公开(公告)号：US20140008871A1

公开(公告)日：2014-01-09

申请号：US13542780

申请日：2012-07-06

Applicant: Rahul Anil Bidkar ,  Massimiliano Cirri ,  Azam Mihir Thatte ,  John Robert Williams

Inventor： Rahul Anil Bidkar ,  Massimiliano Cirri ,  Azam Mihir Thatte ,  John Robert Williams

IPC: F16J15/447

CPC classification number: F16J15/447 ,  F01D11/025 ,  F01D11/04 ,  F01D11/14 ,  F04D29/164 ,  F04D29/526 ,  F16J15/442 ,  F16J15/445

Abstract: An aerodynamic seal assembly for a rotary machine is provided. The assembly includes multiple sealing device segments disposed circumferentially intermediate to a stationary housing and a rotor. Each of the segments includes a shoe plate with a forward-shoe section and an aft-shoe section having multiple labyrinth teeth therebetween facing the rotor. The shoe plate is configured to allow a high pressure fluid to a front portion of the plurality of the labyrinth teeth and a low pressure fluid behind the plurality of the labyrinth teeth and further configured to generate an aerodynamic force between the shoe plate and the rotor. The sealing device segment also includes multiple bellow springs or flexures connected to the shoe plate and to a top interface element, wherein the multiple bellow springs or flexures are configured to allow the high pressure fluid to occupy a forward cavity and the low pressure fluid to occupy an aft cavity. Further, the sealing device segments include a secondary seal attached to the top interface element at one first end and positioned about the multiple bellow springs or flexures and the shoe plate at one second end.

Abstract translation: 提供了一种用于旋转机器的气动密封组件。 该组件包括沿周向设置在固定壳体和转子上的多个密封装置段。 每个部分包括具有前靴部分的鞋板和在其间面向转子的多个迷宫齿的后靴部分。 鞋板构造成允许高压流体到多个迷宫齿的前部，以及在多个迷宫齿之后的低压流体，并进一步构造成在鞋板和转子之间产生空气动力。 密封装置段还包括连接到鞋板和顶部接口元件的多个波纹管弹簧或挠曲件，其中多个波纹管弹簧或挠曲构造成允许高压流体占据前腔，低压流体占据 后腔。 此外，密封装置段包括在一个第一端处附接到顶部界面元件并且在一个第二端处围绕多个波纹管弹簧或挠曲件和鞋板定位的次级密封件。

公开(公告)号：US20130312249A1

公开(公告)日：2013-11-28

申请号：US13703956

申请日：2011-06-09

Applicant: Tobias Buchal ,  Björn Buchholz ,  Thomas Hille ,  Anna Kapustina ,  Mirko Milazar ,  Eric Schwerin

Inventor： Tobias Buchal ,  Björn Buchholz ,  Thomas Hille ,  Anna Kapustina ,  Mirko Milazar ,  Eric Schwerin

IPC: F01D11/14

CPC classification number: F01D11/14 ,  F01D21/003 ,  F01D21/04 ,  F05D2260/80 ,  G01B7/14 ,  G01B2210/58 ,  Y10T29/49004

Abstract: A method for measuring and adjusting gaps between a rotor and a stator of a machine using a sensor is provided. The measuring is conducted when the rotor is operated at a rotational speed below a nominal rotational speed of the machine and without the machine being in operation. The adjusting of the gap is carried out as a function of at least one gap dimension of the gap. The sensor is not resistant to an operating temperature of the machine occurring in a region where the sensor is located. After completion of the measuring the machine is operated with the sensor.

Abstract translation: 提供了使用传感器来测量和调整机器的转子和定子之间的间隙的方法。 当转子以低于机器额定转速的转速操作且没有机器运行时进行测量。 间隙的调整作为间隙的至少一个间隙尺寸的函数进行。 传感器不能抵抗传感器所在区域发生的机器的工作温度。 测量完成后，机器用传感器操作。

公开(公告)号：US20130266428A1

公开(公告)日：2013-10-10

申请号：US13440676

申请日：2012-04-05

Applicant: Suresha Kumar Panambur ,  Nagamohan Govinahalli Prabhakar ,  Subramanya Shankar ,  Daniel Loringer ,  Lukas Johnson ,  Andrew Theogift Jeyanth Selwyn Victor

Inventor： Suresha Kumar Panambur ,  Nagamohan Govinahalli Prabhakar ,  Subramanya Shankar ,  Daniel Loringer ,  Lukas Johnson ,  Andrew Theogift Jeyanth Selwyn Victor

IPC: F04D29/40 ,  B23P15/00

CPC classification number: F01D11/14 ,  F01D21/04 ,  F01D21/045 ,  F01D25/24 ,  F02C6/12 ,  Y10T29/49245

Abstract: Various methods and systems are provided for an axial turbine including a containment shroud. In one example, an axial turbine for use in an engine system comprises a turbine disc/blisk and a shroud housing the turbine disc/blisk, the shroud including a first region, a second region, and a third region. A thickness of the second region is dependent on a length between the first region and the third region, and the third region has a burst strength that under a burst condition retains one or more fragments of the turbine disc/blisk.

Abstract translation: 提供了用于包括容纳罩的轴向涡轮机的各种方法和系统。 在一个示例中，用于发动机系统的轴向涡轮机包括涡轮盘/叶片和容纳涡轮盘/叶片的护罩，护罩包括第一区域，第二区域和第三区域。 第二区域的厚度取决于第一区域和第三区域之间的长度，并且第三区域具有在爆发状态下保持涡轮盘/叶片的一个或多个碎片的爆裂强度。

公开(公告)号：US20110103967A1

公开(公告)日：2011-05-05

申请号：US12917071

申请日：2010-11-01

Applicant: Matthias HOEBEL ,  Alexander SCHNELL ,  Yves PELLATON

Inventor： Matthias HOEBEL ,  Alexander SCHNELL ,  Yves PELLATON

IPC: F01D5/14 ,  C23C14/14

CPC classification number: F01D5/20 ,  B23K26/34 ,  B23K35/304 ,  B23K35/327 ,  B23K2101/001 ,  B23K2101/34 ,  B23K2103/08 ,  C23C26/00 ,  C23C28/3215 ,  C23C28/34 ,  C23C28/347 ,  C30B13/24 ,  C30B29/52 ,  F01D5/005 ,  F01D5/28 ,  F01D5/286 ,  F01D5/288 ,  F01D11/12 ,  F01D11/14 ,  F05D2230/31

Abstract: A turbine blade for a turbine rotor, is provided having a single-crystal basic body which has a blade tip and extends in the radial direction. The turbine blade includes at least one oxidation-resistant intermediate coating, which is applied by laser metal forming and is epitaxially bonded to the basic body, is arranged on the radially outer blade tip, and in that an at least single-layer, wear-resistant and oxidation-resistant coating, which is applied by laser metal forming and consists of oxidation-resistant binder material and abrasive particles embedded therein, is arranged on at least certain regions of said epitaxial intermediate coating.

Abstract translation: 一种用于涡轮转子的涡轮机叶片，其具有具有叶片尖端并沿径向方向延伸的单晶基体。 涡轮叶片包括至少一个抗氧化中间涂层，其通过激光金属成形而被施加并且外延地结合到基体上，被布置在径向外侧叶片尖端上，并且至少具有单层， 由所述外延中间涂层的至少某些区域设置通过激光金属成形施加的抗氧化和抗氧化涂层，其由耐氧化粘合剂材料和嵌入其中的磨料颗粒组成。

公开(公告)号：US07869979B2

公开(公告)日：2011-01-11

申请号：US11632333

申请日：2005-07-04

Applicant: Uwe Pfeifer ,  Michael Zidorn

Inventor： Uwe Pfeifer ,  Michael Zidorn

IPC: G01B11/14

CPC classification number: G01S13/58 ,  F01D11/14 ,  F05D2220/32 ,  F05D2260/80 ,  F05D2270/309 ,  G01B15/00 ,  G01B17/00 ,  G01S15/58

Abstract: The invention relates to a method for determining the size of a radial gap between rotating and torsion-proof parts, particularly the parts of a turbomachine. According to said method, an original signal emitted by a transmitter device located on the surface of the rotating part is received in a modified manner by a receiver device disposed on the torsion-proof part and is redirected to an evaluation unit. Said evaluation device determines and displays the size of the radial gap from the received signal by determining the parameters of the trajectory of the rotating transmitter device.

Abstract translation: 本发明涉及一种用于确定旋转和扭转部件之间的径向间隙的尺寸的方法，特别是涡轮机的部件。 根据所述方法，由位于所述旋转部件的表面上的发射机装置发射的原始信号由设置在所述抗扭部件上的接收装置以修改的方式被接收，并被重定向到评估单元。 所述评估装置通过确定旋转发射机装置的轨迹的参数来确定和显示来自接收信号的径向间隙的尺寸。

公开(公告)号：US20100247283A1

公开(公告)日：2010-09-30

申请号：US12411275

申请日：2009-03-25

Applicant: Philip L. Andrew ,  James M. Fogarty

Inventor： Philip L. Andrew ,  James M. Fogarty

IPC: F01D11/22

CPC classification number: F01D11/14 ,  F01D11/20

Abstract: A system, in certain embodiments, includes a magnetic actuator configured to adjust a radial clearance between a housing and rotary blades via translational movement along a rotational axis. The system includes a controller configured to engage the magnetic actuator to adjust the radial clearance in response to feedback.

Abstract translation: 在某些实施例中，系统包括磁致动器，该致动器经配置以通过沿着旋转轴线的平移运动来调节壳体和旋转叶片之间的径向游隙。 该系统包括控制器，该控制器被配置为接合磁致动器以响应于反馈而调节径向游隙。

公开(公告)号：US20100118914A1

公开(公告)日：2010-05-13

申请号：US12267952

申请日：2008-11-10

Applicant: Dean Matthew Erickson ,  Mitch Mircea Orza ,  Michael George Savale ,  Hua Zhang

Inventor： Dean Matthew Erickson ,  Mitch Mircea Orza ,  Michael George Savale ,  Hua Zhang

IPC: G01K1/14

CPC classification number: F01D9/04 ,  F01D9/06 ,  F01D11/14 ,  F05B2260/301 ,  F05D2260/201

Abstract: A mount includes a mounting bolt attached to a casing; an internal bushing that engages the casing at a distal end of the internal bushing; and an external bushing that engages a manifold and engages the internal bushing. The internal bushing is adjustable with respect to the external bushing thereby allowing the manifold to be adjustable with respect to the casing.

Abstract translation: 安装件包括附接到壳体的安装螺栓; 内套管，其在所述内衬套的远端处接合所述壳体; 以及与歧管接合并接合内部衬套的外部衬套。 内部衬套相对于外部衬套可调节，从而允许歧管相对于壳体可调节。

公开(公告)号：US20090180860A1

公开(公告)日：2009-07-16

申请号：US11575419

申请日：2005-09-13

Applicant: Manuele Bigi ,  Piero Lacopetti ,  Riccardo Cini

Inventor： Manuele Bigi ,  Piero Lacopetti ,  Riccardo Cini

IPC: F01D11/24 ,  F01D25/12

CPC classification number: F01D11/24 ,  F01D11/08 ,  F01D11/14 ,  F01D25/12 ,  F05D2260/2214 ,  F05D2260/22141

Abstract: Protection device (10) for a stator of a gas turbine of the type comprising a series of sectors (12) constrained to each other by connection means, each sector (12) has at least one cavity (14) having a bottom (15), in correspondence with at least one cavity (14), a corresponding sheet (20) equipped with a series of pass-through holes (21) and suitable for covering at least one cavity (14) is fixed on an outer surface of the relative sector (12), each sector (12) is cooled by means of a stream of air coming from the pass-through holes (21) of the corresponding sheet (20) which is passed on the bottom (15) and discharged from at least one outlet hole, the bottom (15) of each sector (12) comprises a series of protuberances (30) to increase the thermal exchange surface and increase the cooling efficiency of the protection device (10).

Abstract translation: 一种用于燃气轮机的定子的保护装置（10），其包括通过连接装置彼此约束的一系列扇区（12），每个扇区（12）具有至少一个具有底部（15）的空腔（14） 与至少一个空腔（14）相对应，配备有一系列通孔（21）并适合于覆盖至少一个空腔（14）的相应片材（20）固定在相对的外表面上 扇区（12），每个扇区（12）通过来自相应片材（20）的通孔（21）的空气流冷却，该通过孔（21）通过底部（15）并从至少排出 一个出口孔，每个扇区（12）的底部（15）包括一系列突起（30），以增加热交换表面并提高保护装置（10）的冷却效率。

公开(公告)号：US20040223846A1

公开(公告)日：2004-11-11

申请号：US10430485

申请日：2003-05-06

Inventor： Steven Mitchell Taylor ,  Christina Marie Spencer ,  Dragos Nicolae Licu

IPC: F01D001/02

CPC classification number: F04D29/584 ,  F01D11/14 ,  F01D25/246 ,  F04D29/526 ,  Y02T50/671

Abstract: A method enables a gas turbine engine compressor including a stator assembly and a rotor assembly to be assembled. The method comprises providing a casing formed from a plurality of rings, and coupling a first of the casing rings around the rotor assembly such that a radially inner surface of the first casing ring is axially aligned with, and radially outward from, a row of rotor blades extending from the rotor assembly. The method also comprises coupling a second of the casing rings to the first casing ring with a fastener assembly, such that the first casing ring radially inner surface facilitates insulating the fastener assembly from the compressor flowpath.

Abstract translation: 一种方法使得能够组装包括定子组件和转子组件的燃气涡轮发动机压缩机。 该方法包括提供由多个环形成的壳体，并且将第一壳体环绕转子组件联接，使得第一壳环的径向内表面与一排转子轴向对准并径向向外 叶片从转子组件延伸。 该方法还包括使用紧固件组件将第二壳体环连接到第一壳环，使得第一壳环径向内表面有助于使紧固件组件与压缩机流动路径绝缘。

公开(公告)号：US20020073714A1

公开(公告)日：2002-06-20

申请号：US09741476

申请日：2000-12-19

Inventor： Thomas K. Yim ,  Robert A. Nims ,  Mike Masoudipour

IPC: F02C007/00

CPC classification number: F02C7/06 ,  F01D11/14 ,  F01D25/16 ,  F02C3/085 ,  F02C3/09 ,  F05D2250/312 ,  Y10T29/4932

Abstract: A gas turbine engine having a housing and an axially extending shaft journaled to the housing by two axially spaced apart bearings. The bearings are located along the shaft so as to define an overhung shaft portion. A rotating component such as a turbine wheel or compressor wheel is mounted on the overhung shaft portion and is concentric about the centerline of the engine. An annular shroud that is part of the housing is disposed about the rotating component, the annular shroud being concentric about a centerline radially offset from the engine.

Abstract translation: 一种燃气涡轮发动机，其具有壳体和轴向延伸的轴，其通过两个轴向间隔开的轴承轴颈连接到壳体。 轴承沿着轴定位，以便限定悬挂轴部分。 诸如涡轮机叶轮或压缩机叶轮的旋转部件安装在悬臂轴部上并且与发动机的中心线同心。 作为壳体的一部分的环形护罩围绕旋转部件设置，环形护罩与围绕发动机径向偏移的中心线同心。