公开(公告)号：EP2964807A4

公开(公告)日：2016-11-23

申请号：EP13876883

申请日：2013-12-30

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  MALONEY MICHAEL J

IPC: C23C4/04

CPC classification number: C09D5/08 ,  C08K3/08 ,  C08K3/38 ,  C08K2003/0812 ,  C08K2003/0862 ,  C08K2003/0881 ,  C08K2003/385 ,  C23C4/04 ,  C23C30/00

Abstract: An abradable coating for application to a gas turbine engine part is formed from a titanium aluminide alloy, a filler material, and porosity. The coating may be applied to a part such as a casing made from a titanium alloy.

Abstract translation: 用于燃气涡轮发动机部件的耐磨涂层由钛铝化合物，填料和孔隙形成。 涂层可以施加到诸如由钛合金制成的壳体的部件上。

公开(公告)号：EP2971560A4

公开(公告)日：2016-06-22

申请号：EP13878721

申请日：2013-12-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： AMINI SHAHRAM ,  STROCK CHRISTOPHER W ,  BURLATSKY SERGEI F ,  NOVIKOV DMITRI ,  FURRER DAVID ULRICH

IPC: F01D5/28 ,  B23K1/00 ,  B23K1/19 ,  B23K20/02 ,  B23K20/22 ,  B23K26/00 ,  B23K26/34 ,  B23K103/16 ,  C04B35/56 ,  C04B35/58 ,  C04B41/51 ,  C23C24/04 ,  F01D5/14 ,  F01D9/04 ,  F01D11/12 ,  F01D11/20 ,  F02C7/30

CPC classification number: F01D11/122 ,  B23K1/0006 ,  B23K1/19 ,  B23K20/02 ,  B23K20/22 ,  B23K26/0006 ,  B23K26/34 ,  B23K2203/16 ,  C23C4/04 ,  C23C24/04 ,  F01D5/288 ,  F01D9/041 ,  F01D11/12 ,  F01D11/20 ,  F05D2220/30 ,  F05D2230/236 ,  F05D2230/237 ,  F05D2230/312 ,  F05D2230/60 ,  F05D2230/90 ,  F05D2240/125 ,  F05D2240/307 ,  F05D2300/6032

Abstract: A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.

Abstract translation: 涡轮发动机系统包括具有翼型部分和尖端的涡轮发动机部件，该涡轮发动机部件具有结合到尖端的MAXMET复合材料。 MAXMET复合材料在金属基体中具有MAX相。

公开(公告)号：EP3071731A4

公开(公告)日：2017-07-19

申请号：EP14864151

申请日：2014-10-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W

IPC: C23C26/00 ,  F02C7/28

CPC classification number: F01D11/08 ,  C09D121/00 ,  C09D175/04 ,  F01D11/02 ,  F01D11/122 ,  F05D2220/32 ,  F05D2220/329 ,  F05D2240/55 ,  F05D2260/607 ,  F05D2300/431 ,  F05D2300/506 ,  F05D2300/615 ,  F05D2300/70 ,  F16J15/44 ,  Y02T50/675

Abstract: A seal is formed of a matrix and includes hard particles. The matrix has a shear strength of greater than or equal to 200 psi and less than or equal to 2000 psi. A gas turbine engine is also disclosed.

Abstract translation: 密封件由基质形成并包含硬质颗粒。 基体具有大于或等于200psi且小于或等于2000psi的剪切强度。 燃气涡轮发动机也被公开。

公开(公告)号：EP3068918A4

公开(公告)日：2017-07-12

申请号：EP14862096

申请日：2014-10-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W

IPC: C23C4/10 ,  C23C4/02 ,  C23C4/04 ,  C23C4/134 ,  C23C4/18 ,  F01D5/28 ,  F23R3/00

CPC classification number: C23C4/134 ,  C23C4/02 ,  C23C4/04 ,  C23C4/10 ,  C23C4/18 ,  F01D5/288 ,  F05D2230/312 ,  F05D2300/6033 ,  F23M2900/05004 ,  F23R3/002 ,  F23R2900/00018

Abstract: A method of manufacturing a fiber reinforced coating. The method includes providing a substrate and plasma spraying a ceramic matrix having fibers encapsulated in a precursor material onto the substrate.

Abstract translation: 一种制造纤维增强涂层的方法。 该方法包括提供衬底并将具有封装在前体材料中的纤维的陶瓷基体等离子喷涂到衬底上。

公开(公告)号：EP3052787A4

公开(公告)日：2017-05-31

申请号：EP14851155

申请日：2014-09-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  LUTJEN PAUL M ,  BRUSKOTTER MICHAEL J

IPC: F01D11/12

CPC classification number: F01D11/122 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C28/32 ,  C23C28/3455 ,  F01D11/02 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2240/11 ,  F05D2240/55 ,  F16J15/40

Abstract: An air seal system for a rotor blade assembly of a gas turbine engine includes a substrate. An optional ceramic interlayer may be disposed on an optional bond coat deposited on the substrate. An erosion resistant thermal barrier coating (E-TBC) layer is disposed on the ceramic interlayer (if present) or on the bond coat, or on the substrate. An abradable layer is disposed on the erosion resistant thermal barrier coating (E-TBC) layer.

Abstract translation: 用于燃气涡轮发动机的转子叶片组件的气封系统包括基板。 可选的陶瓷夹层可以设置在沉积在基底上的可选粘合涂层上。 在陶瓷夹层（如果存在的话）上或在粘合涂层上或在基材上设置抗侵蚀热障涂层（E-TBC）层。 耐磨热障涂层（E-TBC）上设置耐磨层。

公开(公告)号：EP2233599B1

公开(公告)日：2017-05-03

申请号：EP10006996

申请日：2006-08-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  DAVIS CHARLES G

IPC: C23C4/02 ,  C23C4/06 ,  C23C4/12

CPC classification number: C23C4/02 ,  C23C4/06 ,  C23C4/12 ,  C23C4/134 ,  C23C28/3215 ,  C23C28/345 ,  F01D5/288 ,  F01D11/122 ,  F05D2230/90 ,  F05D2240/11 ,  F05D2300/21 ,  Y02T50/672

公开(公告)号：EP3055445A4

公开(公告)日：2017-11-01

申请号：EP14852182

申请日：2014-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  JAWOROWSKI MARK R ,  MASE FRANK W

IPC: C23C4/06 ,  C22C21/02 ,  C23C4/18 ,  C23C24/04

CPC classification number: F01D11/122 ,  C22C21/02 ,  C23C4/04 ,  C23C4/06 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C22/02 ,  C23C24/04 ,  C23C26/00 ,  F01D5/12 ,  F01D9/02 ,  F01D25/24 ,  F05D2220/32 ,  F05D2230/31 ,  F05D2300/173 ,  F05D2300/43

Abstract: A corrosion resistant aluminum alloy abradable coating for use as a seal material consists of a porous base metal alloy layer containing corrosion inhibiting metal compounds dispersed throughout the porous base metal alloy layer. A method of forming a corrosion resistant aluminum alloy abradable coating consists of co-thermal spraying aluminum alloy powder plus polymer powder and particles containing corrosion inhibiting metal compounds.

公开(公告)号：EP3074619A4

公开(公告)日：2017-04-26

申请号：EP14865602

申请日：2014-11-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  AMINI SHAHRAM

IPC: C23C4/06 ,  C23C4/10 ,  C23C28/04 ,  F01D5/28

CPC classification number: C23C28/042 ,  C23C4/06 ,  C23C4/10 ,  F01D5/288 ,  F01D25/00 ,  F02C7/24 ,  F05D2300/182 ,  F05D2300/2261 ,  F05D2300/2283

Abstract: A component for high temperature applications includes a substrate and a layer of an aluminum-containing MAX phase material and another material applied to the substrate.

Abstract translation: 用于高温应用的部件包括衬底和含铝的MAX相材料层以及施加到衬底的另一种材料。

公开(公告)号：EP2961930A4

公开(公告)日：2016-12-07

申请号：EP14756958

申请日：2014-01-30

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FARRIS JOHN R ,  STROCK CHRISTOPHER W ,  LUTJEN PAUL M

IPC: F01D5/02 ,  F01D5/00 ,  F02C7/00

CPC classification number: F01D11/24 ,  F01D5/14 ,  F01D9/023 ,  F05D2240/11 ,  F05D2250/00 ,  F05D2250/182 ,  F05D2250/294

Abstract: A gas turbine engine component according to an exemplary aspect of the present disclosure includes, among other things, a body having a first outer face meeting a second outer face at an intersection, the body having a plurality of apertures extending from an opening in the first outer face to an opening on the second outer face; and a coating filling at least a portion of the plurality of apertures.

Abstract translation: 根据本公开的示例性方面的燃气涡轮发动机部件尤其包括具有在交叉点处会合第二外表面的第一外表面的本体，所述主体具有从第一 外表面到第二外表面上的开口; 以及填充所述多个孔的至少一部分的涂层。

公开(公告)号：EP2971533A4

公开(公告)日：2016-11-16

申请号：EP14769696

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W

IPC: F01D5/14 ,  F01D5/20 ,  F01D5/28 ,  F01D11/12 ,  F02C7/28

CPC classification number: F01D5/288 ,  F01D5/284 ,  F01D11/08 ,  F01D11/122 ,  F01D25/24 ,  F05D2220/32 ,  F05D2230/31 ,  F05D2240/307 ,  F05D2300/171 ,  F05D2300/173 ,  F05D2300/177 ,  F05D2300/2106 ,  F05D2300/211 ,  F05D2300/2112 ,  F05D2300/2118 ,  F05D2300/506 ,  F05D2300/6032 ,  F05D2300/611 ,  Y02T50/673

Abstract: A method of preventing transfer of metal of a gas turbine rotor blade having a metal tip to a blade outer air seal coating on a gas turbine case includes forming a coating on the metal tip. The coating comprises a bond coat layer on the metal tip and a ceramic filled metallic layer having a ceramic component in a matrix of a metal MCr, MCrAl, MCrAlY or a refractory modified MCrAlY where M is nickel, cobalt, iron or mixtures thereof.