专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20150075171A1 TURBOMACHINE COMBUSTOR ASSEMBLY 审中-公开
公开(公告)号：US20150075171A1
公开(公告)日：2015-03-19
申请号：US14389294
申请日：2012-03-29
申请人： Alexander Nikolay Sokolov , Dmitry Vladlenovich Tretyakov , Ilya Aleksandrovich Slobodyanskiy
发明人： Alexander Nikolay Sokolov , Dmitry Vladlenovich Tretyakov , Ilya Aleksandrovich Slobodyanskiy
IPC分类号： F23R3/04 , F23R3/00
CPC分类号： F23R3/04 , F02C3/04 , F02C7/18 , F05D2240/35 , F23C7/02 , F23C9/08 , F23C2900/06041 , F23R3/002 , F23R3/283 , F23R3/286 , F23R2900/03041
摘要： 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.

2. 发明申请

US20140013754A1 POWER AUGMENTATION SYSTEM WITH DYNAMICS DAMPING 审中-公开
标题翻译：动力补偿系统与动力阻尼
公开(公告)号：US20140013754A1
公开(公告)日：2014-01-16
申请号：US14008219
申请日：2011-03-31
申请人： Ilya Aleksandrovich Slobodyanskiy , Sergey Maskhutovich Khayrulin , Dmitry Vladlenovich Tretyakov , Steven Gumpangkum
发明人： Ilya Aleksandrovich Slobodyanskiy , Sergey Maskhutovich Khayrulin , Dmitry Vladlenovich Tretyakov , Steven Gumpangkum
IPC分类号： F23R3/40
CPC分类号： F01D9/023 , F02C3/305 , F02C5/11 , F05D2260/96 , F23L7/005 , F23M20/005 , F23R3/00 , F23R2900/00013 , Y02E20/16
摘要： 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.
摘要翻译：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。

3. 发明申请

US20140238034A1 TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE 审中-公开
标题翻译：涡轮搅拌机总成和操作涡轮机的方法
公开(公告)号：US20140238034A1
公开(公告)日：2014-08-28
申请号：US13983878
申请日：2011-11-17
申请人： Ilya Aleksandrovich Slobodyanskiy , Sergey Aleksandrovich Stryapunin , Dmitry Vladlenovich Tretyakov
发明人： Ilya Aleksandrovich Slobodyanskiy , Sergey Aleksandrovich Stryapunin , Dmitry Vladlenovich Tretyakov
IPC分类号： F23R3/00
CPC分类号： F23R3/002 , F23R3/346
摘要： 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.
摘要翻译：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。

4. 发明申请

US20130086917A1 APPARATUS FOR HEAD END DIRECT AIR INJECTION WITH ENHANCED MIXING CAPABILITIES 审中-公开
标题翻译：头部直接空气注射装置与增强混合能力的装置
公开(公告)号：US20130086917A1
公开(公告)日：2013-04-11
申请号：US13253997
申请日：2011-10-06
申请人： Ilya Aleksandrovich Slobodyanskiy , Gilbert Otto Kraemer , Leonid Yul'evich Ginesin , Dmitry Vladlenovich Tretyakov , Andrey Pavlovich Subbota
发明人： Ilya Aleksandrovich Slobodyanskiy , Gilbert Otto Kraemer , Leonid Yul'evich Ginesin , Dmitry Vladlenovich Tretyakov , Andrey Pavlovich Subbota
IPC分类号： F02C9/00
CPC分类号： F23R3/28 , F23C9/00 , F23C2202/30 , F23C2202/50 , F23R3/10
摘要： 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.
摘要翻译：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。

5. 发明申请

US20120291448A1 Flexible Combustor Fuel Nozzle 有权
标题翻译：柔性燃油喷嘴
公开(公告)号：US20120291448A1
公开(公告)日：2012-11-22
申请号：US13111036
申请日：2011-05-19
申请人： Ilya Aleksandrovich Slobodyanskiy , Joel Hall , Jesse Barton , Vijaykant Sadasivuni
发明人： Ilya Aleksandrovich Slobodyanskiy , Joel Hall , Jesse Barton , Vijaykant Sadasivuni
IPC分类号： F02C7/22
CPC分类号： F23R3/343 , F23L2900/07002 , F23R2900/00002
摘要： The present application provides a flexible combustor fuel nozzle. The flexible combustor fuel nozzle may include a main passage in communication with a source of natural gas and a source of low BTU fuel, a secondary passage surrounding the main passage and in communication with the source of low BTU fuel and a source of purge air, and a tertiary passage surrounding the secondary passage and in communication with the source of low BTU fuel, the source of purge air, and a source of diluent.
摘要翻译：本申请提供了一种柔性燃烧器燃料喷嘴。柔性燃烧器燃料喷嘴可以包括与天然气源和低BTU燃料源连通的主通道，围绕主通道并与低BTU燃料源和净化空气源连通的次级通道，以及围绕次级通道并与低BTU燃料源，吹扫空气源和稀释剂源连通的第三通道。

6. 发明申请

US20130327050A1 CONTROLLING FLAME STABILITY OF A GAS TURBINE GENERATOR 审中-公开
标题翻译：控制燃气涡轮发电机的火焰稳定性
公开(公告)号：US20130327050A1
公开(公告)日：2013-12-12
申请号：US13491087
申请日：2012-06-07
申请人： Ilya Aleksandrovich Slobodyanskiy , Michael John Hughes , Vijaykant Sadasivuni
发明人： Ilya Aleksandrovich Slobodyanskiy , Michael John Hughes , Vijaykant Sadasivuni
IPC分类号： F02C9/00 , F02C3/20 , F02C3/04
CPC分类号： F23L7/00 , F23C7/08 , F23L2900/07003 , F23N1/022 , F23N5/242 , F23N2021/12 , F23N2037/02 , F23N2041/20 , F23R3/26 , F23R2900/00013
摘要： A method and apparatus for controlling a flame stability at a gas turbine generator is disclosed. The method includes forming combustible mixtures at a plurality of fuel nozzles of a combustor of the gas turbine generator; altering an oxygen concentration of at least one of the combustible mixtures at a selected fuel nozzle of the plurality of fuel nozzles; and burning the combustible mixtures at the plurality of fuel nozzles to control the flame stability at the gas turbine generator.
摘要翻译：公开了一种用于控制燃气轮机发电机的火焰稳定性的方法和装置。该方法包括在燃气轮机发电机的燃烧器的多个燃料喷嘴处形成可燃混合物; 在所述多个燃料喷嘴的选定的燃料喷嘴处改变所述可燃混合物中的至少一种的氧浓度; 并在多个燃料喷嘴处燃烧可燃混合物以控制燃气轮机发电机的火焰稳定性。

7. 发明授权

US09127844B2 Fuel nozzle 有权
标题翻译：燃油喷嘴
公开(公告)号：US09127844B2
公开(公告)日：2015-09-08
申请号：US13196611
申请日：2011-08-02
申请人： Ilya Aleksandrovich Slobodyanskiy , William Francis Carnell, Jr.
发明人： Ilya Aleksandrovich Slobodyanskiy , William Francis Carnell, Jr.
IPC分类号： F23R3/14 , B21D53/00 , F23R3/26 , F23R3/36
CPC分类号： F23R3/36 , Y10T29/49323
摘要： A fuel nozzle is provided and includes a nozzle body defining first and second interior regions for providing a supply of first and second fluids, a collar defining a third interior region and radial slots permitting radial ingress of a third fluid to the third interior region and a nozzle tip interposed between the nozzle body and the collar. The nozzle tip defines an annular slot, first discrete passageways by which the first fluid is communicated from the first interior region to the annular slot, second discrete passageways by which the first fluid is communicated from the annular slot to the radial slots, and third discrete passageways by which the second fluid is communicated from the second interior region to the radial slots.
摘要翻译：提供燃料喷嘴并且包括限定用于提供第一和第二流体的第一和第二内部区域的喷嘴体，限定第三内部区域的轴环和允许第三流体径向进入第三内部区域的径向槽，以及喷嘴头插在喷嘴主体和轴环之间。喷嘴尖端限定一个环形槽，第一离散通道，第一流体通过该第一离散通道从第一内部区域连通到环形槽，第二离散通道使第一流体从环形槽连通到径向狭槽，第三离散通道第二流体通过该通道从第二内部区域连通到径向槽。

8. 发明授权

US08448442B2 Flexible combustor fuel nozzle 有权
标题翻译：柔性燃烧器燃油喷嘴
公开(公告)号：US08448442B2
公开(公告)日：2013-05-28
申请号：US13111036
申请日：2011-05-19
申请人： Ilya Aleksandrovich Slobodyanskiy , Joel Hall , Jesse Barton , Vijaykant Sadasivuni
发明人： Ilya Aleksandrovich Slobodyanskiy , Joel Hall , Jesse Barton , Vijaykant Sadasivuni
IPC分类号： F02C1/00
CPC分类号： F23R3/343 , F23L2900/07002 , F23R2900/00002
摘要： The present application provides a flexible combustor fuel nozzle. The flexible combustor fuel nozzle may include a main passage in communication with a source of natural gas and a source of low BTU fuel, a secondary passage surrounding the main passage and in communication with the source of low BTU fuel and a source of purge air, and a tertiary passage surrounding the secondary passage and in communication with the source of low BTU fuel, the source of purge air, and a source of diluent.
摘要翻译：本申请提供了一种柔性燃烧器燃料喷嘴。柔性燃烧器燃料喷嘴可以包括与天然气源和低BTU燃料源连通的主通道，围绕主通道并与低BTU燃料源和净化空气源连通的次级通道，以及围绕次级通道并与低BTU燃料源，吹扫空气源和稀释剂源连通的第三通道。

9. 发明授权

US08334011B1 Method for regenerating oxide coatings on gas turbine components by addition of oxygen into SEGR system 有权
标题翻译：通过在SEGR系统中加入氧来再生燃气轮机部件上的氧化物涂层的方法
公开(公告)号：US08334011B1
公开(公告)日：2012-12-18
申请号：US13209591
申请日：2011-08-15
申请人： Gilbert Otto Kraemer , Ilya Aleksandrovich Slobodyanskiy
发明人： Gilbert Otto Kraemer , Ilya Aleksandrovich Slobodyanskiy
IPC分类号： C23C16/52 , C23C14/54 , B05D3/00 , B05D7/22 , B05C13/00 , B41N1/24
CPC分类号： F01D5/288 , F01D5/005 , F01D5/286 , F02C3/34 , F02C7/30
摘要： A method for regenerating oxide coatings on selected gas turbine engine components in situ, comprising the steps of defining an exhaust gas recirculation (EGR) loop for the gas turbine engine, identifying one or more target locations within the EGR loop for purposes of monitoring the level of metal oxide degradation occurring in key gas turbine engine components over time, collecting and analyzing data corresponding to the level of metal oxide degradation with a fixed time period at each of the target locations, determining which ones of the target locations within the EGR loop require oxide regeneration using injected oxygen, and controlling the amount of oxygen injection at the target locations sufficient to regenerate the metal oxide coatings to desired levels.
摘要翻译：一种用于在原位选择的燃气涡轮发动机部件上再生氧化物涂层的方法，其包括以下步骤：为燃气涡轮发动机定义废气再循环（EGR）回路，识别EGR回路内的一个或多个目标位置，以便监控水平随着时间的推移，在关键燃气轮机发动机部件中发生金属氧化物降解，在每个目标位置处以固定的时间段收集和分析对应于金属氧化物退化水平的数据，确定EGR环路内的目标位置中哪一个需要使用注入的氧气进行氧化物再生，并且控制在足以使金属氧化物涂层再生到期望水平的目标位置处的氧气注入量。

10. 发明申请

US20110265488A1 ALTERNATE METHOD FOR DILUENT INJECTION FOR GAS TURBINE NOx EMISSIONS CONTROL 审中-公开
标题翻译：用于气体涡轮NOx排放控制的备用注射方法
公开(公告)号：US20110265488A1
公开(公告)日：2011-11-03
申请号：US12770065
申请日：2010-04-29
申请人： William James Lawson , Carlos Andres Rodriguez , Ilya Aleksandrovich Slobodyanskiy , Daniel Robert Coffey , Michael Wayne Blaisdell
发明人： William James Lawson , Carlos Andres Rodriguez , Ilya Aleksandrovich Slobodyanskiy , Daniel Robert Coffey , Michael Wayne Blaisdell
IPC分类号： F02C3/30
CPC分类号： F02C3/20 , F02C3/30 , F02C7/232 , F23L7/00 , F23R3/36 , F23R2900/00002
摘要： A method and system for gas turbine emissions management through delivery of a diluent fluid stream (steam, CO2, N2 etc) into a gas turbine combustion system while the gas turbine is operating on a conventional fuel such as light distillate oil or natural gas. The diluent injection system delivers required diluent-to-fuel ratios over the emissions compliance operating range of the gas turbine. The method for diluent injection is coupling the injection system to a gas turbine compressor discharge purge system, such that the diluent fluid is mixed with compressor discharge air. The mixed compressor discharge purge air and diluent stream are injected into the gas turbine combustor through a non-fueled combustion fuel nozzle passage to achieve emissions guarantee compliance.
摘要翻译：一种用于燃气轮机排放管理的方法和系统，其通过在燃气轮机在诸如轻质蒸馏油或天然气的常规燃料上操作时将稀释液流（蒸汽，CO 2，N 2等）输送到燃气轮机燃烧系统中。稀释剂注射系统在燃气轮机的排放顺从操作范围内提供所需的稀释剂与燃料比。稀释剂注射的方法是将喷射系统耦合到燃气轮机压缩机排气净化系统，使得稀释液与压缩机排放空气混合。混合压缩机排出净化空气和稀释剂流通过非燃料燃烧燃料喷嘴通道注入燃气轮机燃烧器，以实现排放保证符合性。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式