公开(公告)号：US12084988B2

公开(公告)日：2024-09-10

申请号：US17593226

申请日：2020-03-06

Applicant: NUOVO PIGNONE TECNOLOGIE—S.r.l.

Inventor： Michelangelo Bellacci ,  Gianfranco Maffulli ,  Lorenzo Cosi ,  Nicola Ciarla

IPC: F01D5/28 ,  C10G11/18 ,  C10G75/00 ,  F01D5/20 ,  F01D11/12

CPC classification number: F01D5/288 ,  C10G11/18 ,  C10G75/00 ,  F01D5/20 ,  F01D11/122 ,  F05D2220/62 ,  F05D2230/90 ,  F05D2240/307 ,  F05D2300/6111

Abstract: A blade for fluid catalytic cracking (FCC) flue hot gas expander with a layer of hard abrasive material localized on the blade tip that contributes to reducing the accumulation of FCC catalyst residuals in the expander.

公开(公告)号：US11851769B2

公开(公告)日：2023-12-26

申请号：US16994810

申请日：2020-08-17

Applicant: General Electric Company

Inventor： Julin Wan ,  Larry Steven Rosenzweig

IPC: C04B41/89 ,  C04B41/00 ,  C04B41/52 ,  C23C4/10 ,  C23C4/12 ,  C23C24/10 ,  F01D5/28 ,  C23C14/08 ,  C23D5/00

CPC classification number: C23C24/103 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  C23C4/10 ,  C23C4/12 ,  C23C14/08 ,  C23D5/005 ,  F01D5/282 ,  F01D5/284 ,  F01D5/288 ,  F05D2230/90 ,  F05D2300/211 ,  F05D2300/514 ,  F05D2300/6033 ,  F05D2300/611 ,  F05D2300/6111 ,  Y02T50/60 ,  C04B41/009 ,  C04B35/80 ,  C04B41/52 ,  C04B41/5096 ,  C04B41/52 ,  C04B41/5071 ,  C04B41/522 ,  C04B41/52 ,  C04B41/5024 ,  C04B41/52 ,  C04B41/4527 ,  C04B41/4572 ,  C04B41/5024 ,  C04B41/52 ,  C04B41/4527 ,  C04B41/4572 ,  C04B41/5027 ,  C04B41/522

Abstract: Methods for preparing an environmental barrier coating and the resulting coating are provided. The methods and products include the incorporation of a continuous ceramic inner layer and a segmented ceramic outer layer on a CMC component. The segmented ceramic outer layer may be formed by thermal spray techniques. The coating is more stable at higher temperatures and provides for a longer lifetime of the coated component.

公开(公告)号：US20160214176A1

公开(公告)日：2016-07-28

申请号：US14333543

申请日：2014-07-17

Applicant: Siemens Energy, Inc.

Inventor： Gerald J. Bruck ,  Ahmed Kamel

IPC: B22F3/11 ,  B22F5/04 ,  B23K26/342 ,  B22F3/105 ,  C23C24/10 ,  C23C24/08

CPC classification number: B22F3/1125 ,  B22F3/1055 ,  B22F5/04 ,  B22F7/006 ,  B22F2999/00 ,  B23K26/342 ,  C23C24/085 ,  C23C24/103 ,  F01D5/288 ,  F05D2300/514 ,  F05D2300/6111 ,  B22F3/105 ,  B22F2202/11

Abstract: A layer of a powdered material (4) is heated with an energy beam (10) such that at least one gas-generating agent (8) reacts to form at least one gaseous substance (14) to produce a void-containing coating (16) adhered to the surface of a substrate (2).The powdered material may contain a metallic material, a ceramic material, or both, and may also contain at least one of a flux material (32) containing the gas-generating agent and an exothermic agent (64). The heating may occur using a laser beam and may induce a melting or sintering of the powdered material to produce the void-containing coating. A gas turbine engine component exhibiting improved thermal and mechanical properties may be formed to include the void-containing coating, which may take the form of a bond coating, a thermal barrier coating, or both.

Abstract translation: 用能量束（10）加热一层粉末材料（4），使得至少一种气体发生剂（8）反应形成至少一种气态物质（14）以产生含空隙的涂层（16） ）附着在基板（2）的表面上。 粉状材料可以含有金属材料，陶瓷材料或两者，并且还可以含有含有气体发生剂的助焊剂材料（32）和放热剂（64）中的至少一种。 可以使用激光束进行加热，并且可以引起粉末材料的熔化或烧结以产生含空隙的涂层。 可以形成具有改善的热和机械性能的燃气涡轮发动机部件，以包括可以采取粘合涂层，热障涂层或两者的形式的含空隙的涂层。

公开(公告)号：US20080256926A1

公开(公告)日：2008-10-23

申请号：US11737794

申请日：2007-04-20

Applicant: Reza ZIAEI ,  Victor Salivon ,  Jaroslaw Wojcik

Inventor： Reza ZIAEI ,  Victor Salivon ,  Jaroslaw Wojcik

IPC: F02K3/00 ,  B21K1/28 ,  F02C1/00

CPC classification number: F04D29/023 ,  F04D29/441 ,  F05D2250/52 ,  F05D2300/22 ,  F05D2300/611 ,  F05D2300/6111 ,  Y10T29/4932

Abstract: A diffuser for a centrifugal compressor in a gas turbine engine, the diffuser including a diffuser ring having a series of bores defined therethrough to receive and direct air exiting the compressor, each bore being defined by a respective bore surface including a boride layer protecting the bore surface from erosion damage.

Abstract translation: 用于燃气涡轮发动机中的离心压缩机的扩散器，所述扩散器包括扩散器环，所述扩散器环具有通过其限定的一系列孔，以接收和引导离开压缩机的空气，每个孔由相应的孔表面限定，包括保护孔的硼化物层 表面受侵蚀破坏。

公开(公告)号：US20170324168A1

公开(公告)日：2017-11-09

申请号：US15477655

申请日：2017-04-03

Applicant: ROLLS-ROYCE plc

Inventor： Daniel CLARK ,  Werner P. SCHIFFERS

IPC: H01Q13/24 ,  H04B3/52 ,  H04B1/40 ,  F01D25/00 ,  H01Q1/28 ,  F01D25/24 ,  H01Q1/32 ,  H01Q1/34 ,  F04D29/52

CPC classification number: H01Q13/24 ,  F01D25/005 ,  F01D25/24 ,  F04D29/522 ,  F05D2300/6111 ,  H01P3/16 ,  H01Q1/287 ,  H01Q1/3225 ,  H01Q1/34 ,  H04B1/40 ,  H04B3/52

Abstract: A component including a substrate with dielectric coating on the substrate. The electrical reactance of the dielectric coating configured for the propagation of electromagnetic surface waves. The dielectric coating is arranged as a plurality of discrete pathways. Also a signal transmission system including a component, an electromagnetic surface wave transmitter coupled to the substrate, and an electromagnetic surface wave receiver also coupled to the substrate.

公开(公告)号：US20170248319A1

公开(公告)日：2017-08-31

申请号：US15595760

申请日：2017-05-15

Applicant: General Electric Company

Inventor： Kevin Weston McMahan ,  Geoffrey David Myers

IPC: F23R3/28 ,  F01D5/28 ,  F01D9/02 ,  F01D9/04 ,  F01D25/00 ,  F04D29/02 ,  F04D29/32 ,  F23R3/00 ,  B33Y10/00 ,  B33Y80/00 ,  B22F3/105 ,  B22F5/00 ,  B22F5/04 ,  B22F7/02 ,  B22F7/00 ,  B23K26/342 ,  B23K26/00 ,  B23K15/00 ,  B28B1/00 ,  F01D5/14

CPC classification number: F23R3/286 ,  B22F3/1055 ,  B22F5/009 ,  B22F5/04 ,  B22F7/008 ,  B22F7/02 ,  B22F7/06 ,  B22F2207/17 ,  B22F2301/15 ,  B22F2301/205 ,  B22F2301/35 ,  B22F2998/10 ,  B23K15/0086 ,  B23K15/0093 ,  B23K26/0006 ,  B23K26/32 ,  B23K26/342 ,  B23K2101/001 ,  B23K2103/05 ,  B23K2103/08 ,  B23K2103/14 ,  B23K2103/166 ,  B23K2103/24 ,  B23K2103/26 ,  B28B1/001 ,  B29C64/153 ,  B32B7/02 ,  B32B15/01 ,  B32B2264/105 ,  B32B2307/102 ,  B32B2307/304 ,  B32B2603/00 ,  B32B2605/18 ,  B33Y10/00 ,  B33Y80/00 ,  F01D5/147 ,  F01D5/28 ,  F01D9/023 ,  F01D9/041 ,  F01D25/005 ,  F04D29/023 ,  F04D29/324 ,  F05D2230/22 ,  F05D2230/31 ,  F05D2300/10 ,  F05D2300/6111 ,  F23K5/00 ,  F23M5/00 ,  F23M2900/05004 ,  F23R3/00 ,  F23R3/002 ,  F23R2900/00018 ,  Y02P10/295 ,  Y10T428/12028

Abstract: A system includes a layered structure. The layered structure includes first and second coalesced layers and an intermediate layer disposed between the first and second coalesced layers. The first and second coalesced layers have a higher degree of coalescence than the intermediate layer.

公开(公告)号：US08852720B2

公开(公告)日：2014-10-07

申请号：US12837051

申请日：2010-07-15

Applicant: Ann Bolcavage ,  Raymond J. Sinatra

Inventor： Ann Bolcavage ,  Raymond J. Sinatra

IPC: B32B3/24 ,  B32B3/30 ,  B32B3/26 ,  B05D1/36 ,  B05D3/00 ,  C23C4/02 ,  F01D5/28

CPC classification number: F01D5/288 ,  B32B3/263 ,  C23C4/02 ,  C23C28/00 ,  C23C28/3215 ,  C23C30/00 ,  F01D5/14 ,  F01D5/20 ,  F01D5/286 ,  F01D11/08 ,  F05D2230/14 ,  F05D2260/231 ,  F05D2300/611 ,  F05D2300/6111 ,  Y10T29/49336 ,  Y10T428/24273 ,  Y10T428/24322 ,  Y10T428/24471 ,  Y10T428/24479 ,  Y10T428/24496 ,  Y10T428/24521 ,  Y10T428/24529 ,  Y10T428/24537 ,  Y10T428/2457 ,  Y10T428/24612 ,  Y10T428/24942 ,  Y10T428/24992 ,  Y10T428/26

Abstract: An article may include an array of features formed in a substrate and may be coated by a thermal barrier coating (TBC). The array of features may mitigate thermal stress experienced by the coated article. In particular, the array of features may reduce or limit crack propagation at or above the interface of a thermally insulative layer and a bond coat in the TBC. In some embodiments, the array may be formed proximate to and substantially aligned with cooling holes formed in the substrate. In other embodiments, an article may include a first array of features formed in a first location of a substrate and a second array of features formed in a second location of a substrate. The first and second locations may be determined or selected based on a prediction of thermal stresses that the substrate will experience at the first and second locations during use.

Abstract translation: 制品可以包括在基底中形成的特征阵列，并且可以由热障涂层（TBC）涂覆。 特征阵列可以减轻涂层制品经受的热应力。 特别地，特征阵列可以减少或限制在TBC中的绝热层和粘结层的界面上或上方的裂纹扩展。 在一些实施例中，阵列可以形成在衬底中形成的冷却孔附近并基本对齐。 在其他实施例中，制品可以包括形成在基板的第一位置中的第一特征阵列和形成在基板的第二位置中的第二特征阵列。 可以基于在使用期间衬底将在第一和第二位置处经历的热应力的预测来确定或选择第一和第二位置。

公开(公告)号：US08505305B2

公开(公告)日：2013-08-13

申请号：US11737794

申请日：2007-04-20

Applicant: Reza Ziaei ,  Victor Salivon ,  Jaroslaw Wójcik

Inventor： Reza Ziaei ,  Victor Salivon ,  Jaroslaw Wójcik

IPC: F02C1/00

CPC classification number: F04D29/023 ,  F04D29/441 ,  F05D2250/52 ,  F05D2300/22 ,  F05D2300/611 ,  F05D2300/6111 ,  Y10T29/4932

Abstract: A diffuser for a centrifugal compressor in a gas turbine engine, the diffuser including a diffuser ring having a series of bores defined therethrough to receive and direct air exiting the compressor, each bore being defined by a respective bore surface including a boride layer protecting the bore surface from erosion damage.

Abstract translation: 用于燃气涡轮发动机中的离心压缩机的扩散器，所述扩散器包括扩散器环，所述扩散器环具有通过其限定的一系列孔，以接收和引导离开压缩机的空气，每个孔由相应的孔表面限定，包括保护孔的硼化物层 表面受侵蚀破坏。

公开(公告)号：US11753957B2

公开(公告)日：2023-09-12

申请号：US17602967

申请日：2020-04-10

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Clément Bourolleau ,  Alexandre Branco ,  Serge Domingues ,  Vincent Fiore ,  Anwer Siraj

IPC: F01D11/12 ,  F01D21/00 ,  F01D25/24

CPC classification number: F01D11/122 ,  F01D21/003 ,  F01D25/24 ,  F05D2230/31 ,  F05D2300/516 ,  F05D2300/6111

Abstract: A method for detecting at least one roughness in a face of an abradable layer in a fan casing is provided. The method includes a step of depositing on the abradable layer a first coating and a second coating covering the first coating. The first and second coatings have respective thicknesses (N1, N2) and a physical appearance that differ from one another. Local appearance of the first coating is indicative of a need for a localized touch-up, and local disappearance of the first coating and the second coating is indicative of a need for a localized replacement of the abradable layer.

公开(公告)号：US11732598B2

公开(公告)日：2023-08-22

申请号：US17554819

申请日：2021-12-17

Applicant: Rolls-Royce Corporation ,  Rolls-Royce High Temperature Composites Inc.

Inventor： Ted J. Freeman ,  Jeremy Roehm

IPC: F01D11/12 ,  F01D25/00 ,  F01D25/28 ,  F01D25/24

CPC classification number: F01D11/122 ,  F01D25/005 ,  F01D25/24 ,  F01D25/28 ,  F05D2240/11 ,  F05D2250/75 ,  F05D2260/30 ,  F05D2300/6033 ,  F05D2300/6111

Abstract: A turbine shroud segment for use in a gas turbine engine includes a ceramic shroud segment formed to define a circumferentially extending channel that opens radially inwardly and a layer of abradable material that extends axially along a radial inner surface of the ceramic shroud segment to provide a flow path surface of the turbine shroud segment.