanskiy ,  Sergey Aleksandrovich Stryapunin ,  Dmitry Vladlenovich Tretyakov

Inventor： Ilya Aleksandrovich Slobodyanskiy ,  Sergey Aleksandrovich Stryapunin ,  Dmitry Vladlenovich Tretyakov

IPC: F23R3/00

CPC classification number: F23R3/002 ,  F23R3/346

Abstract: A turbomachine combustor assembly includes a combustor body having a combustor outlet, and a combustion liner arranged within the combustor body. The combustion liner defines a combustion chamber. An injection nozzle is arranged within the combustor body upstream from the combustion chamber. The injection nozzle is configured and disposed to deliver a first fluid toward the combustion chamber. A fluid module is mounted to the combustor body downstream from the combustion chamber. The fluid module includes a fluid module body that defines a fluid zone, a first injector member mounted to the fluid module body and configured to deliver a second fluid into the fluid zone at a first orientation, and a second injector member mounted to the fluid module body and configured to deliver a third fluid into the fluid zone at a second orientation that is distinct from the first orientation.

Abstract translation: 涡轮机械燃烧器组件包括具有燃烧器出口的燃烧器主体和布置在燃烧器主体内的燃烧衬套。 燃烧衬套限定燃烧室。 在燃烧器主体的上游设置有喷射喷嘴。 注射喷嘴被配置和设置成将第一流体朝向燃烧室输送。 流体模块安装到燃烧器主体在燃烧室下游。 流体模块包括限定流体区域的流体模块主体，安装到流体模块主体并被配置成在第一取向处将第二流体输送到流体区域中的第一喷射器构件，以及安装到流体模块的第二喷射器构件 主体并且构造成在与第一方向不同的第二方向上将第三流体输送到流体区域中。

公开(公告)号：US20130086917A1

公开(公告)日：2013-04-11

申请号：US13253997

申请日：2011-10-06

Applicant: Ilya Aleksandrovich Slobodyanskiy ,  Gilbert Otto Kraemer ,  Leonid Yul'evich Ginesin ,  Dmitry Vladlenovich Tretyakov ,  Andrey Pavlovich Subbota

Inventor： Ilya Aleksandrovich Slobodyanskiy ,  Gilbert Otto Kraemer ,  Leonid Yul'evich Ginesin ,  Dmitry Vladlenovich Tretyakov ,  Andrey Pavlovich Subbota

IPC: F02C9/00

CPC classification number: F23R3/28 ,  F23C9/00 ,  F23C2202/30 ,  F23C2202/50 ,  F23R3/10

Abstract: A method for reducing the amount of carbon monoxide and oxygen emissions in a hydrocarbon combustor in a gas turbine engine by feeding hydrocarbon fuel and an oxidizer component into the head end of the combustor while also injecting substantially inert gas into the combustor with the fuel and oxidizer; forming a combustor exhaust stream that mixes with the recycle; cooling the combustor exhaust; detecting the amount of carbon monoxide and oxygen in the exhaust and adjusting the amount of fuel, oxidizer and inert gas feeds based on the detected amounts.

Abstract translation: 一种通过将碳氢化合物燃料和氧化剂组分供入燃烧器的头端来减少燃气涡轮发动机中的烃燃烧器中的一氧化碳和氧气排放量的方法，同时还将燃料和氧化剂基本上惰性的气体注入燃烧器 ; 形成与再循环混合的燃烧器排气流; 冷却燃烧器排气; 检测排气中的一氧化碳和氧气的量，并基于检测量调节燃料，氧化剂和惰性气体进料的量。