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    SELF CRYSTALLINE ORIENTATION FOR INCREASED COMPLIANCE
    2.
    发明申请
    SELF CRYSTALLINE ORIENTATION FOR INCREASED COMPLIANCE 审中-公开
    自主研发的方向提高了符合性

    公开(公告)号：US20170044918A1

    公开(公告)日：2017-02-16

    申请号：US14825812

    申请日：2015-08-13

    申请人： United Technologies Corporation

    发明人： Michael G. McCaffrey ,  Eric A. Hudson

    IPC分类号： F01D11/02 ,  F16J15/44

    CPC分类号： F01D11/02 ,  F01D5/16 ,  F01D5/22 ,  F01D5/24 ,  F01D11/006 ,  F01D11/16 ,  F02C7/28 ,  F05D2220/323 ,  F05D2240/55 ,  F05D2250/71 ,  F05D2300/17 ,  F05D2300/607 ,  F16J15/44

    摘要： Aspects of the disclosure are directed to a seal comprising: a shoe, and at least one beam coupled to the shoe, wherein the seal includes a single crystal material with a predetermined crystalline orientation. Aspects of the disclosure are directed to a method for designing a seal, comprising: obtaining a requirement associated with at least one of: a geometrical profile of the seal, a temperature range over which the seal is to operate, a natural frequency associated with the seal, or a range of deflection associated with the seal, selecting a crystalline orientation for a single crystal material of the seal based on the requirement, and fabricating the seal based on the selected crystalline orientation.

    摘要翻译： 本公开的方面涉及一种密封件，其包括：鞋，以及耦合到鞋的至少一个梁，其中所述密封件包括具有预定结晶取向的单晶材料。 本公开的方面涉及一种用于设计密封件的方法，包括：获得与以下中的至少一个相关联的要求：密封件的几何轮廓，密封件将在其上操作的温度范围，与 密封或与密封件相关的一系列偏转，基于要求为密封件的单晶材料选择晶体取向，以及基于所选择的晶体取向制造密封件。

    BLADE SYSTEM, AND CORRESPONDING METHOD OF MANUFACTURING A BLADE SYSTEM
    4.
    发明申请
    BLADE SYSTEM, AND CORRESPONDING METHOD OF MANUFACTURING A BLADE SYSTEM 审中-公开
    叶片系统，以及制造叶片系统的相应方法

    公开(公告)号：US20160108737A1

    公开(公告)日：2016-04-21

    申请号：US14889701

    申请日：2014-04-04

    申请人： SIEMENS AKTIENGESELLSCHAFT

    发明人： Stephen Batt ,  Mike McKenna

    IPC分类号： F01D5/16 ,  F01D5/14

    CPC分类号： F01D5/16 ,  F01D5/147 ,  F01D5/225 ,  F01D5/24 ,  F01D11/006 ,  Y02T50/673

    摘要： A blade system for a gas turbine has a blade device and a further blade device. The blade device has a shroud, an airfoil extending from the shroud along the radial direction, the shroud has at a circumferential end a wedge face having a recess extending with a component along the axial direction, and a damping wire arranged within the recess such that the damping wire is adapted for contacting the shroud and a further wedge face of a further shroud of a further blade device arranged adjacent to the shroud along the circumferential direction. The recess includes an inclining side surface which has a normal, non-parallel with the radial direction, the further wedge face has a plane surface onto which the damping wire is abuttable. A method of manufacturing a blade system includes arranging the further shroud adjacent to the shroud and arranging a damping wire within the recess.

    摘要翻译： 用于燃气轮机的叶片系统具有刀片装置和另外的刀片装置。 叶片装置具有护罩，沿着径向方向从护罩延伸的翼型件，护罩在周向端具有楔形面，楔形面具有沿着轴向方向与部件延伸的凹部，以及设置在凹部内的阻尼丝，使得 所述阻尼线适于接触所述护罩和沿着所述圆周方向布置成与所述护罩相邻布置的另外的刀片装置的另一护罩的另一楔形面。 所述凹部包括倾斜侧表面，所述倾斜侧表面具有法向的，与所述径向方向不平行的，所述另外的楔面具有平面，所述阻尼丝可抵靠在该平面上。 制造叶片系统的方法包括将另外的护罩布置在护罩附近并在凹槽内布置阻尼丝。

    Turbine rotor and method for producing the rotor
    6.
    发明申请
    Turbine rotor and method for producing the rotor 审中-公开
    涡轮转子及其制造方法

    公开(公告)号：US20090116964A1

    公开(公告)日：2009-05-07

    申请号：US12005525

    申请日：2007-12-27

    申请人： Hans-Egon Brock

    发明人： Hans-Egon Brock

    IPC分类号： F01D5/30 ,  F01D5/22 ,  B23P15/04

    CPC分类号： F01D5/3038 ,  F01D5/225 ,  F01D5/24 ,  F05D2230/64 ,  Y10T29/49316

    摘要： A turbine rotor has a row of turbine blades associated with a circumferential groove in a disk, each turbine blade having foot received in the groove, a blade profile above the foot, and a shroud plate above the profile. Each blade foot and each shroud plate have end surfaces and side surfaces which form a rhomboid, the end surfaces of each shroud plate tapering toward each other along respective radii and abutting the end surfaces of adjacent shroud plates to form a closed ring. The blade profiles are torsionally stressed by applying a force to each plate in a direction parallel to the axis of the disk, thereby twisting the cover plates through an angle alpha so that the side surfaces of adjacent cover plates are circumferentially aligned in a plane perpendicular to the longitudinal axis. This force is maintained by clamping devices applied to the combs of adjacent blades.

    摘要翻译： 涡轮机转子具有与盘中的周向槽相关联的一排涡轮叶片，每个涡轮叶片具有容纳在凹槽中的脚，在脚之上的刀片轮廓，以及轮廓上方的护罩板。 每个叶片脚和每个护罩板具有形成菱形的端面和侧表面，每个护罩板的端表面沿着相应的半径彼此逐渐变细并且邻接相邻护板的端面以形成闭合环。 刀片轮廓通过在平行于盘的轴线的方向上向每个板施加力而扭转应力，由此将盖板扭转角度α，使得相邻盖板的侧表面在垂直于 纵轴。 该力通过施加到相邻叶片的梳子的夹紧装置来维持。

    High efficiency blade configuration for steam turbine
    7.
    发明授权
    High efficiency blade configuration for steam turbine 有权
    蒸汽轮机的高效率叶片配置

    公开(公告)号：US06769869B2

    公开(公告)日：2004-08-03

    申请号：US10025597

    申请日：2001-12-26

    申请人： Tadashi Tanuma ,  Taro Sakamoto

    发明人： Tadashi Tanuma ,  Taro Sakamoto

    IPC分类号： F01D514

    CPC分类号： F01D5/24 ,  F01D5/141 ,  Y10S416/02 ,  Y10S416/05

    摘要： A steam turbine that passes more turbine driving steam by off-setting the turbine moving blade throat•pitch ratio before operation and, when a blade untwist is generated during operation, causing more turbine driving steam to flow by maintaining an appropriate value, and, at the same time causing the turbine moving blade throat•pitch ratio to swell by giving the blade untwisting angle to the blade cross-sections in regions where the aerodynamic loss is small. The steam turbine is one in which the throat•pitch ratio (S/T) distribution of a turbine moving blade is offset by forming a curve providing at least one minimal value and maximal value by giving blade twist angle to the blade cross-sections in the blade height direction from blade root to blade tip and, at the same time, the distribution of throat•pitch ratio (S/T) taking into consideration blade untwist generated during operation.

    摘要翻译： 一种汽轮机，其在运行之前通过使涡轮机运动叶片喉部折流比偏离，并且当在运行期间产生叶片解锁时，通过维持适当的值使更多的涡轮机驱动蒸汽流动来传递更多的涡轮机驱动蒸汽，并且在 同时通过在空气动力学损失小的区域中给叶片提供与叶片横截面的角度来使涡轮机移动叶片喉部折叠比膨胀。 蒸汽涡轮机是通过形成提供至少一个最小值和最大值的曲线来偏移涡轮机动叶片的喉部比例（S / T）分布的蒸汽轮机，通过给叶片横截面提供叶片扭转角度 刀片高度方向从叶片根部到叶片尖端，同时考虑到在操作过程中产生的叶片扭转的喉部分比（S / T）的分布。

    Turbomachine radial impeller vibration constraining and damping mechanism
    9.
    发明授权
    Turbomachine radial impeller vibration constraining and damping mechanism 失效
    涡轮机叶片振动约束和阻尼机理

    公开(公告)号：US5984638A

    公开(公告)日：1999-11-16

    申请号：US289795

    申请日：1994-08-12

    申请人： M. Theodore Gresh ,  Francis Kushner

    发明人： M. Theodore Gresh ,  Francis Kushner

    IPC分类号： F01D5/24

    CPC分类号： F01D5/24

    摘要： A compressor blade vibration reduction mechanism for a high-speed radial impeller for minimizing fatigue failures from various excitation sources. The vibration reduction mechanism includes a plurality of loose-fitting lashing pins coupling each impeller blade to an adjacent impeller blade. Each lashing pin extends through a first aperture in a blade located adjacent to the blade tip and through a second aperture of an adjacent blade. The second aperture of each blade is located a greater distance from the leading edge of the blade than the first aperture. The second aperture is located in an area of the blade having lower vibration during operation than the blade location where the first aperture is located.

    摘要翻译： 一种用于使来自各种激发源的疲劳失效最小化的用于高速径向叶轮的压缩机叶片减振机构。 减振机构包括将每个叶轮叶片联接到相邻的叶轮叶片的多个松配合的捆扎销。 每个捆扎销延伸穿过位于叶片尖端附近并通过相邻叶片的第二孔的刀片中的第一孔。 每个叶片的第二个孔距离叶片的前缘比第一孔更远的距离。 第二孔位于叶片的操作中比在第一孔所在的叶片位置处具有较低振动的区域。

    Rotor tip shroud damper including damper wires
    10.
    发明授权
    Rotor tip shroud damper including damper wires 失效
    转子叶片护罩减震器包括阻尼丝

    公开(公告)号：US5201850A

    公开(公告)日：1993-04-13

    申请号：US655701

    申请日：1991-02-15

    申请人： Christopher H. Lenhardt ,  Carl Grant ,  Chellappa Balan

    发明人： Christopher H. Lenhardt ,  Carl Grant ,  Chellappa Balan

    IPC分类号： F01D5/10 ,  F01D5/22 ,  F01D5/24

    CPC分类号： F01D5/225 ,  F01D5/10 ,  F01D5/24 ,  F05D2260/96 ,  Y10S416/50

    摘要： A rotor includes a disc having a plurality of blades extending therefrom. The blades include tip shrouds, each having first and second axial ends, and first and second circumferential faces. The first and second faces of adjacent tip shrouds are spaced from each other to define gaps therebetween. The first and second ends each include U-shaped slots, each having an arcuate damper wire disposed therein. The slots are aligned generally parallel to an axial centerline axis of the rotor for allowing ease of manufacture and assembly while providing effective frictional damping by the damper wires urged by centrifugal force against the slots.

    摘要翻译： 转子包括具有从其延伸的多个叶片的盘。 叶片包括具有第一和第二轴向端部以及第一和第二圆周面的顶端罩。 相邻尖端护罩的第一和第二面彼此间隔开以限定它们之间的间隙。 第一和第二端各自包括U形槽，每个槽具有设置在其中的弧形阻尼丝。 槽大致平行于转子的轴向中心线排列，以允许易于制造和组装，同时通过由离心力推压到狭槽的阻尼丝提供有效的摩擦阻尼。