公开(公告)号：US20140328672A1

公开(公告)日：2014-11-06

申请号：US14335203

申请日：2014-07-18

Applicant: ALSTOM Technology Ltd

Inventor： Herbert BRANDL ,  Hans-Peter BOSSMANN

IPC: F01D11/18 ,  F01D11/12

CPC classification number: F01D11/18 ,  F01D9/04 ,  F01D11/08 ,  F01D11/122 ,  F01D25/246 ,  F05D2240/11 ,  F05D2240/55 ,  F05D2260/30 ,  F05D2300/20 ,  F05D2300/21 ,  F05D2300/2112 ,  F05D2300/2118 ,  F05D2300/50212

Abstract: A stator component of a turbomachine is composed substantially of at least one axially extending outer ring (10) which serves as a frame of an inner ring composed of partial segments (20). The partial segments are arranged on one another such that, on the rotor side, they form a coherent circular circumferential surface in relation to the rotational movement of rotor blades (30). The individual partial segment (20) is composed of a material of uniform construction or, at least in a radial direction, of multiple partial bodies constructed from different materials, such as for example ceramic, wherein a partial segment thus formed exhibits predetermined stress and/or expansion behaviour as a function of the load ranges of the turbomachine.

Abstract translation: 涡轮机的定子部件基本上由至少一个轴向延伸的外环（10）组成，其用作由部分段（20）构成的内环的框架。 部分片段彼此布置，使得在转子侧，它们相对于转子叶片（30）的旋转运动形成相干的圆周表面。 单个部分段（20）由均匀构造的材料或至少在径向方向上由由不同材料（例如陶瓷）构成的多个部分体构成，其中如此形成的部分段呈现预定的应力和/ 或膨胀行为作为涡轮机的负载范围的函数。

公开(公告)号：US20140272456A1

公开(公告)日：2014-09-18

申请号：US14209761

申请日：2014-03-13

Applicant: United Technologies Corporation

Inventor： Mladen F. Trubelja ,  Dinesh K. Gupta ,  Brian S. Tryon ,  Mark T. Ucasz ,  Benjamin J. Zimmerman

IPC: F01D5/28 ,  C23C14/08 ,  C23C14/16 ,  C23C14/32 ,  H01J37/32

CPC classification number: C23C14/08 ,  C23C14/16 ,  C23C14/24 ,  C23C14/325 ,  F01D5/288 ,  F05D2300/13 ,  F05D2300/175 ,  F05D2300/2118 ,  Y10T428/12618

Abstract: A coated article has: a metallic substrate (22); a bondcoat (30); and a thermal barrier coating (TBC) (28). The bondcoat has a first layer (32) and a second layer (34), the first layer having a lower Cr content than the second layer.

Abstract translation: 涂覆制品具有：金属基底（22）; 粘合剂涂层（30）; 和热障涂层（TBC）（28）。 键合涂层具有第一层（32）和第二层（34），第一层具有比第二层低的Cr含量。

公开(公告)号：US08402745B2

公开(公告)日：2013-03-26

申请号：US11579212

申请日：2005-05-03

Applicant: William Anthony Denne

Inventor： William Anthony Denne

IPC: F02K5/02

CPC classification number: F02K7/04 ,  F02K7/02 ,  F05D2250/70 ,  F05D2300/2118 ,  Y02T50/671

Abstract: A pulse jet engine comprising a quarter wave gas resonator (1) which is arranged to cycle at an ultrasonic frequency, wherein the resonator (1) is closed, or substantially closed, to gas flow at the pressure antinode (4) thereof. The shape and dimensions of the quarter wave gas resonator (1) at least partially determine the ultrasonic frequency at which the resonator (1) cycles.

Abstract translation: 一种脉冲喷气发动机，包括四分之一波长的气体谐振器（1），其布置成以超声波频率循环，其中所述谐振器（1）关闭或基本上封闭在其压力波腹（4）处的气流。 四分之一波长气体谐振器（1）的形状和尺寸至少部分地确定谐振器（1）在其周期的超声波频率。

公开(公告)号：US08343573B2

公开(公告)日：2013-01-01

申请号：US12679389

申请日：2008-09-19

Applicant: Jens Dahl Jensen ,  Jens Klingemann ,  Ursus Krüger ,  Daniel Körtvelyessy ,  Volkmar Lüthen ,  Ralph Reiche ,  Oliver Stier

Inventor： Jens Dahl Jensen ,  Jens Klingemann ,  Ursus Krüger ,  Daniel Körtvelyessy ,  Volkmar Lüthen ,  Ralph Reiche ,  Oliver Stier

IPC: B05C13/00 ,  C23C4/08

CPC classification number: C23C30/00 ,  B22F5/04 ,  B22F7/08 ,  B23P6/007 ,  B23P6/045 ,  C23C24/04 ,  F01D5/005 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/40 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/2112 ,  F05D2300/2118

Abstract: A method for repairing a component such as a turbine blade is provided. At the end of its operating time, the component has, for example, a depletion of aluminium in a region near the surface. The application of a repair layer is provided including particles with an increased proportion of aluminium. A subsequent heat treatment may achieve the effect of equalizing the concentration of aluminium between the repair layer and the region near the surface, and so the aluminium content required for new components is achieved again.

Abstract translation: 提供了一种用于修理诸如涡轮叶片的部件的方法。 在其运行时间结束时，组件例如在靠近表面的区域中铝的消耗。 提供了修复层的应用，包括具有增加的铝比例的颗粒。 随后的热处理可以实现使修复层和表面附近的区域之间的铝浓度相等的效果，因此再次实现新组分所需的铝含量。

公开(公告)号：US20120244383A1

公开(公告)日：2012-09-27

申请号：US13053378

申请日：2011-03-22

Applicant: Peter Joel Meschter ,  Raymond Grant Rowe

Inventor： Peter Joel Meschter ,  Raymond Grant Rowe

IPC: B32B15/04 ,  F01D5/28 ,  B32B18/00 ,  B32B9/00

CPC classification number: C23C28/042 ,  B32B9/00 ,  B32B9/005 ,  B32B15/04 ,  B32B18/00 ,  C04B35/48 ,  C04B35/50 ,  C04B41/009 ,  C04B41/5044 ,  C04B41/52 ,  C04B41/89 ,  C23C28/3215 ,  C23C28/34 ,  C23C28/3455 ,  F01D5/28 ,  F01D5/284 ,  F01D5/288 ,  F05D2260/95 ,  F05D2300/2118 ,  Y02T50/67 ,  Y02T50/672 ,  Y10T428/12611 ,  Y10T428/12618 ,  Y10T428/12931 ,  Y10T428/12944 ,  Y10T428/12951 ,  Y10T428/12972 ,  Y10T428/31678 ,  C04B35/565 ,  C04B35/806 ,  C04B35/584 ,  C04B35/58085 ,  C04B41/4527 ,  C04B41/5096 ,  C04B41/5024 ,  C04B41/5037 ,  C04B41/5031 ,  C04B41/5042 ,  C04B41/522 ,  C04B41/455 ,  C04B41/5045 ,  C04B41/5048 ,  C04B41/5027

Abstract: A coating system on a superalloy or silicon-containing substrate of an article exposed to high temperatures. The coating system includes a coating layer that overlies the substrate and is susceptible to hot corrosion promoted by molten salt impurities. A corrosion barrier coating overlies the coating layer and contains at least one rare-earth oxide-containing compound that reacts with the molten salt impurities to form a dense, protective byproduct barrier layer.

Abstract translation: 在暴露于高温的制品的超级合金或含硅衬底上的涂层体系。 涂层系统包括覆盖在基底上的涂层，并易受熔融盐杂质促进的热腐蚀。 防腐涂层覆盖在涂层上并含有至少一种与熔融盐杂质反应形成致密的保护性副产物阻挡层的含稀土氧化物的化合物。

公开(公告)号：US20120163984A1

公开(公告)日：2012-06-28

申请号：US12975609

申请日：2010-12-22

Applicant: Ronald Scott Bunker

Inventor： Ronald Scott Bunker

IPC: F03B3/12 ,  B05D3/12 ,  F28F7/00

CPC classification number: F01D5/187 ,  F01D5/288 ,  F04D29/023 ,  F04D29/584 ,  F05D2230/312 ,  F05D2230/313 ,  F05D2300/17 ,  F05D2300/21 ,  F05D2300/2118 ,  F05D2300/611 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676

Abstract: A method for providing a fluid cooling system within a high temperature component is described. At least one microchannel is formed in an external surface of the component; and one or more coolant passage holes are then formed, extending from at least one of the microchannels to an interior region of the component. A layer of a metallic structural coating is then applied over the external surface. At least one slot, or a set of relatively small passive cooling holes, are then formed through the metallic structural coating; extending into at least a portion of the microchannels. A second coating layer is then applied over the first layer. In some embodiments, a sacrificial material is deposited into the microchannels before the first coating layer is applied. Related articles are also described.

Abstract translation: 描述了一种在高温部件内提供流体冷却系统的方法。 在组件的外表面中形成至少一个微通道; 然后形成一个或多个冷却剂通道孔，从微通道中的至少一个延伸到部件的内部区域。 然后将一层金属结构涂层施加在外表面上。 然后通过金属结构涂层形成至少一个狭槽或一组相对小的被动冷却孔; 延伸到微通道的至少一部分。 然后将第二涂层施加在第一层上。 在一些实施例中，在施加第一涂层之前将牺牲材料沉积到微通道中。 还描述了相关文章。

公开(公告)号：US20110299994A1

公开(公告)日：2011-12-08

申请号：US13146495

申请日：2010-01-20

Applicant: Thomas Behnisch ,  Anett Berndt ,  Christoph Ebert ,  René Füssel ,  Heinrich Kapitza ,  Albert Langkamp ,  Markus Mantei ,  Heinrich Zeininger

Inventor： Thomas Behnisch ,  Anett Berndt ,  Christoph Ebert ,  René Füssel ,  Heinrich Kapitza ,  Albert Langkamp ,  Markus Mantei ,  Heinrich Zeininger

IPC: F01D5/14 ,  B23P15/02

CPC classification number: F01D5/282 ,  F01D5/288 ,  F05D2260/95 ,  F05D2300/133 ,  F05D2300/2112 ,  F05D2300/2118 ,  F05D2300/2261 ,  F05D2300/603 ,  F05D2300/614 ,  F05D2300/615 ,  Y10T29/49337

Abstract: A section of a turbine blade includes a fiber composite material having a matrix and fibers embedded therein. The matrix includes nanoparticles that are distributed in or on the matrix. The turbine blade can for example be used as a rotor blade in the final stage of a condensing steam turbine.

Abstract translation: 涡轮叶片的一部分包括具有嵌入其中的基体和纤维的纤维复合材料。 该基质包括分布在基质中或基质上的纳米颗粒。 涡轮叶片可以例如在冷凝蒸汽轮机的最后阶段用作转子叶片。

公开(公告)号：US20110291311A1

公开(公告)日：2011-12-01

申请号：US13206568

申请日：2011-08-10

Applicant: Frigyes Szuecs ,  Alexander Stankowski

Inventor： Frigyes Szuecs ,  Alexander Stankowski

IPC: B32B43/00 ,  B29C73/00

CPC classification number: C04B41/009 ,  C04B41/502 ,  C04B41/53 ,  C04B41/5338 ,  C04B41/85 ,  C04B41/91 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F05D2300/2118 ,  C04B41/457 ,  C04B41/459 ,  C04B35/48

Abstract: A process for extending the cyclic service life of thermal barrier coatings made of yttrium-stabilized zirconium oxide (YSZ) or the like which have been applied to a substrate with an oxidizing bond coat in between includes increasing or long-term stabilizing the strain tolerance of the thermal barrier coating.

Abstract translation: 用于延长由钇稳定的氧化锆（YSZ）等制成的热障涂层的循环使用寿命的方法，其已经施加到其间具有氧化粘结涂层的基底上，包括增加或长期稳定应变耐受性 热障涂层。

公开(公告)号：US08021720B2

公开(公告)日：2011-09-20

申请号：US12014893

申请日：2008-01-16

Applicant: Frigyes Szuecs ,  Alexander Stankowski

Inventor： Frigyes Szuecs ,  Alexander Stankowski

IPC: B05D3/10

CPC classification number: C04B41/009 ,  C04B41/502 ,  C04B41/53 ,  C04B41/5338 ,  C04B41/85 ,  C04B41/91 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F05D2300/2118 ,  C04B41/457 ,  C04B41/459 ,  C04B35/48

Abstract: A process for extending the cyclic service life of thermal barrier coatings made of yttrium-stabilized zirconium oxide (YSZ) or the like which have been applied to a substrate with an oxidizing bond coat in between includes increasing or long-term stabilizing the strain tolerance of the thermal barrier coating.

Abstract translation: 用于延长由钇稳定的氧化锆（YSZ）等制成的热障涂层的循环使用寿命的方法，其已经施加到其间具有氧化粘结涂层的基底上，包括增加或长期稳定的应变耐受性 热障涂层。

公开(公告)号：US07736760B2

公开(公告)日：2010-06-15

申请号：US11453874

申请日：2006-06-16

Applicant: Andrew R. Nicoll ,  Scott Wilson

Inventor： Andrew R. Nicoll ,  Scott Wilson

IPC: B32B9/00 ,  F04D29/08

CPC classification number: F01D11/125 ,  C04B35/48 ,  C04B35/486 ,  C04B35/488 ,  C04B35/4885 ,  C04B35/62655 ,  C04B38/009 ,  C04B38/08 ,  C04B2111/00362 ,  C04B2111/00982 ,  C04B2235/3217 ,  C04B2235/3225 ,  C04B2235/3246 ,  C04B2235/528 ,  C04B2235/96 ,  C04B2235/963 ,  C23C4/11 ,  F01D11/122 ,  F05D2300/121 ,  F05D2300/134 ,  F05D2300/15 ,  F05D2300/2112 ,  F05D2300/2118 ,  F05D2300/702 ,  Y02T50/67 ,  Y02T50/672 ,  C04B38/067

Abstract: A ceramic abradable material is provided for use for clearance control between turbine blade tips and the shroud or casing in gas turbine engines for industrial and/or aerospace applications. The ceramic abradable material includes an yttria stabilized zirconia (YSZ) that is doped in alumina (Al2O3). The ceramic abradable in accordance with the invention is a soft abradable material that provides for increased erosion resistance as well as the ability of the turbine blade tips to cut into the abradable without causing them damage. These properties allow for optimum tolerances within the gas turbine engine which results in superior efficiency and performance.

Abstract translation: 提供陶瓷耐磨材料用于在用于工业和/或航空应用的燃气涡轮发动机中的涡轮机叶片尖端与罩壳或套管之间的间隙控制。 陶瓷耐磨材料包括掺杂在氧化铝（Al 2 O 3）中的氧化钇稳定的氧化锆（YSZ）。 根据本发明可磨损的陶瓷是柔软的耐磨材料，其提供增加的抗侵蚀性，以及涡轮叶片尖端切割成可磨损而不致使其损坏的能力。 这些性能允许在燃气涡轮发动机内的最佳公差，这导致优异的效率和性能。