公开(公告)号：US20120294721A1

公开(公告)日：2012-11-22

申请号：US13576071

申请日：2011-01-21

Applicant: Michael Delapierre ,  Patrick Jean-Louis Reghezza

Inventor： Michael Delapierre ,  Patrick Jean-Louis Reghezza

IPC: F01D5/02

CPC classification number: F01D5/3007 ,  F01D5/3092 ,  F04D29/322 ,  F05C2201/0466

Abstract: A turbine engine air blower including a rotor disk that includes, on an outer periphery thereof, longitudinal ribs, each including a radial lug for attaching the disk onto a downstream compressor rotor. The flanks of the lugs form abutments for holding vanes that are mounted onto the disk. A mechanism protecting flanks of the lugs is circumferentially inserted between the lugs and the vanes.

Abstract translation: 一种涡轮发动机空气鼓风机，包括转子盘，该转子盘在其外周上包括纵向肋，每个肋包括用于将盘附接到下游压缩机转子上的径向凸耳。 凸耳的侧面形成用于保持安装在盘上的叶片的支座。 保护凸缘的侧面的机构周向地插入在凸耳和叶片之间。

公开(公告)号：US08277952B2

公开(公告)日：2012-10-02

申请号：US12641777

申请日：2009-12-18

Applicant: Takahiro Sugioka ,  Takayuki Kato ,  Atsushi Saito ,  Shino Okubo ,  Hiroaki Sato ,  Taichi Nakamizo

Inventor： Takahiro Sugioka ,  Takayuki Kato ,  Atsushi Saito ,  Shino Okubo ,  Hiroaki Sato ,  Taichi Nakamizo

IPC: B32B15/04 ,  B32B15/18 ,  F16H23/00 ,  F16J1/02

CPC classification number: F04B27/1054 ,  F04B27/0886 ,  F04B27/1063 ,  F04B27/109 ,  F05C2201/021 ,  F05C2201/0406 ,  F05C2201/0412 ,  F05C2201/0466 ,  F05C2203/06 ,  F05C2203/0813 ,  F05C2203/0882 ,  F05C2253/12 ,  Y10T74/18336 ,  Y10T428/12625 ,  Y10T428/12736 ,  Y10T428/1275

Abstract: A sliding member for a compressor includes a base metal, a first layer and a second layer. The base metal is made of an aluminum-based metal. The first layer is formed on or over the base metal and made of a nickel-based plating layer containing at least one material of nitrogen (N), silicon (Si), titanium (Ti), chromium (Cr) and aluminum (Al) as an additive. The second layer is formed on the surface of the first layer and made of a diamond-like carbon layer containing the same additive as the additive contained in the first layer.

Abstract translation: 用于压缩机的滑动构件包括基底金属，第一层和第二层。 贱金属由铝基金属制成。 第一层形成在基体金属上或上方，由含有氮（N），硅（Si），钛（Ti），铬（Cr）和铝（Al））的至少一种材料的镍基镀层形成， 作为添加剂。 第二层形成在第一层的表面上，并由含有与第一层中所含添加剂相同的添加剂的类金刚石碳层制成。

公开(公告)号：US20120099978A1

公开(公告)日：2012-04-26

申请号：US13147686

申请日：2010-02-04

Applicant: Roman Beyer ,  Boris Bublath ,  Ingo Just ,  Thomas Podgorski

Inventor： Roman Beyer ,  Boris Bublath ,  Ingo Just ,  Thomas Podgorski

IPC: F01D25/00 ,  B23P17/00

CPC classification number: F01D5/288 ,  B23P15/04 ,  B23P2700/06 ,  C23C28/00 ,  C23C28/022 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/345 ,  C23C28/3455 ,  C23C30/00 ,  F01D5/284 ,  F01D5/286 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/60 ,  F05D2230/90 ,  F05D2240/90 ,  F05D2300/11 ,  F05D2300/15 ,  F05D2300/607 ,  F23R3/06 ,  F23R2900/00018 ,  Y02T50/67 ,  Y02T50/675 ,  Y10T29/49229

Abstract: Turbine components are often shipped individually and are not shipped assembled into a turbine. To this end, the turbine blade has to be protected of external stresses and external damage. This is done by an easily removable protective coating that easily evaporates during the first operation of the newly produced or restored component, so that the protective coating does not have to be removed in an additional operational step before installation.

Abstract translation: 涡轮机组件通常是单独运输的，没有运输组装到涡轮机中。 为此，涡轮机叶片必须受到外部应力和外部损坏的保护。 这是通过易于移除的保护涂层完成的，其在新生产或恢复的部件的第一次操作期间容易蒸发，使得在安装之前不需要在额外的操作步骤中去除保护涂层。

公开(公告)号：US20110286840A1

公开(公告)日：2011-11-24

申请号：US13146372

申请日：2009-02-05

Applicant: Douglas Eric Bissell ,  Athanasios Diakomis ,  Louis J. Lengyel

Inventor： Douglas Eric Bissell ,  Athanasios Diakomis ,  Louis J. Lengyel

IPC: F04D29/40 ,  B23P15/00

CPC classification number: F04C19/00 ,  F01C21/10 ,  F04C2240/802 ,  F04C2280/04 ,  F05C2201/0442 ,  F05C2201/046 ,  F05C2201/0466 ,  F05C2201/0475 ,  F05C2225/00 ,  Y10T29/49243 ,  Y10T29/49245

Abstract: A liquid ring pump is provided that includes an annular housing having an inner surface forming a housing cavity. The annular housing is filled with an operating fluid during operation of the pump. The operating fluid forms an eccentric liquid ring in the annular housing during operation of the pump. A rotor is disposed in the housing cavity and includes a plurality of rotor blades. A shaft extends into the annular housing into the housing cavity. The plurality of rotor blades extend radially outward from the shaft toward the inner surface of the annular housing. A liner formed from a corrosion resistant material is disposed substantially flush with at least a portion of the annular housing inner surface opposite a plurality of rotor blade ends.

Abstract translation: 提供一种液环泵，其包括具有形成壳体腔的内表面的环形壳体。 在泵的操作期间，环形壳体填充有工作流体。 在泵的操作期间，工作流体在环形壳体中形成偏心液体环。 转子设置在壳体腔中并包括多个转子叶片。 轴延伸到环形壳体中进入壳体腔体。 多个转子叶片从轴向径向向外延伸到环形壳体的内表面。 由耐腐蚀材料形成的衬套基本上与环形壳体内表面的与多个转子叶片端部相对的至少一部分齐平。

公开(公告)号：US20110268584A1

公开(公告)日：2011-11-03

申请号：US12771789

申请日：2010-04-30

Applicant: Don Mittendorf

Inventor： Don Mittendorf

IPC: F01D5/18

CPC classification number: F01D5/28 ,  C30B11/00 ,  C30B29/52 ,  F01D5/288 ,  F05C2201/0466 ,  F05D2230/90 ,  F05D2240/307 ,  F05D2300/134 ,  F05D2300/143 ,  F05D2300/607 ,  F05D2300/611 ,  Y02T50/67

Abstract: Blades, turbine blade assemblies, and methods of forming blades are provided. The blade includes an airfoil including a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root, and a tip, the convex suction side wall, the concave pressure side wall, and the tip each including interior surfaces that together define an internal cooling circuit, the airfoil including a single crystal superalloy, and a cladding layer disposed over the tip, the cladding layer including a zirconia grain stabilized platinum alloy.

Abstract translation: 提供叶片，涡轮叶片组件以及形成叶片的方法。 叶片包括具有凸吸入侧壁，凹压侧壁，前缘，后缘，根部和顶端的翼型件，凸起的吸入侧壁，凹形压力侧壁和端部各自包括 共同限定内部冷却回路的内表面，包括单晶超合金的翼型以及设置在尖端上的包层，所述包覆层包括氧化锆晶粒稳定的铂合金。

公开(公告)号：US08016549B2

公开(公告)日：2011-09-13

申请号：US11486743

申请日：2006-07-13

Applicant: Dilip M. Shah ,  Joseph G. Hillebrand ,  Daniel E. Kane

Inventor： Dilip M. Shah ,  Joseph G. Hillebrand ,  Daniel E. Kane

IPC: F01D25/26

CPC classification number: F01D11/005 ,  F01D5/16 ,  F01D5/22 ,  F01D5/24 ,  F01D11/006 ,  F01D17/04 ,  F01D25/06 ,  F02C7/052 ,  F05C2201/0466 ,  F05D2300/11 ,  F05D2300/50 ,  F05D2300/607 ,  F16J15/0806 ,  F16J15/0887 ,  G01H11/08 ,  G10K11/24 ,  Y10T29/4932

Abstract: A method is provided for engineering a single crystal cast gas turbine engine first component for cooperating with a second component. An at least local first operational stress on the first component is determined. The first operational stress has a first direction. A crystal orientation within the component or a physical configuration of the component is selected so that the first operational stress produces a desired engagement of the first component with the second component associated with either a negative Poisson's effect or high Poisson's effect in a second direction. Single crystal or highly textured iron- and nickel-base alloys enable one to use such effect in high temperature and/or corrosive environments.

Abstract translation: 提供了一种用于工程化单晶铸造燃气涡轮发动机第一部件以与第二部件配合的方法。 确定第一部件上的至少局部第一操作应力。 第一个操作压力有第一个方向。 选择部件内的晶体取向或部件的物理结构，使得第一操作应力产生第一部件与第二部件的期望接合，该第二部件与第二方向上的负泊松效应或高泊松效应相关联。 单晶或高度纹理化的铁和镍基合金使得能够在高温和/或腐蚀性环境中使用这种效果。

公开(公告)号：US07850423B2

公开(公告)日：2010-12-14

申请号：US11739358

申请日：2007-04-24

Applicant: Katsuya Yamashita

Inventor： Katsuya Yamashita

IPC: F04D29/44

CPC classification number: F01D5/063 ,  F01D5/066 ,  F05C2201/0466 ,  F05D2220/31 ,  F05D2300/171

Abstract: High-temperature steam at 620° C. or higher is introduced to a reheat steam turbine 100, and a turbine rotor 113 of the reheat steam turbine 100 includes: a high-temperature turbine rotor constituent part 113a positioned in an area extending from a nozzle 114a on a first stage to a moving blade 115a on a stage where temperature of the steam becomes 550° C. and made of a corrosion and heat resistant material; and low-temperature turbine rotor constituent parts 113b connected to and sandwiching the high-temperature turbine rotor constituent part 113a and made of a material different from the material of the high-temperature turbine rotor constituent part 113a.

Abstract translation: 将620℃以上的高温蒸汽引入再热蒸汽轮机100，再热蒸汽轮机100的涡轮转子113包括：高温涡轮机转子构成部113a，其位于从喷嘴延伸的区域 114a在蒸汽温度为550℃并由耐腐蚀和耐热材料制成的台上的动叶片115a上; 以及与高温涡轮机转子构成部113a连接并夹着高温涡轮转子构成部113a并由与高温涡轮转子构成部113a的材料不同的材料构成的低温涡轮转子构成部113b。

公开(公告)号：US07837440B2

公开(公告)日：2010-11-23

申请号：US11160272

申请日：2005-06-16

Applicant: Ronald S. Bunker ,  Gary Michael Itzel

Inventor： Ronald S. Bunker ,  Gary Michael Itzel

IPC: F01D5/08

CPC classification number: F01D5/20 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2260/2212 ,  F05D2260/2214 ,  F05D2260/22141

Abstract: A tip cap piece for use in a turbine bucket. The tip cap piece may include a cold side and a number of pins positioned on the cold side.

Abstract translation: 用于涡轮机桶的顶盖件。 尖端盖可以包括冷侧和位于冷侧的多个销。

公开(公告)号：US20100236217A1

公开(公告)日：2010-09-23

申请号：US11460791

申请日：2006-07-28

Applicant: Kattalaicheri Srinivasan Venkataramani ,  Thomas Ory Moniz ,  Justin P. Stephenson

Inventor： Kattalaicheri Srinivasan Venkataramani ,  Thomas Ory Moniz ,  Justin P. Stephenson

IPC: F02K99/00

CPC classification number: F01D25/125 ,  F01D9/06 ,  F01D25/08 ,  F02C7/047 ,  F02K3/06 ,  F05C2201/0466 ,  F05D2260/207 ,  F05D2260/208 ,  F05D2300/11 ,  F05D2300/133 ,  Y02T50/671 ,  Y02T50/675

Abstract: A heat transfer system is provided for a turbine engine of the type including an annular casing with an array of thermally conductive, generally radially-extending strut members disposed therein. The heat transfer system includes at least one arcuate heat pipe disposed in contact with an outer surface of the casing within fore-and-aft limits of the axial extent of the strut members. The heat pipe is thermally coupled to a heat source, such that heat from the heat source can be transferred through the heat pipe and the casing to the strut members.

Abstract translation: 提供了一种用于这种类型的涡轮发动机的传热系统，其包括具有布置在其中的导热的，大致径向延伸的支柱构件阵列的环形壳体。 传热系统包括至少一个弧形热管，其布置成与支撑构件的轴向范围的前后的极限内的壳体的外表面接触。 热管被热耦合到热源，使得来自热源的热量可以通过热管和壳体传递到支柱构件。

公开(公告)号：US20100119359A1

公开(公告)日：2010-05-13

申请号：US12605533

申请日：2009-10-26

Applicant: Richard Brendon Scarlin ,  Roger Padfield ,  Helen Elizabeth Parker ,  Robert Jupp ,  Ian Michael Vale ,  Martin Reigl ,  Maurus Herzog ,  Rolf Doebler

Inventor： Richard Brendon Scarlin ,  Roger Padfield ,  Helen Elizabeth Parker ,  Robert Jupp ,  Ian Michael Vale ,  Martin Reigl ,  Maurus Herzog ,  Rolf Doebler

IPC: F01D17/12 ,  F01D25/24

CPC classification number: F01D25/26 ,  F01D25/005 ,  F05B2250/86 ,  F05C2201/0466 ,  F05D2220/31 ,  F05D2230/21 ,  F05D2230/232 ,  F05D2230/50 ,  F05D2250/80

Abstract: A steam turbine with an operating temperature of more than 650° C. includes a thermally highly-loaded housing (G) which is produced by a casting technique at least partially from a nickel-based alloy. Production of such a steam turbine is simplified by the housing (G) being divided into a multiplicity of smaller housing sections (G1, . . . , G8; G21, G22, G31, G32) which are interconnected and together form the housing (G).

Abstract translation: 工作温度高于650℃的蒸汽轮机包括通过至少部分由镍基合金的铸造技术制造的热高负载外壳（G）。 通过将壳体（G）分成多个相互连接并一起形成外壳（G，...，G8; G21，G22，G31，G32）的较小外壳部分（G，G21，G22，G31，G32） ）。