专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

131. 发明申请

US20060168965A1 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：US20060168965A1
公开(公告)日：2006-08-03
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： F23R3/42
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。

132. 发明申请

US20060162337A1 Counter Swirl Shear Mixer 有权
标题翻译：逆流搅拌机
公开(公告)号：US20060162337A1
公开(公告)日：2006-07-27
申请号：US10905907
申请日：2005-01-26
申请人： Peter Stuttaford , Yan Chen
发明人： Peter Stuttaford , Yan Chen
IPC分类号： F23R3/14
CPC分类号： F23R3/286 , F23R3/14 , F23R3/343
摘要： The present invention provides a mixer for a gas turbine combustor comprising a plurality of generally annular walls interconnected by at least a plurality of first vanes. The vanes are oriented at angles, so as to create a shear layer between the two flows. A fuel is then injected so as to penetrate the shear layer for enhanced mixing. The mixture passes through an extended mixing passage to provide sufficient time and distance for improved mixedness prior to ignition. Multiple embodiments of the present invention are disclosed comprising a plurality of first vanes and a plurality of first and second vanes.
摘要翻译：本发明提供了一种用于燃气轮机燃烧器的混合器，其包括由至少多个第一叶片互连的多个大体上环形的壁。叶片以角度定向，以便在两个流之间产生剪切层。然后喷射燃料以便穿透剪切层以增强混合。混合物通过延长的混合通道以提供足够的时间和距离，以提高点火之前的混合度。公开了本发明的多个实施例，其包括多个第一叶片和多个第一和第二叶片。

133. 发明申请

US20060150634A1 Apparatus and Method for Reducing Carbon Monoxide Emissions 有权
标题翻译：减少一氧化碳排放的装置和方法
公开(公告)号：US20060150634A1
公开(公告)日：2006-07-13
申请号：US10905497
申请日：2005-01-07
申请人： Khalid Oumejjoud , Peter Stuttaford , Yan Chen , Nuria Margarit-Bel , Stephen Jennings
发明人： Khalid Oumejjoud , Peter Stuttaford , Yan Chen , Nuria Margarit-Bel , Stephen Jennings
IPC分类号： F23R3/30
CPC分类号： F23C9/006 , F23R3/16 , F23R3/343
摘要： The present invention discloses an apparatus and method for reducing the carbon monoxide emissions emitted by a pilot injector of a gas turbine combustor. Multiple embodiments of a means for establishing a recirculation zone are disclosed whereby a portion of the fuel and air mixture from the pilot injector recirculates and a flame is held, thereby increasing the local reaction temperature at the desired location and lowering carbon monoxide emissions.
摘要翻译：本发明公开了一种用于减少由燃气轮机燃烧器的先导喷射器排出的一氧化碳排放的装置和方法。公开了用于建立再循环区的装置的多个实施例，其中来自先导喷射喷射器的燃料和空气混合物的一部分再循环并保持火焰，由此增加所需位置处的局部反应温度并降低一氧化碳排放。

134. 发明授权

US07000403B2 Primary fuel nozzle having dual fuel capability 失效
标题翻译：具有双重燃料能力的主燃料喷嘴
公开(公告)号：US07000403B2
公开(公告)日：2006-02-21
申请号：US10799970
申请日：2004-03-12
申请人： John Henriquez , Jacob McLeroy , Brian R. Mack , Vincent C. Martling
发明人： John Henriquez , Jacob McLeroy , Brian R. Mack , Vincent C. Martling
IPC分类号： F02C7/22 , F23R3/36
CPC分类号： F23R3/286 , F23R3/16 , F23R3/283 , F23R3/36 , F23R2900/00004
摘要： A fuel nozzle and gas turbine combustor capable of operating on multiple fuels with reduced carbon build-up to the fuel nozzle and adjacent combustor components is disclosed. The fuel nozzle incorporates a reconfigured gas fuel assembly and mixing tube to eliminate known areas of recirculation. Furthermore, the liquid fuel assembly includes reconfigured spray characteristics to further reduce droplet interaction with the mixing tube.
摘要翻译：公开了一种燃料喷嘴和燃气轮机燃烧器，其能够对燃料喷嘴和相邻的燃烧器部件的碳积累减少的多种燃料进行操作。燃料喷嘴包括重新配置的气体燃料组件和混合管，以消除已知的再循环区域。此外，液体燃料组件包括重新配置的喷雾特性，以进一步减少与混合管的液滴相互作用。

135. 发明授权

US06986254B2 Method of operating a flamesheet combustor 有权
标题翻译：操作火焰燃烧器的方法
公开(公告)号：US06986254B2
公开(公告)日：2006-01-17
申请号：US10437748
申请日：2003-05-14
申请人： Peter J. Stuttaford , Stephen Jennings , Yan Chen
发明人： Peter J. Stuttaford , Stephen Jennings , Yan Chen
IPC分类号： F02C7/228 , F02C9/26
CPC分类号： F23R3/286 , F23R3/343 , F23R2900/00014
摘要： A method of operating a gas turbine combustion system having reduced emissions and improved flame stability at multiple load conditions is disclosed. The improved combustion system accomplishes this through complete premixing, a plurality of fuel injector locations, combustor geometry, and precise three dimensional staging between fuel injectors. Axial, radial, and circumferential fuel staging is utilized including fuel injection proximate air swirlers. Furthermore, strong recirculation zones are established proximate the introduction of fuel and air premixture from different stages to the combustion zone. Fuel injection staging sequences are disclosed that create the conditions necessary to provide stable combustion and reduced emissions at multiple load conditions.
摘要翻译：公开了一种在多个负载条件下操作具有减少的排放和改善的火焰稳定性的燃气轮机燃烧系统的方法。改进的燃烧系统通过完全预混合，多个燃料喷射器位置，燃烧器几何形状和燃料喷射器之间的精确三维分级来实现。使用轴向，径向和周向燃料分级，包括靠近空气旋流器的燃料喷射。此外，在从不同阶段到燃烧区的燃料和空气预混物的引入附近建立强的再循环区域。公开了燃料喷射分级序列，其产生在多个负载条件下提供稳定燃烧和减少排放所必需的条件。

136. 发明授权

US06886346B2 Gas turbine fuel pilot nozzle 有权
标题翻译：燃气轮机燃油先导喷嘴
公开(公告)号：US06886346B2
公开(公告)日：2005-05-03
申请号：US10644385
申请日：2003-08-20
申请人： Peter A. Sobieski , Kelly Shawn Smith , Alan Lovelace , Hany Rizkalla
发明人： Peter A. Sobieski , Kelly Shawn Smith , Alan Lovelace , Hany Rizkalla
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F23R3/286 , F23R3/343
摘要： A pilot fuel nozzle configuration for use in a combustor is disclosed having a natural frequency outside the range of the operating frequencies of a gas turbine engine. Multiple embodiments are disclosed for the improved pilot fuel nozzle including configurations for newly manufactured nozzles, repair to existing pilot nozzles, as well as multiple natural frequency levels for the improved pilot fuel nozzle. The pilot fuel nozzle comprises an elongated housing, first and second flanges, and a nozzle tip, with the first flange fixed to the elongated housing at a first end and the nozzle tip fixed to the second end, opposite of the first end. The second flange is fixed along the elongated housing and is used for attaching the pilot fuel nozzle to a combustor. The present invention incorporates an increased wall thickness along at least a mid-span portion of the pilot nozzle to increase the stiffness and change the natural frequency.
摘要翻译：公开了一种用于燃烧器的先导燃料喷嘴构造，其具有在燃气涡轮发动机的工作频率范围之外的固有频率。公开了用于改进的引燃燃料喷嘴的多个实施例，其包括用于新制造的喷嘴的构造，对现有导向喷嘴的修理以及用于改进的引燃燃料喷嘴的多个固有频率水平。导向燃料喷嘴包括细长壳体，第一和第二凸缘以及喷嘴尖端，其中第一凸缘在第一端处固定到细长壳体，并且喷嘴尖端固定到与第一端相对的第二端。第二凸缘沿着细长壳体固定，并用于将引燃燃料喷嘴连接到燃烧器。本发明包括沿引导喷嘴的至少中跨部分增加的壁厚，以增加刚度并改变固有频率。

137. 发明授权

US06837052B2 Advanced fuel nozzle design with improved premixing 有权
标题翻译：先进的燃油喷嘴设计，改进了预混
公开(公告)号：US06837052B2
公开(公告)日：2005-01-04
申请号：US10389523
申请日：2003-03-14
申请人： Vincent C. Martling
发明人： Vincent C. Martling
IPC分类号： F23R3/28 , F23R3/34 , F23R3/20
CPC分类号： F23R3/346 , F23R3/283 , F23R3/286
摘要： A fully premixed secondary fuel nozzle assembly for use in a gas turbine combustor having multiple combustion chambers, in which the products of the premixed secondary fuel nozzle assembly are injected into the second combustion chamber for supporting a pilot flame and flame transfer between combustion chambers, is disclosed. The improvement includes the elimination of the pilot fuel circuit, which previously served to establish flame in the second combustion chamber. The secondary fuel nozzle assembly includes at least one first injector extending radially outward from the fuel nozzle body for injecting all fuel from the fuel nozzle to mix with compressed air prior to combustion. The first injector can include a plurality of tubes or an annular manifold circumferentially disposed about the nozzle body. Compressed air is drawn into the nozzle body and passes through holes in an injector plate at the tip region to provide cooling.

138. 发明申请

US20030233833A1 Pressure ram device on a gas turbine combustor 有权
标题翻译：燃气轮机燃烧器上的压力冲击装置
公开(公告)号：US20030233833A1
公开(公告)日：2003-12-25
申请号：US10302229
申请日：2002-11-22
申请人： Power Systems Mfg, LLC
发明人： Vincent Martling , Zenhua Xaio
IPC分类号： F23R003/30
CPC分类号： F23R3/286 , F23R3/005
摘要： A method for providing cooling air to the venturi and the combustion chamber in a low NOx emission combustor as used in a gas turbine engine that includes the steps of providing an annular air passage surrounding said combustion chamber and venturi where said cooling air under pressure enters the combustion chamber/venturi near the aft portion of the combustion chamber, passing the air along the combustion chamber, past the venturi where the air exits near the front portion of the convergent area of the venturi. The method prevents any channel/passage cooling air from being received into the combustion chamber, and at the same time, introduces the outlet of the cooling air, after the air has passed over the combustion chamber of the venturi and has been heated, back into the premix chamber thereby improving the efficiency of the combustor while reducing and lowering NOx emission in the combustion process. In an alternate embodiment, a combustion system is disclosed incorporating a shaped deflector to direct cooling air into a cooling passageway of a venturi. The deflector is configured to provide a cooling system with increased total pressure to increase overall cooling effectiveness.
摘要翻译：一种用于在燃气涡轮发动机中使用的低NOx排放燃烧器中的文丘里管和燃烧室的冷却空气的方法，该方法包括以下步骤：提供围绕所述燃烧室和文丘里管的环形空气通道，其中所述压力下的冷却空气进入在燃烧室的后部附近的燃烧室/文丘里管，沿着燃烧室使空气通过文丘里管，其中空气在文丘里管的会聚区域的前部附近离开。该方法防止任何通道/通道冷却空气被接收到燃烧室中，并且同时在空气已经经过文丘里管的燃烧室并且被加热之后引入冷却空气的出口从而提高了燃烧器的效率，同时降低和降低了燃烧过程中的NOx排放。在替代实施例中，公开了一种结合成形偏转器以将冷却空气引导到文氏管的冷却通道中的燃烧系统。偏转器被配置为提供具有增加的总压力的冷却系统以增加总体冷却效果。

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