公开(公告)号：AT468425T

公开(公告)日：2010-06-15

申请号：AT02251839

申请日：2002-03-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ALLEN WILLIAM P ,  VERONESI WILLIAM A ,  APPLEBY JOHN W ,  HALL ROBERT J ,  MALONEY MICHAEL J ,  HAGUE DOUGLAS C ,  KHAN ABDUS

IPC: C04B41/87 ,  C23C28/00 ,  C23C14/06

Abstract: An article has a protective ceramic coating 26 which reduces radiation heat transport through the ceramic coating. The protective ceramic coating 26 includes one or more embedded reflective metallic layers 30', 30'', 30''' for reducing the radiation heat transport. The article may be a turbine component and the coating 26 may be a thermal barrier coating.

公开(公告)号：AT466968T

公开(公告)日：2010-05-15

申请号：AT03252839

申请日：2003-05-07

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEERS RUSSELL ALBERT ,  NOETZEL ALLAN A ,  KHAN ABDUS

IPC: C23C14/16 ,  C22C19/03 ,  C23C4/08 ,  C23C14/06 ,  C23C14/32 ,  C23C16/06 ,  C23C28/00 ,  C23C30/00

Abstract: The present invention relates to a metallic coating to be deposited on gas turbine engine components. The metallic coating comprises up to 18 wt% cobalt, 3.0 to 18 wt% chromium, 5.0 to 15 wt% aluminum, 0.1 to 1.0 wt% yttrium, up to 0.6 wt% hafnium, up to 0.3 wt% silicon, 3.0 to 10 wt% tantalum, up to 9.0 wt% tungsten, 1.0 to 6.0 wt% rhenium, up to 10 wt% molybdenum, and the balance nickel.

公开(公告)号：DE60236393D1

公开(公告)日：2010-07-01

申请号：DE60236393

申请日：2002-03-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ALLEN WILLIAM P ,  VERONESI WILLIAM A ,  APPLEBY JOHN W ,  HALL ROBERT J ,  MALONEY MICHAEL J ,  HAGUE DOUGLAS C ,  KHAN ABDUS

IPC: C04B41/87 ,  C23C28/00 ,  C23C14/06

公开(公告)号：DE60332413D1

公开(公告)日：2010-06-17

申请号：DE60332413

申请日：2003-05-07

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEERS RUSSELL ALBERT ,  NOETZEL ALLAN A ,  KHAN ABDUS

IPC: C23C14/16 ,  C22C19/03 ,  C23C4/08 ,  C23C14/06 ,  C23C14/32 ,  C23C16/06 ,  C23C28/00 ,  C23C30/00

公开(公告)号：CA2427550C

公开(公告)日：2008-04-22

申请号：CA2427550

申请日：2003-05-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEERS RUSSELL ALBERT ,  NOETZEL ALLAN A ,  KHAN ABDUS

IPC: C23C30/00 ,  C22C19/03 ,  C23C4/08 ,  C23C14/06 ,  C23C14/16 ,  C23C16/06 ,  C23C28/00 ,  C23F15/00

Abstract: The present invention relates to a metallic coating to be deposited on gas turbine engine components. The metallic coating comprises up to 18 wt% cobalt, 3.0 to 18 wt% chromium, 5.0 to 15 wt% aluminum, 0.1 to 1.0 wt% yttrium, up to 0.6 wt% hafnium, up to 0.3 wt% silicon, 3.0 to 10 wt% tantalum, up to 9.0 wt% tungsten, 1.0 to 6.0 wt% rhenium, up to 10 wt% molybdenum, and the balance nickel.

公开(公告)号：CA2427550A1

公开(公告)日：2003-11-07

申请号：CA2427550

申请日：2003-05-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NOETZEL ALLAN A ,  KHAN ABDUS ,  BEERS RUSSELL ALBERT

IPC: C22C19/03 ,  C23C4/08 ,  C23C14/06 ,  C23C14/16 ,  C23C16/06 ,  C23C28/00 ,  C23C30/00 ,  C23C4/06 ,  C23F15/00

Abstract: The present invention relates to a metallic coating to be deposited on gas turbine engine components. The metallic coating comprises up to 18 wt% cobalt, 3.0 to 18 wt% chromium, 5.0 to 15 wt% aluminum, 0.1 to 1.0 wt% yttrium, up to 0.6 wt% hafnium, up to 0.3 wt% silicon, 3.0 to 10 wt% tantalum, up to 9.0 wt% tungsten, 1.0 to 6.0 wt% rhenium, up to 10 wt% molybdenum, and the balance nickel.

公开(公告)号：ZA200303348B

公开(公告)日：2003-11-04

申请号：ZA200303348

申请日：2003-04-30

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEERS RUSSELL ALBERT ,  NOETZEL ALLAN A ,  KHAN ABDUS

IPC: C22C19/03 ,  C23C4/08 ,  C23C14/06 ,  C23C14/16 ,  C23C16/06 ,  C23C28/00 ,  C23C30/00 ,  C23C

Abstract: The present invention relates to a metallic coating to be deposited on gas turbine engine components. The metallic coating comprises up to 18 wt% cobalt, 3.0 to 18 wt% chromium, 5.0 to 15 wt% aluminum, 0.1 to 1.0 wt% yttrium, up to 0.6 wt% hafnium, up to 0.3 wt% silicon, 3.0 to 10 wt% tantalum, up to 9.0 wt% tungsten, 1.0 to 6.0 wt% rhenium, up to 10 wt% molybdenum, and the balance nickel.