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：EP2971240A4

公开(公告)日：2016-12-21

申请号：EP13878078

申请日：2013-12-30

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAZEL BRIAN T ,  LITTON DAVID A ,  MALONEY MICHAEL J

IPC: C23C28/00 ,  C23C4/11 ,  C23C4/134 ,  C23C28/04

CPC classification number: C23C4/134 ,  C23C4/11 ,  C23C28/042

Abstract: A thermal barrier coating is applied to a turbine engine component having a substrate. The thermal barrier coating has a first layer which has a strain tolerant columnar microstructure at an interface with the substrate for spallation resistance and a second layer which is porous conduction and radiation thermally resistant at an outer surface of the thermal barrier coating.