公开(公告)号：WO2014065928A3

公开(公告)日：2014-07-17

申请号：PCT/US2013054088

申请日：2013-08-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SHROCK CHRISTOPHER W ,  MALONEY MICHAEL ,  LITTON DAVID A ,  ZIMMERMAN BENJAMIN JOSEPH ,  HAZEL BRIAN T

IPC: F01D5/18 ,  F01D5/14 ,  F02C7/00

CPC classification number: C23C4/02 ,  C23C4/11 ,  C23C4/134 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/3455 ,  C23C28/347 ,  F01D5/288 ,  F05D2300/13 ,  F05D2300/514 ,  Y10T428/249981 ,  Y10T428/31678

Abstract: A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.

Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板，沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料，所述环境污染物与外层接触以改变外层的微观结构。

公开(公告)号：EP3097219A4

公开(公告)日：2017-02-15

申请号：EP15737817

申请日：2015-01-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TRUBELJA MLADEN F ,  LITTON DAVID A ,  DEPALMA JOSEPH A ,  NEAL JAMES W ,  MALONEY MICHAEL ,  BEERS RUSSELL A ,  HAZEL BRIAN T ,  COTNOIR GLENN A

IPC: C23C14/06 ,  C23C14/08 ,  C23C14/22 ,  C23C14/24 ,  C23C14/30 ,  C23C14/50 ,  C23C14/54 ,  F01D9/04 ,  F01D15/10

CPC classification number: C23C14/542 ,  C23C14/083 ,  C23C14/243 ,  C23C14/30 ,  C23C14/505 ,  C23C14/54 ,  F01D9/041 ,  F01D15/10 ,  F05D2220/32 ,  F05D2230/313 ,  F05D2230/90 ,  F05D2300/2118

Abstract: A method for use in a physical vapor deposition coating process includes depositing a ceramic coating material from a plume onto at least one substrate to form a ceramic coating thereon, and during the deposition, rotating the at least one substrate at rotational speed selected with respect to deposition rate of the ceramic coating material onto the at least one substrate.

Abstract translation: 用于物理气相沉积涂覆方法的方法包括将陶瓷涂层材料从羽状物沉积到至少一个基底上以在其上形成陶瓷涂层，并且在沉积期间，以相对于 陶瓷涂层材料沉积到至少一个基底上。

公开(公告)号：EP2885518A4

公开(公告)日：2015-08-26

申请号：EP13829397

申请日：2013-08-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  MALONEY MICHAEL ,  LITTON DAVID A ,  ZIMMERMAN BENJAMIN JOSEPH ,  HAZEL BRIAN T

IPC: F02C7/00 ,  C23C28/00 ,  F01D5/00 ,  F01D5/28

CPC classification number: F02C7/24 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/3455 ,  C23C28/36 ,  F01D5/286 ,  F01D5/288 ,  F05D2230/90 ,  F05D2300/501 ,  F05D2300/514 ,  Y10T428/24942 ,  Y10T428/249981

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer includes a material that absorbs energy in response to an impact event along at least a portion of the outer layer.

Abstract translation: 根据本公开的示例性方面的部件包括基材，沉积在基材的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层。 外层包括响应于沿外层的至少一部分的冲击事件吸收能量的材料。

公开(公告)号：SG11201501113UA

公开(公告)日：2015-04-29

申请号：SG11201501113U

申请日：2013-08-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  MALONEY MICHAEL ,  LITTON DAVID A ,  ZIMMERMAN BENJAMIN JOSEPH ,  HAZEL BRIAN T

IPC: F02C7/00 ,  F01D5/00

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer includes a material that absorbs energy in response to an impact event along at least a portion of the outer layer.

公开(公告)号：EP2893148A4

公开(公告)日：2015-11-04

申请号：EP13849810

申请日：2013-08-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SHROCK CHRISTOPHER W ,  MALONEY MICHAEL ,  LITTON DAVID A ,  ZIMMERMAN BENJAMIN JOSEPH ,  HAZEL BRIAN T

IPC: F01D5/18 ,  C23C4/02 ,  C23C4/08 ,  C23C4/10 ,  C23C4/12 ,  C23C28/00 ,  F01D5/14 ,  F02C7/00

CPC classification number: C23C4/02 ,  C23C4/11 ,  C23C4/134 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/3455 ,  C23C28/347 ,  F01D5/288 ,  F05D2300/13 ,  F05D2300/514 ,  Y10T428/249981 ,  Y10T428/31678

Abstract: A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.

Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板，沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料，其与外层接触以改变外层的微观结构。