公开(公告)号：US20140308116A1

公开(公告)日：2014-10-16

申请号：US14249489

申请日：2014-04-10

Applicant: ALSTOM Technology Ltd

Inventor： Gregoire Etienne WITZ ,  Mathieu Esquerre ,  Michael Stuer ,  Daniel Renusch ,  Hans-Peter Bossmann

IPC: F01D11/12

CPC classification number: F01D11/122 ,  F01D9/04 ,  F05D2230/642 ,  F05D2240/11 ,  F05D2300/21

Abstract: Shroud device thermally protecting a gas turbine blade, having a ceramic layer and a metallic layer, the metallic layer being thermally protected by the ceramic layer, the ceramic layer being mechanically joined to the metallic layer by a fixation device having a plurality of protrusions located in the metallic layer designed so as to engage with a plurality of cavities located in the ceramic layer, such that there exists a gap between the cavities and the protrusions at ambient temperature, the gap disappearing at high temperature operation of the gas turbine, the protrusions being then locked into the cavities.

Abstract translation: 护罩装置热保护具有陶瓷层和金属层的燃气轮机叶片，金属层被陶瓷层热保护，陶瓷层通过具有多个突起的固定装置机械连接到金属层 金属层设计成与位于陶瓷层中的多个空腔接合，使得在环境温度下在空腔和突起之间存在间隙，在燃气轮机的高温运行时，间隙消失，突起为 然后锁定到空腔中。

公开(公告)号：US20140242411A1

公开(公告)日：2014-08-28

申请号：US14272979

申请日：2014-05-08

Applicant: ALSTOM Technology Ltd ,  Eidgenössische Technische Hochschule Zürich

Inventor： Gregoire Etienne WITZ ,  Hans-Peter BOSSMANN ,  Anup BHATTACHARYA ,  Valery SHKLOVER

IPC: F01D5/28 ,  C23C4/10

CPC classification number: F01D5/288 ,  C04B35/486 ,  C04B2235/3225 ,  C04B2235/3251 ,  C04B2235/765 ,  C23C4/02 ,  C23C4/11 ,  C23C28/3215 ,  C23C28/3455 ,  F05D2230/80 ,  F05D2300/135 ,  F05D2300/2118 ,  Y10T428/12549 ,  Y10T428/12618 ,  Y10T428/31678

Abstract: A high temperature thermal barrier coating which consists of a stabilized ZrO2 composition for the protection of thermally loaded components (10, 10′) of a thermal machine, especially a gas turbine, is disclosed. The thermal barrier coating is stabilized with at least 15 mol % Y1+v Ta1−vO4−v, the ZrO2 is partially substituted by at least 10 mol % HfO2 and the composition is established according to the formula (Y1+vTa1−vO4−v)z(Zr1−xHfxO2)1−z, with x ranging from 0.1 to 0.5, v ranging from −0.1 to 0.2 and z ranging from 0.15 to 0.25.

Abstract translation: 公开了一种由用于保护热机器，特别是燃气轮机的热负荷组件（10,10'）的稳定的ZrO 2组合物组成的高温热障涂层。 热障涂层用至少15mol％的Y1 + v Ta1-vO4-v稳定，ZrO 2被至少10mol％HfO 2部分取代，并且组成按照式（Y1 + vTa1-vO4-v ）z（Zr1-xHfxO2）1-z，x为0.1至0.5，v为-0.1至0.2，z为0.15至0.25。

公开(公告)号：US20150218954A1

公开(公告)日：2015-08-06

申请号：US14601311

申请日：2015-01-21

Applicant: ALSTOM Technology Ltd.

Inventor： Gregoire Etienne WITZ ,  Michael Stuer ,  Hans-Peter Bossmann

IPC: F01D5/28 ,  F01D5/30

CPC classification number: F01D5/282 ,  F01D5/147 ,  F01D5/20 ,  F01D5/284 ,  F01D5/3007 ,  F01D5/3053 ,  F01D5/3061 ,  F01D5/3084 ,  F01D5/3092 ,  F05D2300/6033 ,  F05D2300/611

Abstract: A composite turbine blade for high-temperature applications such as gas turbines or the like includes a root for mounting the blade in a corresponding circumferential assembly groove of a rotor and an airfoil connected to said root. An inner carrying structure is provided extending at least over a portion of the root as well as at least a portion of said airfoil. The inner carrying structure is made of a high strength eutectic ceramic and the airfoil is made of a ceramic matrix composite (CMC) material.

Abstract translation: 用于诸如燃气轮机等的高温应用的复合涡轮叶片包括用于将叶片安装在转子的相应周向组装槽中的根部和连接到所述根部的翼型件。 提供内部承载结构，其延伸至根部的至少一部分以及所述翼型的至少一部分。 内承载结构由高强度共晶陶瓷制成，翼型由陶瓷基复合材料（CMC）制成。

公开(公告)号：US20170341339A1

公开(公告)日：2017-11-30

申请号：US15681705

申请日：2017-08-21

Applicant: ALSTOM TECHNOLOGY LTD.

Inventor： Matthias HOEBEL ,  Hans-Peter BOSSMANN ,  Gregoire Etienne WITZ

IPC: B32B7/08 ,  B32B18/00 ,  B23K26/211 ,  B23K26/342 ,  B23K1/19 ,  B23K26/03 ,  B23K26/32 ,  C04B37/02 ,  F23R3/00 ,  B23K26/60 ,  B23K103/00 ,  B23K103/16

CPC classification number: B32B7/08 ,  B23K1/19 ,  B23K26/032 ,  B23K26/211 ,  B23K26/32 ,  B23K26/342 ,  B23K26/60 ,  B23K2103/172 ,  B23K2103/52 ,  B32B18/00 ,  C04B37/026 ,  C04B2235/945 ,  C04B2237/12 ,  C04B2237/592 ,  C04B2237/595 ,  C04B2237/64 ,  C04B2237/72 ,  F23M2900/05004 ,  F23R3/007 ,  Y10T428/12618

Abstract: A configuration for joining a ceramic layer has a thermal insulating material to a metallic layer. The configuration includes an interface layer made of metallic material located between the ceramic layer and the metallic layer, which includes a plurality of interlocking elements on one of its sides, facing the ceramic layer, the ceramic layer comprising a plurality of cavities aimed at connecting with the corresponding interlocking elements of the interface layer. The configuration also includes a brazing layer by means of which the interface layer is joint to the metallic layer. The invention also refers to a method for obtaining such a configuration.

公开(公告)号：US20160123151A1

公开(公告)日：2016-05-05

申请号：US14925021

申请日：2015-10-28

Applicant: ALSTOM Technology Ltd

Inventor： Mageshwaran RAMESH ,  Thomas SCHREIER ,  Ingo KUEHN ,  Gregoire Etienne WITZ

IPC: F01D5/08

Abstract: The invention relates to a steam turbine rotor wherein the inter blade region rotor surface, the feed region rotor surface, the piston region rotor surface and the stress relief groove rotor surface of the rotor are configured and arranged as steam exposed surfaces during normal operation of the steam turbine rotor. The steam turbine rotor has a thermal barrier coating on at least the piston region rotor surface.

Abstract translation: 本发明涉及一种蒸汽轮机转子，其中叶片区域转子表面，进料区转子表面，活塞区转子表面和转子的应力释放槽转子表面在正常操作期间被配置和布置为蒸汽暴露表面 汽轮机转子。 蒸汽轮机转子至少在活塞区域转子表面上具有热障涂层。

公开(公告)号：US20140308539A1

公开(公告)日：2014-10-16

申请号：US14250665

申请日：2014-04-11

Applicant: ALSTOM Technology Ltd

Inventor： Gregoire Etienne WITZ ,  Matthias HOEBEL ,  Hans-Peter BOSSMANN

IPC: B23K26/20 ,  B23K26/30 ,  B23K26/32 ,  B32B7/08 ,  B23K26/03

CPC classification number: B32B7/08 ,  B23K1/19 ,  B23K26/032 ,  B23K26/211 ,  B23K26/32 ,  B23K26/342 ,  B23K26/60 ,  B23K2103/172 ,  B23K2103/52 ,  B32B18/00 ,  C04B37/026 ,  C04B2235/945 ,  C04B2237/12 ,  C04B2237/592 ,  C04B2237/595 ,  C04B2237/64 ,  C04B2237/72 ,  F23M2900/05004 ,  F23R3/007 ,  Y10T428/12618

Abstract: A configuration for joining a ceramic layer has a thermal insulating material to a metallic layer. The configuration includes an interface layer made of metallic material located between the ceramic layer and the metallic layer, which includes a plurality of interlocking elements on one of its sides, facing the ceramic layer, the ceramic layer comprising a plurality of cavities aimed at connecting with the corresponding interlocking elements of the interface layer. The configuration also includes a brazing layer by means of which the interface layer is joint to the metallic layer. The invention also refers to a method for obtaining such a configuration.

Abstract translation: 用于接合陶瓷层的构造具有对金属层的绝热材料。 该构造包括由位于陶瓷层和金属层之间的金属材料制成的界面层，该界面层包括在其一个侧面上的多个互锁元件，面对陶瓷层，陶瓷层包括多个空腔，其旨在与 接口层的相应互锁元件。 该构造还包括钎焊层，通过该钎焊层，界面层与金属层接合。 本发明还涉及获得这种结构的方法。