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31. 发明授权

US07386980B2 Combustion liner with enhanced heat transfer 有权
标题翻译：具有增强热传递的燃烧衬管
公开(公告)号：US07386980B2
公开(公告)日：2008-06-17
申请号：US10906074
申请日：2005-02-02
申请人： Andrew Green , Peter Stuttaford , John Carella , Vamsi Duraibabu , Stephen Jennings
发明人： Andrew Green , Peter Stuttaford , John Carella , Vamsi Duraibabu , Stephen Jennings
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/42 , F23R3/005 , Y02T50/675
摘要： A combustion liner having enhanced heat transfer over at least a portion of the liner is disclosed. The combustion liner comprises, amongst other features, an outer surface wherein at least a region of the outer surface is textured in a substantially uniform pattern such that the surface area exposed to a passing cooling medium is increased, thereby increasing the heat transfer through the combustion liner. Multiple embodiments of textured patterns are also disclosed.
摘要翻译：公开了一种在衬套的至少一部分上具有增强的热传递的燃烧衬套。除了其它特征之外，燃烧衬套包括外表面，其中外表面的至少一个区域以基本均匀的图案纹理化，使得暴露于通过的冷却介质的表面积增加，从而增加通过燃烧的热传递衬垫。还公开了纹理图案的多个实施例。

32. 发明授权

US06742394B1 Gas turbine combustor hybrid dynamic-static probe 有权
标题翻译：燃气轮机燃烧室混合动静态探头
公开(公告)号：US06742394B1
公开(公告)日：2004-06-01
申请号：US10341573
申请日：2003-01-13
申请人： Peter Stuttaford , Andrew Green
发明人： Peter Stuttaford , Andrew Green
IPC分类号： G01L700
CPC分类号： F01D17/085 , F01D17/08 , F05D2270/301 , F05D2270/303
摘要： A removable instrumentation assembly and probe for use in simultaneously measuring dynamic pressure, at least one static pressure, and temperature for a gas turbine combustor. The instrumentation assembly allows combustor performance analysis as well as monitoring of component integrity through dynamic pressure fluctuations. The instrumentation assembly includes a probe having a plurality of passages, each connected to tubular conduits for measuring and recording respective pressures. In the preferred embodiment, dynamic pressures from within a combustion chamber are measured and recorded along with static pressures within the combustion chamber and outside of the combustion chamber, along with external air temperature.
摘要翻译：用于同时测量燃气轮机燃烧器的动态压力，至少一个静态压力和温度的可拆卸仪器组件和探头。仪表组件允许燃烧器性能分析以及通过动态压力波动监测部件完整性。仪器组件包括具有多个通道的探针，每个通道连接到用于测量和记录相应压力的管状导管。在优选实施例中，燃烧室内的动态压力与外部空气温度一起被测量并记录在燃烧室内和燃烧室外部的静压力。

33. 发明授权

US06508061B2 Diffuser combustor 有权
标题翻译：扩散器燃烧器
公开(公告)号：US06508061B2
公开(公告)日：2003-01-21
申请号：US09840991
申请日：2001-04-25
申请人： Peter Stuttaford
发明人： Peter Stuttaford
IPC分类号： F02C314
CPC分类号： F23R3/286 , F23R3/34
摘要： A combustion system for a power generating gas turbine engine which includes at least a combustion chamber with a annular fuel manifold at one end of the combustion chamber and a passageway having a narrow throat downstream of the fuel manifold whereby air passes around the fuel manifold and mixes with fuel and is diffused through the passageway into the burn zone defined in the combustion chamber in an ultimate location.
摘要翻译：一种用于发电燃气涡轮发动机的燃烧系统，其至少包括在燃烧室的一端处具有环形燃料歧管的燃烧室和在燃料歧管下游具有窄喉部的通道，由此空气绕过燃料歧管并混合并且通过通道扩散到在最终位置处限定在燃烧室中的燃烧区域中。

34. 发明授权

US09121279B2 Tunable transition duct side seals in a gas turbine engine 有权
标题翻译：燃气涡轮发动机中可调节的过渡管道侧密封
公开(公告)号：US09121279B2
公开(公告)日：2015-09-01
申请号：US12901084
申请日：2010-10-08
申请人： Sherman Craig Creighton , Charles Ellis , David John Henriquez , Peter Stuttaford
发明人： Sherman Craig Creighton , Charles Ellis , David John Henriquez , Peter Stuttaford
IPC分类号： F23R3/02 , F23R3/26 , F01D9/02 , F01D11/00
CPC分类号： F01D9/023 , F01D11/005 , F23R3/02 , F23R3/26 , F23R2900/00012
摘要： A system and method for tuning a gas turbine combustion system having a plurality of seals positioned between the combustion system and the turbine inlet is disclosed. The system and method provide ways of permitting a predetermined amount of compressed air to bypass the combustion system and enter the turbine so as to control emissions and dynamics of the combustion system. The seals contain a plurality of holes to meter airflow passing therethrough and are positioned such that they can be removed from the engine and modified to increase or decrease the amount of air passing therethrough.
摘要翻译：公开了一种用于调节具有位于燃烧系统和涡轮机入口之间的多个密封件的燃气轮机燃烧系统的系统和方法。该系统和方法提供允许预定量的压缩空气绕过燃烧系统并进入涡轮机以控制燃烧系统的排放和动力学的方式。密封件包含多个孔，用于测量通过其中的气流并且被定位成使得它们可以从发动机移除并被修改以增加或减少通过其中的空气量。

35. 发明申请

US20130255257A1 METHOD FOR CARBON CAPTURE IN A GAS TURBINE BASED POWER PLANT WITH A CARBON CAPTURE SYSTEM 审中-公开
标题翻译：采用碳捕集系统的燃气轮机发电厂碳捕获方法
公开(公告)号：US20130255257A1
公开(公告)日：2013-10-03
申请号：US13435581
申请日：2012-03-30
申请人： Gian-Luigi Agostinelli , Peter Stuttaford , Richard Carroni , Michal Bialkowski
发明人： Gian-Luigi Agostinelli , Peter Stuttaford , Richard Carroni , Michal Bialkowski
IPC分类号： F01K13/00 , F23D14/02 , F23L7/00 , F23J15/00
CPC分类号： C01B3/56 , B01D53/62 , B01D2251/404 , B01D2257/504 , B01D2258/0283 , C01B3/36 , C01B2203/025 , C01B2203/0283 , C01B2203/04 , C01B2203/0475 , C01B2203/06 , C01B2203/1241 , C01B2203/1276 , C01B2203/82 , C01B2203/86 , Y02C10/04 , Y02E20/326 , Y02P20/13 , Y02P20/152 , Y02P30/30
摘要： Disclosed herein is a system comprising a compressor in mechanical communication with a turbine; the compressor being operative to produce compressed air; a premixer; the premixer being operative to mix a fuel with the compressed air; a carbonator being located downstream of the premixer; the carbonator being operative to receive a mixture of carbon dioxide and syngas and to convert a metal oxide into a metal carbonate by reacting it with the carbon dioxide; a calciner; the calciner being operative to receive the metal carbonate from the carbonator; and to dissociate carbon dioxide from the metal carbonate; and a combustor; the combustor being located downstream of the carbonator; where the combustor is operative to combust syngas received from the carbonator.
摘要翻译：本文公开了一种包括与涡轮机械连通的压缩机的系统; 压缩机可操作以产生压缩空气; 预混料预混合器可操作以将燃料与压缩空气混合; 位于预混合器下游的碳酸化器; 碳酸化器可操作以接收二氧化碳和合成气的混合物，并通过使其与二氧化碳反应将金属氧化物转化为金属碳酸盐; 一台煅烧炉煅烧器可操作以从碳酸化器接收金属碳酸盐; 并从金属碳酸盐中分解二氧化碳; 和燃烧器; 所述燃烧器位于所述碳酸化器的下游; 其中燃烧器操作以燃烧从碳酸化器接收的合成气。

36. 发明授权

US08418474B2 Altering a natural frequency of a gas turbine transition duct 有权
标题翻译：改变燃气轮机过渡管的固有频率
公开(公告)号：US08418474B2
公开(公告)日：2013-04-16
申请号：US12240380
申请日：2008-09-29
申请人： Hany Rizkalla , Stephen W. Jorgensen , Peter Stuttaford
发明人： Hany Rizkalla , Stephen W. Jorgensen , Peter Stuttaford
IPC分类号： F02C7/20 , F02C1/00 , F02G3/00
CPC分类号： F01D9/023 , F05D2260/96
摘要： A transition duct having a thermally free aft frame and being capable of adjusting the natural frequency is disclosed. The aft frame is capable of permitting movement due to thermal gradients with the transition duct. The transition duct utilizes a spring plate located adjacent to an aft mounting bracket, where the spring plate, based on its thickness can either increase or decrease a frequency of the transition duct. Such an arrangement ensures that the transition duct natural frequency does not coincide with or cross other critical engine and/or combustor frequencies.
摘要翻译：公开了一种具有热释放后框架并且能够调节固有频率的过渡管道。后框架能够由于过渡管道的热梯度而允许移动。过渡管道使用位于后部安装支架附近的弹簧板，其中弹簧板基于其厚度可以增加或减小过渡管道的频率。这种布置确保了过渡管道固有频率不与其它关键的发动机和/或燃烧器频率重合或交叉。

37. 发明授权

US08151570B2 Transition duct cooling feed tubes 有权
标题翻译：过渡管冷却进料管
公开(公告)号：US08151570B2
公开(公告)日：2012-04-10
申请号：US11951790
申请日：2007-12-06
申请人： Stephen Jennings , Peter Stuttaford , Stephen W. Jorgensen
发明人： Stephen Jennings , Peter Stuttaford , Stephen W. Jorgensen
IPC分类号： F02C1/00
CPC分类号： F01D25/12 , F01D9/023 , F05D2260/20 , F05D2260/201
摘要： Embodiments for an apparatus and associated method for providing a cooling fluid to a gas turbine transition duct in order to lower the effective operating temperatures of the transition duct are disclosed. The transition duct has an inner liner and an impingement sleeve positioned radially outward with a passageway formed therebetween. The impingement sleeve has a plurality of openings where a portion of the openings each have a feed tube extending through the opening and into the passageway. The feed tubes are oriented at an angle relative to the impingement sleeve, such that an inlet to the feed tube is directed generally towards an oncoming flow of cooling fluid. The feed tubes direct a portion of the cooling fluid toward the inner liner and into the passageway for cooling of the transition duct.
摘要翻译：公开了用于向燃气轮机过渡管道提供冷却流体以降低过渡管道的有效操作温度的装置和相关方法的实施例。过渡管道具有内衬和径向向外定位的冲击套筒，其间形成有通道。冲击套筒具有多个开口，其中开口的一部分各自具有延伸穿过开口并进入通道的进料管。进料管相对于冲击套筒定向成一定角度，使得进料管的入口通常朝着迎面而来的冷却流体流动。进料管将一部分冷却流体引向内衬并进入通道以冷却过渡管道。

38. 发明申请

US20110270502A1 EMPLOYING FUEL PROPERTIES TO AUTO-TUNE A GAS TURBINE ENGINE 有权
标题翻译：使用燃油特性自动调节气体涡轮发动机
公开(公告)号：US20110270502A1
公开(公告)日：2011-11-03
申请号：US13086978
申请日：2011-04-14
申请人： Nicolas Demougeot , Donald Gauthier , Peter Stuttaford , Hany Rizkalla
发明人： Nicolas Demougeot , Donald Gauthier , Peter Stuttaford , Hany Rizkalla
IPC分类号： F02C9/26
CPC分类号： F02C7/224 , F02C9/28 , F02C9/40
摘要： A tuning process is provided for monitoring fuel properties of a fuel being consumed by a gas turbine (GT) engine, and for dynamically tuning the GT engine as a function of changes to the monitored fuel properties. Initially, readings are taken from the GT engine during a reference calibration, or commissioning, and utilized to calculate an initial-pressure-drop reference value. The tuning process during commercial operation takes post-calibration readings from the GT engine to calculate a fuel property parameter, which represents a heating value of the fuel. Specifically, the fuel property parameter is calculated by deriving a corrected-pressure-drop dynamic value as a function of pressure and temperature readings of the fuel at a point upstream of a combustor and pressure drops across fuel nozzles that introduce the fuel into the combustor, and solving a ratio of the dynamic value and the reference value.
摘要翻译：提供了一种调节过程，用于监测由燃气轮机（GT）发动机消耗的燃料的燃料性质，并且用于根据对所监测的燃料性质的变化来动态调节GT发动机。最初，在参考校准或调试期间从GT发动机获取读数，并用于计算初始压降参考值。商业运行过程中的调整过程需要GT发动机的后校准读数，以计算燃料特性参数，该参数代表燃料的热值。具体地说，燃料特性参数通过导出作为燃料在燃烧器上游一点上燃料的压力和温度读数的函数的校正压降动态值来计算，并且将燃料引入燃烧器的燃料喷嘴之间的压力下降，并求解动态值和参考值的比值。

39. 发明申请

US20110265487A1 Dynamically Auto-Tuning a Gas Turbine Engine 有权
标题翻译：动力自动调整燃气轮机发动机
公开(公告)号：US20110265487A1
公开(公告)日：2011-11-03
申请号：US13053910
申请日：2011-03-22
申请人： Donald Gauthier , Nicolas Demougeot , Peter Stuttaford , Hany Rizkalla
发明人： Donald Gauthier , Nicolas Demougeot , Peter Stuttaford , Hany Rizkalla
IPC分类号： F02C9/26
CPC分类号： F02C7/228 , F02C9/28 , F05D2270/301 , F05D2270/303 , F23N1/002 , F23N2037/02 , F23N2037/18 , F23N2037/28 , F23N2041/20 , F23R3/34 , F23R2900/00013
摘要： Tuning processes implemented by an auto-tune controller are provided for measuring and adjusting the combustion dynamics and the emission composition of a gas turbine (GT) engine via a tuning process. Initially, the tuning process includes monitoring parameters, such as combustion dynamics and emission composition. Upon determining that one or more of the monitored parameters exceed a critical value, these “out-of-tune” parameters are compared to a scanning order table. Upon comparison, the first out-of-tune parameter that is matched within the scanning order table is addressed. The first out-of-tune parameter is then plotted as overlaid slopes on respective graphs, where the graph represents a fuel-flow split. Typically, the slopes are plotted as a particular out-of-tune parameter against a particular fuel-flow split. The slopes for each graph are considered together by taking into account the combined impact on each out-of-tune parameter when a fuel-flow split is selected for adjustment.
摘要翻译：提供由自动调谐控制器实现的调谐过程，用于通过调谐过程测量和调整燃气轮机（GT）发动机的燃烧动力学和发射组成。最初，调谐过程包括监测参数，如燃烧动态和排放组成。在确定一个或多个所监视的参数超过临界值时，将这些“失调”参数与扫描顺序表进行比较。相比之下，寻址在扫描顺序表中匹配的第一个失调参数。然后将第一个失调参数作为叠加的斜率绘制在各个图上，其中图表示燃料流分流。通常，斜率被绘制为针对特定燃料流分流的特定失调参数。当选择燃料流分流进行调整时，通过考虑对每个失调参数的组合影响，每个曲线图的斜率被一起考虑。

40. 发明授权

US07299620B2 Tornado torch igniter 有权
标题翻译：龙卷风火炬点火器
公开(公告)号：US07299620B2
公开(公告)日：2007-11-27
申请号：US10880073
申请日：2004-06-29
申请人： Peter Stuttaford , John Henriquez , Paul Economo
发明人： Peter Stuttaford , John Henriquez , Paul Economo
IPC分类号： F02C7/26 , F02C7/264
CPC分类号： F02C7/266 , F05D2210/10 , F05D2210/11 , F05D2210/12
摘要： An ignition system having improved reliability for a gas turbine combustor is disclosed. The ignition system comprises an outer housing having at least one fuel passage and an electrode extending therethrough forming a generally annular passage for cooling air to pass to a mixing chamber. Fuel and air mix in the mixing chamber to form a combustible mixture that is ignited by the electrode. The outer housing further comprises a plurality of air swirl holes to effectively cool the walls of the mixing chamber as well as to provide improved flame stability.
摘要翻译：公开了一种具有改进燃气轮机燃烧器可靠性的点火系统。点火系统包括外壳，其具有至少一个燃料通道和延伸穿过的电极，形成大致环形的通道，用于冷却空气以通过混合室。燃料和空气在混合室中混合以形成被电极点燃的可燃混合物。外壳还包括多个空气旋转孔，以有效地冷却混合室的壁，并提供改进的火焰稳定性。

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