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公开(公告)号：US07093837B2
公开(公告)日：2006-08-22
申请号：US10255896
申请日：2002-09-26
CPC分类号： F23R3/60
摘要： An improved turbine spring clip seal for directing gases to be mixed with fuel in a combustor basket. The turbine spring clip seal is composed of inner and outer housings and a center sealing member disposed between the inner and outer housings. The center sealing member is flexible and prevents a fluid, such as air, from leaking through the seal. In operation, the center sealing member flexes and is sealed against the outer housing by a pressure differential that is created by the relatively higher pressure on the inner housing side and the relatively lower pressure on the outer housing side.
摘要翻译： 改进的涡轮弹簧夹密封件，用于引导与燃料筐中的燃料混合的气体。 涡轮弹簧夹密封件由内壳体和外壳体以及设置在内壳体和外壳体之间的中心密封构件组成。 中心密封构件是柔性的并且防止诸如空气的流体泄漏通过密封件。 在操作中，中心密封构件通过由内壳侧的相对较高的压力和外壳侧的相对较低的压力产生的压差而弯曲并与外壳密封。
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公开(公告)号：US07581402B2
公开(公告)日：2009-09-01
申请号：US11053353
申请日：2005-02-08
摘要： Aspects of the invention relate to a system for attaching a fuel swirler assembly in a turbine engine combustor. According to embodiments of the invention, at least an axial upstream end of the fuel swirler assembly can be attached to a combustor support frame using one or more fasteners, such as bolts. The fuel swirler assembly can include a radial bracket provided on the swirler body to facilitate attachment. The axial downstream end of the fuel swirler assembly can be positioned within an opening defined in a swirler base plate or within an opening in a swirler support plate. Aspects of the invention can reduce the time and cost associated with installation and replacement of fuel swirlers in a combustor while avoiding concerns associated with known welded pin attachment systems.
摘要翻译： 本发明的方面涉及一种用于在涡轮发动机燃烧器中附接燃料旋流器组件的系统。 根据本发明的实施例，燃料旋流器组件的至少轴向上游端可以使用一个或多个紧固件（例如螺栓）附接到燃烧器支撑框架。 燃料旋流器组件可以包括设置在旋流器主体上以便于附接的径向支架。 燃料旋流器组件的轴向下游端可以定位在限定在旋流器基板中或在旋流器支撑板中的开口内的开口内。 本发明的方面可以减少与燃烧器中的燃料旋流器的安装和更换相关联的时间和成本，同时避免与已知的焊接引脚附接系统相关的问题。
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公开(公告)号：US07377116B2
公开(公告)日：2008-05-27
申请号：US11117051
申请日：2005-04-28
IPC分类号： F23R3/60
CPC分类号： F23R3/002 , F01D9/023 , F05D2260/607 , F23R3/60 , F23R2900/00017
摘要： A barrier structure (302) blocks exit of spring clip fragments (317) that may break off from a spring clip assembly disposed between a gas turbine engine combustor (300) and a transition piece component (360). The barrier structure (302) may additionally comprise an aspect (326) effective to restrict a spring clip's (310, 311) radially inward compression, thereby reducing or eliminating damage to the spring clip (310, 311) during shipping and handling. The barrier structure (302) additionally may comprise an aspect (330) to restrict access by a human hand to the free ends (318) of the spring clips (310, 311). This aspect (330) reduces or eliminates the undesired lifting of the compressor by grabbing the spring clips (310, 311) during combustor transport, installation or removal. Accordingly, barrier structure embodiments are provided that reduce stress on spring clips, and that prevent the exit of spring clips from a containment space partly formed by the barrier structure.
摘要翻译： 阻挡结构（302）阻止可能从设置在燃气涡轮发动机燃烧器（300）和过渡件部件（360）之间的弹簧夹组件脱离的弹簧夹片（317）的出口。 阻挡结构（302）可以另外包括有效地限制弹簧夹（310,311）径向向内压缩的方面（326），从而减少或消除在运输和处理期间弹簧夹（310,311）的损坏。 阻挡结构（302）还可以包括限制人手接近弹簧夹（310,311）的自由端（318）的方面（330）。 该方面（330）通过在燃烧器运输，安装或拆卸期间抓住弹簧夹（310,311）来减少或消除压缩机的不期望的提升。 因此，提供了减小弹簧夹子上的应力并且防止弹簧夹从由阻挡结构部分形成的容纳空间的出口的阻挡结构实施例。
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4.发明授权Combustor with two stage primary fuel tube with concentric members and flow regulating 失效具有两级主燃料管的燃烧器具有同心构件和流量调节
公开(公告)号：US5983642A
公开(公告)日：1999-11-16
申请号：US949252
申请日：1997-10-13
摘要： A combustor for a gas turbine having a centrally located fuel nozzle and inner, middle and outer concentric cylindrical liners, the inner liner enclosing a primary combustion zone. The combustor has an air inlet that forms two passages for pre-mixing primary fuel and air to be supplied to the primary combustion zone. Each of the pre-mixing passages has a circumferential array of swirl vanes. A plurality of primary fuel tube assemblies extend through both pre-mixing passages, with each primary fuel tube assembly located between a pair of swirl vanes. Each primary fuel tube assembly is comprised of two tubular members. The first member supplies fuel to the first pre-mixing passage, while the second member, which extends through the first member, supplies fuel to the second pre-mixing passage. An annular fuel manifold is divided into first and second chambers by a circumferentially extending baffle. The proximal end of the first member is attached to the manifold itself while the proximal end of the second member is attached to the baffle. The distal end of the first member is attached directly to the second member at around its mid-point. The inlets of the first and second members are in flow communication with the first and second manifold chambers, respectively. Control valves separately regulate the flow of fuel to the two chambers and, therefore, to the two members of the fuel tube assemblies, thereby allowing the flow of fuel to the first and second pre-mixing passages to be separately controlled.
摘要翻译： 一种用于燃气轮机的燃烧器，其具有位于中心的燃料喷嘴和内部，中部和外部同心圆柱形衬套，所述内衬层包围主燃烧区。 燃烧器具有形成两个通道的空气入口，用于预混合一次燃料和要供应到主燃烧区的空气。 每个预混合通道具有旋转叶片的圆周阵列。 多个主燃料管组件延伸穿过两个预混合通道，每个主燃料管组件位于一对旋流叶片之间。 每个主燃料管组件由两个管状构件组成。 第一构件向第一预混合通道供应燃料，而延伸穿过第一构件的第二构件将燃料供应到第二预混合通道。 环形燃料歧管通过周向延伸的挡板分成第一和第二腔室。 第一构件的近端附接到歧管本身，而第二构件的近端附接到挡板。 第一构件的远端在其中点附近直接附接到第二构件。 第一和第二构件的入口分别与第一和第二歧管腔流动连通。 控制阀单独地调节到两个室的燃料流，并因此调节燃料管组件的两个构件的流动，从而允许单独控制到第一和第二预混合通道的燃料流。
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公开(公告)号：US06415610B1
公开(公告)日：2002-07-09
申请号：US09642462
申请日：2000-08-18
IPC分类号： F23R314
CPC分类号： F23R3/283 , F01D25/28 , F05B2260/301 , F23R3/60
摘要： A support member for removably supporting a swirler on a basket frame of a combustion gas turbine engine includes a plug removably mounted on the basket frame and a pin fixedly mounted on the swirler. A mechanical lock detachably connects the plug and the pin with one another, and the mechanical lock may include cooperating threads or other appropriate structures. The swirler is removed from the basket frame by detaching the plug from the basket frame, disconnecting the plug from the pin, and sliding the swirler longitudinally along its own axis whereby the pin clears the mounting hole within which the plug was mounted.
摘要翻译： 用于可拆卸地支撑燃烧燃气涡轮发动机的筐架上的旋流器的支撑构件包括可移除地安装在筐架上的塞子和固定地安装在旋流器上的销。 机械锁可拆卸地将插头和销彼此连接，并且机械锁可以包括协作螺纹或其它合适的结构。 通过从筐框架上拆下插头，将插头从销上拆下，并沿着其自身的轴线纵向滑动旋流器，从而将旋流器从篮框架中取出，由此销钉清除了安装插头的安装孔。
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公开(公告)号：US6149703A
公开(公告)日：2000-11-21
申请号：US329985
申请日：1999-06-10
CPC分类号： B01D29/117 , B01D35/02 , F02M21/0227 , B01D2201/02 , B01D2201/4092 , F02M37/22 , Y02T10/32
摘要： A fuel filtering apparatus for use in a gas turbine fuel system is provided. The fuel filtering apparatus includes a removable filter housing which receives and maintains a filter element therein to filter a fuel flow when the filter housing is positioned on the apparatus. The fuel filtering apparatus is also provided with a casing which is installed in-line in a portion of the fuel system. The removable filter housing alleviates the need for removal of the casing when a filter element is inserted and removed for cleaning and other routine maintenance. The fuel filtering apparatus also reduces pressure disruption within the fuel system.
摘要翻译： 提供一种用于燃气轮机燃料系统的燃料过滤装置。 燃料过滤装置包括可移除的过滤器壳体，其在过滤器壳体位于设备上时接收并保持其中的过滤元件以过滤燃料流。 燃料过滤装置还设置有在燃料系统的一部分中并排安装的壳体。 当插入和移除过滤元件用于清洁和其他日常维护时，可移除的过滤器壳体减轻了对壳体的移除的需要。 燃料过滤装置还减少燃料系统内的压力中断。
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7.发明授权
公开(公告)号：US5987875A
公开(公告)日：1999-11-23
申请号：US892662
申请日：1997-07-14
CPC分类号： F23L7/005 , F23D23/00 , F23D2900/00008 , F23D2900/00015
摘要： A combustion system has a diffusion flame pilot assembly and a steam delivery assembly. The diffusion flame pilot assembly has a fuel line with a downstream end terminating at a pilot nozzle. The steam delivery assembly has a steam line terminating at a steam outlet proximate to said fuel line and upstream of said pilot nozzle for directing steam to the pilot nozzle. An aspect of the invention has a steam throttle valve for adjusting the steam flow to the pilot nozzle based on the combustion system's NO.sub.X emissions and/or characteristics of said pilot fuel stream.
摘要翻译： 燃烧系统具有扩散火焰导向组件和蒸汽输送组件。 扩散火焰导向组件具有燃料管线，其下游端终止于先导喷嘴。 蒸汽输送组件具有终止于靠近所述燃料管线的蒸汽出口和所述引燃喷嘴上游的蒸汽管线，用于将蒸汽引导到先导喷嘴。 本发明的一个方面具有一个蒸汽节流阀，用于根据燃烧系统的NO x排放和/或所述引燃燃料流的特性调节到导向喷嘴的蒸汽流量。
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