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：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：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.