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    Laser welding method and engine cooling structure
    4.
    发明授权
    Laser welding method and engine cooling structure 有权
    激光焊接法和发动机冷却结构

    公开(公告)号：US09533378B2

    公开(公告)日：2017-01-03

    申请号：US14383791

    申请日：2013-03-04

    申请人： Minoru Kawasaki ,  Kazuhito Sakai ,  Shintaro Utsumi

    发明人： Minoru Kawasaki ,  Kazuhito Sakai ,  Shintaro Utsumi

    IPC分类号： F02F1/10 ,  B23K33/00 ,  F02F1/40 ,  F02F1/14 ,  F01P3/02 ,  F02F1/24

    CPC分类号： B23K33/008 ,  B23K26/323 ,  B23K2103/10 ,  B23K2103/12 ,  F01P2003/024 ,  F02F1/108 ,  F02F1/14 ,  F02F1/40 ,  F02F2001/104 ,  F02F2001/244 ,  Y10T29/49231

    摘要： A cylinder block (10) includes an inter-bore flow passage (14) between adjacent bores (12). Each inter-bore flow passage (14) is formed by closing an opening-side groove portion (15) continuous from a cylinder block deck face and a bottom-side groove portion (16) with the use of a lid member (20) made of copper, and the lid member (20 is laser-welded to a groove wall face of the opening-side groove portion (15). Before the laser-welding, the lid member (20) has recesses (26) that are interspersed in a direction, in which a laser beam travels, at any one of connected portions at which the lid member (20 is connected to the groove wall face of the opening-side groove portion (15).

    摘要翻译： 气缸体（10）包括相邻孔（12）之间的孔间流动通道（14）。 每个孔间流动通道（14）通过使用制成的盖构件（20）封闭从气缸体盖板面和底侧槽部（16）连续的开口侧槽部（15）而形成 的铜构件（20）被激光焊接到开口侧槽部（15）的槽壁面，在激光焊接之前，盖构件（20）具有散置在 激光束行进的方向在盖构件（20）与开口侧槽部（15）的槽壁面连接的连接部的任意一个处。

    METHOD OF MODIFYING ENGINE OIL COOLING SYSTEM
    5.
    发明申请
    METHOD OF MODIFYING ENGINE OIL COOLING SYSTEM 有权
    发动机油冷却系统的改造方法

    公开(公告)号：US20160356202A1

    公开(公告)日：2016-12-08

    申请号：US15243576

    申请日：2016-08-22

    申请人： Neal Technologies, Inc.

    发明人： Gene NEAL ,  Kennieth NEAL

    IPC分类号： F01P3/20 ,  F01M11/03 ,  F01M1/10 ,  F01M5/00 ,  F01P11/08 ,  F01P5/10

    CPC分类号： F01P3/20 ,  F01M1/10 ,  F01M5/002 ,  F01M5/021 ,  F01M11/03 ,  F01M2001/1092 ,  F01M2011/033 ,  F01P5/10 ,  F01P11/08 ,  F01P11/12 ,  F01P2060/04 ,  Y10T29/49231 ,  Y10T29/49233

    摘要： A method of modifying the oil cooling system of a diesel engine includes the steps of removing the original equipment liquid-to-liquid heat exchanger and installing a manifold having a configuration adapted to match the mounting configuration of the oil passages of the original equipment liquid-to-liquid heat exchanger. The manifold has an oil outlet port directed to a remotely mounted oil cooler. The manifold also has a water passage having a configuration that is adapted to match the mounting configuration of the water passages of the original equipment liquid-to-liquid heat exchanger. The water passage causes the entirety of the flow of water to be discharged back to the water cooling system of the engine where it is circulated by the water pump through the water cooling passages in the engine.

    摘要翻译： 一种修改柴油机的油冷却系统的方法包括以下步骤：去除原始设备液 - 液热交换器并安装具有适于匹配原始设备液 - 液流换热器的油路的安装结构的歧管， 液体换热器。 歧管具有一个导向远程安装的油冷却器的出油口。 歧管还具有水通道，其具有适于与原设备液 - 液热交换器的水通道的安装配置相匹配的构造。 水通道使得整个水流被排出到发动机的水冷却系统中，在水冷却系统中，水循环通过水泵通过发动机的水冷却通道。

    Combustion liner guide stop and method for assembling a combustor
    6.
    发明授权
    Combustion liner guide stop and method for assembling a combustor 有权
    燃烧衬管引导止动件和组装燃烧器的方法

    公开(公告)号：US09435535B2

    公开(公告)日：2016-09-06

    申请号：US13400264

    申请日：2012-02-20

    申请人： Anand Prafulchandra Desai ,  Praveen Kumar Tiwari

    发明人： Anand Prafulchandra Desai ,  Praveen Kumar Tiwari

    IPC分类号： F23R3/00 ,  F23R3/60

    CPC分类号： F23R3/002 ,  F23R3/60 ,  F23R2900/00017 ,  Y10T29/49231

    摘要： A combustor for a gas turbine including a casing, a flow sleeve at least partially disposed within the casing, a combustion liner at least partially disposed within the flow sleeve, a liner stop feature extending from the combustion liner, and a liner guide stop including a first end separated from a second end, the second end configured to be at least partially engaged with the liner stop feature, wherein the liner guide stop extends through the casing and the flow sleeve.

    摘要翻译： 一种用于燃气轮机的燃烧器，包括壳体，至少部分地设置在壳体内的流动套管，至少部分地设置在流动套筒内的燃烧衬套，从燃烧衬套延伸的衬垫止动件，以及衬套引导件止动器， 第一端与第二端分离，所述第二端构造成至少部分地与所述衬垫止动部件接合，其中所述衬套引导止动件延伸穿过所述壳体和所述流动套筒。

    ENGINE COVER HAVING A RETAINER TO SECURE AN ENGINE ACCESSORY
    8.
    发明申请
    ENGINE COVER HAVING A RETAINER TO SECURE AN ENGINE ACCESSORY 审中-公开
    具有保护装置以保护发动机附件的发动机罩

    公开(公告)号：US20160153395A1

    公开(公告)日：2016-06-02

    申请号：US15015660

    申请日：2016-02-04

    申请人： Ford Global Technologies, LLC

    发明人： Thomas Edward SMITH ,  Frank Acierno VALENCIA

    IPC分类号： F02F7/00 ,  F01L13/00 ,  F01M9/10 ,  F01L1/344

    CPC分类号： F02F7/006 ,  F01L1/344 ,  F01L9/025 ,  F01L9/04 ,  F01L13/0015 ,  F01L2101/00 ,  F01L2103/00 ,  F01L2103/01 ,  F01L2820/041 ,  F01M9/10 ,  F02P13/00 ,  Y10T29/49231

    摘要： A cover has an aperture through which an accessory gains access to the interior side of the cover and a cavity. The accessory may be any kind of sensor or actuator. To secure the accessory to the cover, an adapter coupled to the cover is provided. In one example, the adapter has a cylindrical connection section that is spin welded into place in the cavity. In another example, the adapter has self-tapping threads that engage with the surface surrounding the cavity. The adapter also has tabs extending outwardly from the cover, the tabs having a proximate section and an engagement section. The accessory has a retaining orifice that couples with the tabs in a snap-fit relationship to secure the accessory to the cover.

    摘要翻译： 盖具有孔，附件通过该孔进入到盖的内侧和腔。 附件可以是任何种类的传感器或致动器。 为了将附件固定到盖上，提供耦合到盖的适配器。 在一个示例中，适配器具有圆柱形连接部分，其被旋转焊接到腔中的适当位置。 在另一示例中，适配器具有与围绕腔体的表面接合的自攻丝。 适配器还具有从盖向外延伸的突片，突片具有近似部分和接合部分。 附件具有保持孔口，其与卡扣配合关系，以将附件固定到盖子上。

    Sliding U-joint hanger for gas turbine engine nozzle
    10.
    发明授权
    Sliding U-joint hanger for gas turbine engine nozzle 有权
    用于燃气轮机发动机喷嘴的滑动U形悬挂架

    公开(公告)号：US09255548B2

    公开(公告)日：2016-02-09

    申请号：US13609907

    申请日：2012-09-11

    申请人： Lon H. Preston, III

    发明人： Lon H. Preston, III

    IPC分类号： F02K1/82 ,  F02K1/80 ,  F23R3/60 ,  F02C7/20

    CPC分类号： F02K1/822 ,  F02C7/20 ,  F02K1/80 ,  F02K1/82 ,  F05D2230/642 ,  F05D2240/90 ,  F05D2260/31 ,  F23R3/60 ,  Y02T50/675 ,  Y10T29/49231

    摘要： A disclosed hanger assembly for supporting a liner within a gas turbine engine exhaust nozzle includes a first mount for attachment to a case and a second mount for attachment to the liner. A u-joint assembly is attached between the first and second mounts and includes a first yoke and a second yoke aligned transverse to the first yoke. A pivot block is includes a first set of pins received by the first yoke and a second set of pins received by the second yoke. The u-joint assembly accommodates relative movement between the liner and case.

    摘要翻译： 用于在燃气涡轮发动机排气喷嘴内支撑衬套的公开的衣架组件包括用于附接到壳体的第一安装件和用于附接到衬套的第二安装件。 U形接头组件安装在第一和第二安装件之间，并且包括第一磁轭和横向于第一磁轭排列的第二磁轭。 枢轴块包括由第一轭接收的第一组销和由第二叉接收的第二组销。 U形接头组件适应衬套和壳体之间的相对运动。