Segmented ceramic layer for member of gas turbine engine

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Dynamically created seal

Reexamination Certificate

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Details

C415S173100, C415S173600, C415S173700, C415S200000

Reexamination Certificate

active

08079806

ABSTRACT:
A turbine seal member for use in a gas turbine engine includes a turbine seal substrate having a gas-path side and a ceramic layer disposed on the gas-path side that includes a plurality of mechanical indentations.

REFERENCES:
patent: 4652209 (1987-03-01), Buddenbohm
patent: 4758480 (1988-07-01), Hecht
patent: 5352540 (1994-10-01), Schienle et al.
patent: 5687679 (1997-11-01), Mullin
patent: 5830586 (1998-11-01), Gray
patent: 5933976 (1999-08-01), Pressutti
patent: 5951892 (1999-09-01), Wolfla
patent: 6102656 (2000-08-01), Nissley
patent: 6113347 (2000-09-01), Forrester
patent: 6224963 (2001-05-01), Strangman
patent: 6435826 (2002-08-01), Allen
patent: 6435835 (2002-08-01), Allen
patent: 6543991 (2003-04-01), Sathianathan et al.
patent: 6589600 (2003-07-01), Hasz et al.
patent: 6703137 (2004-03-01), Subramanian
patent: 6830428 (2004-12-01), Le Biez et al.
patent: 7302990 (2007-12-01), Bunker et al.
patent: 1283278 (2003-02-01), None
patent: 1808507 (2007-07-01), None
patent: 1844863 (2007-10-01), None
patent: 2061397 (1981-05-01), None
European Search Report mailed Mar. 2, 2009.

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