Method for repair and replacement of combustor liner panel
    1.
    发明授权
    Method for repair and replacement of combustor liner panel 有权
    燃烧器衬板的修理和更换方法

    公开(公告)号:US07546684B2

    公开(公告)日:2009-06-16

    申请号:US10901262

    申请日:2004-07-27

    摘要: A method for repairing a damaged portion of a combustor inner liner assembly. The method includes removing the combustor from a gas turbine engine. After inspecting the combustor to determine whether cracks exists in portions of the inner liner assembly, the method includes removing a cracked inner liner assembly from the combustor. Then the portion of the inner liner assembly, comprising a multi-hole panel region, an aft lip region, an aft seal flange region and an aft panel support leg are separated from the inner liner assembly. The multi-hole panel region and aft lip, where fatigue damage typically exists, along with the aft seal flange region, are discarded and a new aft lip region/aft seal flange region and multi-hole panel region are provided. The new parts are joined to the aft panel support leg and the inner liner assembly aft of forward bolt flange region after these parts are refurbished. The inner liner assembly is then reattached to the combustor and reassembled into the engine.

    摘要翻译: 一种用于修理燃烧器内衬组件的损坏部分的方法。 该方法包括从燃气涡轮发动机移除燃烧器。 在检查燃烧器以确定在内衬组件的部分中是否存在裂纹的情况下,该方法包括从燃烧器去除裂纹的内衬组件。 然后,内衬组件的包括多孔面板区域,后唇区域,后密封凸缘区域和后面板支撑腿部的部分与内衬组件分离。 通常存在通常存在疲劳损伤的多孔面板区域和后缘以及后部密封凸缘区域,并且提供新的后缘区域/后部密封凸缘区域和多孔面板区域。 这些部件经过翻新后,新的部件连接到后板支撑腿和内衬组件后方的前螺栓法兰区域。 内衬组件然后重新连接到燃烧器并重新组装到发动机中。

    Silicone coated fabric
    2.
    发明授权
    Silicone coated fabric 失效
    有机硅涂层织物

    公开(公告)号:US4666765A

    公开(公告)日:1987-05-19

    申请号:US782962

    申请日:1985-10-02

    摘要: The present invention is directed to method for making silconecoated woven fabric substrates, and the products produced by such method. The method comprises the steps of applying a first liquid polysilicane elastomer to the substrate so as to form a base coat, curing the base coat, applying a second liquid polysilicane elastomer over the base coat so as to form a top coat, and curing the top coat. By specifically selecting the polysilicane elastomers as well as the substrate, and by further selecting the reaction parameters, a high strength, non-flammable, waterproof, self-cleaning, translucent and weather-resistant fabric is produced.

    摘要翻译: 本发明涉及制造硅油组织织物基材的方法,以及通过这种方法制备的产品。 该方法包括以下步骤:将第一液体聚硅烷弹性体施加到基底上以形成底涂层,固化底涂层,在底涂层上涂敷第二液态聚硅烷弹性体以形成顶涂层,并固化顶部 涂层。 通过特别选择聚硅烷弹性体以及基材,通过进一步选择反应参数,可以生产高强度,不易燃,防水,自清洁,半透明和耐候的织物。

    Methods for replacing a portion of a combustor dome assembly
    3.
    发明授权
    Methods for replacing a portion of a combustor dome assembly 有权
    用于替换燃烧器穹顶组件的一部分的方法

    公开(公告)号:US06782620B2

    公开(公告)日:2004-08-31

    申请号:US10352823

    申请日:2003-01-28

    IPC分类号: B23P1500

    摘要: A method enables a portion of combustor dome assembly to be replaced. The dome assembly includes at least one dome cup including at least one swirl cup including a joint that defines a slot therein, and a deflector plate assembly that is coupled to, and extends downstream from, the swirl cup, such that a portion of the deflector plate assembly is securely fixed within the joint slot. The method comprises cutting through an interface formed between the deflector plate assembly and the joint slot, extending the cut substantially between the deflector assembly and the joint slot through the at least one dome cup, removing the deflector plate assembly from the combustor dome assembly, and coupling a replacement deflector plate assembly within the combustor dome assembly that extends aft from the portion of the combustor dome assembly that is upstream from the cut.

    摘要翻译: 一种方法使得能够更换燃烧器穹顶组件的一部分。 圆顶组件包括至少一个圆顶杯,该圆顶杯包括至少一个包括在其中限定槽的接头的旋转杯,以及偏转板组件,其连接到旋流杯并且在旋流杯的下游延伸,使得偏转器的一部分 板组件牢固地固定在接头槽内。 该方法包括切割形成在偏转板组件和接合槽之间的界面,通过至少一个圆顶杯基本上在导流板组件和接合槽之间延伸切口,从燃烧器顶盖组件移除偏转板组件,以及 将替代偏转板组件联接在燃烧器穹顶组件内,该燃烧器穹顶组件从在切割的上游的燃烧器穹顶组件的部分向后延伸。

    Controlling the porosity and permeation of a web
    4.
    发明授权
    Controlling the porosity and permeation of a web 失效
    控制网的孔隙率和渗透

    公开(公告)号:US5954902A

    公开(公告)日:1999-09-21

    申请号:US476465

    申请日:1995-06-07

    申请人: James M. Caldwell

    发明人: James M. Caldwell

    摘要: Products and methods for controlling the porosity and permeation of a web are provided using a curable thixotropic shear thinnable polymer composition that preferably encapsulates a plurality of fibers of the web and/or forms an internal layer within the web. Webs suitable for several different uses are featured, for example medical garments resistant to permeation by a virus or bacteria. The effective pore size of the web is controlled by regulating various factors such as the thickness of the polymer composition encapsulating the fibers and the thickness and placement of the internal polymer layer. Other factors include the polymer density, structure, and crosslinking orientation, as well as the diffusion, permeation and sorption of the polymer.

    摘要翻译: 使用可固化的触变性剪切稀释聚合物组合物来提供用于控制幅材的孔隙率和渗透性的产品和方法,其优选地封装幅材的多个纤维和/或在幅材内形成内层。 特别适用于几种不同用途的网,例如耐病毒或细菌渗透的医用服装。 通过调节封闭纤维的聚合物组合物的厚度和内部聚合物层的厚度和放置的各种因素来控制幅材的有效孔径。 其他因素包括聚合物密度,结构和交联取向,以及聚合物的扩散,渗透和吸附。

    Dual fuel mixer for gas turbine combustor
    5.
    发明授权
    Dual fuel mixer for gas turbine combustor 失效
    用于燃气轮机燃烧器的双燃料混合器

    公开(公告)号:US5778676A

    公开(公告)日:1998-07-14

    申请号:US581817

    申请日:1996-01-02

    摘要: An air fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct in which a fuel manifold is provided in flow communication with a fuel supply and control means, a set of inner and outer counter-rotating swirlers adjacent the upstream end of the mixing duct for imparting swirl to an air stream, a hub separating the inner and outer annular swirlers to allow independent rotation of the air stream, and a centerbody located axially along and substantially the full length of the mixing duct. In order to inject one type of fuel into the mixing duct, fuel is supplied to the outer annular swirlers which include hollow vanes with internal cavities, wherein the internal cavities of the outer swirler vanes are in fluid communication with the fuel manifold in the shroud. The outer swirler vanes further include a plurality of fuel passages therethrough in flow communication with the internal cavities. A second fuel can be injected into the mixing duct by means of a plurality of orifices in the centerbody wall which are in flow communication with a fuel supply and control means. In this way, high pressure air from a compressor is injected into the mixing duct through the swirlers to form an intense shear region and fuel is injected into the mixing duct from the outer swirler vane passages and/or the centerbody orifices so that the high pressure air and the fuel is uniformly mixed therein so as to produce minimal formation of poullutants when a fuel/air mixture is exhausted out the downstream end of the mixing duct into the combustor and ignited.

    摘要翻译: 公开了一种空气燃料混合器,其具有混合管道,围绕混合管道的上游端的护罩,其中设置有与燃料供应和控制装置流动连通的燃料歧管,一组相邻的内部和外部反向旋转旋流器 混合管道的上游端,用于向气流产生涡流;轮毂,分隔内外环形旋流器,以允许空气流的独立旋转;以及沿着混合管道的大致整个长度方向定位的中心体。 为了将一种类型的燃料喷射到混合管道中,燃料被供应到外部环形旋流器,其包括具有内部空腔的中空叶片,其中外部旋流器叶片的内部空腔与护罩中的燃料歧管流体连通。 外旋流器叶片还包括与内腔流动连通的多个通过其的燃料通道。 第二燃料可以通过与燃料供应和控制装置流动连通的中心体壁中的多个喷嘴喷射到混合管道中。 以这种方式,来自压缩机的高压空气通过旋流器喷射到混合管道中以形成强烈的剪切区域,并且燃料从外部旋流器叶片通道和/或中心体孔口喷射到混合管道中,使得高压 空气和燃料均匀地混合在一起,以便当燃料/空气混合物从混合管道的下游端排出到燃烧器中并点燃时,产生最小的起泡器的形成。

    Turbine nozzle segment and method of repairing same
    6.
    发明授权
    Turbine nozzle segment and method of repairing same 失效
    涡轮喷嘴段及其修理方法

    公开(公告)号:US06785961B1

    公开(公告)日:2004-09-07

    申请号:US09438969

    申请日:1999-11-12

    IPC分类号: B23P1500

    摘要: A method for repairing a turbine nozzle segment having at least two vanes disposed between outer and inner bands includes the steps of separating the nozzle segment into a first singlet containing a repairable vane and a second singlet containing a non-repairable vane, and joining the first singlet to a newly manufactured singlet having a configuration that is similar to the second singlet.

    摘要翻译: 一种用于修复具有设置在外部和内部带之间的至少两个叶片的涡轮喷嘴段的方法包括以下步骤:将喷嘴段分离成包含可修复叶片的第一单瓣瓣和包含不可修复叶片的第二单瓣形,并将第一 单峰到具有类似于第二单峰的构造的新制造的单线态。

    Controlling the porosity and permeation of a web
    7.
    发明授权
    Controlling the porosity and permeation of a web 失效
    控制网的孔隙率和渗透

    公开(公告)号:US6071602A

    公开(公告)日:2000-06-06

    申请号:US14316

    申请日:1998-01-27

    申请人: James M. Caldwell

    发明人: James M. Caldwell

    IPC分类号: B05C11/04 D06N3/12 D03D3/00

    摘要: Articles for controlling the porosity and permeation of a web are provided using a curable thixotropic shear thinnable polymer composition that preferably encapsulates a plurality of fibers of the web and/or forms an internal layer within the web. Webs suitable for several different uses are featured, for example medical garments resistant to permeation by a virus or bacteria. The effective pore size of the web is controlled by regulating various factors such as the thickness of the polymer composition encapsulating the fibers and the thickness and placement of the internal polymer layer. Other factors include the polymer density, structure, and crosslinking orientation, as well as the diffusion, permeation and sorption of the polymer.

    摘要翻译: 使用可固化触变剪切稀释聚合物组合物来提供用于控制幅材的孔隙率和渗透性的制品,其优选地封装多个幅材纤维和/或在幅材内形成内层。 特别适用于几种不同用途的网,例如耐病毒或细菌渗透的医用服装。 通过调节封闭纤维的聚合物组合物的厚度和内部聚合物层的厚度和放置的各种因素来控制幅材的有效孔径。 其他因素包括聚合物密度,结构和交联取向,以及聚合物的扩散,渗透和吸附。

    Automatic garment portion loader
    8.
    发明授权
    Automatic garment portion loader 失效
    自动服装装载机

    公开(公告)号:US4693460A

    公开(公告)日:1987-09-15

    申请号:US861826

    申请日:1986-05-12

    IPC分类号: A41H43/02 D05B33/00 B65H5/00

    CPC分类号: A41H43/0214 D05B33/006

    摘要: A garment portion loader utilizes a plurality of photo-electric sensors to determine the positions of garment portions at selected stations including a delivery assembly which supplies garment portions for loading, a pick-up assembly which removes garment portions from the delivery assembly and places them on an alignment conveyor, and an alignment assembly which aligns the garment portions with a pre-established standard relative to the alignment conveyor. A rejection assembly is provided to remove garments which are not properly aligned. The loader may be controlled by a microprocessor receiving input from the sensors and controlling the various assemblies.

    摘要翻译: 服装部分装载机利用多个光电传感器来确定选定站点处的服装部分的位置,包括提供用于装载的衣服部分的传送组件,将装置部分从传送组件移除并将它们放置在其上的拾取组件 对准传送器和对准组件,其使衣服部分相对于对准传送器以预先建立的标准对准。 提供排斥组件以去除未正确对准的衣服。 加载器可以由微处理器来控制,该微处理器从传感器接收输入并控制各种组件。

    Method of adjusting gas turbine component cooling air flow
    9.
    发明授权
    Method of adjusting gas turbine component cooling air flow 失效
    调整燃气轮机部件冷却风量的方法

    公开(公告)号:US06408610B1

    公开(公告)日:2002-06-25

    申请号:US09618571

    申请日:2000-07-18

    IPC分类号: F02C712

    摘要: A method of adjusting airflow through a plurality of cooling holes by depositing a thermal barrier coating on an exterior surface and/or an interior surface of the component by a physical vapor deposition process. The cooling holes are not masked. Thus, a portion of the thermal barrier coating partially obstructs airflow through the cooling holes and reduces airflow through the cooling holes. A predetermined pressure drop is developed across the cooling holes and airflow through the cooling holes is measured. The measured airflow is compared to a preselected range of desired cooling hole airflows and the steps of depositing the thermal barrier coating, developing the predetermined pressure drop, calculating airflow and comparing the measured airflow to the preselected range are repeated until the measured airflow is within the preselected range of desired cooling hole airflows.

    摘要翻译: 通过物理气相沉积工艺在组件的外表面和/或内表面上沉积热障涂层,来调节通过多个冷却孔的气流的方法。 冷却孔未被遮蔽。 因此,热障涂层的一部分部分阻碍通过冷却孔的空气流并且减少通过冷却孔的气流。 在冷却孔之间产生预定的压降,并测量通过冷却孔的气流。 将测量的气流与期望的冷却孔气流的预选范围进行比较,并重复沉积热障涂层,显影预定压降,计算气流并将测量的气流与预选范围进行比较的步骤,直到所测量的气流在 所需冷却孔气流的预选范围。